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    Design of Structural

    Steel Joints

    Dr. Klaus WeynandFeldmann + Weynand GmbH, Aachen, Germany

    Prof. Jean-Pierre JaspartUniversity of Lige, Belgium

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    Design of Structural

    Steel Joints Introduction

    Integration of joints into

    structural design process Moment resistant joints

    Simple joints

    Design tools

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    Design of Structural

    Steel Joints

    Introduction Integration of joints into

    structural design process

    Moment resistant joints

    Simple joints

    Design tools

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    EN 1993 Part 1.8

    Chapter 1 Introduction

    Chapter 2 Basis of design

    Chapter 3 Connections made with bolts, rivets or pinsChapter 4 Welded connections

    Chapter 5 Analysis, classification and modelling

    Chapter 6 Structural joints connecting H or I sections

    Chapter 7 Hollow section joints

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    Design of simple joints

    ECCS Publication No 126 (EN)

    Background information Design guidelines

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    2 Basis of design Partial safety coefficients

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    3 Connections made mechanical fasteners

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    4 Welded connections

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    Design of Structural

    Steel Joints Introduction

    Integration of joints into

    structural design process Moment resistant joints

    Simple joints

    Design tools

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    Actual joint response

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    Actual joint response

    M

    M Rd

    S j,inicd

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    Influence on the structural response

    Displacements

    Internal forces

    Failure mode and failure load

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    M

    M

    ?

    ?

    ?

    M

    Characterization

    Modelling

    Classification

    Idealization

    Four successive steps for structural integration

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    Characterization

    Search for a unified approach whatever the material

    M

    ?

    ?

    ?

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    Various configurations (1)Continuity

    Beam-to-beam

    Column bases

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    Various configurations (2)

    Joints in portal frames

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    Various configurations (3)

    Connections and joints in

    composite construction

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    Various cross-section shapes (1)

    Hot-rolled and

    cold-formed

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    Various cross-section shapes (2)

    Built-up profiles

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    Various connection elements

    Splices

    Cleats

    End plates

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    Economy

    Reduced fabrication, transportation and erection costs

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    Specific design criteria

    Robustness

    Joints as key elements

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    Characterization (1)

    Search for a unified approach

    M

    ?

    ?

    ?

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    Characterization (2)

    Eurocode 3 Part 1-8

    Beam-to-beam joints, splices, beam-to-column joints and column

    bases: welded connections

    bolted connections (anchors for column bases)

    Background: COMPONENT METHOD

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    Three steps

    First step

    Identification of theactive components

    Second step:

    Response of the

    components

    Third step:

    Assembly of the

    components

    F F F

    E k1 E k2 E k3

    F1,RdF2,Rd

    F3,Rd

    column webin shear

    column webin tension

    column webin compression

    M

    Sj,ini

    Mj,Rd

    cd

    , ,minj Rd i RdM F z 2

    , 1j ini

    i

    E zS

    k

    Characterization (3) - component method

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    Characterization (4) - component method

    EC3 Part 1-8 provides therefore:

    a library of components

    rules for the evaluation of the properties of the components(stiffness, resistance, deformation capacity)

    rules for the evaluation of the possible component interactions

    assembly rules for components

    Applicable for simple joint and moment resistant joint

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    Characterization (4)

    Hollow section joints

    Different approach for lattice girder joints

    For many types of joint configurations:

    Joints considered as a whole

    Check of relevant failure modes Scope of application to be checked

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    M

    M

    ?

    ?

    ?

    M

    Characterization

    Modelling

    Classification

    Idealization

    Four successive steps for structural integration

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    Classification (1)

    Stiffness

    Sj,ini

    Pinned

    Semi-rigid

    RigidM

    Boundaries for stiffness

    Joint initial stiffness

    Semi-rigid

    Rigid

    Pinned

    Classification boundariesInitial joint stiffness

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    Classification (2)

    Resistance

    Mj,Rd

    Partial-strength

    Full-strength

    Pinned

    Mj

    Boundaries for strength

    Joint strength

    Full resistance

    Partial resistance

    Pinned

    Classification boundariesJoint resistance

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    Classification (3)

    Ductility

    Brittle

    Semi-ductile Ductile

    Mj

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    M

    M

    ?

    ?

    ?

    M

    Characterization

    Modelling

    Classification

    Idealization

    Four successive steps for structural integration

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    Modelling

    JOINTMODELLING

    BEAM-TO-COLUMN JOINTSMAJOR AXIS BENDING

    BEAMSPLICES

    COLUMNBASES

    SIMPLE

    SEMI-

    CONTINUOUS

    CONTINUOUS

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    M

    M

    ?

    ?

    ?

    M

    Characterization

    Modelling

    Classification

    Idealization

    Four successive steps for structural integration

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    Design of Structural

    Steel Joints Introduction

    Integration of joints into

    structural design process

    Moment resistant joints

    Simple joints

    Design tools

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    ExampleSingle sided beam-to-column joint configuration, bolted end-plate connection

    + +

    + +

    M

    V

    15

    3

    PE220

    EB140

    120

    60 10

    8030 30

    240

    4 M16 8.8

    140

    u=10=60

    5

    w=

    To be evaluated:

    Design moment resistance , initial stiffness

    0

    1

    1,01,0

    M

    M

    Material: S 235

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    General data

    2 2 140 2 12 2 12 92wc c fc ch h t r mm

    2

    2 2

    4295,6 2 140 12 7 2 12 12 1307,6vc c c fc wc cA A b t t r

    mm

    80 70,8 0,8 12 26,9

    2 2

    fc

    c

    w tm r mm

    140 8030

    2 2

    cb we mm

    2 2

    ,

    0

    12 2350,25 0,25 8460 /

    1,0

    fc yc

    pl fc

    M

    t fm Nmm mm

    Column

    Equivalent T-stub in tensionFt

    m e

    leff

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    General data

    + +

    + +

    15

    3

    IPE220120

    60 10

    8030 30

    240

    4 M16 8.8

    140

    u=10=60

    5

    w=

    9,2220 10 60 165,4

    2 2

    fb

    b

    tz h u p mm

    6,

    ,

    0

    285.406 235 10(classe 1 section) 67,07

    1,0

    pl yb yb

    c Rd

    M

    W fM kNm

    Lever arm

    Beam

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    General data

    2 2

    ,

    0

    15 2350,25 0,25 13.218 /

    1,0

    p yp

    pl p

    M

    t fm Nmm mm

    mp

    mp2

    80 5,90,8 2 0,8 2 3 33,66

    2 2

    wbp w

    w tm a mm

    2 0,8 2 60 10 9,2 0,8 2 5 35,14p fb fm p u t a mm

    140 8030

    2 2

    p

    p

    b we mm

    End plate

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    General data

    5,5

    1

    33,660,53

    33,66 30

    p

    p p

    m

    m e

    22 35,14 0,55

    33,66 30p

    p p

    mm e

    Alpha factor for effective lengths

    End plate

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    General data

    3

    ,0,9 0,9 800 157 10 90,43

    1,25

    ub st Rd

    Mb

    f AF kN

    3

    ,

    0,6 0,6 800 157 10(shear plane in thread) 60,3

    1.25

    ub sv Rd

    Mb

    f AF kN

    1

    0,5 12 15 10 14,8 2 4 47,42

    b fc p bolt nut L t t h h mm

    Bolts

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    Component No 1

    Column web in shear

    Vwp

    Vwp

    F

    M

    z

    F

    3

    ,,

    0

    0,9 0,9 1307,6 235 10 159,7

    3 3 1,0vc y cw

    wc Rd

    M

    A fV kN

    Assumption : 1

    ,

    ,1

    159,7

    159,71

    wc Rd

    Rd

    V

    F kN

    1

    0,38 0,38 1307,63,004

    1 165,4

    vcAk mmh

    Resistance

    Stiffness coefficient

    Transformation parameter

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    Component No 2

    Column web in compression

    , , min 2 2 2 5 ; 2 5

    min 9, 2 2 5 2 2 15 5 12 12 ; 9, 2 5 2 15 10 5 12 12 161, 27

    eff c wc fb f p fc fb f p fcb t a t t s t a t u t s

    mm

    , ,Assumption : min 1,0; 1,7 / 1,0wc com Ed y wck f

    , , ,

    2

    161,27 92 2350,932 0,932 0,543 0,673 1,0

    210000 7 7

    eff c wc c y wc

    p

    wc

    b d f

    E t

    1 2 2

    , ,

    1 10,713

    1 1,3 161,27 7 1307,61 1,3 /eff c wc w c vcb t A

    3

    ,2 , , , 1/ 1 0,713 1 161,27 7 235 10 1,0 189,1Rd wc eff c wc wc y wc MF k b t f kN

    Resistance

    Reduction factors to account for compression stresses and instability

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    Component No 2

    Column web in compression

    F

    F k Ei i i

    , ,

    2

    0,7 0,7 161,27 78,589

    92

    eff c wc wc

    wc

    b tk mm

    h

    Stiffness coefficient

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    Component No 3

    Column web in tension

    , , min 2 ; 4 1,25 min 2 26,9;4 26,9 1,25 30 145,10eff t wcb m m e mm

    1 2 2

    , ,

    1 10,749

    1 1,3 145,1 7 1307,61 1,3 /eff t wc wc vcb t A

    3

    ,3 , , , 0/ 0,749 145,1 7 235 10 1,0 178,7Rd eff t wc wc y wc MF b t f kN

    , ,

    3

    0,7 0,7 145,1 77,728

    92

    eff t wc wc

    wc

    b tk mm

    h

    Resistance

    Stiffness coefficient

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    Equivalent T-stub in tension

    Component No 4

    Column flange in bending

    Component No 5 End plate in bending

    F /4t

    Ft

    F /4t

    F /4t

    F /4t

    m e

    leff

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    T-stub

    Effective length

    Distinction between circular and non-circular yield line patterns

    Circular patterns Non-circular patterns

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    T-stub

    Effective length

    Groups effects to consider in addition to the individual response of each bolt-row

    Group 1+2 Group 2+3 Group 1+2+3

    Row 1

    Row 2

    Row 3

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    T-stub

    Effective length

    Groups effects to consider in addition to the individual response of each bolt-row

    Row 3

    ,3 ,3, ,3, ;( )

    Rd Rd indiv Rd groupF min F F

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    Bolt rows consideredIn this example: only bolt row 1 is considered for tension forces

    + +

    + +

    M

    V

    15

    3

    PE220EB140

    120

    60 10

    8030 30

    240

    4 M16 8.8

    140

    u=10=60

    5

    w=

    Row 1

    Row 2

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    Component No 4

    Column flange in bending

    , , , , 145,1 (see column web in tension)eff t fc eff t wcl b mm

    min ;1, 25 ; / 2 min 30;1, 25 26,9;30 30pn e m b w mm

    Resistance

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    3

    , , , , 3, , 2

    2 2 2 145,1 8460 2 90,4 10 30 10 138,5

    26,9 30eff t fc pl fc t Rd

    fc Rd t

    l m B nF kN

    m n

    , , 3 ,2 2 90,43 180,9fc Rd t t RdF B kN

    Mode 1 - Complete yielding of the flange

    Mode 2 - Bolt failure with yielding of the flange

    Mode 3 - Bolt failure

    Component No 4

    Column flange in bending

    , , , 3

    , , 1

    4 4 145,1 846010 182,5

    26,9

    eff t fc pl fc

    fc Rd t

    l mF kN

    m

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    Component No 4

    Column flange in bending

    ,4 , , 1 , , 2 , , 3min ; ; 138,5Rd fc Rd t fc Rd t fc Rd tF F F F kN

    3 3, ,

    4 3 3

    0,9 0,9 145,1 12

    11,5926,9

    eff fc t fcl t

    k mmm

    Resistance

    Stiffness coefficient

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    Component No 5

    End plate in bending

    , , min 2 ; min 2 33,66; 5,5 33,66 185eff t p p pl m m mm

    min ;1,25 ; min 30;1,25 33,66;30 30p p pn e m e mm

    , , , 3

    , ,1

    4 4 185 13.218Mode 1: 10 291

    33,66

    eff t p pl p

    ep Rd

    p

    l mF kN

    m

    3, , , , 3

    , ,2

    2 2 2 185 13.218 2 90,43 10 30Mode 2: 10 162,1

    33,66 30

    eff p t pl p t Rd p

    ep Rd

    p p

    l m B nF kN

    m n

    ,5 , ,1 , ,2 , ,3min ; ; 162,1Rd ep Rd ep Rd ep RdF F F F kN

    Resistance

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    Component No 5

    End plate in bending

    3 3, ,

    5 3 3

    0,9 0,9 185,0 1514,73

    33,66

    eff t p p

    p

    l tk mm

    m

    Stiffness coefficient

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    Component No 7

    Beam flange and web in compression

    ,7 , 367,07

    / 318,2210,8 10

    Rd c Rd b fbF M h t kN

    7k

    Resistance

    Stiffness coefficient

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    Component No 8

    Beam web in tension

    , , , , 185eff t wb eff t pb l mm

    3

    ,8 , , 0/ 185 5,9 235 10 1, 0 256,5Rd eff t wb wb yb MF b t f kN

    8k

    Resistance

    Stiffness coefficient

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    Component No 10

    Bolts in tension

    ,10 ,2 2 90,43 180,9Rd t RdF B kN

    10

    1571,6 1,6 5,30

    47,4

    s

    b

    Ak mm

    L

    Mode 3 in T-stubs for components:

    column flange in bending

    end plate in bending

    Resistance

    Stiffness coefficient

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    Mj,Rd

    Design moment resistance

    ,min 138,5 (Column flange in bending)Rd Rd iF F kN

    3

    , 138,5 165,4 10 22,91j Rd RdM F z kNm

    , , ,

    215,27

    3j el Rd j RdM M kNm

    Design plastic moment resistance

    Relevant component

    Design elastic moment resistance

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    Stiffness

    Sj,ini2 6

    2

    ,

    210000 165,4 10/ 1 6234 /

    1 1 1 1 1 1

    3,004 8,589 7,728 11,59 14,73 5,30

    j ini i

    i

    S E h k kNm rad

    , / 2 3117 /j j iniS S kNm rad

    Initial stiffness

    Secant stiffness

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    Design moment-rotation characteristic

    M

    Sj,ini

    Sj,ini

    SjS

    j= /

    Ersatzsteifigkeit:

    Mj,Rd

    2/3Mj,Rd

    Secant stiffness

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    Design of Structural

    Steel Joints

    Introduction

    Integration of joints into

    structural design process

    Moment resistant joints

    Simple joints

    Design tools

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    Nominally pinned joints

    Braced frame

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    Nominally pinned joints

    V 0 M = 0

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    Design of simple joints

    ECCS Publication No 126 (EN)

    Background information

    Design guidelines

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    Classification and modelling of joints

    Limits for classification of joints by stiffness

    Nominally pinned

    Semi-rigid

    RigidMj

    Initial stiffness of the joint

    Sj,ini

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    Classification and modelling of joints

    Sj,ini

    Limits for classification of joints by stiffness

    Nominally pinned

    Semi-rigid

    RigidMj

    Initial stiffness of the joint

    Semi-rigid joints :

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    Classification and modelling of joints

    As an alternative to a semi-continuous modelling (semi-rigid joints), is it safe to

    model the joints as nominally pinned whilst they are actually semi-rigid?

    Semi-rigid Sj,ini> 0,5EIb/Lb

    Partial strength Mj,Rd> 0,25 Mfull-strength

    Nominally pinned Sj,ini= 0

    Nominally pinned Mj,Rd= 0??

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    Classification and modelling of joints

    Yes, under the reservation the joint has:

    a sufficient rotation capacity

    = capacity to rotate

    a sufficient ductility

    = capacity to follow the actual

    loading path in a ductile way

    VRd

    V

    MYielding criterionMRd

    Supposed

    loading path

    Actual loading

    path

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    Supplementary design requirement

    Sufficient resistance to catenary effects so as to provide required structural

    robustness

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    Example: Partial depth end-plate

    Components

    Bolts in shear

    End-plate in bearing

    End-plate in shear (gross section)

    End-plate in shear (net section)

    End-plate in shear block

    End-plate in bending

    Beam web in shear Welds in shear

    Column flange in bearing

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    Partial depth end-plate

    Strength requirement

    Use of component method for the assessment of VRd

    Assessment of the strength of all the constitutive

    components of the joint

    +

    Assembly of these components

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    Partial depth end-plate

    Rotation capacity requirement

    Bending moment

    Rotationavail

    Contact between

    supported beam and

    supporting element

    Compression force

    Bending

    moment

    Bolts in tension

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    Partial depth end-plate

    Rotation capacity requirement

    hp

    he

    tp

    hbdb

    avail

    p bh d

    p

    availe

    t

    h

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    Partial depth end-plate

    Ductility requirement

    Prevent premature fracture of the bolts

    Prevent premature fracture of the welds

    under unavoidable bending moment in the joint

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    Partial depth end-plate

    Ductility requirements

    Prevent premature collapse of the bolts

    2,8 yp

    p ub

    fd

    t f

    2,8 ycf

    p ub

    fd

    t f for the supporting column

    d and fub : diameter and tensile strength of bolts

    for the end-plate

    Yielding of end-plate prior to tensile fracture of bolts

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    Design of Structural

    Steel Joints

    Introduction

    Integration of joints into

    structural design process

    Moment resistant joints

    Simple joints

    Design tools

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    Practical design tools

    Tables of standardized joints

    Dedicated software

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    Worked Example Configuration Beam IPE 500

    Column HEA 340

    End plate connection

    Design assumption

    Rigid joint

    Frame analysisMEd = 220 kNm

    CoP software used for this example: http://cop.fw-ing.com

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    Design resistance: MRd = 196 kNm < 220 kNm

    Classification: Semi-rigid

    Failure mode: Column web in compression

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    Failure mode:

    End plate in bending

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    Failure mode:

    Column web panel in shear

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    Failure mode:

    Column web panel in shear

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    Failure mode:

    Column web panel in shear

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    Design of Structural

    Steel Joints

    Dr. Klaus WeynandFeldmann + Weynand GmbH, Aachen, Germany

    Prof. Jean-Pierre JaspartUniversity of Lige, Belgium