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    Improved Column-Beam Joint in Glulam Semi-Rigid Portal Frame

    Kohei KomatsuProfessor, Research Institute for Sustainable Humanosphere, Kyoto University

    Uji, Japan

    Mitsushi AkagiFormer Engineer, Yamasa Mokuzai Co., Ltd.

    Kagoshima, Japan

    Chiori KawaiFormer Engineer, D.fact Co., Ltd.

    Nagoya, Japan

    Takuro MoriAssistant Professor, Research Institute for Sustainable Humanosphere, Kyoto University

    Uji, Japan

    Shingo HattoriPresident, D.fact Co., Ltd.,

    Nagoya, Japan

    Kiyoshi HosokawaPresident, Mokkozo Giken Ltd.,

    Hamamatsu, Japan

    Summary

    Previous column joint was composed of pass-through bolts to connect steel gusset with column.

    The joint, however, tended to bring larger deformation due to embedment of bearing plate to sidegrain of column. To prevent this deformation, LagscrewboltRwas introduced, and evaluation tests

    were done using three different kinds of specimens (120 x 300, 120 x 360, and 120 x 450 mm in

    cross section of column member). Experimental results showed that at maximum about 40%

    increase of maximum moment and stiffness, while same percentage of decrease of ductility. The

    decrease of ductility was caused by a simple mistake in preparing test specimen. Thus, it can be

    possible to expect that the new type of column-beam joint give excellent total performance by

    executing careful further development on joints details.

    1. Introduction

    In WCTE2006 [1] held at Portland, we presented performance of glulam portal frames of 4m and6m span, which were composed of specially designed column-beam as well as column-base joints.

    In our presentation, we emphasized that the glulam portal frame developed had an excellent

    performance especially on the ductility that kept increasing bending moment even if the portal

    frames were deformed over 1/10 radian. As previous column joint, however, was composed of

    pass-though bolts to connect special shaped steel gusset with column member as shown in Fig.1,

    it was a disadvantage point that embedment due to bolt nuts made initial stiffness weakened. In this

    research, therefore, in order to prevent this initial deformation due to embedment by bearing plate,

    LagscrewboltR, which was developed by the first author, was used instead of using pass-through-

    bolt, and some evaluation tests were performed by employing full-scale column-beam joint

    specimens. In this article, details of theoretical analysis as well as comparisons between

    experimental results and theoretical results are to be reported.

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    2. Mechanical Model for Column-Beam Joint

    2.1 Beam Side Model

    As the theoretical derivation of mechanical model on

    the beam side joint shown in Fig.1 was reported in

    details in the previous proceedings [1], only the finalexpressions for the rotational rigidity of the beam side

    joint are shown in this part. The rotational rigidity of

    the beam side joint is expressed in equations (1) and

    (2).

    ( )200

    390

    3

    312bez

    ebfef

    BJCB gkAkbkHb

    R

    +

    +

    =

    (1)

    +=

    f

    z

    f

    z

    f

    z

    b b

    A

    gb

    A

    b

    A

    2

    (2)

    where,

    ZA : Area of bearing plate of M12 bolt at centre of steel gusset plate (mm2)

    fb : Width of double sided flange (mm)

    : Distance from most outer compression side to the line of tension side bolt (mm)

    H: Longitudinal length of steel gusset having double sided flanges (mm)

    ( )2

    00

    /H

    Ek we = : Embedment constant of glulam parallel to the grain (N/mm

    3) (3)

    0wE : Modulus of elasticity of glulam parallel to the grain (kN/mm2)

    143

    090

    .

    kk ee = : Embedment constant of glulam perpendicular to the grain, which is assumed that the

    same relationship used in AIJ design standard [2] can by applied. (N/mm3) (4)

    2.2 Rotational Rigidity of Column Side Joint in Previous Type Assembly

    Figure 2 indicates a mechanical model on the

    previous type of beam-column joint in whichpass-through-bolts were used for connecting

    steel gusset plate with glulam column. When

    the pass-through-bolt is subjected to the tensile

    force T, the bearing plate is bent as shown in

    Fig.2. Resistance force T1acting at constant

    embedment stress region is expressed in

    equation (5).

    ( )zcTe bakT 2901 = (5)

    While, resistance force T2, which is defined asa resultant force of lineally distributed

    Glulam Column

    Glulam-Beam

    Fixed with Nuts

    M12 Bolt

    Flange

    Bearing

    Plate

    hb

    y

    Cg

    a

    H

    T

    g

    b

    bg

    x

    H/2

    Cw

    2/3H/2

    b3/2

    b

    M

    x

    2/3H/2Cw

    Fig.1 Beam side mechanical model for

    the previous joint.

    Fig.2 Mechanical model for column-beam joint.

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    embedment stress, is expressed in equation (6).

    2

    1 1

    2190z

    02

    1

    exz kbdybT == (6)

    Considering relationships of )(and11 == gTT , and equilibrium between tensile resultant

    force and compression force, following relationship is obtained.

    zc

    Sc

    ceScezcezc

    b)g(

    b

    kb)g(kb)g(kbaCTTT

    =+

    =+=+=

    22a

    2

    2

    1

    2

    12

    2

    c1

    2901909021

    (7)

    From geometrical relationship in Fig.2,

    cc ag += 1 (8)

    From equations (7) and (8), following equation for the neutral potion of column-side is obtained.

    ( ) ( ) ( ) 0323 22 =+++ gbgbagbbabb zzcczzccsz (9)

    where, zb is width of bearing plate of column side, and Sb is contact width of beam end to the side

    face of column. As the difference between zb and Sb is usually small, it will be reasonable to

    neglect the difference, hence the location of neutral potion of column-side is obtained as equation

    (10).

    +

    +=

    ga

    gag

    c

    cc

    23

    3 (10)

    From equilibrium of external momentMand moments due to tensile force Tas well as compression f

    orce C, relationship between moment and rotational angle is derived as equation (11).

    32(2a

    3

    23

    21c90

    ++=+=c

    czecc )g)(bkT)g(CM (11)

    Considering equation (7), the rotational rigidity for column-side joint of previous type joint is derive

    d as equation (12).

    =

    32

    1 290

    ccezCJCB gkbR

    (12)

    As the column-side joint and beam-side joint is connected in series with shearing approximately the

    same moment, apparent rotational rigidity for beam-column joint of previous type assembly is

    expressed as equation (13).

    CJCBBJCB

    CJCBBJCBBoltJCB

    RR

    RRR

    +

    = (13)

    2.3 Yield Moment of Column-Beam Joint in Previous Type Assembly

    It is assumed that the yielding of column-beam joint occurs when the embedment stress x reaches

    to the partial compression strength 90cf perpendicular to the grain of glulam column. The force

    embedment relationship is,

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    cec kf 9090 = (14)

    Relationship between embedment and rotational angle at yielding level is,

    ccc = (15)

    Relationship between rotational angle and moment at yielding level is,

    cBoltJCBy RM = (16)

    Hence, substituting equations (14) and (15) into equation (16), equation for predicting yield

    moment at column-beam joint is obtained as equation (17).

    ce

    BoltJCBcy

    k

    RfM

    90

    90 = (17)

    2.4 Rotational Rigidity of Column-Side Joint in New Type Assembly

    Figure 3 shows a mechanical model for new type column-beam joint in which LagscrewboltRis

    used instead of using pass-through-bolts for

    connecting steel gusset plate with glulam column.

    In this model, number of LSB for width direction

    was assumed to be m for making mechanical

    model has generalization. Relationship between

    load and elongation at tensile side of LSB is

    expressed in equation (18).

    TLSBmKT = 90 (18)

    Relationship between load and deformation at

    compression side of LSB is expressed in equation(19).

    CLSBL mKC = 90 (19)

    where,

    90LSBK : Slip modulus of LSB and it was assumed

    that for both tension and compression

    load, same value could be given by the following equations.

    ( )

    ( )9090909090909090

    90 cosh

    sinh

    wwss

    ssww

    LSB AElkAEk

    lkAEAERK

    +

    +=

    (kN/mm) (20)

    +=

    ssww AEAERk

    11

    9090

    9090 (21)

    90 : Shear stiffness of LSB defined as stiffness between shear stress and displacement measured on

    the specimen in which LSB inserted into thin plate. (N/mm3)

    90wE : Modulus of elasticity of glulam perpendicular to the grain (=Ew0/25). ( kN/mm2)

    90wA : Effective area defined as hatched part surrounded by 4.0R in width directiontimes nRin fibre

    direction as shown in Fig.4, and can be evaluated by equation (22) [3] (mm2)

    T

    Cw

    hb

    g

    T

    hc

    x

    Column

    M

    0

    3

    2x

    y

    bs

    g

    ac

    C

    CL ac

    m-LSB

    m-LSB

    m

    m

    Lag-Screw-Bolt=LSB

    Fig.3 Mechanical model for new type

    column-beam joint.

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    ( )( ) ( )

    =

    =

    c

    w

    h

    l.exp.n

    R.RnRA

    59436832

    5042

    90

    (22)

    where,

    R : Peak diameter of LSB (mm)

    l : Effective insert length of LSB (mm)

    ch : Height of column (mm)

    sE : Modulus of elasticity of steel. (kN/mm2)

    sA : Cross sectional area of LSB based on the bottom diameter (mm2)

    Relationship between elongation and rotational angle at tensile LSB is,

    ( ) = gT (23)

    Relationship between deformation and rotational angle at compression LSB is,

    ( )cC a= (24)

    Resultant compression force by embedment stress due to contact of end flange of steel gusset plate

    to side grain of glulam column is,

    2

    290

    0

    ==es

    xsw

    kbdybC (25)

    From equations (18) and (23),

    ( ) =

    gmKT LSB 90 (26)

    From equations (19) and (24),

    ( ) = cLSBL amKC 90 (27)

    Equilibrium of T, CLand Cwis,

    Lw CCT += (28)

    Substituting equations (25),(26), and (27) into equation (28), following equation for determining

    is obtained.

    022

    290

    90

    90

    902=

    +

    b

    es

    LSB

    es

    LSB hkb

    mK

    kb

    mK (29)

    Solving equation (29), is expressed as,

    +

    =

    90

    90

    90

    90

    90

    90 222

    es

    LSBb

    es

    LSB

    es

    LSB

    kb

    mKh

    kb

    mK

    kb

    mK (30)

    Equilibrium of external moment and those due to tensile force and compression force is

    Fig.4 Effective area Aw90for LSB inserted

    erpendicular to the grain.

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    ( ) ( ) ( ) ( ){ }

    ++=++=

    390

    2290

    3

    1

    3

    2escLSBLcw kbagmKCaCTgM (31)

    Therefore, the rotational rigidity for column-side joint is,

    ( ) ( ){ }3

    90

    22

    90 3

    1

    ++= escLSBLSBJc kbagmKR (32)

    Finally, apparent rotational rigidity for beam-column joint of new type assembly is expressed as

    equation (33).

    LSBJCBJCB

    LSBJCBJCBLSBJCB

    RR

    RRR

    +

    = (33)

    2.5 Yield Moment of Column-Beam Joint in New Type Assembly

    It is assumed that apparent yielding of column-beam joint occurs when the tensile force Ton LSB

    reaches to its maximum strength 90maxP perpendicular to the grain of glulam column. Hence,

    apparent yielding moment is expressed as,

    ( )

    =

    gmK

    RPM

    LSB

    LSBJCBmaxy

    90

    90 (34)

    where,

    ( )( )90909090

    9090909090

    cosh

    sinh

    wwss

    sswwvmax

    AElkAEk

    lkAEAERfP

    +

    +=

    (35)

    90vf : Shear strength perpendicular to the grain obtained from thin plate specimen with penetrating

    LSB[3]. (kN/mm2

    )

    3. Experiments

    Table 1 shows

    specification of test

    specimens used in this

    experiment. In each

    specification, three

    replications were

    prepared. For column andbeam members, glulam

    having a grade of

    JASE105-f300 (fb=30MPa,

    MOE=10.5 GPa) mixed species glulam, which is the same as those used in the previous

    experiments [1], were used. Figure 5 shows a test set-up of beam-column joint. This configuration

    represents the upper half and lateral half portion of portal frame subjected to a horizontal load. In

    this experiment, lengthL was 2500mm and heightHwas 1480mm, thus moment at beam column

    joint was estimated asM=HP=1.48P(kNm). While the rotational angle at beam-column joint was

    defined as ( ) 3434 h/## = . Loading protocol applied was1/300,1/200,1/120,1/60,

    1/30 rad. and finallyPmaxthen returns back to zero. In this experiment, only one cycle repeat wasadopted within each peak deformation.

    Specimen

    Code Name

    Common

    Width

    b (mm)

    Height of

    Column

    h c(mm)

    Height of

    Beam

    hb(mm)

    Joint Between Column-Steel

    Gusset

    B300-1,2,3 120 300 360 4-M12 Bolts Previous Type

    B360-1,2,3 120 360 420 4-M12 Bolts Previous Type

    B450-1,2,3 120 450 540 4-M12 Bolts Previous Type

    L300-1,2,3 120 300 360 LSB2-30New Type

    L360-1,2,3 120 360 420 LSB2-30New Type

    L450-1,2,3 120 450 540 LSB2-30New Type

    Table Specification of Test Specimens Used for Experiments

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    4. Results and Discussion

    Figures 6 to 8 show comparisons

    between observed envelope curve

    and predicted stiffness and yield

    moment calculated using equations

    derived in clause 2 in this paper.

    From these comparisons, it is clear

    that the equations for predicting

    initial stiffness as well as yielding

    moment of both previous and new

    type joint specimen had fairly good

    applicability on the real beam-

    column joints.

    Previous TypeB300)

    -40

    -30

    -20

    -10

    0

    10

    20

    30

    40

    -0.06 -0.04 -0.02 0.00 0.02 0.04 0.06 0.08 0.10

    Rotational Angle (rad.)

    MomentM(k

    Nm)

    B300-1

    B300-2

    B300-3

    Stiffness M-cal

    Yield My-cal

    New TypeL300)

    -40

    -30

    -20

    -10

    0

    10

    20

    30

    40

    -0.06 -0.04 -0.02 0.00 0.02 0.04 0.06 0.08 0.10

    Rotational Angle (rad.)

    MomentM(k

    Nm)

    L300-1

    L300-2

    L300-3

    Stiffness M-cal

    Yield My-cal

    Fig.6 Comparisons between observed values and predicted ones in case of B300 and L300.

    Previous TypeB360)

    -50

    -40

    -30

    -20

    -10

    0

    10

    20

    30

    40

    50

    -0.06 -0.04 -0.02 0.00 0.02 0.04 0.06 0.08 0.10

    Rotational Angle (rad.)

    MomentM(kNm)

    B360-1

    B360-2

    B360-3

    Stiffness M-cal

    Yield My-cal

    New TypeL360)

    -50

    -40

    -30

    -20

    -10

    0

    10

    20

    30

    40

    50

    -0.06 -0.04 -0.02 0.00 0.02 0.04 0.06 0.08 0.10

    Rotational Angle (rad.)

    MomentM(kNm)

    L360-1

    L360-2

    L360-3

    Stiffness M-cal

    Yield My-cal

    Fig.7 Comparisons between observed values and predicted ones in case of B360 and L360.

    H

    P

    #3

    #1

    500 kN Oil Jack

    300kN Load Cell

    #4

    L

    Pined Support#2

    h34

    Beam

    Column

    Fig.5 Test set-up for beam-column joint specimen.

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    Previous Type B450)

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80

    -0.06 -0.04 -0.02 0.00 0.02 0.04 0.06 0.08

    Rotational Angle (rad.)

    MomentM(k

    Nm)

    B450-1

    B450-2

    B450-3

    Stiffness M-cal

    Yield My-cal

    New TypeL450)

    -80

    -60

    -40

    -20

    0

    20

    40

    60

    80

    -0.06 -0.04 -0.02 0.00 0.02 0.04 0.06 0.08

    Rotational Angle (rad.)

    MomentM(kNm)

    L40-1

    L40-2

    L40-3

    Stiffness M-cal

    Yield My-cal

    Fig.8 Comparisons between observed values and predicted ones in case of B450 and L450.

    Photo 1 shows typical ultimate situations in different type of test specimens.

    Photo1 Left: Large deformation at bearing plate in previous type. Middle: Pull-out of LSB in new

    type (L300). Right: Tear off of high-tension bolt in new type (L450).

    5. Conclusions

    Experimental results showed that at maximum about 40% increase of maximum moment and

    stiffness, while same percentage of decrease of ductility due to simple mistake in preparing test

    specimen occurred. Equations derived in this research showed excellent applicability, hence,

    consequently column-beam joint proposed in this research was proved to express enough structuralperformance both in experimentally and theoretically.

    6. References

    [1] Komatsu K., Hosokawa K., Hattori S., Matsuoka H., Yanaga K. and Mori T.: Developmentof Ductile and High-Strength Semi-Rigid Portal Frame Composed of Mixed-Species Glulamsand H-shaped Steel Gusset Joints,Proceedings of the World Conference on Timber

    Engineering 2006, (CD-ROM only), Portland, Aug. 2006.

    [2] Architectural Institute of Japan (edited): Design of Joints, Standard for Structural Design ofTimber Structures, Maruzen, Tokyo, 2006, pp.200-320. (in Japanese)

    [3] Japan Lagscrewbolt Society (edited): Design and Construction Guideline on Glulam Joints byLagscrewbolt, Kyoto, 2007, p.13. (in Japanese)