130210.0286.11A Strength Calculation - Lifting Cradles
Transcript of 130210.0286.11A Strength Calculation - Lifting Cradles
FMT
Strength Calculation
Lifting Cradles – Holm-kl
(OSK-ShipTech 130210.0286.11A)
Date: 11.06.2013 Sign: KAF
______________________________________________________________________________________ 130210.0266.01 Lifting and transport Cradles
Table of Contents
1 Introduction ............................................................................................................................. 1
1.1 Reference documents ............................................................................................................... 1
2 Summary .................................................................................................................................. 1
3 Conclusion ............................................................................................................................... 2
4 3D Beam Element Analysis .................................................................................................... 3
5 Software ................................................................................................................................... 3
6 Coordinatee system ................................................................................................................ 3
7 Vessel data ............................................................................................................................... 3
8 Model Description ................................................................................................................... 4
9 Boundary Conditions .............................................................................................................. 5
10 Design Criteria ......................................................................................................................... 5
11 Beam Model Loads ................................................................................................................. 6
11.1.1 Loaded Model .................................................................................................................... 7
12 Results ...................................................................................................................................... 8
12.1 Strength Evaluation ................................................................................................................... 8
12.1.1 Evaluation criteria .............................................................................................................. 8
12.1.2 Deflection ........................................................................................................................... 8
12.1.3 Stresses in Structure ......................................................................................................... 9
12.2 Shell Core strength. ................................................................................................................ 11
12.3 Springs .................................................................................................................................... 11
12.4 Lashing .................................................................................................................................... 12
12.4.1 Bolted connection in transverse lashing beams .............................................................. 13
Appendix Appendix A - Drawings Appendix B - 3d model results - aft cradle Appendix C - 3d model results - fore cradle Appendix D – PVC core material datasheet
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1 Introduction The intent of this analysis is to verify and document the strength of lifting and transport cradles for Danish navy Holm-class ships. The ships are considered lifted and transported onboard an unspecified heavy-lift ship. The transport is considered to have unrestricted service. The ship is considered lifted in two (2) cradles, aft (5.6m forward of AP) and fore (19.5m forward of AP). The strength analysis cover:
- Strength of cradles in lifting scenario - Calculation on springs for cradles. - Sea fastening of ship in transport scenario
For the lifting and transport scenario relevant design criteria are used to verify the strength.
1.1 Reference documents Reference is made to following documents:
1. 130210.0109.01A – Løftevugger General Arrangement 2. 130210.1007.01A – Løftevugger - Surringsarrangement 3. 130210.0286.01A – Løftevugge - Agter 4. 130210.0286.02A – Løftevugge – For 5. 130210.0286.04A – Løftevugger - Fjeder System
2 Summary The lifting and transport cradles are designed and verified according to the relevant criteria:
Lifting Scenario: Design verified according to DNV Rules for planning and executing of Marine Operations, pt. 2 Ch. 5 – Lifting.
Transport Scenario: Sea fastening verified according to accelerations calculated DNV rules for ships Pt. 3 Ch. 1 Sec 4 Design Loads – Ship Motions and Accelerations
The strength analysis is performed using a simplified beam model reflecting the design of the lifting Cradles. Material: Steel construction to be made of mild steel unless otherwise stated on the drawings, to meet DNV standards: NV D36, min yield stress of 355 N/mm2. The calculations are based on steel with yield stress of 235, which gives further margin in the strength calculations of the cradles. Springs: The springs are designed to hold the arms open while lifting the empty cradle and to allow the arms to close once the weight of the vessel is on the cradle. The spring constant should be 13.2 kg/mm.
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The spring considered in the calculation is described below: Type Compression Spring Wire diameter 14.00 mm Outer diameter of spring 75.00 mm Free Length 450.00 mm Total number of coils 15 Number of active coils 13 Shear Modulus 79300 MPa (Steel) Lashings: The lashings are designed to hold the vessel in position in the cradles. The cradles are secured to the heavy lift vessel by a set of lashings too. The Arrangement of the lifting cradles is presented in Appendix A Page A1 The structural design of the aft lifting cradles is presented in Appendix A Page A3 The structural design of the aft lifting cradles is presented in Appendix A Page A4
3 Conclusion The Strength of the aft and fore lifting and transport cradles has been analyzed on the basis of the loads and accelerations calculated in Ch.10 Based on the modeling reflecting the drawings in Ref 4) and 5) and loads applied obtained from Ch. 10, the stresses in the structure have been calculated and analyzed as documented in this report and its attachments. It is concluded that the calculated stress levels of the Lifting and transport Cradles is found to be within the requirements specified in this document. The compression stresses in the hull core material has been calculated and found to be within the limits given by the manufacturer. The springs holding arms away from the ship is dimensioned to support the ship when lifted. Lashings holding the ship when transporting the ship have been dimensioned. The lashings are able to hold the ship in the cradles when transported.
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4 3D Beam Element Analysis A 3D beam model of each of the lifting cradles has been prepared to evaluate the strength of the cradles.
5 Software Software used: Dlubal programs RSTAB for beam calculations. Further information can be forwarded on request.
6 Coordinatee system The coordinate system is defined as a right hand coordinate system:
X: Vessel longitudinal direction (positive in forward direction) X=0 at AP Y: Vessel transverse direction (positive towards port side) Y=0 at CL Z: Vertical direction (positive upwards) Z=0 at heavy lift deck
7 Vessel data Name: Holm-kl Type: Patrol, Naval Support Class: DNV Flag: Danish Length over all: 28.90 m Length btw. PP: 26.15 m Breadth mld: 6.40 m Depth to deck: 3.54 m Design draught: 1.74 m Deadweight: 55 tons Speed 12.0 kn Weight 125 tons LCG 11.49 m forward AP VCG 3.5 m above Baseline
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8 Model Description The 3D Beam models describe the structures:
- Aft lifting and transport cradle - Fore lifting and transport cradles.
The models are build according to drawings:
- 130210.0286.01 – Løftevugge - Agter - 130210.0286.02 – Løftevugge - For -
As the calculation is performed as a beam calculation the model is built without brackets and plates. Racking plates are simulated by crossing rigid elements.
Figure 1: Lifting Cradles
Y
Z
X
Isometric
Y
Z
X
Isometric
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9 Boundary Conditions The boundary conditions for the structures:
- For the lifting scenario the ship is considered as a rigid structure. The “ship” is rigid supported in the centerline. The connection between the ship and the cradle are simulated by compression only members acting perpendicular to the local hull surface.
- The model is loaded at the points where the lifting slings are lifting the cradles.
10 Design Criteria The design of the cradles is verified according to below described criteria: Lifting Situation: DNV Rules for planning and executing of Marine Operations. Sea fastening: DNV Rules for ships Pt. 3 Ch. 1 Sec.4 Design Loads – Ship Motions
and Accelerations Lifting Loads The load due to lifting of the ship from a floating structure has to be considered. The Dynamic Amplification Factor for such an operation, considering a lift<100t performed in sheltered areas (inshore), is according to DNV Rules for planning and executing of Marine Operations, 1.15 x Lifted weight. Further the lifting equipment has to be dimensioned obtain the wind forces and skew loads due to a 2 crane lift. Sea Fastening Loads The loads on the sea fastening structures due to ship motions of the heavy lift vessel are calculated by using DNV Rules for ships Pt. 3 Ch. 1 Sec.4. Three (3) different heavy lift ships have been chosen and accelerations have been calculated. The largest accelerations will be used in calculation of the lifting cradles and sea-fastening. The three (3) ships and the calculated motions and accelerations are shown in below table:
M/V PATRIA M/V Palessa M/V EIT Palmina Lpp [m] 95 111 130 B [m] 18.7 1917 23,2 Service speed [kn] 15 15 15 GM [m] 1.5 1.5 1.5 Roll Angle [deg] 35 34 31 Pitch Angle [deg] 10 9 8 Longitudinal Acc. [m/s2] 4.02 5.08 3.32 Transverse Acc. [m/s2] 7.61 7.34 6.51 Vertical Acc. [m/s2] 5.60 5.08 4.80
Table 1: Calculated accelerations
The accelerations is dependent on the heavy lift vessels GM and sea conditions, so accelerations must be calculated separately for each operation by the heavy lift operator.
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For conservative calculations the following accelerations has been chosen: Longitudinal and Transverse: 9.81 m/s2 Vertical: 5.60 m/s2
11 Beam Model Loads Reaction in Lifting Cradles The lifting operations are considered to take place in sheltered areas (inshore). Due to this the Dynamic Amplification Factor (DAF) is considered to be 1.15 x lifted weight. The cradles are designed according to below condition of the vessel: Weight of vessel: 125 tons LCG 11.49 m forward AP Position of cradles: Aft: 5.60 m forward AP Fore: 19.50 m forward AP Weight on cradles: Aft: 72.0 tons Fore: 53.0 tons The weight of each cradle is for strength calculation purposes been estimated to be 6.5 tons. Actual detailed calculations confirm a weight below this figure. See Ref/3/ and ref/4/. The loads on the cradles for the lifting scenario are calculated based on the tension in the lifting web slings. The loads can be seen in the force diagrams below.
Figure 2: Force Diagrams
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The loads in above sketch are seen in below table:Loads on model
Aft Cradle Fore Cradle
Lifted weight w/o DAF 78.5 t Lifted weight w/o DAF 59.5 t
Lifted weight w/o DAF 770.4 kN Lifted weight w/o DAF 583.4 kN
T ‐ Tension force one side 443.0 kN T ‐ Tension force one side 335.4 kN
R1 ‐ Reaction on cradle side 437.6 kN R1 ‐ Reaction on cradle side 345.5 kN
R2 ‐ Reaction on Bottom 308.8 kN R2 ‐ Reaction on Bottom 212.9 kN
R3 ‐ Reaction on ship side 80.3 kN R3 ‐ Reaction on ship side 55.0 kN Table 2: Calculated forces
11.1.1 Loaded Model
Figure 3: Aft Cradle, Loaded. Loads in kN
Figure 4: Fore Cradle, Loaded. Loads in kN
218.800 218.800
Y
154.400 154.400
Z
X
218.800 218.800
IsometricLC1
X
218.800
218.800
154.400
Z
Y
218.800
218.800
154.400
In X-directionLC1
172.750 172.750
Y
106.450 106.450
Z
X
172.750 172.750
IsometricLC1
X
172.750
172.750
106.450
Z
Y
172.750
172.750
106.450
In X-directionLC1
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12 Results As all calculation data is a large amount of data a reduced selection of the calculation results, supporting the strength evaluation is listed in Appendix B and C. If further details of the calculation are needed, data can be forwarded on request.
12.1 Strength Evaluation
12.1.1 Evaluation criteria Deflection: The deflection criteria for the lifting cradles are decided to be 1:600. This means that the members are allowed to deflect 1mm in a beam of 600mm length Allowable Stresses The allowable stresses are calculated according to DnV rules. Design Verification allowable stresses for the design is calculated as follows:
σ /1.5 This gives for the steel used in calculations:
Normal strength steel (S235):
235N/mm
,σ1.5
156N/mm
σ
1.5 ∙ √390N/mm
,σ1.5
156N/mm
12.1.2 Deflection The maximum deflection of the aft cradle is 0.8 mm. The deflection is well below the deflection criteria. The maximum deflection of the fore cradle is 0.5 mm. The deflection is well below the deflection criteria.
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Figure 5: Deformation of models, Aft Left, Fore right
12.1.3 Stresses in Structure The largest stresses in each beam member type are calculated in RSTAB module General Stress Analysis. The result of the stress calculation can be seen in Appendix B and C. In the stress analysis no stresses are seen above the allowable stresses. The largest stresses are approximately 120 N/mm2, which correspond to a utilization factor of approx. 0.77. In general the stresses are well below the limit.
Table 3: Aft Cradle Stresses
218.800 218.800
154.400
Y
154.400
Z
X
0.8
218.800 218.800
IsometricLC1u
Factor of deformations: 200.00Max u: 0.8, Min u: 0.0 [mm]
Y
Z
X
0.5
IsometricLC1u
Factor of deformations: 1800.00Max u: 0.5, Min u: 0.0 [mm]
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Table 4: Fore Cradle Stresses
The full result of the stress calculations can be seen in Appendix B and C page 11-14.
Figure 6: Members stresses. Shown as stress ratio
0.58
0.580.04
0.09
0.04
0.10
0.09
0.07
0.31
0.10
0.07
0.31
0.06
0.04
0.06
0.04
0.41
0.20
0.03
Y
0.050.20
Z
0.41
X
0.03
0.06
0.04
0.06
0.04
0.07
0.09
0.07
0.10
0.31
0.09
0.04
0.10
0.31
0.040.58
0.58
IsometricSTEEL CA1Tau Total
Max Tau Total: 0.58, Min Tau Total: 0.00
Stress ratioTau Totale [-]
0.58
0.00
Max : 0.58Min : 0.00
0.70
0.02
0.70
0.35
0.020.02
0.19
0.33
0.32
0.32
0.12
0.02
0.19
0.33
0.32
0.32
0.12
0.02
0.08
0.50
0.35 0.48
0.08
0.18
0.50
0.02
0.29
Y
0.06
0.35
0.37
Z
X
0.18
0.02
0.29
0.23
0.06
0.08
0.12
0.08
0.48
0.19
0.12
0.02
0.19
0.33
0.12
0.32
0.02
0.33
0.02
0.32
0.02
0.35
0.70
0.70
IsometricSTEEL CA1Sigma-eqv
Max Sigma-eqv: 0.70, Min Sigma-eqv: 0.00
Stress ratioSigma-v [-]
0.70
0.00
Max : 0.70Min : 0.00
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12.2 Shell Core strength. The GRP core materials, where the cradles are making contact to the shell, are checked. The core material is a PVC foam structure. From the beam calculations the load, where the cradles are supporting the hull are seen. The forces on the sides, from where the arms are supporting the hull are calculated separately. The forces acting on the hull are seen in the table below:
Aft Cradle Fore Cradle Forces on bottom 258 kN 248 kN Forces on side 80.3 kN 55 kN
Table 5: Forces on hull
The forces are considered distributed evenly due to the wood. The shell is considered supported by the core of the hull structure (Stringers and bulkheads). The hull structure is general of 50 mm core material. The nominal compressive strength of the PVC core material is 2.6 MPa on the bottom and 1.9 MPa at the sides. For further info of the PVC core material see appendix D. A safety factor of 5% has been added to the strength levels for the material. A safety factor of 5% is considered together with the DAF factor, which is 1.15. Further the stress distribution through the core material, giving a larger area, is not considered. This is considered to be an overall conservative approach. The aft cradle bottom support is supporting 1150mm longitudinal and 1000mm transverse. The fore cradle bottom support is supporting 1150mm longitudinal and 920mm transverse. The height of the support on the arms is aft 890mm and fore 610mm. This gives the below stresses in the core material.
Permissible Pressure Aft Cradle Fore Cradle Pressure on bottom 2.470 N/ mm2 2.46 N/mm2 2.46 N/mm2 Pressure on side 1.805 N/ mm2 1.80 N/mm2 1.80 N/mm2
Table 6: Forces on hull
12.3 Springs The springs are designed to hold the arms open while lifting the empty cradle and to allow the arms to close once the weight of the vessel is on the cradle. When lifting the empty cradles, the aft cradle chain will need a tension of 1530 kg to hold the arm away from the ship side. The fore cradle needs a tension of 1520 kg. The arms should not close until the cradles are having contact to the ship, thus the pretension need to be 10% more than the empty cradle weight. The spring will be tensioned to 1710 kg
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The spring should have a constant of: k=13.2 kg/mm With above spring the spring will have the tensions as shown in below table:
mm kg Pretention 120 1710 Hull contact 162 2263 Max 216 3157
Table 7: Tension in spring
The spring considered in the calculation is described below: Type Compression Spring Wire diameter 14.00 mm Outer diameter of spring 75.00 mm Free Length 450.00 mm Total number of coils 15 Number of active coils 13 Shear Modulus 79300 MPa (Steel) Drawing of spring is seen in appendix A5
12.4 Lashing The sea fastening of the ship in the cradles is to be done by lashings to the deck of the heavy-lift ship. The cradles are lashed to the heavy-lift vessel from the four 10t D-Rings. The transported ship is lashed separately. The lashings and sea fastenings needs to be calculated to the accelerations described in chapter 10 Design Criteria. Design accelerations: Longitudinal and Transverse: 9.81 m/s2 Vertical: 5.60 m/s2
The longitudinal and transverse acceleration are considered to be the same, to allow the ship being stowed transverse on the heavy-lift vessel. The lashings need to be calculated for following ship particulars: Ship weight 125.00 t LCG 11.49 m forward AP VCG 3.50 m above BL The sea fastening forces are thus: Longitudinal and Transverse: 1226.25 kN Vertical: 1926.25 kN / 700.0 kN
The worst scenario is considered to be when the vertical acceleration is not acting the same direction as the gravity. Simple calculation has been made to calculate the lashings.
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The calculations are based on drawings in ref /2/. The lashings are considered to support the vessel from rolling off the cradle. Example: Transverse force acting towards Port side. The transverse lashing beam will add a vertical force at the ship starboard side and a horizontal force at the port side. Considering that the lashings beams should be able to keep the vessel in the cradles the forces in the lashings to the transport ship is calculated. Considering the aft lashings to distribute the load equally, the maximum load on 1 lashing part is 10.02 tons. Maximum load on forward lashing are calculated to be 12.4 t.
12.4.1 Bolted connection in transverse lashing beams The transverse lashing beams needs to be assembled by several pieces. The connections are considered bolted together by 6 pcs. M16 bolts of quality 8.8. Due to the design of the lashing beams the bolts will only experience tension. The bolts are considered to be loaded equal at all times. The stresses in the bolts are checked to be within the stress limits, considering a safety factor of 2.0. The stresses in the bolts are calculated below. Transverse force in lashing beam 80.7 kN Core area of M16 bolt 149.6 mm2 Max. permissible tension stress of bolt:
σ2
6402
320N/mm
Stresses in the bolts:
80.7 ∙ 10006 ∙ 149.6
89.9N/mm
The bolts are loaded to 28% of the permissible load. From above it is seen that the 6 pcs. M16 bolts, quality 8.8 is capable of transferring the forces in the lashing beam.
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Appendix A
Drawings
A1 - 130210.0109.01 – GA A2 - 130210.1007.01 – Surrings Arr. A3 - 130210.0286.01 – Løftevugge agter A4 - 130210.0286.02 – Løftevugge For A5 - 130210.0286.04A - Løftevugger - Fjeder System
0 5 10 15 20 25
Løft af Skib
0 5 10 15 20 25
Bjælker ved Dæk
Fender fjernes
Pakning af 40' open top container
Løft af Skib
Typisk
Forreste Vugge
Basislinje
4940 ov. BL.
Basislinje
Agterste Vugge
Basislinje
Bjælke ved spant 8½Bjælke ved spant #3
Basislinje Basislinje
Bjælke ved spant #25½
Basislinje
Set mod for Set mod forSet mod for
1500 1000 9001200 1200 800
450
1000 1000
Knæ til låsning tværskibs
Boltet samling
Bjælke låses langskibs i klyds
Knæ til låsning tværskibs
Boltet samling
Bjælke låses langskibs i pullert
Knæ låses tværskibs mod skrog Knæ låses tværskibs mod skrog
Knæ låses tværskibs mod skrog
Knæ til låsning tværskibs
Boltet samling
Bjælke låses langskibs i klyds
Id.no.:
Sign: Scale:
Sheet: Date:
Aarhus
Balticagade 15 2 floor
Copenhagen
2100 Copenhagen Oe - DENMARK8000 Aarhus C - DENMARK
nd
Bryggervangen 55 1.tv
[email protected] www.osk-shiptech.com phone +45 4576 4210phone +45 8617 8099
Rev.
Check:
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
CAD - drawing - Not to be modified by hand !
All measurements in mm unless otherwise stated.
Approv. byRev. Init.Date Description of modifications Date
ISO:
HOLM Klassen - Løftevugger
General Arrangement
JWE CFA 1:100
1/1
11.06.2013
130210.0109.01 A
A 05.07.2013 JWE Generel opdateret grundet vægt CFA 05.07.2013
LÆNGDE O.A. 28.90 m
LÆNGDE MELLEM P.P. 26.15 m
BREDDE MLD. 6.40 m
SIDEHØJDE 3.54 / 4.94 m
Tyngdepunkt for beregning (Oplyst af FMT):
LCG: 11.49 m foran for AP
TCG: 0.00 m fra CL
VCG: 3.50 m over BL
Vægt: 125 t
Accelerationer:
Langskibs: +/- 9.81 m/s2 1.0 g
Tværskibs: +/- 9.81 m/s2 1.0 g
Vertikalt: +/- 5.60 m/s2 0.6 g
Samme acceleration langskibs/tværskibs, for at vugger kan stilles tværskibs og langskibs på Heavy Lift skib.
0 5 10 15 20 25
Surring af Skib
0 5 10 15 20 25
Surring ved Dæk
Fender fjernes
Rør fjernes
Transport Skib
Kølklods
Stål/træ
365 1970 470 470 470 470 6970 4701030 1030 1030 1030 1030 1030 10301530
4
5
.
0
°
1275 6525
Surring til positionering
af løftevugger
Surring til positionering
af løftevugger
Kølklodser kiles mod skrog
Surring Forreste Vugge
Basislinje
Surring Agterste Vugge
Basislinje
Transport SkibTransport Skib
45.0°45.0°
Surring ved spant #3
Basislinje
Set mod for
Knæ til låsning tværskibs
Boltet samling
1200 1200
Transport Skib
m
in
.
2
8
.0
°
Bjælke låses langskibs i klyds
med trækiler (SB + BB).
Bjælke klodses op (CL, SB, BB).
Obs! Ingen lodret kontakt
mellem bjælke og klyds.
Knæ låses tværskibs mod skrog
med trækiler (SB + BB).
Surring ved spant 8½
Basislinje
Set mod for
1500 1000 900800
450
Transport Skib
m
in
.
2
8
.0
°
Knæ til låsning tværskibs
Boltet samling
Bjælke låses langskibs i klyds
med trækiler (SB + BB).
Bjælke klodses op (CL, SB, BB).
Obs! Ingen lodret kontakt
mellem bjælke og klyds.
Knæ låses tværskibs mod skrog
med trækiler (SB + BB).
Basislinje
Surring ved spant #25½
Set mod for
1000 1000
Transport Skib
m
in
.
2
8
.0
°
Knæ til låsning tværskibs
Boltet samling
Bjælke låses langskibs i pullert
med trækiler (SB + BB).
Bjælke klodses op (CL, SB, BB).
Obs! Ingen lodret kontakt
mellem bjælke og pullert.
Knæ låses tværskibs mod skrog
med trækiler (SB + BB).
Id.no.:
Sign: Scale:
Sheet: Date:
Aarhus
Balticagade 15 2 floor
Copenhagen
2100 Copenhagen Oe - DENMARK8000 Aarhus C - DENMARK
nd
Bryggervangen 55 1.tv
[email protected] www.osk-shiptech.com phone +45 4576 4210phone +45 8617 8099
Rev.
Check:
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
CAD - drawing - Not to be modified by hand !
All measurements in mm unless otherwise stated.
Approv. byRev. Init.Date Description of modifications Date
ISO:
HOLM Klassen - Løftevugger
Surrings Arrangement
JWE CFA 1:100
1/1
21.06.2013
130210.1007.01 A
A 05.07.2013 JWE Generel opdateret grundet øget vægt CFA 05.07.2013
LÆNGDE O.A. 28.90 m
LÆNGDE MELLEM P.P. 26.15 m
BREDDE MLD. 6.40 m
SIDEHØJDE 3.54 / 4.94 m
Tyngdepunkt for beregning (Oplyst af FMT):
LCG: 11.49 m foran for AP
TCG: 0.00 m fra CL
VCG: 3.50 m over BL
Vægt: 125 t
Accelerationer:
Langskibs: +/- 9.81 m/s2 1.0 g
Tværskibs: +/- 9.81 m/s2 1.0 g
Vertikalt: +/- 5.60 m/s2 0.6 g
Samme acceleration langskibs/tværskibs, for at vugger kan stilles tværskibs og langskibs på Heavy Lift skib.
Volmunen træklodser:
Agterste vugge: 0,45 m3
Foreste vugge: 0,65 m3
Kølklodser: 2,0 m3
Bjælker Spt. 3, 8½, 25½: 0,1 m3
Reference tegninger:
130210.0109.01 General Arrangement
130210.0131.01 Løftevugger - Specifikation
130210.0286.02 Løftevugge - Agter
130210.0286.02 Løftevugge - For
130210.0286.03 Løftevugge - Træklodser
130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl
130210.0327.01 Løftevugger - Positionering af vugger
130210.1007.02 Surrings Arrangement - Bjælker & Kølbokse
Detalje 1
A-AC-C
D-DB-B
Detalje 1
AA
C
C
D
D
B
B
STYKLISTE
KommentarerRev.BeskrivelseStk.Pos.
Bundramme - Vandret11
Topramme - Skrå
22
Topramme - Lodret (bagbord)13
Topramme - Lodret (styrbord)14
Bjælke - Lodret45
Bjælke - Lodret46
Indskud - Lodret tværskibs37
Knæ - Tværskibs28
4 stk. bruges på Pos. 3 & 4 Knæ - Tværskibs4+49
Indskud - Lodret langskibs110
2 stk. bruges på Pos. 3 & 4 Stropstyr - Langsskibs3+211
Box - Vandret (til træklods)112
Box - Skrå (til træklods) - Styrbord113
Box - Skrå (til træklods) - Bagbord114
Drejeakse415
Låsebeslag til drejeakse416
Bolt - M16 x 45mm817
Bolt - M16 x 55mm4018
Skiver - M168819
Møtrik - M164020
Se tegning 130210.0286.04 Fjedersystem421
RUD - Type nr. VLBS-10 (10 tons WLL) D-Ring for surring til dæk422
Inventor CAD-drawing - not to be modified by hand !
All measurements in mm unless otherwise stated.
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
OS
K-S
hip
Naval Architects & Marine Engineers
Aarhus
Balticagade 15 2nd floor
8000 Aarhus C - DENMARK
phone +45 8617 8099
Copenhagen
Fruebjergvej 3 - PO Box 26
2100 Copenhagen Oe - DENMARK
phone +45 4576 [email protected] www.osk-shiptech.com
Sign:
Sheet:
Id.no.:
Check: Scale:
Date:
Rev.:
Rev. Date Init.
Description of modifications Approv. by
Date
Tech A
/S
HOLM Klassen - Løftevugger
Løftevugge - Agter
Samlingstegning
JWE CFA 1:25
1/3
10.06.2013
130210.0286.01 A
A 05.07.2013 JWE General opdatering grundet øget vægt CFA 05.07.2013
ISO:
Set mod for
Set oppefra
BB SB
Set mod bagbord
1
2
13
8
12
6
7
5
34
6
7
5
211
11
15
16
M16 - Bolt (45mm), skive
4
0
°
12
85
200
13
60
,7
11
5 5
1150
18
50
10
11
15 15
1616
11
66
14
2
12
11
68
18
,4
7346,1
272,8 1217,5272,81609,71217,5
7100
450450
1609,7
30
8
21
21
Fuld gennembrænding
Fuld gennembrænding
Fuld gennembrænding
Fuld gennembrænding
128
5
128
5
22
22
99
14
M16 Bolt (55mm), Skive, Møtrik
1314
11
Tyngdepunkt for beregning (Oplyst af FMT)
LCG: 11.49 m foran for AP
TCG: 0.00 m fra CL
VCG: 3.50 m over BL
Vægt: 125 t
Accelerationer:
Langskibs: +/- 9.81 m/s2 1.0 g
Tværskibs: +/- 9.81 m/s2 1.0 g
Vertikalt: +/- 5.60 m/s2 0.6 g
Samme acceleration langskibs/tværskibs, for at vugger kan stilles tværskibs og langskibs på Heavy Lift skib.
FMT - svejse og kvalitets specifikation:
Konstruktionen udføres i overensstemmelse med DS/EN 1090 - 2, udførelsesklasse EXC3.
Konstruktionen skal udføres af certificerede svejsere. Certificeringen skal dokumenteres før arbejdet iværksættes.
Der skal udarbejdes godkendte Welding Procedure Specifications (WPS) for alle svejsninger, før svejsning iværksættes.
Omfanget af procedureprøver skal aftales med svejseinspektør og procedureprøverne skal godkendes af samme, inden
noget svejsearbejde på nogen konstruktionsdel må iværksættes.
Svejsninger og svejseforberedelser (skærpning) skal godkendes af svejseinspektør, før svejsning iværksættes.
Svejseinspektør skal være godkendt efter gældende regler og standarder, således at vedkommende er kvalificeret til at
godkende arbejder efter DS/EN 1090-2.
Det anvendte stål skal svare til S355 J2 og skal enten være:
1. Stål med 3.2 certifikat.
2. Stål som er passende dokumenteret ved måling af flydespænding, brudforlængelse og slagsejhed.
Brudforlængelse skal være minimum 10 % og slagsejheden skal dokumenteres ved - 20 graders celcius. Se note *)
*) Note: Klassificeret plademateriale er relativt tilgængeligt på markedet, men profiler er ikke særlig tilgængelige.
Det vil ofte være nødvendigt at udføre særskilt prøvning.
Svejsegeometri:
Hvis ikke andet er anført på tegningerne gælder følgende:
Kantsømme: A-mål = 0.5 af mindste pladetykkelse.
K-sømme og X-sømme: fuldt gennembrændte.
Hvor svejsning udføres med fuld gennembrænding fuges og efterløbes.
Tvivlsspørgsmål afklares med svejseinspektør, så vidt muligt før arbejdet iværksættes.
Det færdige arbejde skal besigtiges af FMT før maling og sandblæsning.
Vægt
Stål vægt i alt: 5810 kg.
Reference tegninger:
130210.0109.01 General Arrangement
130210.0131.01 Løftevugger - Specifikation
130210.0286.02 Løftevugge - For
130210.0286.03 Løftevugge - Træklodser
130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl
130210.1007.01 Løftevugger - Surringsarrangement
130210.1007.02 Løftevugger - Surringsarrangement - Bjælker & Kølbokse
B-B
A-A
STYKLISTE
KommentarerRev.BeskrivelseStk.Pos.
Bundramme - Vandret11
Topramme - Skrå
22
Topramme - Lodret (bagbord)13
Topramme - Lodret (styrbord)14
Bjælke - Lodret45
Knæ - Tværskibs28
4 stk. bruges på Pos. 3 & 4 Knæ - Tværskibs4+49
2 stk. bruges på Pos. 3 & 4 Stropstyr - Langsskibs3+211
Box - Vandret (til træklods)112
Box - Skrå (til træklods) - Styrbord113
Box - Skrå (til træklods) - Bagbord114
B
B
A
A
Inventor CAD-drawing - not to be modified by hand !
All measurements in mm unless otherwise stated.
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
OS
K-S
hip
Naval Architects & Marine Engineers
Aarhus
Balticagade 15 2nd floor
8000 Aarhus C - DENMARK
phone +45 8617 8099
Copenhagen
Fruebjergvej 3 - PO Box 26
2100 Copenhagen Oe - DENMARK
phone +45 4576 [email protected] www.osk-shiptech.com
Sign:
Sheet:
Id.no.:
Check: Scale:
Date:
Rev.:
Rev. Date Init.
Description of modifications Approv. by
Date
Tech A
/S
HOLM Klassen - Løftevugger
Løftevugge - Agter
Samlingstegning - Delsamlinger
JWE CFA 1:25
2/3
10.06.2013
130210.0286.01 A
A 05.07.2013 JWE General opdatering grundet øget vægt CFA 05.07.2013
ISO:
Pos. 1
Pos. 2
Pos. 3
(Pos. 4 kontra)
Pos. 3B
(Pos. 4B kontra)
Pos. 5
Pos. 8
1:20
Pos. 9
1:20
Pos. 11
1:20
Pos. 12
1:20
Pos. 13
(Pos. 14 kontra)
Pos. 3D
(Pos. 4D ens)
450 200
1017,5
200
1409,7 545,6 1409,7
200
1017,5
200
7100
115
0
25
90
90
25
1A
1B
1C
1C
1C
1C
1D1D
Fuld gemmenbrænding
Fuld gemmenbrænding
Fuld gennembrænding
Fuld gennembrænding
268,4
3064,4
1035
175,9
835
1483
2C
2D 2D
2E
2F
2F
11
50
Fuld Gennembrænding
2A
2B
11
3E
115
0
3F
11
Fuld gennembrænding
Fuld gennembrænding
3746,8
25
3
0
90
90
3C
3A
61
2,1
1250
2
2
°
3B
3B
7
9
°
1218,2
270
15
15
Fuld gennembrænding
3B-4
3B-3
3B-1
3B-2
Fuld gennembrænding
54
54
42
Fuld gennembrænding
Fuld gennembrænding
15
15
1480 270
95
152,6
84,9
5A 5B
5C
90 90
8A
8B
725,6
15
92,5
77,5
9A
9C
9B
9D
11A
941
11B
163 300 300
1150
10
12A
12B
12C
13A
13C
13C
13D
13H 13H
13E
95
472,5 477,5
105
10
7,5
720
30
0
10
7,5
567
,7
13B
13E
440,19 268,59 441,22
2224
Fuld gennembrænding
Fuld gennembrænding
50
3D
3D
750
135
15
3D-1
3D-2
Tyngdepunkt for beregning (Oplyst af FMT)
LCG: 11.49 m foran for AP
TCG: 0.00 m fra CL
VCG: 3.50 m over BL
Vægt: 125 t
Accelerationer:
Langskibs: +/- 9.81 m/s2 1.0 g
Tværskibs: +/- 9.81 m/s2 1.0 g
Vertikalt: +/- 5.60 m/s2 0.6 g
Samme acceleration langskibs/tværskibs, for at vugger kan stilles tværskibs og langskibs på Heavy Lift skib.
FMT - svejse og kvalitets specifikation:
Konstruktionen udføres i overensstemmelse med DS/EN 1090 - 2, udførelsesklasse EXC3.
Konstruktionen skal udføres af certificerede svejsere. Certificeringen skal dokumenteres før arbejdet iværksættes.
Der skal udarbejdes godkendte Welding Procedure Specifications (WPS) for alle svejsninger, før svejsning iværksættes.
Omfanget af procedureprøver skal aftales med svejseinspektør og procedureprøverne skal godkendes af samme, inden
noget svejsearbejde på nogen konstruktionsdel må iværksættes.
Svejsninger og svejseforberedelser (skærpning) skal godkendes af svejseinspektør, før svejsning iværksættes.
Svejseinspektør skal være godkendt efter gældende regler og standarder, således at vedkommende er kvalificeret til at
godkende arbejder efter DS/EN 1090-2.
Det anvendte stål skal svare til S355 J2 og skal enten være:
1. Stål med 3.2 certifikat.
2. Stål som er passende dokumenteret ved måling af flydespænding, brudforlængelse og slagsejhed.
Brudforlængelse skal være minimum 10 % og slagsejheden skal dokumenteres ved - 20 graders celcius. Se note *)
*) Note: Klassificeret plademateriale er relativt tilgængeligt på markedet, men profiler er ikke særlig tilgængelige.
Det vil ofte være nødvendigt at udføre særskilt prøvning.
Svejsegeometri:
Hvis ikke andet er anført på tegningerne gælder følgende:
Kantsømme: A-mål = 0.5 af mindste pladetykkelse.
K-sømme og X-sømme: fuldt gennembrændte.
Hvor svejsning udføres med fuld gennembrænding fuges og efterløbes.
Tvivlsspørgsmål afklares med svejseinspektør, så vidt muligt før arbejdet iværksættes.
Det færdige arbejde skal besigtiges af FMT før maling og sandblæsning.
Vægt
Stål vægt i alt: 5810 kg.
Reference tegninger:
130210.0109.01 General Arrangement
130210.0131.01 Løftevugger - Specifikation
130210.0286.02 Løftevugge - For
130210.0286.03 Løftevugge - Træklodser
130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl
130210.1007.01 Løftevugger - Surringsarrangement
130210.1007.02 Løftevugger - Surringsarrangement - Bjælker & Kølbokse
9
3G3G
25
2289
13I
13G13G
13F
13F
62
8
44
9,8
51
0
Fuld gennembrænding
440
270
44
0
STYKLISTE
KommentarerRev.MaterialeBeskrivelseStk.Pos.
Bundramme - Vandret11
HEB 200Tværskibs bjælke21A
HEB 200Langskibs bjælke21B
15.0 mmIndskud281C
20.0 mmØjeplade41D
Topramme - Skrå22
HEB 200Tværskibs bjælke1+12A
HEB 200Tværskibs bjælke1+12B
9.0 mmTværskibs indskud2+22C
15.0 mmLangskibs indskud2+22D
15.0 mmLangskibs indskud2+22E
15.0 mmIndskud6+62F
Topramme - Lodret (bagbord)13
HEB 200Lodret bjælke13A
Lodret bjælke23B
HEB 200Lodret bjælke23B-1
20.0 mmEndeplade23B-2
40.0 mmDrejebeslag23B-3
40.0 mmDrejebeslag23B-4
HEB 200Lodret bjælke13C
Langsskibs indskud23D
15.0 mmLangsskibs indskud23D-1
15.0 mmLangsskibs indskud23D-2
10.0 mmLodret indskud23E
20.0 mmØjeplade23F
10.0 mmIndskud til Wire43G
Topramme - Lodret (styrbord)14
HEB 200Lodret bjælke14A
Lodret bjælke24B
HEB 200Lodret bjælke24B-1
20.0 mmEndeplade24B-2
40.0 mmDrejebeslag24B-3
40.0 mmDrejebeslag24B-4
HEB 200Lodret bjælke14C
Langsskibs indskud24D
15.0 mmLangsskibs indskud24D-1
15.0 mmLangsskibs indskud24D-2
10.0 mmLodret indskud24E
20.0 mmØjeplade24F
10.0 mmIndskud til Wire44G
Bjælke - Lodret45
HEB 200Lodret bjælke45A
20.0 mmEndeplade45B
40.0 mmDrejebeslag45C
HEB 200Bjælke - Lodret46
10.0 mmIndskud - Lodret tværskibs37
Knæ - Tværskibs28
10.0 mmKnæ - Tværskibs28A
15.0 mmLodret indskud48B
4 stk. bruges på Pos. 3 & 4 Knæ - Tværskibs4+49
15.0 mmKnæ - Tværskibs4+49A
15.0 mmEndeplade4+49B
10.0 mmFlange4+49C
5.0 mm GummiEndeplade - Tryklag4+49D
15.0 mmIndskud - Lodret langskibs110
2 stk. bruges på Pos. 3 & 4 Stropstyr - Langsskibs3+211
Ø 190 x 15.0Stropstyr - Rør511A
15.0 mmStropstyr - Ledeplade1511B
Box - Vandret (til træklods)112
15.0 mmBox - Plade112A
50 x 10 FladjernBox - Profil212B
50 x 10 FladjernBox - Profil212C
Box - Skrå (til træklods) - Styrbord113
10.0 mmBox - Bundplade113A
10.0 mmBox - Topplade113B
15.0 mmBox - Sideplader213C
10.0 mmBox - Indskud113D
15.0 mmBox - Indskud113E
50 x 10 FladjernBox - Profil213F
50 x 10 FladjernBox - Profil213G
50 x 10 FladjernBox - Profil213H
10.0 mmBox - Indskud113I
Box - Skrå (til træklods) - Bagbord114
10.0 mmBox - Bundplade114A
10.0 mmBox - Topplade114B
15.0 mmBox - Sideplader214C
10.0 mmBox - Indskud114D
15.0 mmBox - Indskud114E
50 x 10 FladjernBox - Profil214F
50 x 10 FladjernBox - Profil214G
50 x 10 FladjernBox - Profil214H
10.0 mmBox - Indskud114I
Ø 100Drejeakse415
15.0 mmLåsebeslag til drejeakse416
Inventor CAD-drawing - not to be modified by hand !
All measurements in mm unless otherwise stated.
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
OS
K-S
hip
Naval Architects & Marine Engineers
Aarhus
Balticagade 15 2nd floor
8000 Aarhus C - DENMARK
phone +45 8617 8099
Copenhagen
Fruebjergvej 3 - PO Box 26
2100 Copenhagen Oe - DENMARK
phone +45 4576 [email protected] www.osk-shiptech.com
Sign:
Sheet:
Id.no.:
Check: Scale:
Date:
Rev.:
Rev. Date Init.
Description of modifications Approv. by
Date
Tech A
/S
HOLM Klassen - Løftevugger
Løftevugge - Agter
Detaljer
JWE CFA 1:25
3/3
10.06.2013
130210.0286.01 A
A 05.07.2013 JWE General opdatering grundet øget vægt CFA 05.07.2013
ISO:
Pos. 1A Pos. 1BPos. 1C
1:10
Pos. 1D
1:10
Pos. 2A
(Pos. 2B - Kontra)
Pos. 2C
1:10
Pos. 2D Pos. 2E Pos. 2F
1:10
Pos. 3A
(Pos. 4A Kontra)
Pos. 3B-1
(Pos. 4B-1 Kontra)
Pos. 3C
(Pos. 4C Kontra)
Pos. 3B-2
(Pos. 4B-2 Ens)
1:20
Pos. 3B-3
(Pos. 4B-3 Ens)
1:20
Pos. 3B-4
(Pos. 4B-4 Ens)
1:20
Pos. 3E
(Pos. 4E Ens)
1:20
Pos. 5A Pos. 5B
1:20
Pos. 5C
1:20
Pos. 6 Pos. 7
600
x
400
Pos. 9A
1:10
Pos. 8B
1:10
Pos. 8A
1:20
Pos. 9B
1:20
Pos. 9C
1:20
Pos. 9D
1:20
Pos. 10
1:20
Pos. 11A
1:20
Pos. 11B
1:20
Pos. 12A
1:20
Pos. 12B
1:20
Pos. 12C
1:10
Pos. 13A
(Pos. 14A ens)
Pos. 13B
(Pos. 14B ens)
610
x
230
610
x
230
Pos. 13C
(Pos. 14C ens)
Pos. 13D
(Pos. 14D ens)
Pos. 13E
(Pos. 14E ens)
Pos. 13F
(Pos. 14F ens)
1:10
Pos. 13G
(Pos. 14G ens)
1:10
Pos. 13H
(Pos. 14H ens)
1:10
Pos. 15
1:10
Pos. 16
1:5
Det. 1 Det. 2 Det. 3 Det. 4 Det. 5 Det. 6 Det. 7
Pos. 3F
(Pos. 4F Ens)
1:20
Pos. 3D-1
(Pos. 4D-1 Ens)
Pos. 3D-2
(Pos. 4D-2 Ens)
Pos. 3G
(Pos. 4G ens)
1:10
Pos. 13I
(Pos. 14I ens)
7100 941
95,5 95,5
Det. 1Det. 1
95,5
17
0
R
1
8
200
10
0
3
4
R
5
7
Det. 2
Det. 3
Det. 4
16
0
243,5
R
2
5
7
4
,
2
°
1
0
5
,
8
°
47
,5
223,4
3065,5
Det. 5
79
,1
170,9
R
2
5
188,1
Det. 5
750
200
47
,5
Det. 1Det. 1
58,5
941
95,5 95,5
R
1
8
17
0
R
2
0
0
10
0
6
0
°
R
1
8
17
0
95,5
945
84,8
1522,8
7
9
°
Det. 6
Det. 7
7
9
°
1218,2
Det. 6
Det. 7
7
9
°
2717
84,8
3746,8
230
230
200
15
0
10
2
R
1
0
0
15
0
78
,2
10
2
R
10
0
75
200
30
M16
Det. 1
Det. 1
Det. 2Det. 2
Det. 6
Det. 7
910,8
Det. 1
1242,6 84,8
1480
230
230
Det. 2
R
1
0
0
10
2
15
0
200
7
4
°
865,7
1017,5
504
,8
508,8
15
137,2
300
R
3
0
90
,9
18
3,9
40,7
725,6
R
1
0
0
362,8
102
,4
43
6,7
R
1
0
0
25
2
5
95
407
230
20
0
230
20
0
444
55
60
3
0
°
17
0
941
R
2
5
90
31
7,5
120,5 120,5
941
19
0
120°
R
5
0
R
1
9
5
R
9
5
1150
37
6,3
1150
50
336,3
50
200
200
1235
11
50
47
,5
47,5
228 228 228 228 228
211
211
211
211
211
1155
102
0
155155
50
1150
500
1020
44
9,5
498
1020
30
0
92,5
710
50
50
300
50
442,5
25
17
147
55
70
100
4
5
°
127
38,5 38,5
30
4
0
°
R
3
6
1
8
4
0
°
5
5
°
4
0
°
4
0
°
3
5
°
2
0
°
3
0
°
2
0
°
Det. 1
Det. 1
3
0
°
3
0
°
300
25
100
3
4
R57
57
1
8
75
44
3
750
1020
15
4
5
°
Det. 2Det. 2
Reference tegninger:
130210.0109.01 General Arrangement
130210.0131.01 Løftevugger - Specifikation
130210.0286.01 Løftevugge - Agter, side 1 & 2
130210.0286.02 Løftevugge - For
130210.0286.03 Løftevugge - Træklodser
130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl
130210.1007.01 Løftevugger - Surringsarrangement
130210.1007.02 Løftevugger - Surringsarrangement - Bjælker & Kølbokse
8
4
,
1
°
211 211 211228 228 228 228 228
1
8
1
8
92,5
3
0
°
R
2
0
0
95,5
170
85
30
R
1
8
1
6
865
,7
115
2,9
R
5
0
61
8
1020
54
7
75
A-A
C-C
D-DB-B
Detalje 1
A
A
C
C
D
D
B
B
STYKLISTE
KommentarerRev.BeskrivelseStk.Pos.
Bundramme - Vandret11
TopRamme - Skrå22
Topramme - Lodret (bagbord)13
Topramme - Lodret (styrbord)14
Bjælke - Lodret45
Bjælke - Lodret46
Indskud - Lodret tværskibs47
Knæ - Tværskibs28
4 stk. bruges på Pos. 3 & 4 Knæ - Tværskibs4+49
Indskud - Lodret langskibs110
2 stk. bruges på Pos. 3 & 4 Stropstyr - Langsskibs3+211
Box - Vandret (til træklods)112
Box - Skrå (til træklods) - Styrbord
113
Box - Skrå (til træklods) - Bagbord114
Drejeakse415
Låsebeslag til drejeakse416
Bolt - M16 x 45mm817
Bolt - M16 x 55mm4018
Bolt - M16 x 60mm1219
Skiver - M1611220
Møtrik - M165221
Se tegning 130210.0286.04 Fjedersystem422
RUD - Type nr. VLBS-10 (10 tons WLL) D-Ring for surring til dæk423
Detalje 1
Inventor CAD-drawing - not to be modified by hand !
All measurements in mm unless otherwise stated.
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
OS
K-S
hip
Naval Architects & Marine Engineers
Aarhus
Balticagade 15 2nd floor
8000 Aarhus C - DENMARK
phone +45 8617 8099
Copenhagen
Fruebjergvej 3 - PO Box 26
2100 Copenhagen Oe - DENMARK
phone +45 4576 [email protected] www.osk-shiptech.com
Sign:
Sheet:
Id.no.:
Check: Scale:
Date:
Rev.:
Rev. Date Init.
Description of modifications Approv. by
Date
Tech A
/S
HOLM Klassen - Løftevugger
Løftevugge - For
Samlingstegning
JWE CFA 1:25
1/3
10.06.2013
130210.0286.02 A
A 05.07.2013 JWE General opdatering grundet øget vægt CFA 05.07.2013
ISO:
Set mod for
Set oppefra
BB SB
Set mod bagbord
1
8
12
6
7
5
6
5
11
11
4
0
°
10
75
,2
200
13
65
,2
11
5 5
1150
18
50
,1
10
11
15 15
1616
11
6 6
12
11
99
82
09
,3
257,8 1431,1257,81311,11431,1
6900
450450
1311,1
30
,0
1
8
22
22
Fuld gennembrænding
Fuld gennembrænding
Fuld gennembrænding
2
15
16
M16 Bolt (45mm), skive
7296,2
7
Fuld gennembrænding
128
5
128
5
23
23
Tyngdepunkt for beregning (Oplyst af FMT)
LCG: 11.49 m foran for AP
TCG: 0.00 m fra CL
VCG: 3.50 m over BL
Vægt: 125 t
Accelerationer:
Langskibs: +/- 9.81 m/s2 1.0 g
Tværskibs: +/- 9.81 m/s2 1.0 g
Vertikalt: +/- 5.60 m/s2 0.6 g
Samme acceleration langskibs/tværskibs, for at vugger kan stilles tværskibs og langskibs på Heavy Lift skib.
FMT - svejse og kvalitets specifikation:
Konstruktionen udføres i overensstemmelse med DS/EN 1090 - 2, udførelsesklasse EXC3.
Konstruktionen skal udføres af certificerede svejsere. Certificeringen skal dokumenteres før arbejdet iværksættes.
Der skal udarbejdes godkendte Welding Procedure Specifications (WPS) for alle svejsninger, før svejsning iværksættes.
Omfanget af procedureprøver skal aftales med svejseinspektør og procedureprøverne skal godkendes af samme, inden
noget svejsearbejde på nogen konstruktionsdel må iværksættes.
Svejsninger og svejseforberedelser (skærpning) skal godkendes af svejseinspektør, før svejsning iværksættes.
Svejseinspektør skal være godkendt efter gældende regler og standarder, således at vedkommende er kvalificeret til at
godkende arbejder efter DS/EN 1090-2.
Det anvendte stål skal svare til S355 J2 og skal enten være:
1. Stål med 3.2 certifikat.
2. Stål som er passende dokumenteret ved måling af flydespænding, brudforlængelse og slagsejhed.
Brudforlængelse skal være minimum 10 % og slagsejheden skal dokumenteres ved - 20 graders celcius. Se note *)
*) Note: Klassificeret plademateriale er relativt tilgængeligt på markedet, men profiler er ikke særlig tilgængelige.
Det vil ofte være nødvendigt at udføre særskilt prøvning.
Svejsegeometri:
Hvis ikke andet er anført på tegningerne gælder følgende:
Kantsømme: A-mål = 0.5 af mindste pladetykkelse.
K-sømme og X-sømme: fuldt gennembrændte.
Hvor svejsning udføres med fuld gennembrænding fuges og efterløbes.
Tvivlsspørgsmål afklares med svejseinspektør, så vidt muligt før arbejdet iværksættes.
Det færdige arbejde skal besigtiges af FMT før maling og sandblæsning.
Vægt
Stål vægt i alt: 6200 kg.
Reference tegninger:
130210.0109.01 General Arrangement
130210.0131.01 Løftevugger - Specifikation
130210.0286.01 Løftevugge - Agter
130210.0286.03 Løftevugge - Træklodser
130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl
130210.1007.01 Løftevugger - Surringsarrangement
130210.1007.02 Løftevugger - Surringsarrangement - Bjælker & Kølbokse
2
2
3
4
1314
B-B
A-A
B-B
STYKLISTE
KommentarerRev.BeskrivelseStk.Pos.
Bundramme - Vandret11
TopRamme - Skrå22
Topramme - Lodret (bagbord)13
Topramme - Lodret (styrbord)14
Bjælke - Lodret45
Knæ - Tværskibs28
4 stk. bruges på Pos. 3 & 4 Knæ - Tværskibs4+49
2 stk. bruges på Pos. 3 & 4 Stropstyr - Langsskibs3+211
Box - Vandret (til træklods)112
Box - Skrå (til træklods) - Styrbord113
Box - Skrå (til træklods) - Bagbord114
B
B
A
A
B
B
Inventor CAD-drawing - not to be modified by hand !
All measurements in mm unless otherwise stated.
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
OS
K-S
hip
Naval Architects & Marine Engineers
Aarhus
Balticagade 15 2nd floor
8000 Aarhus C - DENMARK
phone +45 8617 8099
Copenhagen
Fruebjergvej 3 - PO Box 26
2100 Copenhagen Oe - DENMARK
phone +45 4576 [email protected] www.osk-shiptech.com
Sign:
Sheet:
Id.no.:
Check: Scale:
Date:
Rev.:
Rev. Date Init.
Description of modifications Approv. by
Date
Tech A
/S
HOLM Klassen - Løftevugger
Løftevugge - For
Samlingstegning - Delsamlinger
JWE CFA 1:25
2/3
10.06.2013
130210.0286.02 A
A 05.07.2013 JWE General opdatering grundet øget vægt CFA 05.07.2013
ISO:
Pos. 1
Pos. 2
Pos. 3
(Pos. 4 kontra)
Pos. 3B
Pos. 3C kontra
(Pos. 4B kontra - Pos 4C ens)
Pos. 5 Pos. 8
1:20
Pos. 9
1:20
Pos. 11
1:20
Pos. 12
1:20
Pos. 3A
Pos. 4A kontra
Pos. 13
(Pos. 14 kontra)
Pos. 3D
(Pos. 4D ens)
450 200
1231,1
200
1111,1 515,6 1111,1
200
1231,1
200
6900
11
50
25
90
90
25
1A
1B
1C
1C
1C
1C
1D1D
Fuld gemmenbrænding
Fuld gemmenbrænding
Fuld gennembrænding
Fuld gennembrænding
629,6
2885,5
850
650
1147,5
2C
2D
2E
2F
2F
2A
2B
90
3B
270
15
15
Fuld gennembrænding
3B-4
3B-33B-1
3B-2
Fuld gennembrænding
54
54
42
Fuld gennembrænding
Fuld gennembrænding
15
1480 270
95
152,6
84,9
5A 5B
5C
90 90
8A
8B
693,4
15
92,5
77,5
9A
9C
9B
9D
11A
941
11B
163 300 300
1150
10
12A
12B
12C
537,1
2D
Fuld gennembrænding
2034,384,9
8
4
,
5
°
Fuld gennembrænding
11
115
0
11°
61
5,2
3
0
M16 Bolt (60mm), skive, møtrik
3A
3E
3F
3B&3C
3C
Fuld gennembrænding
5
0
15
15
105
2526
10
5
15
Fuld gennembrænding
3A-1
3A-2
3B-5
107
,5
835
107
,5
95
472,5 477,5
105
13H
13I
13H
13J
13H
13A
13C
13D
13E
13G
13F
9
3A-3 3A-3
25 3500
13K
13O
13B
13M
20
20
710
433
10
10
10
50
13F
13L13N
Tyngdepunkt for beregning (Oplyst af FMT)
LCG: 11.49 m foran for AP
TCG: 0.00 m fra CL
VCG: 3.50 m over BL
Vægt: 125 t
Accelerationer:
Langskibs: +/- 9.81 m/s2 1.0 g
Tværskibs: +/- 9.81 m/s2 1.0 g
Vertikalt: +/- 5.60 m/s2 0.6 g
Samme acceleration langskibs/tværskibs, for at vugger kan stilles tværskibs og langskibs på Heavy Lift skib.
FMT - svejse og kvalitets specifikation:
Konstruktionen udføres i overensstemmelse med DS/EN 1090 - 2, udførelsesklasse EXC3.
Konstruktionen skal udføres af certificerede svejsere. Certificeringen skal dokumenteres før arbejdet iværksættes.
Der skal udarbejdes godkendte Welding Procedure Specifications (WPS) for alle svejsninger, før svejsning iværksættes.
Omfanget af procedureprøver skal aftales med svejseinspektør og procedureprøverne skal godkendes af samme, inden
noget svejsearbejde på nogen konstruktionsdel må iværksættes.
Svejsninger og svejseforberedelser (skærpning) skal godkendes af svejseinspektør, før svejsning iværksættes.
Svejseinspektør skal være godkendt efter gældende regler og standarder, således at vedkommende er kvalificeret til at
godkende arbejder efter DS/EN 1090-2.
Det anvendte stål skal svare til S355 J2 og skal enten være:
1. Stål med 3.2 certifikat.
2. Stål som er passende dokumenteret ved måling af flydespænding, brudforlængelse og slagsejhed.
Brudforlængelse skal være minimum 10 % og slagsejheden skal dokumenteres ved - 20 graders celcius. Se note *)
*) Note: Klassificeret plademateriale er relativt tilgængeligt på markedet, men profiler er ikke særlig tilgængelige.
Det vil ofte være nødvendigt at udføre særskilt prøvning.
Svejsegeometri:
Hvis ikke andet er anført på tegningerne gælder følgende:
Kantsømme: A-mål = 0.5 af mindste pladetykkelse.
K-sømme og X-sømme: fuldt gennembrændte.
Hvor svejsning udføres med fuld gennembrænding fuges og efterløbes.
Tvivlsspørgsmål afklares med svejseinspektør, så vidt muligt før arbejdet iværksættes.
Det færdige arbejde skal besigtiges af FMT før maling og sandblæsning.
Vægt
Stål vægt i alt: 6200 kg.
Reference tegninger:
130210.0109.01 General Arrangement
130210.0131.01 Løftevugger - Specifikation
130210.0286.01 Løftevugge - Agter
130210.0286.03 Løftevugge - Træklodser
130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl
130210.1007.01 Løftevugger - Surringsarrangement
130210.1007.02 Løftevugger - Surringsarrangement - Bjælker & Kølbokse
440
27
04
40
3D3D
Fuld gennembrænding
Fuld gennembrænding
3D-1
15
750
135
3D-2
STYKLISTE
KommentarerRev.MaterialeBeskrivelseStk.Pos.
Bundramme - Vandret11
HEB 200Tværskibs bjælke21A
HEB 200Langskibs bjælke21B
15.0 mmIndskud281C
20.0 mmØjeplade41D
TopRamme - Skrå
22
HEB 200Tværskibs bjælke1+12A
HEB 200Tværskibs bjælke1+12B
9.0 mmTværskibs indskud2+22C
15.0 mmLangskibs indskud2+22D
15.0 mmLangskibs indskud2+22E
15.0 mmIndskud6+62F
Topramme - Lodret (bagbord)13
Lodret bjælke13A
HEB 200Lodret bjælke13A-1
15.0 mmSamlebeslag13A-2
10.0 mmIndskud til wire43A-3
Lodret bjælke1+13B+C
HEB 200Lodret bjælke1+13B+C-1
20.0 mmEndeplade1+13B+C-2
40.0 mmDrejebeslag1+13B+C-3
40.0 mmDrejebeslag1+13B+C-4
15.0 mmSamlebeslag1+13B+C-5
Langsskibs Indskud23D
15.0 mmLangsskibs Indskud13D-1
15.0 mmLangsskibs Indskud13D-2
10.0 mmLodret indskud23E
Topramme - Lodret (styrbord)14
Lodret bjælke14A
HEB 200Lodret bjælke14A-1
15.0 mmSamlebeslag14A-2
10.0 mmIndskud til wire34A-3
Lodret bjælke1+14B+C
HEB 200Lodret bjælke1+14B+C-1
20.0 mmEndeplade1+14B+C-2
40.0 mmDrejebeslag1+14B+C-3
40.0 mmDrejebeslag1+14B+C-4
15.0 mmSamlebeslag1+14B+C-5
Langsskibs Indskud24D
15.0 mmLangsskibs Indskud14D-1
15.0 mmLangsskibs Indskud14D-2
10.0 mmLodret indskud24E
Bjælke - Lodret45
HEB 200Lodret bjælke45A
20.0 mmEndeplade45B
40.0 mmDrejebeslag45C
HEB 200Bjælke - Lodret46
10.0 mmIndskud - Lodret tværskibs47
Knæ - Tværskibs28
10.0 mmKnæ - Tværskibs28A
15.0 mmLodret indskud48B
4 stk. bruges på Pos. 3 & 4 Knæ - Tværskibs4+49
15.0 mmKnæ - Tværskibs4+49A
15.0 mmEndeplade4+49B
10.0 mmFlange4+49C
5.0 mm GummiEndeplade - Tryklag4+49D
15.0 mmIndskud - Lodret langskibs110
2 stk. bruges på Pos. 3 & 4 Stropstyr - Langsskibs3+211
Ø 190 x 15.0Stropstyr - Rør511A
15.0 mmStropstyr - Ledeplade1511B
Box - Vandret (til træklods)112
15.0 mmBox - Plade112A
50 x 10 FladjernBox - Profil212B
50 x 10 FladjernBox - Profil212C
Box - Skrå (til træklods) - Styrbord113
10.0 mmBox - Bundplade113A
10.0 mmBox - Topplade113B
15.0 mmBox - Sideplade113C
15.0 mmBox - Sideplade113D
10.0 mmBox - Indskud113E
10.0 mmBox - Indskud113F
15.0 mmBox - Indskud113G
50 x 10 FladjernBox - Profil313H
50 x 10 FladjernBox - Profil113I
50 x 10 FladjernBox - Profil113J
50 x 10 FladjernBox - Profil113K
50 x 10 FladjernBox - Profil113L
50 x 10 FladjernBox - Profil113M
50 x 10 FladjernBox - Profil113N
50 x 10 FladjernBox - Profil113O
Box - Skrå (til træklods) - Bagbord114
10.0 mmBox - Bundplade114A
10.0 mmBox - Topplade114B
15.0 mmBox - Sideplade114C
15.0 mmBox - Sideplade114D
10.0 mmBox - Indskud114E
10.0 mmBox - Indskud114F
15.0 mmBox - Indskud114G
50 x 10 FladjernBox - Profil314H
50 x 10 FladjernBox - Profil114I
50 x 10 FladjernBox - Profil114J
50 x 10 FladjernBox - Profil114K
50 x 10 FladjernBox - Profil114L
50 x 10 FladjernBox - Profil114M
50 x 10 FladjernBox - Profil114N
50 x 10 FladjernBox - Profil114O
Ø 100Drejeakse415
15.0 mmLåsebeslag til drejeakse416
Inventor CAD-drawing - not to be modified by hand !
All measurements in mm unless otherwise stated.
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
OS
K-S
hip
Naval Architects & Marine Engineers
Aarhus
Balticagade 15 2nd floor
8000 Aarhus C - DENMARK
phone +45 8617 8099
Copenhagen
Fruebjergvej 3 - PO Box 26
2100 Copenhagen Oe - DENMARK
phone +45 4576 [email protected] www.osk-shiptech.com
Sign:
Sheet:
Id.no.:
Check: Scale:
Date:
Rev.:
Rev. Date Init.
Description of modifications Approv. by
Date
Tech A
/S
HOLM Klassen - Løftevugger
Løftevugge - For
Detaljer
JWE CFA 1:25
3/3
10.06.2013
130210.0286.02 A
A 05.07.2013 JWE General opdatering grundet øget vægt CFA 05.07.2013
ISO:
Pos. 1A Pos. 1BPos. 1C
1:10
Pos. 1D
1:10
Pos. 2A
(Pos. 2B - Kontra)
Pos. 2C
1:10
Pos. 2D Pos. 2E Pos. 2F
1:10
Pos. 3A-1
(Pos. 4A-1 Kontra)
Pos. 3B-1
Pos. 3C-1 Kontra
(Pos. 4B-1 kontra - Pos. 4C-1 ens)
Pos. 3B-2
(Pos. 4B-2 Ens)
1:20
Pos. 3B-3
(Pos. 4B-3 Ens)
1:20
Pos. 3B-4
(Pos. 4B-4 Ens)
1:20
Pos. 3E
(Pos. 4E Ens)
1:20
Pos. 5APos. 5B
1:20
Pos. 5C
1:20
Pos. 6Pos. 7
600
x
400
Pos. 9A
1:10
Pos. 8B
1:10
Pos. 8A
1:20
Pos. 9B
1:20
Pos. 9C
1:20
Pos. 9D
1:20
Pos. 10
1:20
Pos. 11A
1:20
Pos. 11B
1:20
Pos. 12A
1:20
Pos. 12B
1:20
Pos. 12C
1:10
Pos. 13A
(Pos. 14A ens)
Pos. 13B
(Pos. 14B kontra)
Pos. 13E
(Pos. 14E ens)
Pos. 13G
(Pos. 14G ens)
Pos. 13J
(Pos. 14J ens)
1:10
Pos. 13O
(Pos. 14O ens)
1:10
Pos. 13H
(Pos. 14H ens)
1:10
Pos. 15
1:10
Pos. 16
1:5
Det. 1 Det. 2 Det. 3 Det. 4 Det. 5 Det. 6 Det. 7
Pos. 3A-2
(Pos. 4A-2 ens)
Pos. 3B+C-5
(Pos. 4B+C-5 ens)
Pos. 3F
(Pos. 4F Ens)
Pos. 13C
(Pos. 14C kontra)
Pos. 13I
(Pos. 14I ens)
1:10
Pos. 13K
(Pos. 14K ens)
1:10
Pos. 13L
(Pos. 14L ens)
1:10
Pos. 13M
(Pos. 14M ens)
1:10
Pos. 13D
(Pos. 14D kontra)
Pos. 13F
(Pos. 14F ens)
Pos. 13N
(Pos. 14N ens)
1:10
Pos. 3A-3
(Pos. 4A-3 ens)
Pos. 3D-1
(Pos. 4D-1 Ens)
Pos. 3D-2
(Pos. 4D-2 Ens)
6900 941
95,5 95,5
Det. 1Det. 1
95,5
17
0
R
1
8
200
10
0
3
4
R
5
7
Det. 2
59
,7
160,1
R
2
5
180
Det. 5
750
200
47
,5
Det. 1Det. 1
58,5
941
95,5 95,5
R
1
8
17
0
R
2
0
0
10
0
6
0
°
R
1
8
17
0
95,5
230
23
0
200
150
1
0
2
R
1
0
0
15
0
78
,2
10
2
R
1
0
0
75
200
30
M16
Det. 1
Det. 2
Det. 2
630
75
Det. 1
1242,6 84,8
1480
230
230
Det. 2
R
1
0
0
10
2
150
200
7
9
°
927
1231,1
52
3,2
615,6
15
155,7
300
R
3
0
96,7
188
,6
23,1
693,4
346,7
66
697
,1
25
95
677,1
230
200
230
200
480
55
60
3
0
°
170
941
R
2
5
236
,5
44
2,7
120,5 120,5
941
1
90
120°
R
5
0
R
1
9
5
R
9
5
1150
36
0
1150
50
320
50
10
50
769
,7
84
8
92,5 92,5717,3
50
50
413
50
446,6
25
17
147
55
70
10
0
4
5
°
127
38,5 38,5
30
4
0
°
R
3
6
1
8
4
0
°
5
0
°
4
0
°
4
0
°
3
1
0
°
2
5
°
4
5
°
3
5
°
Det. 1Det. 1
1
0
0
,
8
°
Det. 4
Det. 3
215,6
R
2
5
160
Det. 5
546,5
47
,5
7
9
,
2
°
211 211 211
Det. 6
Det. 7
3732,2
8
4
,
5
°
2034,384,9
2526
Det. 6
Det. 7
8
4
,
5
°
230
41
0
57,5
45
45
160
16
0
115
115
160
16
0
45
45
57,5
41
0
230 300
57
10
0
25
3
4
R
5
7
Det. 2
R
5
0
2
5
R
1
0
0
R
1
0
0
3
0
°
3
0
°
271,7
1150
47,5
211 211 211 211 211
47,5
19
1
19
1
191
191
19
1
20
0
200
1
8
1150
95
2,1
35
3,1
25
0
R
2
0
0
43
1,4
270
50
407
50
324,7
50
226
50
Reference tegninger:
130210.0109.01 General Arrangement, 130210.0131.01 Løftevugger - Specifikation
130210.0286.01 Løftevugge - Agter, 130210.0286.02 Løftevugge - For, side 1 & 2
130210.0286.03 Løftevugge - Træklodser, 130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl, 130210.1007.01 Løftevugger - Surringsarrangement
130210.1007.01 Løftevugger - Surringsarrangement - Bjælker & Kølbokse
191 191 191 191 191
1165,7
8
5
,
8
°
73,1
99
7,4
15
6,2
155
,9
23
0,5
230
83,4
20
1,2
41
1,4
R
5
0
R
5
0
76
1,3
9
Det. 5
1150
52
8,1
33
7,3
Det. 5
835835
835
535,5
50
927
,2
51
0,6
17
0
95,5
R
1
8
85
1
6
92
9,8
116
4,2
Det. 2Det. 2
750
30
2,6
1020
4
5
°
15
75
8
1
,
6
°
8
1
,
6
°
8
1
,
6
°
Fjeder Data
Vugge d (mm) k (kg/mm) Forbelastet (kg) Normal last (kg) Max Udstrækning (kg)
For 14 13,2 1710 2263 3157
Agter 14 13,2 1710 2263 3157
45
0
d
13
03
20
17
22
78
42
Fri Længde Forbelastet Normal Belastet
24
02
10
Max Udstrækning
75
Vantskrue M24 -
Fyns Kran Udstyr
Varenr.: 260400-M24
M24 Møtrik m. skive
Låses i forbelastet
position
M10 Bolt
M24 Møtrik
med skive
Fuld
Gennembr.
(Se det. 2)
Kval. 8.8
4
2
4
0
°
Detalje 1
Skala 1:2
Detalje 2
Skala 1:2
4
0
°
Ø
8
0
Ø
1
8
12
80
12
60
30
Ø
1
1
0
Bundprop
Fuld
Gennembr.
(Se det. 1)
Fuld
Gennembr.
(Se det. 2)
Ø
1
1
Ø
8
8
.
9
(
D
I
N
2
4
4
0
)
Inspektions
sprække
Forspændings
markering
46
2
Ø
1
0
0
5
Ø
1
1
30
Cylinder
Præc. Rør DIN 2393 100/5,0 mm.
15
30
7
13
0
14
2
92
M24 Gevindstang
55
0
Ø
1
1
0
12
Top Plade
12
Stempelplade
Ø
8
8
Ø
2
6
Ø
2
6
Id.no.:
Sign: Scale:
Sheet: Date:
Aarhus
Balticagade 15 2 floor
Copenhagen
2100 Copenhagen Oe - DENMARK8000 Aarhus C - DENMARK
nd
Bryggervangen 55 1.tv
[email protected] www.osk-shiptech.com phone +45 4576 4210phone +45 8617 8099
Rev.
Check:
This Document is the property of OSK-ShipTech A/S and may not be altered
or passed on to third parties without written consent from OSK-ShipTech A/S
CAD - drawing - Not to be modified by hand !
All measurements in mm unless otherwise stated.
Approv. byRev. Init.Date Description of modifications Date
ISO:
HOLM Klassen - Løftevugger
Fjeder System
JAK KAF 1:5
1/1
21.06.2013
130210.0286.04 A
A 05.07.2013 JAK Generel opdateret grundet øget vægt KAF 05.07.2013
Tyngdepunkt for beregning (Oplyst af FMT)
LCG: 11.49 m foran for AP
TCG: 0.00 m fra CL
VCG: 3.50 m over BL
Vægt: 125 t
Accelerationer:
Langskibs: +/- 9.81 m/s2 1.0 g
Tværskibs: +/- 9.81 m/s2 1.0 g
Vertikalt: +/- 5.60 m/s2 0.6 g
Samme acceleration langskibs/tværskibs, for at vugger kan stilles tværskibs og langskibs på Heavy Lift skib.
FMT - svejse og kvalitets specifikation:
Konstruktionen udføres i overensstemmelse med DS/EN 1090 - 2, udførelsesklasse EXC3.
Konstruktionen skal udføres af certificerede svejsere. Certificeringen skal dokumenteres før arbejdet
iværksættes.
Der skal udarbejdes godkendte Welding Procedure Specifications (WPS) for alle svejsninger, før svejsning
iværksættes.
Omfanget af procedureprøver skal aftales med svejseinspektør og procedureprøverne skal godkendes af
samme, inden
noget svejsearbejde på nogen konstruktionsdel må iværksættes.
Svejsninger og svejseforberedelser (skærpning) skal godkendes af svejseinspektør, før svejsning
iværksættes.
Svejseinspektør skal være godkendt efter gældende regler og standarder, således at vedkommende er
kvalificeret til at
godkende arbejder efter DS/EN 1090-2.
Det anvendte stål skal svare til S355 J2 og skal enten være:
1. Stål med 3.2 certifikat.
2. Stål som er passende dokumenteret ved måling af flydespænding, brudforlængelse og slagsejhed.
Brudforlængelse skal være minimum 10 % og slagsejheden skal dokumenteres ved - 20 graders celcius.
Se note *)
*) Note: Klassificeret plademateriale er relativt tilgængeligt på markedet, men profiler er ikke særlig
tilgængelige.
Det vil ofte være nødvendigt at udføre særskilt prøvning.
Svejsegeometri:
Hvis ikke andet er anført på tegningerne gælder følgende:
Kantsømme: A-mål = 0.5 af mindste pladetykkelse.
K-sømme og X-sømme: fuldt gennembrændte.
Hvor svejsning udføres med fuld gennembrænding fuges og efterløbes.
Tvivlsspørgsmål afklares med svejseinspektør, så vidt muligt før arbejdet iværksættes.
Det færdige arbejde skal besigtiges af FMT før maling og sandblæsning.
Reference tegninger:
130210.0109.01 General Arrangement
130210.0131.01 Løftevugger - Specifikation
130210.0286.01 Løftevugge - Agter
130210.0286.02 Løftevugge - For
130210.0286.03 Løftevugge - Træklodser
130210.0286.04 Løftevugger - Fjedersystem
130210.0286.11 Strength calculation - Lifting Cradles - HOLM-Kl
130210.0327.01 Løftevugger - Positionering af vugger
130210.1007.01 Løftevugger - Surrings Arrangement
130210.1007.02 Løftevugger - Surrings Arrangement - Bjælker & Kølklodser
______________________________________________________________________________________ 130210.0266.01 Lifting and transport Cradles Page 15
Appendix B
3D Model Results. Aft Cradle
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CONTENTS CONTENTS General Data 1 3.3 Cross sections - Internal Forces 7Structure 1 3.4 Nodes - Support Forces 8
1.1 Nodes 1 Graph. Deformations u, LC1: Self-weight 81.2 Materials 2 Graph. Members N, LC1: Self-weight 91.3 Cross-sections 2 STEEL 101.7 Members 2 CA1 - General stress analysis of 101.8 Nodal Supports 3 steel members 10Graph. Structure 3 1.1.1 General Data 10Graph. Structure 4 1.1.2 Details 10
Loads 5 1.2.1 Materials 10 Load Cases 5 1.3.1 Cross-Sections 10 LC 1 5 Results 11
Graph. LC1 5 2.1 Stresses by Cross-Section 11Graph. LC1 6 2.3 Stresses by Member 11
Results - Load Cases, Load Groups 7 Graph. STEEL - Members Sigma-eqv, CA1 143.0 Results - Summary 7
GENERAL DATA
COMPUTING METHOD
Structural Analysis Linear Static Analysis Design Second-Order Analysis (Non-linear, Timoshenko) Dynamic Analysis Large Deformation Analysis (Non-linear, Newton-Raphson)
Postcritical Analysis (Non-linear, Newton-Raphson)
Load Cases Design Cases Load Groups Dynamic Cases Load Combinations Buckling Curves
STRUCTURAL DATA PARAMETERS
1D Continuous Beam 38 Nodes 64 Elements 2D Construction Type 1 Materials 0 Cables 3D Construction Type 4 Sections 0 Tapered Elements Grid 1 Element Hinges 0 Elastic Foundations
0 Element Partitions 0 Sets of Elements
1.1 NODES NodeNo.
ReferenceNode
CoordinateSystem
Node coordinatesX [mm] Y [mm] Z [mm] Comment
1 - Cartesian 0 -949 47002 - Cartesian 475 0 03 - Cartesian -475 0 04 - Cartesian 475 2900 05 - Cartesian -475 2900 06 - Cartesian 0 949 47008 - Cartesian 475 0 5409 - Cartesian -475 0 540
10 - Cartesian 475 2900 142511 - Cartesian -475 2900 142512 - Cartesian 475 -2900 013 - Cartesian -475 -2900 016 - Cartesian 475 3350 017 - Cartesian -475 3350 018 - Cartesian 475 -2900 142519 - Cartesian -475 -2900 142520 - Cartesian 475 -3350 021 - Cartesian -475 -3350 024 - Cartesian 475 1890 111725 - Cartesian 475 -1890 111726 - Cartesian -475 1890 111727 - Cartesian -475 -1890 111728 - Cartesian -475 1890 029 - Cartesian 475 1890 030 - Cartesian -475 -1890 031 - Cartesian 475 -1890 032 - Cartesian -475 0 27033 - Cartesian 475 0 27044 - Cartesian -475 1706 171945 - Cartesian 475 1706 171946 - Cartesian -475 -1706 171947 - Cartesian 475 -1706 171949 - Cartesian 0 -1706 171950 - Cartesian 0 1706 171951 - Cartesian 0 0 54054 - Cartesian 0 2900 055 - Cartesian 0 -2900 056 - Cartesian 0 0 4700
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1.2 MATERIALS Material
No.Material
DescriptionE-ModulusE [kN/cm2]
G-ModulusG [kN/cm2]
Sp. Weight [kN/m3]
Coeff. Thermal [1/°C]
Saf. FactorM [-]
1 Steel S 235 | DIN 18800:1990-11 21000.00 8100.00 78.50 1.2000E-05 1.100
1.3 CROSS-SECTIONS Section
No.Cross-sectionDescription
Mater.No.
IT [cm4]A [cm2]
Iy [cm4]Ay [cm2]
Iz [cm4]Az [cm2]
1 HE-B 200 1 59.50 5700.00 2000.0078.10 50.07 15.37
2 Pipe 190/15/K 1 6421.93 3180.13 3180.1382.47 41.08 41.08
3 Dummy Rigid 0.00
4 IS 600/200/10/20/0 1 119.28 81941.33 2671.33136.00 80.00 56.00
1.7 MEMBERS Member
No. MemberNode
Start EndRotation
Type [°] / PlaneCross-sectionStart End
Release No.Start End
Ecc.No.
Div.No.
LengthL [mm]
1 Beam 33 2 Angle 90.00 1 1 - - - - 270 Z2 Beam 4 10 Angle 90.00 1 1 - - - - 1425 Z3 Beam 4 16 Angle 0.00 1 1 - - - - 450 Y4 Beam 32 3 Angle 90.00 1 1 - - - - 270 Z5 Beam 26 11 Angle 0.00 1 1 - - - - 1056 YZ6 Beam 24 10 Angle 0.00 1 1 - - - - 1056 YZ7 Beam 26 44 Angle 180.00 4 4 - - - - 630 YZ8 Beam 8 33 Angle 90.00 1 1 - - - - 270 Z9 Beam 2 29 Angle 0.00 1 1 - - - - 1890 Y
10 Beam 24 45 Angle 180.00 4 4 - - - - 630 YZ11 Beam 18 12 Angle 270.00 1 1 - - - - 1425 Z12 Beam 20 12 Angle 0.00 1 1 - - - - 450 Y13 Beam 19 27 Angle 0.00 1 1 - - - - 1056 YZ14 Beam 18 25 Angle 0.00 1 1 - - - - 1056 YZ15 Beam 29 4 Angle 0.00 1 1 - - - - 1010 Y16 Beam 46 27 Angle 180.00 4 4 - - - - 630 YZ17 Beam 5 11 Angle 90.00 1 1 - - - - 1425 Z18 Beam 5 17 Angle 0.00 1 1 - - - - 450 Y19 Beam 31 2 Angle 0.00 1 1 - - - - 1890 Y20 Beam 47 25 Angle 180.00 4 4 - - - - 630 YZ21 Beam 12 31 Angle 0.00 1 1 - - - - 1010 Y22 Beam 19 13 Angle 270.00 1 1 - - - - 1425 Z23 Beam 9 32 Angle 90.00 1 1 - - - - 270 Z24 Beam 3 28 Angle 0.00 1 1 - - - - 1890 Y25 Beam 21 13 Angle 0.00 1 1 - - - - 450 Y26 Beam 30 3 Angle 0.00 1 1 - - - - 1890 Y27 Beam 49 46 Node 25 / x-y 3 3 - - - - 475 X28 Beam 50 45 Node 24 / x-y 3 3 - - - - 475 X29 Compression 56 51 Angle 90.00 3 3 - - - - 4160 Z30 Beam 28 5 Angle 0.00 1 1 - - - - 1010 Y31 Beam 13 30 Angle 0.00 1 1 - - - - 1010 Y32 Beam 51 8 Angle 90.00 4 4 - - - - 475 X33 Beam 4 54 Angle 0.00 1 1 - - - - 475 X34 Beam 13 55 Angle 0.00 1 1 - - - - 475 X35 Beam 8 24 Angle 0.00 1 1 - - - - 1976 YZ36 Beam 25 8 Angle 0.00 1 1 - - - - 1976 YZ37 Beam 9 26 Angle 0.00 1 1 - - - - 1976 YZ38 Beam 27 9 Angle 0.00 1 1 - - - - 1976 YZ39 Compression 1 49 Angle 90.00 3 3 - - - - 3075 YZ40 Beam 26 28 Angle 90.00 1 1 - - - - 1117 Z41 Beam 24 29 Angle 90.00 1 1 - - - - 1117 Z42 Beam 30 27 Angle 270.00 1 1 - - - - 1117 Z43 Beam 31 25 Angle 270.00 1 1 - - - - 1117 Z44 Compression 6 50 Angle 90.00 3 3 - - - - 3075 YZ45 Beam 54 5 Angle 0.00 1 1 - - - - 475 X46 Beam 1 56 Angle 0.00 3 3 - - - - 949 Y47 Beam 55 12 Angle 0.00 1 1 - - - - 475 X48 Beam 32 33 Angle 0.00 2 2 - - - - 950 X49 Beam 56 6 Angle 0.00 3 3 - - - - 949 Y65 Beam 11 10 Angle 50.20 2 2 - - - - 950 X66 Beam 44 50 Node 24 / x-y 3 3 - - - - 475 X67 Beam 9 51 Angle 90.00 4 4 - - - - 475 X68 Beam 18 19 Angle 50.20 2 2 - - - - 950 X69 Beam 47 49 Node 25 / x-y 3 3 - - - - 475 X70 Beam 24 4 Angle 90.00 3 3 - - - - 1506 YZ71 Beam 26 5 Angle 90.00 3 3 - - - - 1506 YZ72 Beam 25 12 Angle 90.00 3 3 - - - - 1506 YZ73 Beam 27 13 Angle 90.00 3 3 - - - - 1506 YZ74 Beam 49 51 Angle 0.00 3 3 - - - - 2074 YZ75 Beam 51 50 Angle 0.00 3 3 - - - - 2074 YZ76 Beam 19 30 Angle 0.00 3 3 - - - - 1747 YZ77 Beam 31 18 Angle 0.00 3 3 - - - - 1747 YZ78 Beam 29 10 Angle 0.00 3 3 - - - - 1747 YZ79 Beam 28 11 Angle 0.00 3 3 - - - - 1747 YZ
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1.8 NODAL SUPPORTS Support
No. Nodes No.Rotation [°]
Sequen. about X about Y about ZSupport Conditions
uX' uY' uZ' X' Y' Z'
3 56 XYZ 0.00 0.00 0.004 54,55 XYZ 0.00 0.00 0.00
Y
Z
X
Isometric
STRUCTURE
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Y
Z
X
Isometric
STRUCTURE
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LOAD CASES LCNo. LC Description LC Factor Property of load case Self-weight
Method ofAnalysis
1 1.0000 Variable - Linear
2.2 MEMBER LOADS LC1LC1
No. Reference toOn members No.On sets of m. No.
LoadType
LoadDistribution
LoadDirection
ReferenceLength
Load ParametersSymbol Value Unit
2 Members 48 Force 2 x P Z True Length P1 154.39 kNP2 154.39 kNA 33.330 %B 33.330 %
7 Members 65,68 Force 2 x P z True Length P1 -218.8 kNP2 -218.8 kNA 33.330 %B 33.330 %
218.800 218.800
Y
154.400 154.400
Z
X
218.800 218.800
IsometricLC1
LC1
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X
218.800
218.800
154.400
Y
Z
218.800
154.400
218.800
In X-directionLC1
1000.00 [mm]
LC1
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3.0 RESULTS - SUMMARY Description Value Unit Comment
LC1 Sum of Loads in X 0.00 kN Sum of Support Reactions in X 0.00 kN Sum of Loads in Y 0.00 kN Sum of Support Reactions in Y 0.00 kN Sum of Loads in Z 869.02 kN Sum of Support Reactions in Z 869.02 kN Deviation 0.00% Max Displacement in X 0.2 mm Member No. 31, x: 707 mm Max Displacement in Y 0.6 mm Member No. 68, x: 475 mm Max Displacement in Z 0.6 mm Member No. 48, x: 475 mm Max Vectorial Displacement 0.8 mm Member No. 68, x: 475 mm Max rotation about X 0.3 mrad Member No. 5, x: 581 mm Max Rotation about Y 0.9 mrad Member No. 48, x: 808 mm Max Rotation about Z 1.1 mrad Member No. 68, x: 808 mm Method of Analysis Linear Linear Static Analysis Number of Iterations 1Summary Number of 1D Finite Elements (member elements) 64 Number of FE nodes 38 Number of Equations 228 Matrix Solver Method Direct Max Number of Iterations 100 Number of Load Increments 1 Divisions of members for member results 10 Divisions of cable, foundation or tapered members 10 Activate shear rigidity (A-y, A-z) of members No Activate Failed Members Yes
3.3 CROSS SECTIONS - INTERNAL FORCES Member
No. LC/LGNodeNo.
Locationx [mm]
Shear Forces [kN]N Vy Vz
Moments [kNm]MT My Mz
Section No. 1: HE-B 20017 LC1 MAX N 0 138.34 8.42 -4.94 -0.03 4.28 4.3914 LC1 MIN N 0 -189.28 -10.59 14.03 -0.04 -6.38 -8.1731 LC1 MAX Vy 0 56.57 21.85 -10.37 -0.03 4.16 7.5330 LC1 MIN Vy 0 56.57 -21.85 10.37 0.03 -6.31 -14.5414 LC1 MAX Vz 0 -189.28 -10.59 14.03 -0.04 -6.38 -8.175 LC1 MIN Vz 0 -189.28 -10.59 -14.03 -0.04 8.43 -3.02
40 LC1 MAX MT 0 -41.99 10.28 -8.82 0.04 3.95 3.6942 LC1 MIN MT 0 -41.98 -10.28 8.82 -0.04 -5.89 -7.8024 LC1 MAX My 1890 87.34 -6.09 8.80 0.00 9.64 7.5124 LC1 MIN My 0 87.34 -6.09 8.80 0.00 -6.99 -4.008 LC1 MAX Mz 270 -136.79 -18.47 0.00 0.00 0.00 20.53
23 LC1 MIN Mz 270 -136.82 18.47 0.00 0.00 0.00 -20.53Section No. 2: Pipe 190/15/K
65 LC1 MAX N 0 3.31 0.00 -218.82 0.00 32.12 -0.4448 LC1 MIN N 0 -6.29 0.00 -154.42 0.00 23.81 0.0048 LC1 MAX Vy 0 -6.29 0.00 -154.42 0.00 23.81 0.0065 LC1 MIN Vy 0 3.31 0.00 -218.82 0.00 32.12 -0.4468 LC1 MAX Vz 633 3.31 0.00 218.78 0.00 -37.17 -0.4465 LC1 MIN Vz 0 3.31 0.00 -218.82 0.00 32.12 -0.4448 LC1 MAX MT 0 -6.29 0.00 -154.42 0.00 23.81 0.0068 LC1 MIN MT 0 3.31 0.00 -218.82 0.00 32.12 -0.4468 LC1 MAX My 950 3.31 0.00 218.78 0.00 32.12 -0.4465 LC1 MIN My 633 3.31 0.00 -0.02 0.00 -37.17 -0.4448 LC1 MAX Mz 950 -6.29 0.00 154.38 0.00 23.81 0.0065 LC1 MIN Mz 0 3.31 0.00 -218.82 0.00 32.12 -0.44
Section No. 3: Dummy Rigid77 LC1 MAX N 0 48.24 5.48 -7.28 -22.54 21.84 6.3929 LC1 MIN N 0 -369.57 0.00 0.00 0.00 0.00 0.0069 LC1 MAX Vy 0 9.35 223.14 149.35 14.84 0.01 -2.4828 LC1 MIN Vy 0 9.36 -223.13 -149.33 -14.84 70.94 -108.4874 LC1 MAX Vz 0 -238.79 0.01 274.38 0.01 -29.68 0.0275 LC1 MIN Vz 0 -238.79 0.01 -274.38 0.00 539.41 0.0176 LC1 MAX MT 0 48.23 -5.48 7.28 22.54 9.13 -3.1979 LC1 MIN MT 0 48.24 5.48 -7.28 -22.54 21.84 6.3974 LC1 MAX My 2074 -238.79 0.01 274.38 0.01 539.41 0.0175 LC1 MIN My 2074 -238.79 0.01 -274.38 0.00 -29.68 0.0077 LC1 MAX Mz 0 48.24 5.48 -7.28 -22.54 21.84 6.3969 LC1 MIN Mz 475 9.35 223.14 149.35 14.84 70.95 -108.48
Section No. 4: IS 600/200/10/20/067 LC1 MAX N 0 19.75 94.87 0.00 0.00 0.00 16.2220 LC1 MIN N 0 -223.14 9.35 -149.35 -0.01 14.84 2.4867 LC1 MAX Vy 0 19.75 94.87 0.00 0.00 0.00 16.2232 LC1 MIN Vy 0 19.75 -94.85 0.00 0.00 0.00 -28.847 LC1 MAX Vz 0 -223.13 9.35 149.33 -0.01 -79.24 3.41
20 LC1 MIN Vz 0 -223.14 9.35 -149.35 -0.01 14.84 2.4816 LC1 MAX MT 0 -223.12 -9.36 -149.31 0.01 14.83 -2.497 LC1 MIN MT 0 -223.13 9.35 149.33 -0.01 -79.24 3.41
20 LC1 MAX My 0 -223.14 9.35 -149.35 -0.01 14.84 2.4820 LC1 MIN My 630 -223.14 9.35 -149.35 -0.01 -79.25 -3.4167 LC1 MAX Mz 0 19.75 94.87 0.00 0.00 0.00 16.2267 LC1 MIN Mz 475 19.75 94.87 0.00 0.00 0.00 -28.84
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3.4 NODES - SUPPORT FORCES NodeNo. LC/LG
Support forces [kN]PX' PY' PZ'
Support moments [kNm]MX' MY' MZ'
54 LC1 -0.01 0.00 0.00 0.02 0.01 0.0055 LC1 0.01 0.00 0.00 -0.02 0.00 0.0056 LC1 0.00 0.00 869.02 0.00 0.00 0.00
Suppo LC1 0.00 0.00 869.02 Loads 0.00 0.00 869.02
Y
Z
X
0.8
IsometricLC1u
Factor of deformations: 500.00Max u: 0.8, Min u: 0.0 [mm]
DEFORMATIONS U, LC1: SELF-WEIGHT
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-19.40
56.57
138.3148.24
-151.53
-189.28
56.57
-41.9948.23
-151.55
-189.25
-41.98
87.34
9.36
-51.55
-223.13
87.34Y
-238.79
17.59
-257.67
-136.8219.75
Z
X
19.75
17.59
-136.79
87.34
-63.46
-238.79
-369.57
87.35
-51.53
-41.98
-223.12
-63.46
56.57
9.36
-257.67
-151.54 -41.99
-223.14
48.23
9.35
-189.25
56.57
-151.55
-19.40
48.24
-19.39
3.31
IsometricLC1N
Max N: 138.34, Min N: -369.57 [kN]
MEMBERS N, LC1: SELF-WEIGHT
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1.1.1 GENERAL DATA STEELCA1General stress analysis ofsteel members
Members to design: AllLoad cases to design: LC1
1.1.2 DETAILS Allow local plastification:Calculate normal stresses with Alpha-pl:
FACTORS FOR SIGMA-EQVSigma 1.00Tau 3.00
Simplified consideration of eccentric loading:
1.2.1 MATERIALS MatNo
MaterialDescription
Partial FactorM [-]
Yield Strengthfyk [N/mm2]
Limit Stresses [N/mm2]Manually limit x limit limit eqv
1 Steel S 235* 1.50 235.0 156.7 90.5 156.7
1.3.1 CROSS-SECTIONS SecNo
MatNo
Cross-Section Description It [cm4]A [cm2]
Iy [cm4]Alphapl,y
Iz [cm4]Alphapl,z Comment
1 1 HE-B 200 59.50 5700.00 2000.0078.10 1.126 1.529
2 1 Pipe 190/15/K 6421.93 3180.13 3180.1382.47 1.376 1.376
3 0 Dummy Rigid 0.00 0.00 0.000.00 1.00 1.00
The section will not be designed because the characteristic stresses are invalid!4 1 IS 600/200/10/20/0 119.28 81941.30 2671.33
136.00 1.136 1.55
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2.1 STRESSES BY CROSS-SECTION STEELCA1General stress analysis ofsteel members
SecNo
MemberNo
Loc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
1 HE-B 200 23 270 1 LC1 Sigma Total -120.2 156.7 0.77 5 0 13 LC1 Tau Total -9.3 90.5 0.10 23 270 6 LC1 Sigma-eqv 120.2 156.7 0.77 2 Pipe 190/15/K 65 633 28 LC1 Sigma Total 111.5 156.7 0.71 68 0 1 LC1 Tau Total -52.2 90.5 0.58 65 633 28 LC1 Sigma-eqv 111.5 156.7 0.71 4 IS 600/200/10/20/0 67 475 10 LC1 Sigma Total 109.4 156.7 0.70 20 0 13 LC1 Tau Total -28.4 90.5 0.31 67 475 10 LC1 Sigma-eqv 109.4 156.7 0.70
2.3 STRESSES BY MEMBER Member
NoLoc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
1 Cross-section No. 1 - HE-B 200 0 10 LC1 Sigma Total 18.7 156.7 0.12 0 3 LC1 Tau Total -3.1 90.5 0.03 0 10 LC1 Sigma-eqv 18.7 156.7 0.12 2 Cross-section No. 1 - HE-B 200 1425 1 LC1 Sigma Total 60.6 156.7 0.39 0 3 LC1 Tau Total -3.6 90.5 0.04 1425 1 LC1 Sigma-eqv 60.6 156.7 0.39 3 Cross-section No. 1 - HE-B 200 0 1 LC1 Sigma Total 0.0 156.7 0.00 0 13 LC1 Tau Total 0.0 90.5 0.00 0 1 LC1 Sigma-eqv 0.0 156.7 0.00 4 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total 18.7 156.7 0.12 0 3 LC1 Tau Total 3.1 90.5 0.03 0 6 LC1 Sigma-eqv 18.7 156.7 0.12 5 Cross-section No. 1 - HE-B 200 1056 10 LC1 Sigma Total -76.3 156.7 0.49 0 13 LC1 Tau Total -9.3 90.5 0.10 1056 10 LC1 Sigma-eqv 76.3 156.7 0.49 6 Cross-section No. 1 - HE-B 200 1056 6 LC1 Sigma Total -76.2 156.7 0.49 0 13 LC1 Tau Total -9.3 90.5 0.10 1056 6 LC1 Sigma-eqv 76.3 156.7 0.49 7 Cross-section No. 4 - IS 600/200/10/20/0 0 10 LC1 Sigma Total -58.2 156.7 0.37 0 13 LC1 Tau Total 28.4 90.5 0.31 0 10 LC1 Sigma-eqv 58.2 156.7 0.37 8 Cross-section No. 1 - HE-B 200 270 5 LC1 Sigma Total -120.1 156.7 0.77 0 3 LC1 Tau Total -4.6 90.5 0.05 270 10 LC1 Sigma-eqv 120.1 156.7 0.77 9 Cross-section No. 1 - HE-B 200 1890 10 LC1 Sigma Total 65.6 156.7 0.42 0 13 LC1 Tau Total 5.5 90.5 0.06 1890 10 LC1 Sigma-eqv 65.6 156.7 0.42
10 Cross-section No. 4 - IS 600/200/10/20/0 0 6 LC1 Sigma Total -58.2 156.7 0.37 0 13 LC1 Tau Total 28.4 90.5 0.31 0 6 LC1 Sigma-eqv 58.2 156.7 0.37
11 Cross-section No. 1 - HE-B 200 0 1 LC1 Sigma Total 60.6 156.7 0.39 0 3 LC1 Tau Total 3.6 90.5 0.04 0 1 LC1 Sigma-eqv 60.6 156.7 0.39
12 Cross-section No. 1 - HE-B 200 450 10 LC1 Sigma Total 0.0 156.7 0.00 0 13 LC1 Tau Total 0.0 90.5 0.00 450 10 LC1 Sigma-eqv 0.0 156.7 0.00
13 Cross-section No. 1 - HE-B 200 0 10 LC1 Sigma Total -76.3 156.7 0.49 0 13 LC1 Tau Total 9.3 90.5 0.10 0 10 LC1 Sigma-eqv 76.3 156.7 0.49
14 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total -76.3 156.7 0.49 0 13 LC1 Tau Total 9.3 90.5 0.10 0 6 LC1 Sigma-eqv 76.3 156.7 0.49
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2.3 STRESSES BY MEMBER Member
NoLoc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
15 Cross-section No. 1 - HE-B 200 0 1 LC1 Sigma Total 91.0 156.7 0.58 0 3 LC1 Tau Total 7.8 90.5 0.09 0 1 LC1 Sigma-eqv 91.0 156.7 0.58
16 Cross-section No. 4 - IS 600/200/10/20/0 630 10 LC1 Sigma Total -58.2 156.7 0.37 0 13 LC1 Tau Total -28.4 90.5 0.31 630 10 LC1 Sigma-eqv 58.2 156.7 0.37
17 Cross-section No. 1 - HE-B 200 1425 5 LC1 Sigma Total 60.6 156.7 0.39 0 8 LC1 Tau Total -3.6 90.5 0.04 1425 5 LC1 Sigma-eqv 60.6 156.7 0.39
18 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total 0.0 156.7 0.00 0 13 LC1 Tau Total 0.0 90.5 0.00 0 12 LC1 Sigma-eqv 0.0 156.7 0.00
19 Cross-section No. 1 - HE-B 200 0 10 LC1 Sigma Total 65.6 156.7 0.42 0 13 LC1 Tau Total -5.5 90.5 0.06 0 10 LC1 Sigma-eqv 65.6 156.7 0.42
20 Cross-section No. 4 - IS 600/200/10/20/0 630 6 LC1 Sigma Total -58.2 156.7 0.37 0 13 LC1 Tau Total -28.4 90.5 0.31 630 6 LC1 Sigma-eqv 58.2 156.7 0.37
21 Cross-section No. 1 - HE-B 200 1010 1 LC1 Sigma Total 91.0 156.7 0.58 0 3 LC1 Tau Total -7.8 90.5 0.09 1010 1 LC1 Sigma-eqv 91.0 156.7 0.58
22 Cross-section No. 1 - HE-B 200 0 5 LC1 Sigma Total 60.6 156.7 0.39 0 8 LC1 Tau Total 3.6 90.5 0.04 0 5 LC1 Sigma-eqv 60.6 156.7 0.39
23 Cross-section No. 1 - HE-B 200 270 1 LC1 Sigma Total -120.2 156.7 0.77 0 3 LC1 Tau Total 4.6 90.5 0.05 270 6 LC1 Sigma-eqv 120.2 156.7 0.77
24 Cross-section No. 1 - HE-B 200 1890 6 LC1 Sigma Total 65.6 156.7 0.42 0 13 LC1 Tau Total 5.5 90.5 0.06 1890 6 LC1 Sigma-eqv 65.6 156.7 0.42
25 Cross-section No. 1 - HE-B 200 450 6 LC1 Sigma Total 0.0 156.7 0.00 0 13 LC1 Tau Total 0.0 90.5 0.00 450 12 LC1 Sigma-eqv 0.0 156.7 0.00
26 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total 65.6 156.7 0.42 0 13 LC1 Tau Total -5.5 90.5 0.06 0 6 LC1 Sigma-eqv 65.6 156.7 0.42
30 Cross-section No. 1 - HE-B 200 0 5 LC1 Sigma Total 91.0 156.7 0.58 0 8 LC1 Tau Total 7.8 90.5 0.09 0 5 LC1 Sigma-eqv 91.0 156.7 0.58
31 Cross-section No. 1 - HE-B 200 1010 5 LC1 Sigma Total 91.0 156.7 0.58 0 8 LC1 Tau Total -7.8 90.5 0.09 1010 5 LC1 Sigma-eqv 91.0 156.7 0.58
32 Cross-section No. 4 - IS 600/200/10/20/0 0 10 LC1 Sigma Total 109.4 156.7 0.70 0 3 LC1 Tau Total -17.7 90.5 0.20 0 10 LC1 Sigma-eqv 109.4 156.7 0.70
33 Cross-section No. 1 - HE-B 200 475 6 LC1 Sigma Total -8.0 156.7 0.05 0 3 LC1 Tau Total -0.3 90.5 0.00 475 6 LC1 Sigma-eqv 8.0 156.7 0.05
34 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total -8.0 156.7 0.05 0 3 LC1 Tau Total -0.3 90.5 0.00 0 6 LC1 Sigma-eqv 8.0 156.7 0.05
35 Cross-section No. 1 - HE-B 200 0 10 LC1 Sigma Total -21.7 156.7 0.14 0 13 LC1 Tau Total 4.1 90.5 0.04 0 10 LC1 Sigma-eqv 21.7 156.7 0.14
36 Cross-section No. 1 - HE-B 200 1976 10 LC1 Sigma Total -21.7 156.7 0.14
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2.3 STRESSES BY MEMBER Member
NoLoc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
0 13 LC1 Tau Total -4.1 90.5 0.04 1976 10 LC1 Sigma-eqv 21.7 156.7 0.14
37 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total -21.7 156.7 0.14 0 13 LC1 Tau Total 4.1 90.5 0.04 0 6 LC1 Sigma-eqv 21.7 156.7 0.14
38 Cross-section No. 1 - HE-B 200 1976 6 LC1 Sigma Total -21.7 156.7 0.14 0 13 LC1 Tau Total -4.1 90.5 0.04 1976 6 LC1 Sigma-eqv 21.7 156.7 0.14
40 Cross-section No. 1 - HE-B 200 1117 6 LC1 Sigma Total -54.7 156.7 0.35 0 13 LC1 Tau Total -6.0 90.5 0.07 1117 6 LC1 Sigma-eqv 54.7 156.7 0.35
41 Cross-section No. 1 - HE-B 200 1117 10 LC1 Sigma Total -54.7 156.7 0.35 0 13 LC1 Tau Total -6.0 90.5 0.07 1117 10 LC1 Sigma-eqv 54.7 156.7 0.35
42 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total -54.7 156.7 0.35 0 13 LC1 Tau Total 6.0 90.5 0.07 0 6 LC1 Sigma-eqv 54.7 156.7 0.35
43 Cross-section No. 1 - HE-B 200 0 10 LC1 Sigma Total -54.7 156.7 0.35 0 13 LC1 Tau Total 6.0 90.5 0.07 0 10 LC1 Sigma-eqv 54.7 156.7 0.35
45 Cross-section No. 1 - HE-B 200 475 6 LC1 Sigma Total -8.0 156.7 0.05 0 3 LC1 Tau Total -0.3 90.5 0.00 475 6 LC1 Sigma-eqv 8.0 156.7 0.05
47 Cross-section No. 1 - HE-B 200 0 6 LC1 Sigma Total -8.0 156.7 0.05 0 3 LC1 Tau Total -0.3 90.5 0.00 0 6 LC1 Sigma-eqv 8.0 156.7 0.05
48 Cross-section No. 2 - Pipe 190/15/K 633 10 LC1 Sigma Total -75.7 156.7 0.48 0 1 LC1 Tau Total -36.9 90.5 0.41 633 10 LC1 Sigma-eqv 75.7 156.7 0.48
65 Cross-section No. 2 - Pipe 190/15/K 633 28 LC1 Sigma Total 111.5 156.7 0.71 0 19 LC1 Tau Total 52.2 90.5 0.58 633 28 LC1 Sigma-eqv 111.5 156.7 0.71
67 Cross-section No. 4 - IS 600/200/10/20/0 475 10 LC1 Sigma Total 109.4 156.7 0.70 0 8 LC1 Tau Total -17.7 90.5 0.20 475 10 LC1 Sigma-eqv 109.4 156.7 0.70
68 Cross-section No. 2 - Pipe 190/15/K 633 28 LC1 Sigma Total 111.5 156.7 0.71 0 1 LC1 Tau Total -52.2 90.5 0.58 633 28 LC1 Sigma-eqv 111.5 156.7 0.71
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0.30
0.62
0.33
0.71
0.39
0.15
0.49
0.30
0.62
0.05
0.33
0.17
0.39
0.15
0.49
0.25
0.58
0.42
0.37
0.17
0.35
0.20
0.35
0.250.12
0.58
0.33
0.42
0.37
0.35
0.20
0.77
0.07
0.61
0.14
0.70
0.77
0.07
Y
0.46
0.61
0.12
0.04
0.14
0.48
Z
0.14
0.46
0.12
X
0.14
0.07
0.42
0.35
0.42
0.17
0.35
0.33
0.37
0.33
0.35
0.25
0.17
0.05
0.35
0.33
0.37
0.30
0.25
0.49
0.05
0.15
0.62
0.30
0.39
0.490.71 0.62
0.39
IsometricSTEEL CA1Sigma-eqv
Max Sigma-eqv: 0.77, Min Sigma-eqv: 0.00
Stress ratioSigma-v [-]
0.77
0.00
Max : 0.77Min : 0.00
STEEL - MEMBERS SIGMA-EQV, CA1
______________________________________________________________________________________ 130210.0266.01 Lifting and transport Cradles Page 16
Appendix C
3D Model Results. Fore Cradle
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CONTENTS CONTENTS General Data 1 3.3 Cross sections - Internal Forces 7Structure 1 3.4 Nodes - Support Forces 8
1.1 Nodes 1 Graph. Deformations u, LC1 81.2 Materials 2 Graph. Members N, LC1 91.3 Cross-sections 2 STEEL 101.7 Members 2 CA1 - General stress analysis of 101.8 Nodal Supports 3 steel members 10Graph. Structure 3 1.1.1 General Data 10Graph. Structure 4 1.1.2 Details 10
Loads 5 1.2.1 Materials 10 Load Cases 5 1.3.1 Cross-Sections 10 LC 1 5 Results 11
Graph. LC1 5 2.1 Stresses by Cross-Section 11Graph. LC1 6 2.3 Stresses by Member 11
Results - Load Cases, Load Groups 7 Graph. STEEL - Members Sigma-eqv, CA1 143.0 Results - Summary 7
GENERAL DATA
COMPUTING METHOD
Structural Analysis Linear Static Analysis Design Second-Order Analysis (Non-linear, Timoshenko) Dynamic Analysis Large Deformation Analysis (Non-linear, Newton-Raphson)
Postcritical Analysis (Non-linear, Newton-Raphson)
Load Cases Design Cases Load Groups Dynamic Cases Load Combinations Buckling Curves
STRUCTURAL DATA PARAMETERS
1D Continuous Beam 41 Nodes 73 Elements 2D Construction Type 2 Materials 0 Cables 3D Construction Type 4 Sections 0 Tapered Elements Grid 1 Element Hinges 0 Elastic Foundations
0 Element Partitions 0 Sets of Elements
1.1 NODES NodeNo.
ReferenceNode
CoordinateSystem
Node coordinatesX [mm] Y [mm] Z [mm] Comment
1 - Cartesian 475.0 0.0 387.52 - Cartesian 475.0 0.0 0.03 - Cartesian -475.0 0.0 0.04 - Cartesian 475.0 2235.5 651.55 - Cartesian -475.0 2235.5 651.56 - Cartesian 475.0 -2900.0 0.07 - Cartesian -475.0 -2900.0 0.08 - Cartesian 475.0 0.0 775.09 - Cartesian -475.0 0.0 775.0
10 - Cartesian 475.0 -2235.5 651.511 - Cartesian 475.0 2900.0 0.012 - Cartesian -475.0 0.0 387.513 - Cartesian 0.0 -2900.0 0.014 - Cartesian 475.0 -3350.0 0.015 - Cartesian -475.0 -3350.0 0.016 - Cartesian -475.0 2900.0 0.017 - Cartesian -475.0 -2235.5 651.518 - Cartesian 0.0 2900.0 0.019 - Cartesian 475.0 -1700.0 1176.620 - Cartesian -475.0 -1700.0 1176.622 - Cartesian 475.0 -2900.0 1460.023 - Cartesian -475.0 -2900.0 1460.026 - Cartesian 475.0 3350.0 0.027 - Cartesian -475.0 3350.0 0.028 - Cartesian 475.0 1700.0 1176.629 - Cartesian -475.0 1700.0 1176.630 - Cartesian 475.0 2900.0 1460.031 - Cartesian -475.0 2900.0 1460.042 - Cartesian -475.0 -1700.0 0.043 - Cartesian 0.0 0.0 4700.044 - Cartesian 475.0 -1700.0 0.045 - Cartesian -475.0 1700.0 0.046 - Cartesian 475.0 1700.0 0.050 - Cartesian 475.0 -1600.0 1910.051 - Cartesian 0.0 0.0 4100.052 - Cartesian 475.0 1600.0 1910.053 - Cartesian 0.0 0.0 775.055 - Cartesian -475.0 -1600.0 1910.056 - Cartesian 0.0 -1600.0 1910.058 - Cartesian -475.0 1600.0 1910.059 - Cartesian 0.0 1600.0 1910.0
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1.2 MATERIALS Material
No.Material
DescriptionE-ModulusE [kN/cm2]
G-ModulusG [kN/cm2]
Sp. Weight [kN/m3]
Coeff. Thermal [1/°C]
Saf. FactorM [-]
1 Steel S 235 | DIN 18800:1990-11 21000.00 8100.00 78.50 1.2000E-05 1.1002 Steel S 235 | DIN 18800:1990-11 21000.00 8100.00 78.50 1.2000E-05 1.100
1.3 CROSS-SECTIONS Section
No.Cross-sectionDescription
Mater.No.
IT [cm4]A [cm2]
Iy [cm4]Ay [cm2]
Iz [cm4]Az [cm2]
1 HE-B 200 2 59.50 5700.00 2000.0078.10 50.07 15.37
2 Pipe 190/15/K 2 6421.93 3180.13 3180.1382.47 41.08 41.08
3 Dummy Rigid 0.00
5 IS 600/200/10/20/0 1 119.28 81941.33 2671.33136.00 80.00 56.00
1.7 MEMBERS Member
No. MemberNode
Start EndRotation
Type [°] / PlaneCross-sectionStart End
Release No.Start End
Ecc.No.
Div.No.
LengthL [mm]
1 Beam 14 6 Angle 0.00 1 1 - - - - 450.0 Y2 Beam 11 26 Angle 0.00 1 1 - - - - 450.0 Y3 Beam 4 46 Angle 90.00 3 3 - - - - 843.3 YZ4 Beam 22 6 Angle 90.00 1 1 - - - - 1460.0 Z5 Beam 11 30 Angle 90.00 1 1 - - - - 1460.0 Z6 Beam 1 2 Angle 90.00 1 1 - - - - 387.5 Z7 Beam 4 11 Angle 90.00 3 3 - - - - 930.6 YZ8 Beam 8 1 Angle 90.00 1 1 - - - - 387.5 Z9 Beam 3 12 Angle 90.00 1 1 - - - - 387.5 Z
10 Beam 5 45 Angle 90.00 3 3 - - - - 843.3 YZ11 Beam 5 16 Angle 90.00 3 3 - - - - 930.6 YZ12 Beam 53 8 Angle 90.00 5 5 - - - - 475.0 X13 Beam 10 22 Angle 90.00 3 3 - - - - 1046.5 YZ14 Beam 10 19 Angle 90.00 3 3 - - - - 749.9 YZ15 Beam 17 23 Angle 90.00 3 3 - - - - 1046.5 YZ16 Beam 15 7 Angle 0.00 1 1 - - - - 450.0 Y17 Beam 16 27 Angle 0.00 1 1 - - - - 450.0 Y18 Beam 17 20 Angle 90.00 3 3 - - - - 749.9 YZ24 Beam 23 7 Angle 90.00 1 1 - - - - 1460.0 Z25 Beam 12 9 Angle 90.00 1 1 - - - - 387.5 Z26 Beam 7 42 Angle 0.00 1 1 - - - - 1200.0 Y27 Beam 6 44 Angle 0.00 1 1 - - - - 1200.0 Y28 Beam 16 31 Angle 90.00 1 1 - - - - 1460.0 Z29 Beam 45 16 Angle 0.00 1 1 - - - - 1200.0 Y30 Beam 46 11 Angle 0.00 1 1 - - - - 1200.0 Y31 Beam 7 13 Angle 0.00 1 1 - - - - 475.0 X32 Beam 18 16 Angle 0.00 1 1 - - - - 475.0 X34 Beam 13 6 Angle 0.00 1 1 - - - - 475.0 X35 Beam 11 18 Angle 0.00 1 1 - - - - 475.0 X36 Beam 22 19 Angle 0.00 1 1 - - - - 1233.0 YZ37 Beam 28 30 Angle 0.00 1 1 - - - - 1233.0 YZ38 Beam 23 20 Angle 0.00 1 1 - - - - 1233.0 YZ39 Beam 29 31 Angle 0.00 1 1 - - - - 1233.0 YZ42 Beam 42 20 Angle 90.00 1 1 - - - - 1176.6 Z43 Beam 44 19 Angle 90.00 1 1 - - - - 1176.6 Z44 Beam 42 3 Angle 0.00 1 1 - - - - 1700.0 Y45 Beam 44 2 Angle 0.00 1 1 - - - - 1700.0 Y46 Beam 19 8 Angle 0.00 1 1 - - - - 1746.8 YZ47 Beam 20 9 Angle 0.00 1 1 - - - - 1746.8 YZ48 Beam 56 50 Node 20 / x-y 3 3 - - - - 475.0 X49 Beam 50 19 Angle 180.00 5 5 - - - - 740.2 YZ50 Beam 55 20 Angle 180.00 5 5 - - - - 740.2 YZ51 Beam 29 45 Angle 90.00 1 1 - - - - 1176.6 Z52 Beam 28 46 Angle 90.00 1 1 - - - - 1176.6 Z53 Beam 3 45 Angle 0.00 1 1 - - - - 1700.0 Y54 Beam 2 46 Angle 0.00 1 1 - - - - 1700.0 Y55 Beam 8 28 Angle 0.00 1 1 - - - - 1746.8 YZ56 Beam 9 29 Angle 0.00 1 1 - - - - 1746.8 YZ57 Beam 52 59 Node 29 / x-y 3 3 - - - - 475.0 X58 Beam 28 52 Angle 180.00 5 5 - - - - 740.2 YZ59 Beam 29 58 Angle 180.00 5 5 - - - - 740.2 YZ66 Beam 22 23 Angle 50.20 2 2 - - - - 950.0 X68 Beam 30 31 Angle -50.20 2 2 - - - - 950.0 X70 Beam 53 9 Angle 90.00 5 5 - - - - 475.0 X73 Beam 43 51 Angle 0.00 3 3 - - - - 600.0 Z74 Compression 51 56 Angle 0.00 3 3 - - - - 2712.2 YZ75 Compression 51 53 Angle 0.00 3 3 - - - - 3325.0 Z76 Beam 12 1 Angle 0.00 2 2 - - - - 950.0 X77 Beam 56 53 Angle 0.00 3 3 - - - - 1961.7 YZ78 Compression 59 51 Angle 0.00 3 3 - - - - 2712.2 YZ79 Beam 55 56 Node 20 / x-y 3 3 - - - - 475.0 X80 Beam 19 20 Angle 0.00 1 1 - - - - 950.0 X81 Beam 53 59 Angle 0.00 3 3 - - - - 1961.7 YZ82 Beam 59 58 Node 29 / x-y 3 3 - - - - 475.0 X83 Beam 29 28 Angle 0.00 1 1 - - - - 950.0 X84 Beam 30 4 Angle 90.00 3 3 - - - - 1046.5 YZ
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1.7 MEMBERS Member
No. MemberNode
Start EndRotation
Type [°] / PlaneCross-sectionStart End
Release No.Start End
Ecc.No.
Div.No.
LengthL [mm]
85 Beam 28 4 Angle 90.00 3 3 - - - - 749.9 YZ86 Beam 31 5 Angle 90.00 3 3 - - - - 1046.5 YZ87 Beam 29 5 Angle 90.00 3 3 - - - - 749.9 YZ88 Beam 44 10 Angle 90.00 3 3 - - - - 843.3 YZ89 Beam 6 10 Angle 90.00 3 3 - - - - 930.6 YZ90 Beam 42 17 Angle 90.00 3 3 - - - - 843.3 YZ91 Beam 7 17 Angle 90.00 3 3 - - - - 930.6 YZ
1.8 NODAL SUPPORTS Support
No. Nodes No.Rotation [°]
Sequen. about X about Y about ZSupport Conditions
uX' uY' uZ' X' Y' Z'
1 43 XYZ 0.00 0.00 0.002 13,18 XYZ 0.00 0.00 0.00
Y
Z
X
Isometric
STRUCTURE
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Y
Z
X
Isometric
STRUCTURE
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LOAD CASES LCNo. LC Description LC Factor Property of load case Self-weight
Method ofAnalysis
1 1.0000 Variable - Linear
2.2 MEMBER LOADS LC1LC1
No. Reference toOn members No.On sets of m. No.
LoadType
LoadDistribution
LoadDirection
ReferenceLength
Load ParametersSymbol Value Unit
11 Members 66,68 Force 2 x P z True Length P1 -172.7 kNP2 -172.7 kNA 33.330 %B 33.330 %
13 Members 76 Force 2 x P Z True Length P1 106.44 kNP2 106.44 kNA 33.330 %B 33.330 %
172.750 172.750
Y
106.450 106.450
Z
X
172.750 172.750
IsometricLC1
LC1
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X
172.750
172.750
106.450
Y
Z
172.750
172.750
106.450
In X-directionLC1
1000.00 [mm]
LC1
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3.0 RESULTS - SUMMARY Description Value Unit Comment
LC1 Sum of Loads in X 0.00 kN Sum of Support Reactions in X 0.00 kN Sum of Loads in Y 0.00 kN Sum of Support Reactions in Y 0.00 kN Sum of Loads in Z 655.22 kN Sum of Support Reactions in Z 655.22 kN Deviation 0.00% Max Displacement in X -0.2 mm Member No. 6, x: 387.5 mm Max Displacement in Y -0.2 mm Member No. 68, x: 475.0 mm Max Displacement in Z 0.5 mm Member No. 76, x: 475.0 mm Max Vectorial Displacement 0.5 mm Member No. 76, x: 475.0 mm Max rotation about X -0.2 mrad Member No. 53, x: 765.0 mm Max Rotation about Y 0.7 mrad Member No. 76, x: 807.5 mm Max Rotation about Z -0.4 mrad Member No. 66, x: 190.0 mm Method of Analysis Linear Linear Static Analysis Number of Iterations 1Summary Number of 1D Finite Elements (member elements) 73 Number of FE nodes 41 Number of Equations 246 Matrix Solver Method Direct Max Number of Iterations 100 Number of Load Increments 1 Divisions of members for member results 10 Divisions of cable, foundation or tapered members 10 Activate shear rigidity (A-y, A-z) of members No Activate Failed Members Yes
3.3 CROSS SECTIONS - INTERNAL FORCES Member
No. LC/LGNodeNo.
Locationx [mm]
Shear Forces [kN]N Vy Vz
Moments [kNm]MT My Mz
Section No. 1: HE-B 20045 LC1 MAX N 0.0 73.93 -2.05 -7.16 0.01 6.59 -1.7525 LC1 MIN N 0.0 -92.15 11.83 0.00 0.00 0.00 13.1625 LC1 MAX Vy 0.0 -92.15 11.83 0.00 0.00 0.00 13.168 LC1 MIN Vy 0.0 -92.13 -11.83 0.00 0.00 0.00 8.57
53 LC1 MAX Vz 0.0 73.93 -2.04 7.16 0.01 -5.58 -1.7344 LC1 MIN Vz 0.0 73.93 2.04 -7.16 -0.01 6.59 1.7545 LC1 MAX MT 0.0 73.93 -2.05 -7.16 0.01 6.59 -1.7554 LC1 MIN MT 0.0 73.93 2.05 7.16 -0.01 -5.58 1.7344 LC1 MAX My 0.0 73.93 2.04 -7.16 -0.01 6.59 1.7544 LC1 MIN My 1700.0 73.93 2.04 -7.16 -0.01 -5.58 -1.7325 LC1 MAX Mz 0.0 -92.15 11.83 0.00 0.00 0.00 13.1645 LC1 MIN Mz 0.0 73.93 -2.05 -7.16 0.01 6.59 -1.75
Section No. 2: Pipe 190/15/K66 LC1 MAX N 0.0 0.11 0.00 -172.77 0.00 36.38 0.0076 LC1 MIN N 0.0 -7.74 0.00 -106.46 0.00 14.77 0.0068 LC1 MAX Vy 0.0 0.11 0.00 -172.77 0.00 36.38 0.0066 LC1 MIN Vy 0.0 0.11 0.00 -172.77 0.00 36.38 0.0066 LC1 MAX Vz 633.3 0.11 0.00 172.73 0.00 -18.33 0.0066 LC1 MIN Vz 0.0 0.11 0.00 -172.77 0.00 36.38 0.0068 LC1 MAX MT 0.0 0.11 0.00 -172.77 0.00 36.38 0.0066 LC1 MIN MT 0.0 0.11 0.00 -172.77 0.00 36.38 0.0066 LC1 MAX My 0.0 0.11 0.00 -172.77 0.00 36.38 0.0076 LC1 MIN My 633.3 -7.74 0.00 -0.01 0.00 -18.94 0.0068 LC1 MAX Mz 0.0 0.11 0.00 -172.77 0.00 36.38 0.0066 LC1 MIN Mz 0.0 0.11 0.00 -172.77 0.00 36.38 0.00
Section No. 3: Dummy Rigid3 LC1 MAX N 0.0 41.42 -61.65 -2.05 1.34 2.85 -58.58
73 LC1 MIN N 0.0 -655.22 0.00 0.00 0.00 0.00 0.0084 LC1 MAX Vy 0.0 1.17 172.75 0.11 36.38 -0.24 0.0013 LC1 MIN Vy 0.0 1.17 -172.75 -0.11 -36.38 -0.13 -180.7877 LC1 MAX Vz 0.0 -113.67 0.00 164.40 0.01 -75.37 0.0181 LC1 MIN Vz 0.0 -113.67 0.00 -164.40 -0.01 247.13 0.0148 LC1 MAX MT 0.0 1.12 -154.65 146.88 37.69 -69.77 -73.8457 LC1 MIN MT 0.0 1.12 154.65 -146.88 -37.69 0.00 -0.3877 LC1 MAX My 1961.7 -113.67 0.00 164.40 0.01 247.13 0.0177 LC1 MIN My 0.0 -113.67 0.00 164.40 0.01 -75.37 0.0189 LC1 MAX Mz 930.6 0.00 -0.01 21.36 0.05 19.98 0.0113 LC1 MIN Mz 0.0 1.17 -172.75 -0.11 -36.38 -0.13 -180.78
Section No. 5: IS 600/200/10/20/012 LC1 MAX N 0.0 13.68 -60.83 0.00 0.00 0.00 -19.8249 LC1 MIN N 0.0 -154.65 1.12 -146.88 0.00 37.69 0.3859 LC1 MAX Vy 0.0 -154.64 1.13 146.84 0.00 -71.01 0.4570 LC1 MIN Vy 0.0 13.67 -60.84 0.00 0.00 0.00 -19.8258 LC1 MAX Vz 0.0 -154.65 -1.12 146.88 0.00 -71.03 -0.4549 LC1 MIN Vz 0.0 -154.65 1.12 -146.88 0.00 37.69 0.3849 LC1 MAX MT 0.0 -154.65 1.12 -146.88 0.00 37.69 0.3858 LC1 MIN MT 0.0 -154.65 -1.12 146.88 0.00 -71.03 -0.4549 LC1 MAX My 0.0 -154.65 1.12 -146.88 0.00 37.69 0.3849 LC1 MIN My 740.2 -154.65 1.12 -146.88 0.00 -71.03 -0.4570 LC1 MAX Mz 475.0 13.67 -60.84 0.00 0.00 0.00 9.0870 LC1 MIN Mz 0.0 13.67 -60.84 0.00 0.00 0.00 -19.82
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3.4 NODES - SUPPORT FORCES NodeNo. LC/LG
Support forces [kN]PX' PY' PZ'
Support moments [kNm]MX' MY' MZ'
13 LC1 0.00 0.00 0.00 -0.01 -0.01 0.0018 LC1 0.00 0.00 0.00 0.01 -0.01 0.0043 LC1 0.00 0.00 655.22 0.00 0.00 0.00
Suppo LC1 0.00 0.00 655.22 Loads 0.00 0.00 655.22
Y
Z
0.5
X
IsometricLC1u
Factor of deformations: 500.00Max u: 0.5, Min u: 0.0 [mm]
DEFORMATIONS U, LC1
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Y
-245.76
Z
X
-258.33
-245.76
IsometricLC1N
Max N: -245.76, Min N: -258.33 [kN]
MEMBERS N, LC1
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1.1.1 GENERAL DATA STEELCA1General stress analysis ofsteel members
Members to design: AllLoad cases to design: LC1
1.1.2 DETAILS Allow local plastification:Calculate normal stresses with Alpha-pl:
FACTORS FOR SIGMA-EQVSigma 1.00Tau 3.00
Simplified consideration of eccentric loading:
1.2.1 MATERIALS MatNo
MaterialDescription
Partial FactorM [-]
Yield Strengthfyk [N/mm2]
Limit Stresses [N/mm2]Manually limit x limit limit eqv
1 Steel S 235* 1.50 235.0 156.7 90.5 156.72 Steel S 235* 1.50 235.0 156.7 90.5 156.7
1.3.1 CROSS-SECTIONS SecNo
MatNo
Cross-Section Description It [cm4]A [cm2]
Iy [cm4]Alphapl,y
Iz [cm4]Alphapl,z Comment
1 2 HE-B 200 59.50 5700.00 2000.0078.10 1.126 1.529
2 2 Pipe 190/15/K 6421.93 3180.13 3180.1382.47 1.376 1.376
3 0 Dummy Rigid 0.00 0.00 0.000.00 1.00 1.00
The section will not be designed because the characteristic stresses are invalid!5 1 IS 600/200/10/20/0 119.28 81941.30 2671.33
136.00 1.136 1.55
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2.1 STRESSES BY CROSS-SECTION STEELCA1General stress analysis ofsteel members
SecNo
MemberNo
Loc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
1 HE-B 200 25 0.0 5 LC1 Sigma Total -77.6 156.7 0.50 44 0.0 13 LC1 Tau Total -4.7 90.5 0.05 25 0.0 10 LC1 Sigma-eqv 77.6 156.7 0.50 2 Pipe 190/15/K 66 0.0 10 LC1 Sigma Total 108.7 156.7 0.69 68 0.0 19 LC1 Tau Total 41.2 90.5 0.46 66 0.0 10 LC1 Sigma-eqv 108.7 156.7 0.69 5 IS 600/200/10/20/0 70 0.0 10 LC1 Sigma Total 75.2 156.7 0.48 49 0.0 13 LC1 Tau Total -27.8 90.5 0.31 70 0.0 10 LC1 Sigma-eqv 75.2 156.7 0.48
2.3 STRESSES BY MEMBER Member
NoLoc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
1 Cross-section No. 1 - HE-B 200 450.0 6 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 450.0 12 LC1 Sigma-eqv 0.0 156.7 0.00 2 Cross-section No. 1 - HE-B 200 0.0 6 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 6 LC1 Sigma-eqv 0.0 156.7 0.00 4 Cross-section No. 1 - HE-B 200 0.0 5 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 5 LC1 Sigma-eqv 0.0 156.7 0.00 5 Cross-section No. 1 - HE-B 200 1460.0 6 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1460.0 6 LC1 Sigma-eqv 0.0 156.7 0.00 6 Cross-section No. 1 - HE-B 200 0.0 10 LC1 Sigma Total 9.9 156.7 0.06 0.0 8 LC1 Tau Total 1.0 90.5 0.01 0.0 10 LC1 Sigma-eqv 9.9 156.7 0.06 8 Cross-section No. 1 - HE-B 200 387.5 5 LC1 Sigma Total -77.6 156.7 0.50 0.0 8 LC1 Tau Total 3.0 90.5 0.03 387.5 10 LC1 Sigma-eqv 77.6 156.7 0.50 9 Cross-section No. 1 - HE-B 200 387.5 10 LC1 Sigma Total 9.9 156.7 0.06 0.0 3 LC1 Tau Total 1.0 90.5 0.01 387.5 10 LC1 Sigma-eqv 9.9 156.7 0.06
12 Cross-section No. 5 - IS 600/200/10/20/0 0.0 10 LC1 Sigma Total 75.2 156.7 0.48 0.0 8 LC1 Tau Total 11.4 90.5 0.13 0.0 10 LC1 Sigma-eqv 75.2 156.7 0.48
16 Cross-section No. 1 - HE-B 200 450.0 1 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 450.0 11 LC1 Sigma-eqv 0.0 156.7 0.00
17 Cross-section No. 1 - HE-B 200 0.0 6 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 3 LC1 Sigma-eqv 0.0 156.7 0.00
24 Cross-section No. 1 - HE-B 200 0.0 1 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 1 LC1 Sigma-eqv 0.0 156.7 0.00
25 Cross-section No. 1 - HE-B 200 0.0 5 LC1 Sigma Total -77.6 156.7 0.50 0.0 3 LC1 Tau Total 3.0 90.5 0.03 0.0 10 LC1 Sigma-eqv 77.6 156.7 0.50
26 Cross-section No. 1 - HE-B 200 1200.0 10 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1200.0 10 LC1 Sigma-eqv 0.0 156.7 0.00
27 Cross-section No. 1 - HE-B 200 1200.0 6 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1200.0 6 LC1 Sigma-eqv 0.0 156.7 0.00
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2.3 STRESSES BY MEMBER Member
NoLoc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
28 Cross-section No. 1 - HE-B 200 1460.0 10 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1460.0 10 LC1 Sigma-eqv 0.0 156.7 0.00
29 Cross-section No. 1 - HE-B 200 0.0 10 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 10 LC1 Sigma-eqv 0.0 156.7 0.00
30 Cross-section No. 1 - HE-B 200 0.0 6 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 6 LC1 Sigma-eqv 0.0 156.7 0.00
31 Cross-section No. 1 - HE-B 200 475.0 10 LC1 Sigma Total -3.2 156.7 0.02 0.0 3 LC1 Tau Total -0.2 90.5 0.00 475.0 10 LC1 Sigma-eqv 3.2 156.7 0.02
32 Cross-section No. 1 - HE-B 200 0.0 10 LC1 Sigma Total -3.2 156.7 0.02 0.0 3 LC1 Tau Total 0.2 90.5 0.00 0.0 10 LC1 Sigma-eqv 3.2 156.7 0.02
34 Cross-section No. 1 - HE-B 200 475.0 10 LC1 Sigma Total -3.2 156.7 0.02 0.0 3 LC1 Tau Total -0.2 90.5 0.00 475.0 10 LC1 Sigma-eqv 3.2 156.7 0.02
35 Cross-section No. 1 - HE-B 200 0.0 10 LC1 Sigma Total -3.2 156.7 0.02 0.0 3 LC1 Tau Total 0.2 90.5 0.00 0.0 10 LC1 Sigma-eqv 3.2 156.7 0.02
36 Cross-section No. 1 - HE-B 200 1233.0 5 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1233.0 5 LC1 Sigma-eqv 0.0 156.7 0.00
37 Cross-section No. 1 - HE-B 200 0.0 5 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 5 LC1 Sigma-eqv 0.0 156.7 0.00
38 Cross-section No. 1 - HE-B 200 1233.0 1 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1233.0 1 LC1 Sigma-eqv 0.0 156.7 0.00
39 Cross-section No. 1 - HE-B 200 0.0 1 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 1 LC1 Sigma-eqv 0.0 156.7 0.00
42 Cross-section No. 1 - HE-B 200 0.0 5 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 5 LC1 Sigma-eqv 0.0 156.7 0.00
43 Cross-section No. 1 - HE-B 200 0.0 1 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 0.0 1 LC1 Sigma-eqv 0.0 156.7 0.00
44 Cross-section No. 1 - HE-B 200 0.0 6 LC1 Sigma Total 29.8 156.7 0.19 0.0 13 LC1 Tau Total -4.7 90.5 0.05 0.0 6 LC1 Sigma-eqv 29.8 156.7 0.19
45 Cross-section No. 1 - HE-B 200 0.0 10 LC1 Sigma Total 29.8 156.7 0.19 0.0 13 LC1 Tau Total -4.7 90.5 0.05 0.0 10 LC1 Sigma-eqv 29.8 156.7 0.19
46 Cross-section No. 1 - HE-B 200 1746.8 10 LC1 Sigma Total -19.0 156.7 0.12 0.0 13 LC1 Tau Total -3.9 90.5 0.04 1746.8 10 LC1 Sigma-eqv 19.0 156.7 0.12
47 Cross-section No. 1 - HE-B 200 1746.8 6 LC1 Sigma Total -19.0 156.7 0.12 0.0 13 LC1 Tau Total -3.9 90.5 0.04 1746.8 6 LC1 Sigma-eqv 19.0 156.7 0.12
49 Cross-section No. 5 - IS 600/200/10/20/0 740.2 6 LC1 Sigma Total -39.1 156.7 0.25 0.0 13 LC1 Tau Total -27.8 90.5 0.31 740.2 12 LC1 Sigma-eqv 50.8 156.7 0.32
50 Cross-section No. 5 - IS 600/200/10/20/0 740.2 10 LC1 Sigma Total -39.1 156.7 0.25
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2.3 STRESSES BY MEMBER Member
NoLoc x[mm]
S-PointNo
LoadCase
Stress Type
Stress [N/mm2]existing Limit
StressRatio
0.0 13 LC1 Tau Total -27.8 90.5 0.31 740.2 12 LC1 Sigma-eqv 50.8 156.7 0.32
51 Cross-section No. 1 - HE-B 200 1176.6 6 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1176.6 6 LC1 Sigma-eqv 0.0 156.7 0.00
52 Cross-section No. 1 - HE-B 200 1176.6 10 LC1 Sigma Total 0.0 156.7 0.00 0.0 13 LC1 Tau Total 0.0 90.5 0.00 1176.6 10 LC1 Sigma-eqv 0.0 156.7 0.00
53 Cross-section No. 1 - HE-B 200 1700.0 6 LC1 Sigma Total 29.8 156.7 0.19 0.0 13 LC1 Tau Total 4.7 90.5 0.05 1700.0 6 LC1 Sigma-eqv 29.8 156.7 0.19
54 Cross-section No. 1 - HE-B 200 1700.0 10 LC1 Sigma Total 29.8 156.7 0.19 0.0 13 LC1 Tau Total 4.7 90.5 0.05 1700.0 10 LC1 Sigma-eqv 29.8 156.7 0.19
55 Cross-section No. 1 - HE-B 200 0.0 10 LC1 Sigma Total -19.0 156.7 0.12 0.0 13 LC1 Tau Total 3.9 90.5 0.04 0.0 10 LC1 Sigma-eqv 19.0 156.7 0.12
56 Cross-section No. 1 - HE-B 200 0.0 6 LC1 Sigma Total -19.0 156.7 0.12 0.0 13 LC1 Tau Total 3.9 90.5 0.04 0.0 6 LC1 Sigma-eqv 19.0 156.7 0.12
58 Cross-section No. 5 - IS 600/200/10/20/0 0.0 6 LC1 Sigma Total -39.1 156.7 0.25 0.0 13 LC1 Tau Total 27.8 90.5 0.31 0.0 12 LC1 Sigma-eqv 50.8 156.7 0.32
59 Cross-section No. 5 - IS 600/200/10/20/0 0.0 10 LC1 Sigma Total -39.1 156.7 0.25 0.0 13 LC1 Tau Total 27.8 90.5 0.31 0.0 12 LC1 Sigma-eqv 50.8 156.7 0.32
66 Cross-section No. 2 - Pipe 190/15/K 0.0 10 LC1 Sigma Total 108.7 156.7 0.69 0.0 19 LC1 Tau Total 41.2 90.5 0.46 0.0 10 LC1 Sigma-eqv 108.7 156.7 0.69
68 Cross-section No. 2 - Pipe 190/15/K 0.0 10 LC1 Sigma Total 108.7 156.7 0.69 0.0 19 LC1 Tau Total 41.2 90.5 0.46 0.0 10 LC1 Sigma-eqv 108.7 156.7 0.69
70 Cross-section No. 5 - IS 600/200/10/20/0 0.0 10 LC1 Sigma Total 75.2 156.7 0.48 0.0 8 LC1 Tau Total 11.4 90.5 0.13 0.0 10 LC1 Sigma-eqv 75.2 156.7 0.48
76 Cross-section No. 2 - Pipe 190/15/K 633.3 10 LC1 Sigma Total -57.5 156.7 0.37 0.0 19 LC1 Tau Total 25.4 90.5 0.28 633.3 10 LC1 Sigma-eqv 57.5 156.7 0.37
80 Cross-section No. 1 - HE-B 200 0.0 5 LC1 Sigma Total 2.6 156.7 0.02 0.0 3 LC1 Tau Total 0.0 90.5 0.00 0.0 5 LC1 Sigma-eqv 2.6 156.7 0.02
83 Cross-section No. 1 - HE-B 200 950.0 5 LC1 Sigma Total 2.6 156.7 0.02 0.0 3 LC1 Tau Total 0.0 90.5 0.00 950.0 5 LC1 Sigma-eqv 2.6 156.7 0.02
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0.690.69
0.35
0.02 0.02
0.19
0.32
0.32
0.32
0.120.02
0.19
0.32
0.32
0.120.02
0.08
0.50
0.35
Y
0.48
0.08
0.18
0.50
0.29
0.06
0.35
0.37
Z
0.18
0.29X
0.08
0.12
0.08
0.48
0.19
0.120.02
0.19
0.32
0.12
0.32
0.02
0.32
0.32
0.02
0.35
0.690.69
IsometricSTEEL CA1Sigma-eqv
Max Sigma-eqv: 0.69, Min Sigma-eqv: 0.00
Stress ratioSigma-v [-]
0.69
0.00
Max : 0.69Min : 0.00
STEEL - MEMBERS SIGMA-EQV, CA1
______________________________________________________________________________________ 130210.0266.01 Lifting and transport Cradles Page 17
Appendix D
PVC core material Data Sheet
Data Sheet AA / Issue 10/03 / Replaces Issue 11/02
AIREX® C70UNIVERSALLY STRUCTURAL FOAM
Description A unique closed cell, cross-linked polymer foam that combines high stiffnessand strength to weight ratios with superior toughness. It is non-friable, containsno CFC’s, has negligible water absorption, and provides an excellent resis-tance to chemicals. A fine cell structure offers an excellent bonding surfacethat is compatible with most resins and manufacturing processes. It is ideallysuited as a core material for a wide variety of light-weight sandwich structuressubjected to both static and dynamic loads in service.
Applications • MarineHulls, decks, bulkheads, superstructures, interiors
• Road and RailRoof panels, interiors, floors, doors, partition walls, side skirts
• Wind EnergyRotor blades, nacelles, turbine generator housings
• Air General aviation (sport aircraft) parts, galley carts
• RecreationSurfboards, snowboards, wakeboards
• Industrial Tooling, tanks, ductwork, containers, covers
Characteristics • high strength and stiffness to weight ratios• good impact strength (highest elongation in class)• low resin absorption• high fatigue resistance• good fire performance (self-extinguishing)• sound and thermal insulation• non biodegradable• good styrene resistance
Processing • contact molding (hand/spray)• resin injection (RTM)• adhesive bonding• pre-preg processing• vacuum infusion
Data Sheet AA/ Issue 10/03 / Replaces Issue 11/02
Alcan Airex AG Alcan Baltek CorporationCH-5643 Sins, Switzerland 10 Fairway Court, P.O. Box 195Tel: +41 41 789 66 00 Northvale, NJ 07647, USAFax: +41 41 789 66 60 Tel: +1 201 767 14 00www.alcanairex.com Fax: +1 201 387 66 31
www.baltek.com
Typical properties AIREX® C70 C70.40 C70.48 C70.55 C70.75 C70.90 C70.130 C70.200
Apparent nominal density ISO 845kg/m³lb/ft3
402.5
483.0
603.7
805.0
1006.2
1308.1
20012.5
Compressive strengthperpendicular to the plane
ISO 844N/mm²psi
0.4565
0.6087
0.90130
1.3190
1.9275
2.6380
4.8700
Compressive modulusperpendicular to the plane
DIN 53421N/mm²psi
344930
446’400
588410
8312000
11016000
15522500
26037700
Tensile strength in the plane DIN 53455N/mm²psi
0.70100
1.0145
1.3190
2.0290
2.7390
3.8550
6.2900
Tensile modulus in the plane DIN 53457N/mm²psi
284060
405’800
456530
639140
8111800
11516700
18026100
Shear strength ISO 1922N/mm²psi
0.4565
0.5580
0.80120
1.2175
1.6230
2.3330
3.5510
Shear modulus ASTM C393N/mm²psi
131900
152’200
223190
304350
385510
507250
7510900
Shear elongation at break ISO 1922 % 8 10 16 23 27 30 30
Thermal conductivityat room temperature
ISO 8301W/m.KBTU.in/ft2.hr.°F
0.0310.21
0.0310.21
0.0310.21
0.0330.23
0.0350.24
0.0390.27
0.0480.33
Plain sheet width mm ± 10in
1330 53.36
1270 50
1150 45.27
1020 / 108040.16 / 42.5
950 37.4
850 33.5
750 29.5
lengthmm ± 10in
2850 **112.2
2730 **107.48
2450 ** 96.5
2180 / 150085.8 / 59
205080.7
190074.8
160063
thicknessmm ± 0.5in
5 to 800.2 to 3.15
5 to 700.2 to 2.76
5 to 700.2 to 2.76
3* to 700.118 to 2.76
3* to 600.118 to 2.36
5 to 500.2 to 1.97
5 to 400.2 to 1.57
Block thicknessmm ± 2in
84 3.31
80 3.15
78 3.07
72 2.83
68 2.68
58 2.28
48 1.89
Scrim widthmm ± 5in
690 27.16
660 25.98
600 23.62
480 18.89
510 20.07
on request on request
lengthmm ± 5in
1200 47.24
1200 47.24
1140 44.88
1068 42.52
930 36.61
thicknessmm ± 0.5in
5 to 303.57 to 1.18
5 to 253.54 to 0.98
5 to 253.54 to 0.98
5 to 253.54 to 0.98
5 to 253.54 to 0.98
Color light green olive yellow Green red light green brownOther dimensions, configurations, and closer tolerances upon request * Tolerance for 3mm: + 0.8mm / - 0.2mm ** Half size plane sheets for thickness ≤ 8mm (0.315”)
The data provided gives approximate values for the nominal density. Due to density variations these values can be lower than indicated above. Minimum values to calculate sandwich constructions can beprovided upon request. The information contained herein is believed to be correct and to correspond to the latest state of scientific and technical knowledge. However, no warranty is made, either expressed or implied, regarding itsaccuracy or the results to be obtained from the use of such information. No statement is intended or should be construed as a recommendation to infringe any existing patent.