Design of Seismic Resistant Steel Building Structures-Concentrically_Braced_Frames

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  • 1Design of SeismicDesign of Seismic--Resistant SteelResistant Steel

    Building StructuresBuilding Structures

    Prepared by:Djoni Simanta

    Concentrically Braced Frames

    Concentrically Braced FramesConcentrically Braced Frames

    Description and Types of Concentrically BracedFrames

    Basic Behavior of Concentrically Braced Frames SNI Seismic Provisions for Special Concentrically

    Braced Frames

    Concentrically Braced FramesConcentrically Braced Frames

    Description and Types of Concentrically BracedFrames

    Basic Behavior of Concentrically Braced Frames SNI Seismic Provisions for Special Concentrically

    Braced Frames

    Concentrically Braced Frames (CBFs)Concentrically Braced Frames (CBFs)Beams, columns and braces arranged to form avertical truss. Resist lateral earthquake forces bytruss action.

    Develop ductility through inelastic action in braces.- braces yield in tension- braces buckle in compression

    Advantages- high elastic stiffness

    Disadvantages- less ductile than other systems (SMFs, EBFs, BRBFs)

    - reduced architectural versatility

  • 2Types of CBFsTypes of CBFs

    Single Diagonal Inverted V- Bracing V- Bracing

    X- Bracing Two Story X- Bracing

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  • 4Concentrically Braced FramesConcentrically Braced Frames

    Description and Types of Concentrically BracedFrames

    Basic Behavior of Concentrically Braced Frames SNI Seismic Provisions for Special Concentrically

    Braced Frames

    Inelastic Response of CBFs under Earthquake LoadingInelastic Response of CBFs under Earthquake Loading

    Inelastic Response of CBFs under Earthquake LoadingInelastic Response of CBFs under Earthquake Loading

    Tension Brace: Yields(ductile)

    Compression Brace: Buckles(nonductile)

    Columns and beams: remain essentially elastic

    Inelastic Response of CBFs under Earthquake LoadingInelastic Response of CBFs under Earthquake Loading

    Compression Brace(previously in tension):Buckles(nonductile)

    Tension Brace (previously incompression): Yields(ductile)

    Columns and beams: remain essentially elastic

  • 5

  • 6Developing Ductile Behavior in CBFsDeveloping Ductile Behavior in CBFs

    Design brace connections for maximumforces and deformations imposed by braceduring cyclic yielding/buckling

    General ApproachGeneral Approach

    Developing Ductile Behavior in CBFsDeveloping Ductile Behavior in CBFs

    Design beams and columns (and columnsplices and column bases) for maximumforces imposed by braces

    General ApproachGeneral ApproachDeveloping Ductile Behavior in CBFsDeveloping Ductile Behavior in CBFs

    General ApproachGeneral Approach

    Design braces based oncode specifiedearthquake forces.

    Design all other frameelements for maximumforces that can bedeveloped by braces.

  • 7Maximum Forces Developed by BracesMaximum Forces Developed by Braces

    Braces in TensionBraces in Tension -- Axial Force:Axial Force:

    P

    P

    Pmax = PyFor design:

    Take Pmax = Ry Fy Ag

    Maximum Forces Developed by BracesMaximum Forces Developed by BracesBraces in CompressionBraces in Compression -- Axial ForceAxial Force

    P

    P

    Pmax

    For design:

    Take Pmax = 1.1 Ry Pn( Pn = Ag Fcr )

    Take Presidual = 0.3 Pn

    Presidual 0.3 Pcr

    Maximum Forces Developed by BracesMaximum Forces Developed by Braces

    Braces in CompressionBraces in Compression -- Bending Moment:Bending Moment:

    PP

    MM

    For "fixed" end braces: flexural plastic hinges will form atmid-length and at brace ends. Brace will impose bendingmoment on connections and adjoining members.

    Plastic Hinges

    For design:

    Take Mmax = 1.1 Ry Fy Zbrace (for critical buckling direction)

    Maximum Forces Developed by BracesMaximum Forces Developed by Braces

    Braces in CompressionBraces in Compression -- Bending Moment:Bending Moment:

    For "pinned" end braces: flexural plastic hinge will form atmid-length only. Brace will impose no bending moment onconnections and adjoining members.

    Must design brace connection to behave like a "pin"

    PP

    PP

    Plastic Hinge

  • 8Maximum Forces in Columns and BeamsMaximum Forces in Columns and Beams

    To estimate maximum axial forcesimposed by braces on columns andbeams:

    Braces in tension:Braces in tension:Take P = Ry Fy Ag

    Braces in compression:Braces in compression:

    Take P = 1.1 Ry Pn or P = 0.3 Pnwhichever produces critical design case

    ExampleExample

    Find maximum axialcompression in column.

    Tension Braces:Take P = Ry Fy Ag

    Compression Braces:Take P = 0.3 Pn

    ExampleExample

    Ry Fy Ag

    Ry Fy Ag

    Ry Fy Ag

    0.3 Pn

    0.3 Pn

    Column Axial Compression =

    [ (Ry Fy Ag ) cos + (0.3 Pn) cos ] + Pgravity

    (sum brace forces for all levelsabove column)

    0.3 Pn

    ExampleExample

    Find maximum axialtension in column.

    Tension Braces:Take P = Ry Fy Ag

    Compression Braces:Take P = 0.3 Pn

  • 9ExampleExample

    Ry Fy Ag

    0.3 Pn

    Ry Fy Ag

    Ry Fy Ag

    0.3 Pn

    0.3 Pn

    Column Axial Tension =

    [ (Ry Fy Ag ) cos + (0.3 Pn) cos ] - Pgravity

    (sum brace forces for all levelsabove column)

    ExampleExample

    Find maximum axialcompression in column.

    Tension Brace:Take P = Ry Fy Ag

    Compression Brace:Take P = 0.3 Pn

    ExampleExample

    Ry Fy Ag0.3 Pn Column Axial Compression =

    (Ry Fy Ag ) cos + (0.3 Pn) cos + Pgravity

    Note

    Based on elastic frame analysis:

    Column Axial Force = Pgravity

    ExampleExample

    Find maximum bendingmoment in beam.

    Tension Brace:Take P = Ry Fy Ag

    Compression Brace:Take P = 0.3 Pn

  • 10

    ExampleExample

    Ry Fy Ag0.3 Pn

    ExampleExample

    ( Ry Fy Ag - 0.3 Pn ) sin

    Compute moment in beamresulting from application ofconcentrated load at midspanof ( Ry Fy Ag + 0.3 Pn ) sin

    and add moment due togravity load

    Note

    Based on elastic frame analysis:

    Moment in beam 0

    ExampleExample

    Find maximum axialtension and compressionthat will be applied togusset plate.

    Tension Brace:Take P = Ry Fy Ag

    Compression Brace:Take P = 1.1 Ry Pn

    ExampleExample

    1.1 Ry PnRy Fy Ag

    Check gusset buckling,beam web crippling, etc.

    Check gusset yield, gussetnet section fracture, gussetblock shear fracture, localbeam web yielding, etc.

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    Concentrically Braced FramesConcentrically Braced Frames

    Description and Types of Concentrically BracedFrames

    Basic Behavior of Concentrically Braced Frames SNI Seismic Provisions for Special Concentrically

    Braced Frames

    SNISNI Seismic ProvisionsSeismic Provisions

    Section F1 Ordinary Concentrically Braced Frames (OCBF)

    Section F2 Special Concentrically Braced Frames (SCBF)

    Section F1Ordinary Concentrically Braced Frames

    (OCBF)Scope

    Basis of Design

    Analysis

    System Requirements

    Members

    Connections

    SNI Steel Seismic Provisions - OCBFF1.1 Scope

  • 12

    Section F2Special Concentrically Braced Frames (SCBF)

    Scope

    Basis of Design

    Analysis

    System Requirements

    Members

    Connections

    SNI Steel Seismic Provisions - SCBFF2.1 Scope

    Special concentrically braced frames (SCBF) areexpected to withstand significant inelastic deformationswhen subjected to the forces resulting from the motionsof the design earthquake.

    SNI Steel Seismic Provisions - SCBFF2.5 MembersSlenderness

    Bracing members shall have:yF

    E4r

    KL

    Fy = 36 ksi: KL/r 114

    Fy = 42 ksi: KL/r 105

    Fy = 46 ksi: KL/r 100

    Fy = 50 ksi: KL/r 96

  • 13

    Slenderness

    Bracing members shall have:yF

    E4r

    KL

    Exception:

    Braces with: 200r

    KLFE4

    y

    are permitted in frames in which the availablestrength of the columns is at least equal to themaximum load transferred to the columnconsidering Ry times the nominal strengths ofthe brace elements.

    ExampleExample

    Find required axialcompression strength ofcolumn.

    ExampleExample

    Ry Fy Ag

    Ry Fy Ag

    Ry Fy Ag

    0.3 Pn

    0.3 Pn

    Required column axial compressionstrength =

    [ (Ry Fy Ag ) cos + (0.3 Pn) cos ]+ [(1.2 + 0.2SDS) D + 0.5L]

    0.3 Pn

    OR

    0 QE+ [(1.2 + 0.2SDS) D + 0.5L]

    yFE4

    rKL

    All bracing members:

    Note: 0 = 2 for SCBF and OCBF

    ExampleExample

    Ry Fy Ag

    Ry Fy Ag

    Ry Fy Ag

    0.3 Pn

    0.3 Pn

    Required column axial compressionstrength =

    [ (Ry Fy Ag ) cos - (0.3 Pn) cos ]+ [(1.2 + 0.2SDS) D + 0.5L]

    0.3 Pn

    0 QE+ [(1.2 + 0.2SDS) D + 0.5L]

    Bracing members with: 200rKL

    FE4

    y

    NOT PERMITTED

  • 14

    F2.5 MembersBasic Required Strength

    Where the effective net area of bracing members isless than the gross area, the required tensilestrength of the brace, based on a limit state offracture of the net section shall be at least Ry Fy Ag ofthe bracing member.

    Objective: yield of gross section ofbrace prior to fracture of net section

    ExampleExample

    double angle bracing membergusset plate

    Check double angle bracing member forlimit state of net section fracture

  • 15

    Pu= Ry Fy Ag

    Required axial tension strengthof brace for limit state offracture of the net section

    Pu= Ry Fy Ag

    Critical Net Section

    Ae = U AnAe < Ag due to:

    bolt hole (An < Ag ), and

    shear lag (U < 1)

    Pu= Ry Fy Ag

    Limit state: fracture of net section

    Pn = (0.75) Ae (Rt Fu)

    Per Section 6.2: use expected tensile strength Rt FU when checking net sectionfracture of bracing member, since Ry Fy of the same member is used tocomputed the required strength

    Pu= Ry Fy Ag

    Limit state: fracture of net section(0.75) Ae (Rt Fu) Ry Fy Ag

    utyy

    g

    e

    FR75.0FR

    AA

    OR:

  • 16

    Pu= Ry Fy Ag

    Limit state: fracture of net section

    utyy

    g

    e

    FR75.0FR

    AA

    For A36 Angles:

    03.1ksi582.175.0ksi365.1

    AA

    g

    e

    For A572 Gr. 50 Angles:

    03.1ksi651.175.0ksi501.1

    AA

    g

    e

    Need to Reinforce Net Section (Ae need not exceed Ag )

    Pu= Ry Fy Ag

    Also check block shear rupture of bracing member....

    Pn = (0.75) Ubs Ant Rt Fu + lesser of0.6 Anv Rt Fu0.6 Agv Ry Fy

    Reinforcing net section of bracing member.... ExampleExample gusset platerectangular HSS bracingmember

    Check HSS bracing member for limit stateof net section fracture

  • 17

    Pu= Ry Fy Ag

    Required axial tension strengthof brace for limit state offracture of the net section

    Pu= Ry Fy Ag

    Critical Net Section

    Ae = U AnAe < Ag due to:

    slot (An < Ag ), and

    shear lag (U < 1)

    Pu= Ry Fy Ag

    Limit state: fracture of net section(0.75) Ae (Rt Fu) Ry Fy Ag

    utyy

    g

    e

    FR75.0FR

    AA

    OR:For A500 Gr B rectangular HSS:

    14.1ksi583.175.0ksi464.1

    AA

    g

    e

    Need to Reinforce Net Section (Ae need not exceed Ag )

  • 18

    Pu= Ry Fy Ag

    Also check block shear rupture of bracing member....

    Pn = (0.75) Ubs Ant Rt Fu + lesser of0.6 Anv Rt Fu0.6 Agv Ry Fy

    Ant 0

    L t = design wall thickness of HSS

    Ant = Agv = 4 L t

    For A500 Gr B rectangular HSS: Rt Fu = 1.3 x 58 ksi = 75.4 ksi

    Ry Fy = 1.4 x 46 ksi = 64.2 ksi

    Pu= Ry Fy Ag

    Also check block shear rupture of bracing member....

    L t = design wall thickness of HSS

    Pn = (0.75) ( 4 L t x 0.6 x 64.2 ksi) 1.4 x 46 ksi x Ag

    tA557.0

    L g

    = minimum length of welded overlapneeded based on block shearrupture in HSS bracing member

    Reinforcing net section of bracing member.... F2.4.4a Lateral Force Distribution

    Along any line of bracing, braces shall be deployedin opposite directions such that, for either directionof force parallel to the bracing, at least 30 percent butnot more than 70% of the total horizontal force alongthat line is resisted by braces in tension..

  • 19

    Deploy braces so that about half are in tension (and theother half in compression)

    All braces in tension (or compression) NG

    OK

    F2.4.4a Lateral Force Distribution Width-Thickness Limitations

    Columns and braces shall meet requirements ofSection D1.1.b.

    i.e. columns and braces must be seismicallycompact : ps

    Width-Thickness Limitations

    Columns: ps

    Width-Thickness Limitations

    Braces: form plastic hinge during buckling

    P

    plastic hinge

    With high b/t's - local buckling and possiblyfracture may occur at plastichinge region

  • 20

    Width-Thickness Limitations

    Bracing Members: ps

    For rectangular HSS (A500 Gr B steel):

    1.16ksi46

    ksi2900064.0FE64.0

    tb

    y

  • 21

    SNI Steel Seismic Provisions - SCBFF2.6.c. Required Strength of Bracing ConnectionsRequired Tensile Strength

    The required tensile strength of bracing connections (includingbeam-to-column connections if part of the bracing system) shallbe the lesser of the following:

    1. Ry Fy Ag of the bracing member.

    2. The maximum load effect, indicated by analysis thatcan be transferred to the brace by the system.

    Few practical applications of Item 2.

    Note that oQE is NOT an acceptable method to establish"maximum load effect"

    Ry Fy Ag

  • 22

    Pu = Ry Fy Ag

    Pu cos

    Pu sin

    Consider load paththrough connection region Pu = Ry Fy Ag

    Pu cos

    Pu sin

    Consider load paththrough connectionregion:

    Uniform Force Method -Vertical Component of Putransferred to column.

    VucVub

    Vuc + Vub = Pu sin Vuc is transferred directly to column

    Vub is transferred indirectly to columnthrough beam and beam tocolumn connectionVub

    Pu = Ry Fy Ag

    Pu cos

    Pu sin

    Huc

    Hub

    Huc + Hub = Pu cos Hub is transferred directly to beam

    Huc is transferred indirectly to beamthrough column and beam tocolumn connection

    Huc

    Consider load paththrough connectionregion:

    Uniform Force Method -Horizontal Component ofPu transferred to beam.

    Pu = Ry Fy Ag

    Pu cos

    Pu sin

    Consider load path throughconnection region:

    Use caution in use of boltsand welds.

    Section 7.2:"Bolts and welds shall not bedesigned to share force in ajoint or the same forcecomponent in a connection."

  • 23

    Pu = Ry Fy Ag

    Pu cos

    Pu sin

    If designed by uniform forcemethod - this connectionviolates Section 7.2

    Bolts and welds must transfer sameforce components.

    SNI Steel Seismic Provisions - SCBFF2.6.c. Required Strength of Bracing ConnectionsRequired Flexural Strength

    The required flexural strength of bracing connections is1.1 Ry Mp of bracing member.

    P

    MM

    For "fixed" end braces: flexural plastic hinges will form atmid-length and at brace ends. Brace will impose bendingmoment on connections and adjoining members.

    Plastic Hinges

    Mu = 1.1 Ry Mp = 1.1 Ry Fy Zbrace(for critical buckling direction)

    1.1 Ry Mp-brace

  • 24

    SNI Steel Seismic Provisions - SCBFF2.6.c.Required Strength of Bracing ConnectionsRequired Flexural Strength

    The required flexural strength of bracing connections is1.1 Ry Mp of bracing member.

    Exception:

    Brace connections that can accommodate theinelastic rotations associated with brace post-buckling deformations need not meet thisrequirement.

    For "pinned" end braces: flexural plastic hinge will form atmid-length only. Brace will impose no bending moment onconnections and adjoining members.

    Must design brace connection to behave like a "pin"

    PP

    PP

    Plastic Hinge

    Buckling perpendicularto gusset plate

    Line of rotation ("foldline") when the bracebuckles out-of-plane(thin direction of plate)

    To accommodate brace end rotation: provide "fold line"

  • 25

    2t

    2tConcrete floor slab

    2t

  • 26

    Concrete floor slab

    Styrofoam

    2t

  • 27

    > 2t

    >2t

    > 2t

  • 28

    SNI Steel Seismic Provisions - SCBFF2.6.c Required Strength of Bracing ConnectionsRequired Compressive Strength

    The required compressive strength of bracing connections shallbe at least 1.1 Ry Pn

    Pn = Ag Fcr of bracing member(per Chapter E of AISC Main Specification)

    1.1 Ry Pn

    Check:- buckling of gusset plate

    - web crippling for beam and column

    SNI Steel Seismic Provisions - SCBF

    F2.4a V-Type and Inverted V-Type Bracing

  • 29

    SNI Steel Seismic Provisions - SCBF

    F2.4a V-Type and Inverted V-Type Bracing

    (1) Design beams for unbalanced load that will occurwhen compression brace buckles and tension braceyields.

    Take force in tension brace: Ry Fy AgTake force in compression brace: 0.3 Pn

    Assume beam has no vertical supportbetween columns.

    Ry Fy Ag0.3 Pn

    wgravity = (1.2 + 0.2 SDS) D + 0.5L

    ExampleL

    Beam-to-column connections:simple framing

    wgravity = (1.2 + 0.2 SDS) D + 0.5L

    Example

    L

    ( Ry Fy Ag - 0.3 Pn ) sin ( Ry Fy Ag + 0.3 Pn ) cos

    Forces acting on beam:

    SNI Steel Seismic Provisions - SCBF

    F2.4a V-Type and Inverted V-Type Bracing

    (2) Both flanges of beams must be provided with lateralbraces with a maximum spacing of Lpd

    and

    Both flanges of the beam must be braced at the pointof intersection of the braces.

    Per Main AISC Specification (Appendix 1):

    yy2

    1pd rF

    EMM076.012.0L

  • 30

    SNI Seismic Provisions - SCBF

    F2.4b K-Type Bracing

    K-Type Braces are not Permitted for SCBF