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青岛理工大学毕业设计(论文)



外文翻译及原文



from



journal of Constructional Steel Research.V


olume 59,Number 1,January 2003


Cyclic behavior of steel moment frame


connections under varying axial load and lateral displacements


Abstract


: This paper discusses the cyclic behavior of four steel moment connections


tested


under


variable


axial


load


and


lateral


displacements.


The


beam


specim-


ens


consisted of a reduced beam section, wing plates and longitudinal stiffeners. The test


specimens


were


subjected


to


varying


axial


forces


and


lateral


displace-


ments


to


simulate the effects on beams in a Coupled-Girder Moment- Resisting Framing system


under


lateral


loading.


The


test


results


showed


that


the


specim-


ens


responded


in


a


ductile manner since the plastic rotations exceeded 0.03 rad without significant drop


in


the


lateral


capacity.


The


presence


of


the


longitudin-


al


stiffener


assisted


in


transferring the axial forces and delayed the formation of web local buckling.


1. Introduction








Aimed at evaluating the structural performance of reduced-beam section(RBS)


connections


under


alternated


axial


loading


and


lateral


displacement,


four


full-scale


specimens


were


tested.


These


tests


were


intended


to


assess


the


performance


of


the


moment connection design for the Moscone Center Exp- ansion


under


the


Design


Basis Earthquake (DBE) and the Maximum Considered Earthquake (MCE). Previous


research


conducted


on


RBS


moment


connections


[1,2]


showed


that


connections


with


RBS profiles can achieve rotations in excess of 0.03 rad. However, doubts have


been


cast


on


the


quality


of


the


seismic


performance


of


these


connections


under


combined


axial and lateral loading.


The


Moscone


Center


Expansion


is


a


three-story,


71,814


m2


(773,000


ft2)


structure


with steel moment frames as its primary lateral


force- resisting


system.


A


three


dimensional


perspective illustration is


shown in


Fig. 1. The


overall


height


of


the


building,


at


the


highest


point of the exhibition roof, is approxima- tely 35.36 m (116ft) above ground level.


The


ceiling


height


at


the


exhibition


hall


is


8.23


m


(27


ft)


,


and


the


typical


floor-to-floor height in the building is 11.43 m (37.5 ft). The building was designed as


type I according to the requi- rements of the 1997 Uniform Building Code.







The


framing


system


consists


of


four


moment


frames


in


the


East



West


direct-














































1





青岛理工大学毕业设计(论文)



ion,


one


on


either


side


of


the


stair


towers,


and


four


frames


in


the


North



South


direction, one on either side of the stair and elevator cores in the east end and two at


the


west


end


of


the


structure


[4].


Because


of


the


story


height,


the


con-


cept


of


the


Coupled- Girder Moment-Resisting Framing System (CGMRFS) was utilized.







By


coupling


the


girders,


the


lateral


load-resisting


behavior


of


the


moment


framing


system


changes


to


one


where


structural


overturning


moments


are


resisted


partially by an axial compression



tension couple across the girder system, rather than


only by the individual flexural action of the girders. As a result, a stiffer lateral load


resisting system is achieved. The vertical element that connects the girders is referred


to as a coupling link. Coupling links are analogous to and serve the same structural


role as link beams in eccentrically braced frames. Coupling links are generally quite


short, having a large shear- to-moment ratio.


Under earthquake-type loading, the CGMRFS subjects its girders to wariab- ble axial


forces in addition to their end moments.


The axial forces in


the


Fig. 1. Moscone Center Expansion Project in San Francisco, CA


girders result from the accumulated shear in the link.


2. Analytical model of CGMRF


Nonlinear


static


pushover


analysis


was


conducted on a typical one-bay model of the


CGMRF.


Fig.


2


shows


the


dimensions


and


the


various


sections


of


the


model.


The


link


flange plates were 28.5 mm


??


254 mm (1 1/8


??


10 in) and the web plate was 9.5 mm


??


476


mm


(3


/8


in


??


18


3/4


in).


The


SAP


2000


computer


program


was


utilized


in


the


pushover


analysis


[5].


The


frame


was


characterized


as


fully


restrained(FR).


FR


moment


frames


are


those


frames


for


1170which


no


more


than


5%


of


the


lateral


deflections


arise


from


connection


deformation


[6].


The


5%


value


refers


only


to


deflection due to beam



column deformation and not to frame deflections that result


from column panel zone deformation [6, 9].













































in


















































2





青岛理工大学毕业设计(论文)



The analysis was performed using an


expected value


of the yield stress and ultimate strength. These values


were equal to 372 MPa (54 ksi) and 518 MPa (75 ksi),


respectively.


The


plastic


hinges’


load–


deformation


behavior was


approximated by the


generalized curve


suggested


by


NEHRP


Guidelines


for


the


Seismic


Rehabilitation of Buildings [6] as shown . 3.



y


was calcu-


lated based on Eqs. (5.1) and (5.2) from


[6], as follows:



P



M


hinge


load



deformation


model


points


C,


D


and


E


are


based


on


Table


5.4


from [6] for



y was taken as 0.01 rad per Note 3 in [6], Table 5.8. Shear hinge load-


load



deformation model points C, D and E are based on Table 5.8 [6], Link Beam,


Item a. A strain hardening slope between points B and C of 3% of the elastic slope


was assumed for both models.








The


following


relationship


was


used


to


account


for


moment



axial


load


interaction [6]:


where


MCE


is


the


expected


moment


strength,


ZRBS


is


the


RBS


plastic


section


modulus


(in3),


is


the


expected


yield


strength


of


the


material


(ksi),


P


is


the


axial


force


in


the


girder


(kips)


and


is


the


expected


axial


yield


force


of


the


RBS,


equal


to


(kips). The ultimate flexural capacities of the beam and the link of the model are


shown in Table 1.






Fig. 4 shows qualitatively the distribution of the bending moment, shear force,


and


axial


force


in


the


CGMRF


under


lateral


load.


The


shear


and


axial


force


in


the


beams are less significant to the response of the beams as compared with the bending


moment, although they must be considered in design. The qualita- tive distribution of


internal


forces


illustrated


in


Fig.


5


is


fundamentally


the


same


for


both


elastic


and


inelastic ranges of behavior. The specific values of the internal forces will change as


elements of the frame yield and internal for-


ces are redistributed. The basic patterns


illustrated in Fig. 5, however, remain the same.


Inelastic static pushover analysis was carried out by applying monotonically


increasing lateral displacements, at the top of both columns, as shown in Fig. 6. After


the four RBS have yielded simultaneously, a uniform yielding in the web and at the


ends of the flanges of the vertical link will form. This is the yield mechanism for the


frame , with plastic hinges also forming at the base of the columns if they


are fixed.


The base shear versus drift angle of the model is shown in Fig. 7 . The sequence of














































3





青岛理工大学毕业设计(论文)



inelastic activity in


the frame is


shown on the figure. An elastic component, a long


transition (consequence of the beam plastic hinges being formed simultaneously) and


a narrow yield plateau characterize the pushover curve.



The


plastic


rotation


capacity,


qp,


is


defined


as


the


total


plastic


rotation


beyond


which


the


connection


strength


starts


to


degrade


below


80%


[7].


This


definition


is


different from that outlined in Section 9 (Appendix S) of the AISC Seismic Provisions


[8, 10]. Using Eq. (2) derived by Uang and Fan [7], an estimate of the RBS plastic


rotation capacity was found to be 0.037 rad:



Fyf


was


substituted


for


Ry?Fy


[8],


where


Ry


is


used


to


account


for


the


differ


-


ence


between the nominal and the expected yield strengths (Grade 50 steel, Fy=345


MPa and Ry =1.1 are used).


mental program



The experimental set-up for studying the behavior of a connection was based on Fig.


6(a).


Using


the


plastic


displacement


dp,


plastic


rotation


gp,


and


plastic


story


drift


angle qp shown in the figure, from geometry, it follows that:And: in which d and g


include the elastic components. Approximations as above are used


for large inelastic


beam


deformations.


The


diagram


in


Fig.


6(a)


suggest


that


a


sub


assemblage


with


displacements controlled in the manner shown in Fig. 6(b) can


represent the inelastic


behavior of a typical beam in a CGMRF.





The


test


set-up


shown


in


Fig.


8


was


constructed to develop the mechanism shown


in


Fig.


6(a)


and


(b).


The


axial


actuators


were


attached to three


2438 mm ×


1219 mm ×


1219


mm (8 ft ×


4 ft ×


4 ft) RC blocks. These blocks


were


tensioned to the laboratory floor by means


of


twenty-four


32


mm


diameter


dywidag


rods.


This arrangement permitted replacement of the specimen after each test.














































4





青岛理工大学毕业设计(论文)







Therefore, the force applied by the axial actuator, P, can be resolved into two or


thogonal


components,


Paxial


and


Plateral.


Since


the


inclination


angle


of


the


axial


actuator


does


not


exceed


3.0


?


,


therefore


Paxial


is


approximately


equal


to


P


[4].


However, the lateral component, Plateral, causes an additional moment at the beam-to


column


joint.


If


the


axial


actuators


compress


the


specimen,


then


the


lateral


components will be adding to the lateral actuator forces, while if the axial actuators


pull the specimen, the Plateral will be an opposing force to the lateral actuators. When


the axial actuators undergo



axial actuators undergo a lateral displacement _, they cause an additional moment at


the beam-to-column joint (P-



effect). Therefore, the moment at the beam-to column


joint is equal to:



where


H


is


the


lateral


forces,


L


is


the


arm,


P


is


the


axial


force


and


_


is


the


lateral


displacement.


Four full- scale experiments of beam column connections were conducted.


The member sizes and the results of tensile coupon tests are listed in Table 2


All of the columns and beams were of A572 Grade 50 steel (Fy


344.5 MPa). The


actual measured beam flange yield stress value was equal to 372 MPa (54 ksi), while


the


ultimate strength ranged from 502 MPa (72.8 ksi) to 543 MPa (78.7 ksi).


Table


3


shows


the


values


of


the


plastic


moment


for


each


specimen


(based


on


measured tensile coupon data) at the full cross-section and at the reduced section


at


mid-length of the RBS cutout.


The specimens were designated as


specimen 1 through specimen 4. Test specimens


details are shown in Fig. 9 through Fig. 12. The following features were utilized in the


design of the beam



column connection:


The use of RBS in beam flanges. A circular cutout was provided, as illustr- ated in


Figs. 11 and 12. For all specimens, 30% of the beam flange width was removed.


The


cuts


were


made


carefully,


and


then


ground


smooth


in


a


direct-


tion


parallel


to


the


beam flange to minimize notches.



Use of a fully welded web connection. The connection between the beam web and the


column flange was made with a complete joint penetration groove weld


(CJP). All














































5





青岛理工大学毕业设计(论文)



CJP welds were performed according to AWS D1.1 Structural Welding Code


Use of two side plates welded with CJP to exterior sides of top and bottom beam flan-


ges, from


the face of the column flange to


the beginning of the RBS, as


shown


in


Figs. 11 and 12. The end of the side plate was smoothed to meet the beginning of the


RBS. The side plates were welded with CJP with the column flanges. The


side plate


was


added


to


increase


the


flexural


capacity


at


the


joint


location,


while


the


smooth


transition was to reduce the stress raisers, which may initiate fracture.




Two


longitudinal


stiffeners,


95


mm


×



35


mm


(3


3/4


in


×



1


3/8


in),


were


welded


with


12.7


mm


(1/2 in) fillet weld at the middle height of the web


as


shown


in


Figs.


9


and


10.


The


stiffeners


were


welded with CJP to column flanges.


Removal


of


weld


tabs


at


both


the


top


and


bottom


beam


flange


groove


welds.


The


weld


tabs


were


removed


to


eliminate


any


potential


notches


introduced


by


the


tabs


or


by


weld


discontinuities


in the groove weld run out regions.


Use


of


continuity


plates


with


a


thickness


approximately


equal


to


the


beam


flange


thickness. One-inch thick continuity plates were used for all specimens.


While


the


RBS


is


the


most


distinguishing


feature


of


these


test


specimens,


the


longitudinal stiffener played an important role in delaying the formation of web local


buckling and developing reliable connection performance4. Loading history




Specimens were tested by applying cycles of alternated load with tip displacement


increments of _y as shown in Table 4. The tip displacement of the beam was imposed


by


servo- controlled


actuators


3


and


4.


When


the


axial


force


was


to


be


applied,


actuators 1 and 2 were activated such that its force simulates the shear force in


the


link to be transferred to the beam. The variable axial force was increased up to 2800


kN (630 kip)


at


?


0.5_y.


After that, this


lo-


ad was maintained


constant


through the


maximum lateral displacement.



maximum


lateral


displacement.


As


the


specimen


was


pushed


back


the


axial


force


remained


constant


until


0.5


y


and


then


started


to


decrease


to


zero


as


the


specimen


passed through the neutral position [4]. According to the upper bound for


beam


axial


force


as


discussed


in


Section


2


of


this


paper,


it


was


concluded


that


P














































6




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