Design of Steel Chimney and Rcc Foundation as Per Indian Code 22052014

12
Sheet : Cont'd : this only Design of Self supporting Steel Chimney for Data Wind Loads as per India Standards. Prepared by : Date : Job No. : Verified by : CALCULATION Note : Enter Data in Cells marked Height of Steel Chimney 80.00 m Outside Diameter at Top 3.00 m Revision Notes : Calculation Sheet Project : 3 mm Subject : Consider outside diameter of the chimney at base dbase := 5.00 m Shape factor of Steel chimney circullar in plan. 0.70 Adopt height of Flared Portion 25.00 m Minimum outside diameter of flared chimney at base = 1.60*Dtop 4.80 m Intensity of Wind Pressure upto a height of 30 m as per Is 875 1.50 kn/m2 Recommended height of Flared Portion = H/3 26.67 m Yeild stress of Chimney Steel as per IS 2062- 2006 fy = 250 mpa Temperature of Steel Chimney 400 °C External corrosion allowance Tce mm (ref.Table- 1; IS-6533 part-2:1989 for non-copper bearing steel and design life 20 years) Temperature Coefficient Kt 0.50 mm Load Combinations Reference: clauses 6.5, IS 6533(Part-2):1989 (a) Dead load+ Wind load (b) Dead load+ Load due to lining+ Imposed load on service platforms + Wind load 2: Forces acting on Steel Chimney : = density of steel = 1) Self weight of chimney . Ws = . (π d) . (t) .(h) Ws = Ws (tension) Ws = 1.2 . Ws (compression) 2) Weight of Lining . = density of lining = Ws = . (π d) . (t) .(h) = thickness of lining = efficiency of joint on tension side η t = efficiency of joint on tension side ηc = Internal corrosion allowance Tci mm (ref.Table- 1; IS-6533 part-2:1989 for non-copper bearing steel and design life 20 years) Unit wt of Brick lining 20.12 kn/m3 Steel density 78.50 kn/m3 Consider a shell thickness = TtopA 6 Ttop = TtopA + Tce + Tci = 6 + 3 + 5 = 14 mm Thickness of Brick Lining 100 mm 5 mm Minimum thickness of the shell without corrosion = Tmin = dtop/500 6 mm 0.70 1.00 Weight of the (platform+ access ladder+ helical strake+ rain cap + etc) is assumed to be 20% of the self weight of chimney shell. ρ 78.50 kn/m3 ρ ρ 20.12 kn/m3 t 100.00 mm Allowable tensile stress in steel plate as per IS 800-2007 = 0.6*fy*kt*ηt = 53 mpa 200000 mpa E = Youngs modulus of Elasticity of steel ρ Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com Visit Abqconsultants.com This program Designs and Optimises Steel Chimney and the RCC Foundation. Written and programmed by :- A B Quadri www.abqconsultants.com [email protected] [email protected] 9959010210 9959010211

description

Visit Abqconsultants.comThis program Designs andOptimises Steel Chimney andthe RCC Foundation as per Indian Code.Written and programmed by:-A B [email protected]@gmail.com99590102109959010212

Transcript of Design of Steel Chimney and Rcc Foundation as Per Indian Code 22052014

  • Sheet :

    Cont'd :

    this only

    Design of Self supporting Steel Chimney forData Wind Loads as per India Standards.

    Prepared by : Date :

    Job No. :

    Verified by :

    CALCULATION

    Note : Enter Data in Cells marked

    Height of Steel Chimney 80.00 m

    Outside Diameter at Top 3.00 m

    Revision Notes :

    Calculation Sheet

    Project :

    3 mm

    Subject :

    Consider outside diameter of the chimney at base dbase :=

    5.00 m

    Shape factor of Steel chimney circullar in plan.0.70

    Adopt height of Flared Portion 25.00 m

    Minimum outside diameter of flared chimney at base = 1.60*Dtop 4.80 m

    Intensity of Wind Pressure upto a height of 30 m as per Is 875 1.50 kn/m2

    Recommended height of Flared Portion = H/326.67 m

    Yeild stress of Chimney Steel as per IS 2062-2006 fy = 250 mpa

    Temperature of Steel Chimney 400 C

    External corrosion allowance Tce mm (ref.Table-1; IS-6533 part-2:1989 for non-copper bearing steel and design life 20 years)

    Temperature Coefficient Kt 0.50

    mm

    Load Combinations Reference: clauses 6.5, IS 6533(Part-2):1989

    (a) Dead load+ Wind load

    (b) Dead load+ Load due to lining+ Imposed load on service platforms + Wind load

    2: Forces acting on Steel Chimney : = density of steel =

    1) Self weight of chimney .

    Ws = . ( d) . (t) .(h)

    Ws = Ws (tension) Ws = 1.2 . Ws (compression)

    2) Weight of Lining . = density of lining =

    Ws = . ( d) . (t) .(h) = thickness of lining =

    efficiency of joint on tension side t =efficiency of joint on tension side c =

    Internal corrosion allowance Tci mm (ref.Table-1; IS-6533 part-2:1989 for non-copper bearing steel and design life 20 years)

    Unit wt of Brick lining 20.12 kn/m3

    Steel density 78.50 kn/m3

    Consider a shell thickness = TtopA 6

    Ttop = TtopA + Tce + Tci = 6 + 3 + 5 = 14 mm

    Thickness of Brick Lining 100 mm

    5 mm

    Minimum thickness of the shell without corrosion = Tmin = dtop/500 6 mm

    0.70

    1.00

    Weight of the (platform+ access ladder+ helical strake+ rain cap +

    etc) is assumed to be 20% of the self weight of chimney shell.

    78.50 kn/m3

    20.12 kn/m3

    t 100.00 mm

    Allowable tensile stress in steel plate as per IS 800-2007 = 0.6*fy*kt*t = 53 mpa

    200000 mpaE = Youngs modulus of Elasticity of steel

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    Visit Abqconsultants.com

    This program Designs and

    Optimises Steel Chimney and

    the RCC Foundation.

    Written and programmed by

    :-

    A B Quadri

    www.abqconsultants.com

    [email protected]

    [email protected]

    9959010210

    9959010211

  • Wind Pressure , Moment and Shear from Top at every Segment

    Nos of horizontal Segments chimney divided into = Each Segment depth m.

    0

    1

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    12

    13

    14

    15

    16

    17

    18

    19

    20

    21

    22

    23

    24

    25 3.20

    s .n

    o

    Height from ground

    Wind Pressure

    diameter effective D = D*0.7

    Force on each

    segment P @

    cg

    Shear @

    bottom of each

    segment

    Moment @ bottom of each

    segment.

    m kn/m2 m D*S.f Kn Kn Kn.m

    80.00 1.73 3.00 2.10 11.60

    76.80 1.72 3.00 2.10 11.53 12 37

    0 0

    73.60 1.71 3.00 2.10 11.46 23 111

    70.40 1.69 3.00 2.10 11.39

    67.20 1.68 3.00 2.10 11.31 46 369

    35 222

    64.00 1.67 3.00 2.10 11.23 57 552

    60.80 1.66 3.00 2.10 11.15

    57.60 1.65 3.00 2.10 11.06 80 1026

    69 771

    54.40 1.63 3.00 2.10 10.97 91 1317

    51.20 1.62 3.00 2.10 10.88

    48.00 1.60 3.00 2.10 10.78 113 2002

    102 1642

    44.80 1.59 3.00 2.10 10.67 123 2397

    41.60 1.57 3.00 2.10 10.56

    38.40 1.55 3.00 2.10 10.44 145 3289

    134 2826

    35.20 1.53 3.00 2.10 10.31 155 3785

    32.00 1.51 3.00 2.10 10.17

    28.80 1.50 3.00 2.10 10.08 176 4876

    165 4314

    25.60 1.50 3.00 2.10 10.08 186 5470

    22.40 1.50 3.19 2.23 10.71

    19.20 1.50 3.42 2.39 11.48 206 6756

    196 6096

    16.00 1.50 3.65 2.55 12.26 218 7454

    12.80 1.50 3.88 2.71 13.03

    9.60 1.50 4.11 2.88 13.81 243 8968

    230 8190

    6.40 1.50 4.34 3.04 14.58 257 9790

    3.20 1.50 4.57 3.20 15.35 272 10659

    0.00

    10.00

    20.00

    30.00

    40.00

    50.00

    60.00

    70.00

    80.00

    90.00

    0.00 0.50 1.00 1.50 2.00

    Wind pressure diagram

    Wind force

    He

    igh

    t in

    me

    ters

    Wind pressure KN/m2

    9959010211

    24

    25

    3.20 1.50 4.57 3.20 15.35

    0.00 1.50 4.80 3.36 0.00 287 11577

    272 10659

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    -10.00

    0.00

    10.00

    20.00

    30.00

    40.00

    50.00

    60.00

    70.00

    80.00

    90.00

    0.00 2000.00 4000.00 6000.00 8000.00 10000.00 12000.00 14000.00

    Moment Diagram

    Moment Diagram

    -10.00

    0.00

    10.00

    20.00

    30.00

    40.00

    50.00

    60.00

    70.00

    80.00

    90.00

    0.00 50.00 100.00 150.00 200.00 250.00 300.00 350.00

    Shear Diagram

    Shear Diagram

    Shear Force in KN

    He

    igh

    t in

    me

    ters

    He

    igh

    t in

    me

    ters

    Moment in Kn.m

    -10.00

    0.00

    10.00

    20.00

    30.00

    40.00

    50.00

    60.00

    70.00

    80.00

    90.00

    0.00 0.50 1.00 1.50 2.00

    Wind pressure diagram

    Wind force

    He

    igh

    t in

    me

    ters

    Wind pressure KN/m2

    9959010211

  • 4 : Thickness of Chimney Plate without corrosion allowance :

    0

    1

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    12

    667

    0.08316 340.92 728

    0.08316

    303

    425

    0.05544 151.52 485

    0.06930

    Kn

    0.04158 0 0

    0.04158 14.21

    Ok

    29.23

    36.96 36.96

    14.933 7.467 36.96 36.96

    38400 12.800 6.400 29.23 29.23

    Ok

    Ok

    0.00 3000

    30006

    500

    19.20 30006

    500

    16.00 30006

    500

    12.80 30006

    500

    10300

    28.80 300010

    300

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    6400 2.133 1.067

    32000 10.667

    51200 17.067 8.533

    44800

    Ok

    Ok

    Ok

    Sect

    ion M

    odulu

    s Z

    =

    0.7

    7 d

    2 t

    Self w

    t W

    s fr

    om

    top

    Wt

    of

    Lin

    ing f

    rom

    top

    s .n

    o

    Heig

    ht

    from

    top

    dia

    mete

    r of

    chim

    ney

    from

    top

    Thic

    kness

    of

    Ste

    el Pla

    te

    without

    corr

    osi

    on

    D/t ratio

    m3 Kn

    0.00

    mm N/mm2

    Allow

    able

    str

    ess

    in

    bendin

    g a

    s per

    table

    3 *

    kt

    N/mm2

    Eff

    ect

    ive h

    eig

    ht

    for

    axia

    l st

    ress

    h1

    ratio h

    1/D

    for

    axia

    l st

    ress

    ratio h

    1/D

    for

    bendin

    g s

    tress

    =

    0.5

    *h1/D

    Allow

    able

    str

    ess

    in

    axia

    l co

    mpre

    ssio

    n a

    s per

    table

    3

    *

    kt

    8375

    22.40 30008

    375

    6500

    m mm mm

    29.23

    19200 6.400 3.200 29.23

    4.267 29.23

    5.333

    0 0.000 0.000 0.00

    3.20

    38.40 300012

    250

    9.60 30006

    500

    6.40 30006

    500

    35.20 300012

    25.60 3000

    250

    32.00 3000

    45.90

    29.23

    12800 4.267 2.133 29.23 29.23

    49.41

    70400 23.467 11.733 47.56 49.41

    64000 21.333 10.667 43.50 43.69

    43.69 43.69

    76800 25.600 12.800

    29.23

    29.2325600 8.533

    29.23

    57600 19.200 9.600

    364

    0.05544

    213.08 546

    0.06930 236.75 607

    312.51

    85.23

    132.58

    182

    0.04158 56.82 243

    0.04158 71.03

    0.04158

    61

    0.04158 28.41 121

    0.04158 42.62

    13

    14

    15

    16

    17

    18

    19

    20

    21

    22

    23

    24

    25

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    0.25999 1426.71 1828

    57.84

    789

    0.09702 464.03

    56.95

    54.13

    54.13

    0.35482 1894.00 2427

    58.53

    568.20

    1032

    1160

    850

    341820

    171

    57.60 318720

    159

    54.40 300020

    60.80

    Ok

    Ok

    80.00 480020

    240

    76.80 457020

    228

    73.60 433920

    217

    70.40

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    44.80 300014

    214

    41.60 300014

    214

    51.20 300016

    188

    48.00 300016

    188

    410920

    205

    67.2020

    194

    64.00 364820

    182 128000 35.088 17.544 45.57

    3878

    14.933 46.58

    27.733 13.867 48.43

    96000 32.000 16.000 47.81

    134400 34.653 17.327 44.72

    150

    83200

    45.88

    61.37

    108800 36.267 18.133 47.35 62.25

    102400 34.133

    160000 33.333 16.667 40.84 50.68

    153600 33.613 16.807 41.83 52.20

    147200 33.923 16.962 42.82 53.76

    140800 34.268 17.134 43.79 55.35

    57.84

    89600 29.867

    121600

    0.23165

    1476

    910

    0.11088 606.08 971

    0.09702 430.89

    0.17987 1313

    0.20494 1151.55

    1024.8835.581 17.790 46.29 60.03

    115200 36.145

    17.067

    0.13860 804.95

    0.15644 905.49

    0.11088

    18.072 46.79

    0.32157 1730.97 2218

    0.28996 1575.20 2019

    1285.50 1647

  • 01

    2

    3

    4

    5

    6

    7

    8

    9

    10

    18

    16 Ok

    Ok

    Ok

    16

    Tota

    l th

    ickness

    of

    Ste

    el p

    late

    re

    quir

    ed w

    ith inte

    rnal and e

    xte

    rnal

    corr

    osi

    on =

    SW

    tota

    l

    mm

    14

    14

    14

    14

    14

    Ok

    Ok

    14

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Thic

    kness

    check

    28.894 -26.382

    8.872 -7.867

    -12.024

    -17.045

    18.513 -16.754

    23.749 -21.740

    23.696 -21.435

    tensi

    le a

    nd c

    om

    pre

    eiv

    e s

    tress

    due

    to w

    ind.

    Win

    dw

    ard

    sid

    e t

    ensi

    le s

    tress

    in

    steel due t

    o (

    Win

    d +

    Self w

    t of

    Chim

    ney.)

    N/mm2 N/mm2

    0.000 0.000

    0.892 -0.641

    2.672 -2.170

    5.334 -4.580

    s .n

    o

    Heig

    ht

    from

    top

    m

    0.00

    3.20

    6.40

    9.60

    13.280

    2.010 6.438

    2.261 5.795

    2.512 6.438

    18.553

    Com

    pre

    ssiv

    e s

    tress

    in s

    teel due t

    o

    Self w

    t

    Com

    pre

    ssiv

    e s

    tress

    in s

    teel due t

    o

    Lin

    ing

    wt

    N/mm2 N/mm2

    0.000 0.000

    0.251 1.073

    0.502 2.146

    0.754 3.219

    1.005 4.292

    1.256 5.365

    1.507 6.438

    1.758 5.634

    12.80

    16.00

    19.20

    22.40

    25.60

    28.80

    32.00

    Leew

    ard

    sid

    e c

    om

    pre

    ssiv

    e s

    tress

    in

    steel due t

    o (

    Win

    d +

    Self w

    t of

    Chim

    ney.)

    N/mm2

    0.000

    1.144

    3.175

    6.087

    9.876

    14.536

    20.060

    20.271

    25.759

    25.957

    31.406

    Leew

    ard

    sid

    e c

    om

    pre

    ssiv

    e s

    tress

    in

    steel due t

    o (

    Tota

    l dead load =

    1.2

    5*W

    s) +

    wt

    of

    linin

    g +

    Win

    d

    N/mm2

    0.000

    2.280

    5.446

    9.495

    14.420

    20.215

    26.875

    26.344

    32.700

    32.316

    38.473

    Win

    dw

    ard

    sid

    e t

    ensi

    le s

    tress

    in

    steel due t

    o (

    Tota

    l dead load =

    1.2

    5*W

    s) +

    wt

    of

    linin

    g -

    Win

    d

    N/mm2

    0.000

    0.495

    0.102

    -1.172

    -3.323

    -6.345

    -10.230

    -10.681

    -14.799

    -15.075

    -19.316

    14

    18

    21 3 4 5 6

    10

    11

    12

    13

    14

    15

    16

    17

    18

    19

    20

    21

    22

    23

    24

    25

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    35.355 -30.080

    34.495 -28.968

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    -27.987

    33.148 -27.119

    37.562 -32.789

    36.369 -31.345

    33.898

    32.630 -26.350

    28.894 -26.382

    28.826 -26.062

    33.983 -30.969

    -30.632

    39.012 -35.495

    38.907 -35.139

    43.973 -39.954

    39.464

    38.967 -34.445

    44.80

    48.00

    41.60

    7.404

    6.029 7.726

    73.60

    76.80

    33.765

    4.773 6.116

    5.024 6.438

    5.275 6.760

    60.80

    64.00

    67.20

    38.40

    5.526 7.08270.40

    2.512 6.438

    2.763 5.902

    3.014 6.438

    3.266 5.979

    3.517 6.438

    3.768 6.036

    4.019 6.438

    4.270 5.473

    4.522 5.795

    51.20

    54.40

    57.60

    80.00

    32.00

    35.20

    5.778

    6.280 8.048

    31.406

    31.589

    36.998

    37.164

    -19.138

    38.473

    38.182

    44.190

    -19.316

    -19.470

    -23.777

    -23.837

    50.413

    49.644

    49.087

    48.710

    48.485

    48.391

    48.410

    48.528

    -17.886

    -16.732

    43.958

    49.846

    49.653

    55.435

    50.274

    18

    20

    20

    22

    22

    24

    24

    28

    28

    28

    28

    28

    28

    28

    -28.17742.528

    42.675

    47.992

    43.734

    43.488

    42.335

    41.393

    40.631

    40.021

    39.542

    39.177

    38.910

    -35.193

    Ok

    28

    28

    -28.161

    -32.511

    -28.653

    -27.520

    -25.479

    -23.651

    -22.001

    -20.504

    21 3 4 5 6

  • Check total thickness of Chimney with corrosion allowance :

    0

    1

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    12

    13

    62.25 0.13860 568.20 728

    s .n

    o

    Height from top

    diameter of

    chimney from

    top

    Total thickness of Steel

    Plate with corrosion

    allowance.

    D/t ratio

    Effective height for

    axial stress--h1

    ratio h1/D for axial stress

    ratio h1/D for bending

    stress = 0.5*h1/D

    Allowable stress in

    axial compression as per table

    3 * kt

    Allowable stress in

    bending as per table 3

    * kt

    Section Modulus Z = 0.77 d2 t

    Self wt Ws (total) from

    top

    Wt of Lining from top

    m mm mm mm N/mm2 N/mm2 m3 Kn Kn

    0.00 300014

    214 Ok 0 0.000 0.000 0.00 0.00 0.09702 0 0

    12800 4.267 2.133 54.13 54.13 0.09702 66.29 121

    3.20 300014

    214 Ok 6400 2.133 1.067 54.13 54.13 0.09702 33.15 61

    9.60 300014

    214 Ok 19200 6.400 3.200 54.13 54.13 0.09702 99.44 182

    6.40 300014

    214 Ok

    12.80 300014

    214 Ok 25600 8.533 4.267 54.13 54.13 0.09702 132.58 243

    16.00 300014

    214 Ok 32000 10.667 5.333 54.13 54.13 0.09702 165.73 303

    300014

    214 Ok 38400 12.800 6.400 54.13 54.13 0.09702 198.87 364

    51200 17.067 8.533 57.84 57.84 0.11088 303.04 485

    22.40 300016

    188 Ok 44800 14.933 7.467 57.84 57.84 0.11088 265.16 425

    19.20

    60.55 0.12474 426.15 607

    28.80 300018

    167 Ok 57600 19.200 9.600 60.55 60.55 0.12474 383.54 546

    25.60 300016

    188 Ok

    35.20 300020

    150 Ok 70400 23.467 11.733 59.93 62.25 0.13860 520.85 667

    32.00 300018

    167 Ok 64000 21.333 10.667 60.29

    41.60 300022

    136 Ok 83200 27.733 13.867 56.32 62.95 0.15246 677.11 789

    38.40 300020

    150 Ok 76800 25.600 12.800 57.82

    2214

    15

    16

    17

    18

    19

    20

    21

    22

    23

    24

    25

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    2218

    0.36398 1997.40 1828

    48.00 300024

    125 Ok 96000 32.000 16.000 51.67 62.50 0.16632 852.30 910

    44.80 300022

    136 Ok 89600 29.867 14.933 54.17 62.95 0.15246 729.19 850

    51.20 300024

    125 Ok 102400 34.133 17.067 49.58 62.50 0.16632 909.12 971

    Ok 115200 36.145 18.072 47.65 62.50 0.21901 1267.68 1160

    54.40 300028

    107 Ok 108800 36.267 18.133 47.54 62.50 0.19404 1126.93 1032

    48.98 62.92 0.28692 1612.18 1476

    60.80 341828

    122 Ok 121600 35.581 17.790 48.19 62.50 0.25182 1434.84 1313

    57.60 318728

    114

    62.49

    67.20 387828

    139 Ok 134400 34.653 17.327 49.39 62.90 0.32431 1799.70 1647

    64.00 364828

    130 Ok 128000 35.088 17.544

    73.60 433928

    155 Ok 147200 33.923 16.962 49.24 61.81 0.40595 2205.29 2019

    70.40 410928

    147 Ok 140800 34.268 17.134 49.44

    80.00 480028

    171 Ok 160000 33.333 16.667 48.32 59.96 0.49674 2651.60 2427

    76.80 457028

    163 Ok 153600 33.613 16.807 48.84 60.95 0.45020 2423.35

  • 01

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    N/mm2

    0.00 0.000 0.000 0.000 0.000 0.000 0.000 0.000

    3.20 0.251 0.460 0.382 -0.131 0.634 0.391 1.156

    s .n

    o

    Height from top

    Compressive stress in

    steel due to Self wt (total).

    Compressive stress in

    steel due to Lining wt

    tensile and compreeive stress due to wind.

    Windward side tensile stress in

    steel due to (Wind + Self

    wt of Chimney.)

    Leeward side

    compressive stress in

    steel due to (Wind + Self

    wt of Chimney.)

    Windward side tensile

    stress in steel due to (Total dead

    load = 1.25*Ws) + wt of lining -

    Wind

    Leeward side

    compressive stress in

    steel due to (Total dead

    load = 1.25*Ws) + wt of lining

    + Wind

    m N/mm2 N/mm2 N/mm2 N/mm2 N/mm2 N/mm2

    12.80 1.005 1.840 3.802 -2.797 4.807 -0.707 6.898

    16.00 1.256 2.299 5.691 -4.435 6.947 -1.822 9.561

    6.40 0.502 0.920 1.145 -0.643 1.648 0.403 2.693

    9.60 0.754 1.380 2.286 -1.532 3.039 0.036 4.608

    25.60 2.010 3.219 11.875 -9.865 13.884 -6.144 17.606

    28.80 2.261 3.219 13.164 -10.904 15.425 -7.119 19.210

    19.20 1.507 2.759 7.951 -6.444 9.458 -3.308 12.594

    22.40 1.758 2.817 9.256 -7.498 11.015 -4.242 14.271

    32.00 2.512 3.577 16.052 -13.540 18.564 -9.336 22.769

    35.20 2.763 3.541 17.295 -14.532 20.059 -10.300 24.291

    7 8 19 10 11 12

    12

    13

    14

    15

    16

    17

    18

    19

    20

    21

    22

    23

    24

    25

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    38.40 3.014 3.863 20.390 -17.376 23.404 -12.759 28.021

    41.60 3.266 3.805 21.571 -18.306 24.837 -13.685 29.458

    51.20 4.019 4.292 29.315 -25.296 33.335 -19.999 38.632

    54.40 4.270 3.909 28.188 -23.918 32.459 -18.941 37.435

    44.80 3.517 4.097 24.826 -21.309 28.342 -16.332 33.319

    48.00 3.768 4.024 25.938 -22.170 29.706 -17.204 34.672

    70.40 5.526 5.059 24.639 -19.113 30.165 -12.672 36.606

    57.60 4.522 4.139 27.833 -23.312 32.355 -18.043 37.624

    60.80 4.773 4.369 26.830 -22.057 31.603 -16.495 37.165

    64.00 5.024 4.599 25.978 -20.954 31.002 -15.099 36.857

    67.20 5.275 4.829 25.254 -19.979 30.529 -13.831 36.677

    73.60 5.778 5.289 24.118 -18.340 29.895 -11.607 36.628

    29.587 -9.708 36.905

    29.706 -10.622 36.732

    80.00 6.280 5.749 23.307 -17.027

    76.80 6.029 5.519 23.677 -17.648

    7 8 19 10 11 12

  • 10 :- Design of Anchor Bolts (Holding Down Bolts) :- mm dia

    Maximum tensile force per unit length of circumferance =

    * = n/mm

    Provide M dia Anchor bolt

    Area at root of threads = mm2

    Strength of Anchor Bolt = * = Kn

    Spacing of Bolt = * =

    d2 =

    Provide Anchor Bolt at mm spacing Nos of Anchor Bolts Required =

    Spacing of Bolt provided =

    9 :- Design of Base Plate :-

    Maximum stress on Chimney base plate due to Load case 1 to 12 =

    * = n/mm

    =

    = = mm 18 dia

    Allowable stress in bending of Base Plate = 0.75 fy A A

    = * = n/mm2

    Moment on wide plate = * * *

    thk base pl

    = Kn.m

    Z of plate = *

    .: t = * 6 * = thickness of base plate.

    44

    45

    N/mm2

    Width of base Plate required

    [ 10511188 ]188

    290

    0.75 250 187.5

    4.00

    188 mm 4.00 188 290

    Allowable Bearing Stress for Steel on Concrete

    6

    Oknos

    44

    1186

    1186 120

    1000

    142.32

    142.32 1000

    738

    193 mm

    Allowable Stress in Anchor bolt = 120 N/mm2

    190

    Ok

    mm

    26.350 28.0 738 Ok

    84

    188

    5023 mm

    mm

    84 nos

    188 mm

    @

    44

    290

    6000000

    10.511

    188 t^2

    48.528 28.0 1359 Ok

    1359 340

    4.00

    Ok

    *

    = Adopt t =

    9 :- Design of Vertical Stiffner Plate :- mm

    Axial load on stiffner = Tensile load on one bolt = Fa =

    Effective length of stiffner = * =

    Width of stiffner =

    Net thickness of stiffner =

    = mm L/r = = fcc = = *

    Allowable stress in compression ac = =

    Allowable Load = ac x A = * * = kn kn

    .: Provide Vertical stiffner Plate = thick

    18 thk 45

    thk

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    200000

    61.71 mpa

    61.71

    122.687 E

    (l/r)

    9.870

    15052

    mpa

    3.464 425

    290 12 215 Ok>= 142

    340

    mm 45 mm

    [ 188 187.50 ] Sect A-A

    12 mm

    Assume thickness of stiffner , including external corrosion allowance =

    mm

    18 290 mm

    4250.85 500

    Ok

    3.464

    131

    mm

    142.32 Kn

    Ok42.31

    18 mm

    r

  • 10 :- Deflection of Chimney :-

    0

    1

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    12

    13

    14

    15 Ok

    0.00E+00

    1.27E-09

    3.82E-09

    7.62E-09

    1.27E-08

    1.90E-08

    2.65E-08

    check less than

    H/200

    9.88E-05

    1.20E-04

    1.12E+01

    6

    6

    6

    3.20

    22.40 30008

    25.60 30008

    28.80 300010

    M/EI

    1/mm

    3000

    12.80 3000

    19.20

    6

    16.00 30006

    Ok

    Ok

    Ok

    Ok

    30006

    6.40 30006

    9.60

    143000

    3000

    s .n

    o

    Height from top

    diameter of

    chimney from

    top

    Assumed thickness of Steel

    Plate without

    corrosion

    m mm mm m4

    Moment of Inertia I

    (m4)

    0.16632

    Area M/EI

    mm

    0.00E+00

    2.04E-06

    8.15E-06

    1.83E-05

    3.25E-05

    5.06E-05

    7.28E-05

    Wind Moment at bottom of

    each segment.

    Kn.m

    0

    37

    111

    222

    369

    552

    771

    1026

    1317

    0.00

    Ok

    35.20 300012

    38.40 300012

    41.60 300014

    44.80

    48.00 300016

    32.00 300010

    1.31E+01

    9.41E+00

    3000

    Moment of (Area M/EI)

    from top

    mm2

    0.00E+00

    4.35E-03

    3.91E-02

    1.46E-01

    3.64E-01

    7.29E-01

    1.28E+00

    2.06E+00

    2.87E+00

    4.94E-08

    5.35E-08

    6.41E-08

    6.80E-08

    7.91E-08

    2.59E-04

    2.83E-04

    1642

    2002

    2397

    2826

    3289

    0.18711

    0.18711

    0.20790

    0.20790

    0.22869

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    3785

    4314

    0.22869

    0.24948

    8.28E-08

    9.43E-08

    233

    218

    204

    189

    174

    160

    146

    132

    118

    105

    92

    80

    69

    58

    48

    39

    1.42E-04

    1.65E-04

    1.88E-04

    2.11E-04

    2.35E-04

    3.53E-08

    3.96E-08

    0.14553

    0.14553

    0.14553

    0.14553

    0.14553

    0.14553

    0.14553

    0.16632

    deflect

    ion

    mm

    height to

    deflection ratio (h/)

    344

    352

    362

    373

    386

    400

    417

    437

    461

    488

    521

    559

    607

    664

    736

    827

    mm

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    3.87E+00

    5.00E+00

    6.32E+00

    7.77E+00

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    30.00

    40.00

    50.00

    60.00

    70.00

    80.00

    90.00

    De

    fle

    ctio

    nD

    iag

    ram

    15

    16

    17

    18

    19

    20

    21

    22

    23

    24

    25

    Maximum deflection at top = mm

    Height to deflection ratio (h/) at top = = =

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    20

    Ok

    3.32E-04 1.75E+01

    1.92E+01

    1.91E+01

    410920

    64.00 3648

    57.60

    20

    76.80 457020

    80.00 480020

    54.40 Ok

    16

    1.65E+01

    1.58E+01

    3187

    67.20 3878

    70.40

    1.52E+01

    73.60 433920

    48.00 3000

    51.20 3000

    20

    60.80 341820

    0.74776

    0.88074

    1.31E+01

    7.82E-08

    300020

    1.52E+01

    1.47E+01

    233

    3.43E-04

    3.22E-04

    2.93E-04

    2.64E-04

    2.39E-04

    2.19E-04

    2.02E-04

    1.87E-04

    2.83E-04

    3.07E-04

    1.83E+01

    1.73E+01

    Ok

    Ok

    4314

    4876

    7.13E-08

    6.55E-08

    6.05E-08

    5.63E-08

    0.24948

    0.29106

    0.34902

    0.24948

    0.43031

    0.52334

    0.62889

    1.02862

    1.19218

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    9.43E-08

    9.77E-08

    1.10E-07

    1.05E-07

    9.68E-08

    8.66E-08

    39

    Ok Ok

    5

    3

    1

    0

    0

    827

    944

    1095

    1295

    1562

    1935

    2491

    3413

    Ok

    10703

    0

    5470

    6096

    6756

    7454

    8190

    8968

    9790

    10659

    11577

    5248

    31

    23

    17

    12

    8

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    Ok

    80000

    233

    344

  • 10 :- Design of Chimney Foundation :-

    Loads on Foundation :-

    Self Weight of Chimney without corrosion allowance = 100As

    = bd

    = 15 20 25 30 35 40

    0.25 0.22 0.22 0.23 0.23 0.23 0.23

    0.50 0.29 0.30 0.31 0.31 0.31 0.32

    0.75 0.34 0.35 0.36 0.37 0.37 0.38

    1.00 0.37 0.39 0.40 0.41 0.42 0.42

    1.25 0.40 0.42 0.44 0.45 0.45 0.46

    1.50 0.42 0.45 0.46 0.48 0.49 0.49

    = 1.75 0.44 0.47 0.49 0.50 0.52 0.52

    = 2.00 0.44 0.49 0.51 0.53 0.54 0.55

    2.25 0.44 0.51 0.53 0.55 0.56 0.57

    2.50 0.44 0.51 0.55 0.57 0.58 0.60

    2.75 0.44 0.51 0.56 0.58 0.60 0.62

    3.00 0.440.51 0.57 0.60 0.62 0.63

    D =

    T =

    =

    Area = =

    9.00 10.00

    Allowable compressive stress (Bending) N/mm2 5.00 7.00 8.50 10.00 11.50 13.00

    Allowable tebsile stress (Direct) N/mm2 -3.60 -4.00 -4.40

    Moment at foundation top due to wind load

    Shear at foundation top due to wind load 287 Kn

    Sw1

    Sw2

    SL

    Grade of Steel (N/mm2)

    8.00

    15MGrade of conc (N/mm2)

    140 230

    250

    7.18

    Allowable compressive stress (Direct) N/mm2 4.00 5.00 6.00

    Kn.m

    -2.00 -2.80 -3.20

    9.33 8.11

    415

    Allowable tebsile stress

    N/mm2

    kn/m3

    530 Kn

    1894 Kn

    2652 Kn

    2427 Kn

    Weight of the (platform+ access ladder+ helical strake+ rain cap + etc) is assumed to be 20% of the self weight of chimney shell without corrosion allowance

    Weight of the (platform+ access ladder+ helical strake+ rain cap + etc) is assumed to be 20% of the self weight of chimney shell with corrosion allowance

    20 25 30 35 40

    modular ratio m 18.67 13.33 10.98

    Adopt the diameter of Chimney foundation

    m

    SBC of Soil At foundation Base 300 kn/m

    Depth of foundation from NGL 6.00 m

    Concrete density25

    Mwl1

    Swl1

    Self Weight of Chimney with corrosion allowance

    Self Weight of Chimney Lining.

    Swp1 = 379 Kn

    Swp2 =

    Moment due to wind shear at foundation base Mswl1 = 1721 Kn.m

    12.00

    D

    m

    113.10

    11577

    1450 mm

    Self wt of Footing Swf1 7687 kn

    Adopt the thickness of Chimney foundation

    Ok

    Permissible Shear Stress in Concrete Tc

    N/mm2 for grade of concrete

    Ok

    Load Combinations Reference: clauses 6.5, IS 6533(Part-2):1989

    (a) Dead load+ Wind load = =

    (b) Dead load+ Load due to lining+ Imposed load on service platforms + Wind load

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    Dl+Wl

    12387 13299 187.91

    Dl+Wl

    13296 13299

    31.13 1.074 5.588 OkSw1+swp1+SL+swf1+Mwl1+Mswl1

    3

    Dl+Wl

    10338 13299 169.80 13.02

    DL (Axial)

    1

    2

    39.17Sw2+swp2+SL+swf1+Mwl1+Mswl1

    Kn

    Sw2+swf1+Mwl1+Mswl1

    4

    s.no

    Dl+Wl

    kn/m2 kn/m2

    195.95 1.000 5.999 Ok

    Sw1+swf1+Mwl1+Mswl1

    9581 13299 163.10 6.32 1.388 4.322 Ok

    4

    D

    D 169.65

    Kn.m

    Load caseF.S due to

    over turning

    m

    e = (M/P) eccentricity < D/8, no

    uplift checkDL/A - MWL/ZDL/A + MWL/ZWL (Moment)

    m

    32

    Z

    1.286 4.664 Ok

  • eP

    Data FFLH

    Soil filling inside

    Actual Loading Pattern.Actual Loading Pattern.Actual Loading Pattern.Actual Loading Pattern.

    = P'

    A

    Depth of Footing T = 1450 mm

    6000

    Totd

    Outer dia of chimney base plate d = 5.323 m

    1450

    T

    Dia of Footing OD = 12.00 m

    A = 200 mm

    Depth of Soil D = 4550

    Concrete Grade fc' = 25 N/mm2

    200

    AReinforcement Steel Grade fy = 415 N/mm2

    S.B.C of Soil Qs = 200 Kn/m2

    4550

    D

    Design of Footing slab

    Level of footing below ground

    Totd = 6000 mm

    FGL

    mm

    12000

    Reinforcement cover c = 75 mm

    OD

    OD

    M'

    Zxx

    5323

    d

    12000

    12000

    Footing Reinforcement dia = 20 18 mm

    Assume initially of mm bars nos

    + mm bars = mm2 Spacing between bars at

    = = radians end. =

    = = mm

    = = mm

    = mm Length of segment 'PQ'

    = mm Length of segment 'RS'

    Net Uniform pressure Main Reinforcement

    =

    =

    =

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    569

    2.40 0.0419

    Radius of Chimney ro 2662

    Radius of Foundation fro 6000

    Bar Spacing at ro 111

    Area of Segment 'PQRS' 0.606 m2

    = 1.884 mfrom 'PQ'

    fig 9

    Area covered by

    one unit of main

    reinforcement.

    spaced radially along the circumferance.

    37699

    150

    251

    300

    =

  • Section A - A

    Shear Stirrups

    Main Radial reinforcement Circullar reinf

    nos 16 @ c/c

    cover

    .: = + = =

    .: k = * = =

    * + =

    j = 1 - k = 1 - = =

    3 =

    R = 1 j k = 1 * * * =

    2 2

    Hence d = = * =

    * R * = m3

    + m3

    .: adopt T = cover = d = - + m3

    .: d = effective depth + m3

    As = = = = m3

    Fyall * j * d * *

    Ok

    Not Required

    2662 2500 838

    Straight portion Sloping portion

    fig 10

    Moment at 'PQ' Mf

    1.52

    r

    415

    10.98

    105.72

    1450

    900

    20 150 200

    688 75

    1375

    6000

    N/mm2

    25 N/mm2

    8.5 N/mm2

    Mf 152.29 1000000 1110

    b 111 1.109

    1450 mm 75 mm 1450 75

    1375 mm Ok

    M 152293825

    m

    533 mm2

    29.39

    230 0.904 1375

    230 N/mm2

    16

    10.98 8.5 0.289

    10.98 8.5 230

    0.289 0.904

    3

    fc'all 8.5 0.904 0.289 1.109

    critical punching shear section

    critical shear Section

    122.90

    top radial

    reinforcement

    46.04

    101.79

    53.92

    307.46

    volume of footing

    Wt of Footing

    mm

    152.29 Kn .m

    fyall

    fy

    fc'

    fc'all

    1

    C / L of foundation

    C / L

    Fyall * j * d * *

    = .: Adopt As = = kn

    .: + = * ( + )

    4 = kn

    =

    @ c/c = * = %

    *

    Check Punching shear at ro + d/2 from the c/L

    r = d = r + d =

    2 2

    = = radians

    = = mm

    = = mm

    = mm

    = mm

    =

    .: F = + =

    = = * =.: Depth required for punching shear do

    * *=

    25 0.8 N/mm2

    Bar Spacing at rps 140 Length of segment 'a1a2'

    Bar Spacing at fro 251 Length of segment 'RS'

    = 73.0 Kn / m2Area of Segment 'PQa1a2' 0.519052 m2

    CG of Segment 'PQa1a2'= 1.451 m

    =

    Kn / m2

    60.59 8.99

    Main radial reinforcement 569

    Allowable Punching Shear stress

    Punching Shear at 'a1a2'

    distribution steel 111

    Provide 20

    1

    1375 OK

    = 43.8

    230 0.904 1375

    567 mm 2 >= 533 mm2 567 mm2

    0.16 fck 0.16

    78.4 Kn / m2from 'a1a2'

    Radius of Punching shear rps 3349

    Radius of Foundation fro 6000

    layer of

    Net Uniform pressure

    under area 'PQRS'

    Pressure due to

    Moment at 'RS'

    Pressure due to

    Moment at 'PQ'

    Minimum As required

    Punching Shear :Punching Shear :Punching Shear :Punching Shear :

    mm provided

    = =69574

    Wt of Footing

    7687

    F

    0.16 fck 140 0.8 140

    620

    Net Wt of Footing

    5044

    69.57 Kn

    C / L of foundation

    C / L

  • Check shear at r + d from the c/L, End of Straight portion,

    and at three points at sloping portion.

    20 + 18 20 + 10 20 + 14 20 + 16 20 + 14 20 + 14

    Shear :Shear :Shear :Shear :

    distance from c/L mm 2662 3349 4037 5162 5581 6000

    Reinforcement Spacing mm 110 140 168 216 232 250

    Effective depth mm 1375 1375 1375 1192 1008 825

    Bar dia mm

    As mm2 569 393 468 515 468 468

    p% 0.3760 0.2040 0.2026 0.2002 0.2001 0.2270

    Ok Ok Ok Ok Ok Ok

    Net Uniform pressure kn/m2 73.0 73.0 73.0 73.0 73.0 73.0

    Pressure due to moment @ rs kn/m2 78.4 78.4 78.4 78.4 78.4 78.4

    Pressure due to moment at section kn/m2 34.8 43.8 52.7 67.4 72.9 78.4

    Area of Segment 'PQxx' m2 0.606 0.519 0.413 0.196 0.102 0.000

    CG of Segment 'PQxx' m 1.89 1.45 1.05 0.43 0.21 0.00

    M actual / bar Kn.m 153 104 61 12 3 0

    M allowable / bar Kn.m 163 112 134 128 98 80

    Ok Ok Ok Ok Ok Ok

    p% for Shear 0.25 0.25 0.25 0.25 0.25 0.25

    Shear Stress tc N/mm2 0.23 0.23 0.23

    Shear allowable Kn 53 59 54

    Shear actual Kn 52 28 15

    mm 0 0 0

    .: Provided spacing = mm 0 0 0

    Shear Reinf Not Reqd Not Reqd Not Reqd

    Shear - Vs per main bar Kn 1 1 1

    Shear - MS bar dia fyall 230 1 1 1

    spacing mm 0 0 0

    Minimum shear s = 2.5Asvfy/b

    Prep By : A B Quadri- Abq Consultants - 9959010210 - [email protected]/2 Royal Residency, Besides Amba talkies, Mehdipatnam , Hyderabad-500028-www.abqconsultants.com

    .: Provided spacing = mm 0 0 0