CN201660965U - Beam-end enhanced-flange splice plate weaken improved rigid nodes of steel frame beam column - Google Patents

Beam-end enhanced-flange splice plate weaken improved rigid nodes of steel frame beam column Download PDF

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Publication number
CN201660965U
CN201660965U CN2009202466176U CN200920246617U CN201660965U CN 201660965 U CN201660965 U CN 201660965U CN 2009202466176 U CN2009202466176 U CN 2009202466176U CN 200920246617 U CN200920246617 U CN 200920246617U CN 201660965 U CN201660965 U CN 201660965U
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China
Prior art keywords
scab
steel frame
wing
post
edge
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Expired - Fee Related
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CN2009202466176U
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Chinese (zh)
Inventor
张艳霞
吴徽
王路遥
刘金瑶
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Beijing University of Civil Engineering and Architecture
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Beijing University of Civil Engineering and Architecture
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Abstract

The utility model discloses a beam-end enhanced-flange splice plate weaken improved rigid nodes of a steel frame beam column, which is formed by cantilever beams and columns. The rigid nodes are characterized in that the cantilever beams are fixed with the columns; cover plates which are simultaneously fixed with the columns and the cantilever beams are respectively arranged on upper flange and lower flange of the combined end of the cantilever beams and the columns; the cantilever beams are connected with beam web plates through web plate and splice plate bolts and are respectively connected with the upper flanges and the lower flanges of the beams through dual-layer splice plate bolts; and weakening parts are arranged in the middle of an flange outer layer splice plates. Therefore, the utility model ensures the outer movement of plastic hinges at the beam end, increases the plastic corners at the beam end, improves the earthquake-resistant performance of the nodes, is convenient for maintenance and reinforcement after the earthquake and simultaneously achieves the optimal economic effect.

Description

The modified steel frame beam column rigid joint that beam-ends reinforcement-edge of a wing scab weakens
Technical field
The utility model relates to the building steel framed structure, the modified steel frame beam column rigid joint that especially a kind of beam-ends reinforcement-edge of a wing scab weakens.
Background technology
Traditional steel frame beam column rigid joint is the edge of a wing of beam 3 and post 1 ' welding, and web directly passes through bolt 7 bolts with post scab 8 ', as Fig. 1 (a) with (b); Or for being with the beam-column connection of semi girder 2, the beam column junction of this node is that the edge of a wing of semi girder 2 and web and post 1 ' weld by factory, the other end of semi girder 2 and beam 3 are by web scab 8 " carry out the bolt weldering and mix and is connected; as Fig. 2 (a); or splice by bolt 7 full bolts fully, shown in Fig. 2 (b).
Though above-mentioned node has been widely used in the steel framed structure, node is the weak link of whole frame construction, in the destructive insident such as bursts such as earthquake disasters, has fatal defective.For example, California, USA earthquake in 1994 and nineteen ninety-five Japan's slope earthquake centre celestially, rupture failure has all taken place in many traditional beam-column connections, and wherein most fracture starts from the bottom flange weld seam of node beam-ends, the surrender and the flexing of the steel member of expection do not occur.Therefore, how improving the anti-seismic performance of node, is the crucial part that improves whole frame construction anti-seismic performance.But, adopt reinforced node can increase column cross-section size merely, beam section utilizes insufficient, and is less economical, and can influence the lateral rigidity of beam.Therefore, the design people proposes improved technical scheme at above-mentioned situation.
The utility model content
The utility model purpose is, the modified steel frame beam column rigid joint that provides a kind of beam-ends reinforcement-edge of a wing scab to weaken, to improve the mechanical property of traditional bean column node, anti-seismic performance particularly, design principles according to " strong column and weak beam, the weak rod member of strong node " in the seismic design, the node beam-ends is adopted rational reinforcement, improve the anti-seismic performance of node, and reach preferable economic effect simultaneously.
According to above-mentioned purpose, the modified steel frame beam column rigid joint that a kind of beam-ends reinforcement-edge of a wing scab weakens, it is characterized in that semi girder and post weld in factory, the bottom flange respectively is provided with a cover plate that is connected simultaneously with post and semi girder in the binding end place of semi girder and post; Semi girder is connected by web scab bolt with web, and semi girder then respectively is connected by double-deck edge of a wing scab bolt with the last bottom flange of beam, and outer scab middle part, the edge of a wing is provided with weakening portion.
Wherein, described weakening portion is the arc notch of symmetry, and is separately positioned on the both sides in the middle part of the outer scab in bottom flange.
Wherein, semi girder and post are that full welding is fixing.
Wherein, described post is box column or the I shape post with rectangle or square-section.
Wherein, be equipped with diaphragm in described box column or the I shape post.
Wherein, connect that each double-deck scab of bottom flange is connected and fixed with bolt on described semi girder and the described beam.
Wherein, the cover plate that is positioned at the semi girder top flange is a trapezium structure, is trapezoidal base one side it combines with post; The cover plate that is positioned at the semi girder bottom flange then is rectangular configuration.
Pass through said structure, the utility model adds cover plate to the semi girder end and strengthens, and last bottom flange scab carried out suitable reasonable weakening, by strengthening and weaken the corrective measure of combination, guarantee that plastic hinge moves outward, increase the plasticity corner of beam-ends, improved the anti-seismic performance of node, reach preferable economic effect simultaneously.
Secondly, the bottom flange respectively adds double-deck scab on splicing place beam, help the even transmission of power, the outer scab of wherein going up the bottom flange carries out circular arc type and weakens, thereby destruction is at first appeared on the scab of the edge of a wing, rather than appear on the web and the edge of a wing of beam, so both improved the node anti-seismic performance, the maintenance and reinforcement after being convenient to again shake.Should connect adopt factory's welding simultaneously, the building site weld seam has been avoided in high-strength bolt splicing in building site, has advantages such as the good and speed of application of weldquality is fast.
Below in conjunction with accompanying drawing a kind of specific embodiment of the present utility model is described, to disclose spiritual essence of the present utility model in more detail.Wherein, identical part is represented with identical Reference numeral.For the details of each several part in the exploded view clearly, the same structure in the different map sheets is not in strict accordance with the scale of reality.
Description of drawings
Fig. 1 is one of conventional steel frame beam column rigid joint form, and wherein (a) is plan view, (b) is the 1-1 sectional view of (a);
Fig. 2 is two of a conventional junction steel frame beam column rigid joint form, and wherein (a) is the bolt weldering splicing of beam, (b) is the full bolt splicing of beam;
Fig. 3 is the elevation of a preferred embodiment of the modified steel frame beam column rigid joint that weakens of beam-ends of the present utility model reinforcement-edge of a wing scab;
Fig. 4 is along the sectional drawing that is the 1-1 line intercepting among Fig. 3;
Fig. 5 is the sectional drawing along the intercepting of the 2-2 line among Fig. 3;
Fig. 6 is the sectional drawing along the intercepting of the 3-3 line among Fig. 4;
Fig. 7 is the 3 d effect graph of the preferred embodiment of the modified steel frame beam column rigid joint that weakens of the beam-ends of the present utility model reinforcement-edge of a wing scab shown in Fig. 3-6.
The specific embodiment
With reference to Fig. 3-7, the modified steel frame beam column rigid joint that a kind of beam-ends of the utility model reinforcement-edge of a wing scab weakens, be connected with post 1 by semi girder 2, be example with box column in the present embodiment with rectangle or square-section, semi girder 2 is fixing with post 1 full welding, and post 1 middle part has level and strengthens the lateral rigidity of diaphragm 10 with reinforcing prop 1; Semi girder 2 has with post 1 with post 1 binding end place and fixes, and top flange cover plate 60 and the bottom flange cover plate 61 that is fixed together with the last bottom flange applying of semi girder 2 simultaneously, top flange cover plate 60 is a trapezium structure, its one side that combines with post 1 is trapezoidal base, be positioned at semi girder bottom flange cover plate 61 and then be rectangular configuration, its width and semi girder bottom flange width adapt; Be positioned at web 30 places of beam 3 in order to the web scab 8 of joggle beam 3 webs, and beam 3 is connected with semi girder 2 by bolt 7, the top flange 31 of beam 3 respectively is connected with semi girder 2 by double-deck edge of a wing scab with 32 of bottom flanges, it comprises top flange internal layer scab 40, the outer scab 41 in top flange, and the outer scab 43 of bottom flange internal layer scab 42, bottom flange, internal layer scab in the described double-deck scab, outer scab is longer than at its two ends, and is connected with semi girder 2 by bolt 7 together; Outer scab middle part, each edge of a wing has a weakening portion 5, and described weakening portion 5 be the arc notch of symmetry, and it is separately positioned on the both sides at outer scab 41 in top flange and skin scab 43 middle parts, bottom flange.

Claims (10)

1. modified steel frame beam column rigid joint that beam-ends reinforcement-edge of a wing scab weakens, be connected with post (1) by semi girder (2), it is characterized in that, semi girder (2) and post (1) fix, in the binding end place of semi girder (2) and post (1) bottom flange respectively be provided with one with post and semi girder (2) the top flange cover plate and the bottom flange cover plate (60,61) of secure bond simultaneously; Semi girder (2) is connected by web scab (8) bolt (7) with beam (3) web, and semi girder (2) then respectively is connected and fixed by double-deck scab with the last bottom flange of beam (3), and outer scab middle part, the edge of a wing is provided with weakening portion (5).
2. the modified steel frame beam column rigid joint that beam-ends as claimed in claim 1 reinforcement-edge of a wing scab weakens, it is characterized in that, described weakening portion (5) is the arc notch of symmetry, and is separately positioned on the both sides at outer scab in top flange and the outer scab in bottom flange (41,43) middle part.
3. the modified steel frame beam column rigid joint that beam-ends as claimed in claim 1 or 2 reinforcement-edge of a wing scab weakens is characterized in that, the internal layer scab in the described double-deck scab, and outer scab is longer than at its two ends.
4. the modified steel frame beam column rigid joint that weakens of beam-ends reinforcement-edge of a wing scab as claimed in claim 1 or 2 is characterized in that semi girder (2) be that full welding is fixed with post (1).
5. the modified steel frame beam column rigid joint that beam-ends as claimed in claim 3 reinforcement-edge of a wing scab weakens is characterized in that, semi girder (2) is that full welding is fixing with post (1).
6. the modified steel frame beam column rigid joint that weakens of beam-ends reinforcement-edge of a wing scab as claimed in claim 1 or 2 is characterized in that described post (1) is for having the box column or the I shape post of square-section.
7. the modified steel frame beam column rigid joint that beam-ends as claimed in claim 4 reinforcement-edge of a wing scab weakens is characterized in that, described post (1) is for having the box column of square-section.
8. the modified steel frame beam column rigid joint that beam-ends as claimed in claim 4 reinforcement-edge of a wing scab weakens is characterized in that, is equipped with diaphragm (10) in described box column (1) or the I shape post (1).
9. the modified steel frame beam column rigid joint that weakens as each described beam-ends reinforcement-edge of a wing scab in the claim 1,2,5,7,8, it is characterized in that each the double-deck scab that connects the last bottom flange of described semi girder (2) and described beam (3) is connected and fixed with bolt (7).
10. the modified steel frame beam column rigid joint that weakens as the end reinforcement-edge of a wing scab of each described beam in the claim 1,2,5,7,8, it is characterized in that, the top flange cover plate (60) that is positioned at semi girder (2) top flange is a trapezium structure, its with post (1) one side what combine is trapezoidal base; The bottom flange cover plate (61) that is positioned at semi girder (2) bottom flange then is rectangular configuration.
CN2009202466176U 2009-10-16 2009-10-16 Beam-end enhanced-flange splice plate weaken improved rigid nodes of steel frame beam column Expired - Fee Related CN201660965U (en)

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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102817413A (en) * 2012-07-05 2012-12-12 北京工业大学 Steel frame precast prestressed beam column joint with post-earthquake recovering function
CN102888929A (en) * 2011-07-18 2013-01-23 湖南邱则有专利战略策划有限公司 Shearing force prefabricated component for assembled-type hollow grid plate floor system structure
CN102888933A (en) * 2011-07-18 2013-01-23 湖南邱则有专利战略策划有限公司 Shearing prefabricated component for assembling type hollow gridding plate floor structure
CN102888930A (en) * 2011-07-18 2013-01-23 湖南邱则有专利战略策划有限公司 Assembled type hollow grid plate floor system
RU2478760C2 (en) * 2011-06-09 2013-04-10 Всеволод Эдуардович Глуховцев Metal frame assembly for low-rise building
CN104386263A (en) * 2014-11-12 2015-03-04 沈阳航空航天大学 Splicing and repairing method of Z-shaped stringer on airplane
CN105332422A (en) * 2015-11-03 2016-02-17 北京工业大学 Vertical outer rib beam-column joint connector applicable to prefabricated steel structural systems
CN105625585A (en) * 2016-02-03 2016-06-01 山东大学 Buckling constraint steel structure beam-column connection and steel structure building
CN105839776A (en) * 2016-05-19 2016-08-10 山东大学 Buckling constraint type steel-beam-and-column end-plate connection joint and steel structure building
CN109972733A (en) * 2019-04-08 2019-07-05 扬州大学 A kind of novel expansion wing T shape energy consumption connection steel structure frame
CN110273482A (en) * 2019-06-28 2019-09-24 西安建筑科技大学 A kind of box column connecting joint structure and assembly method
CN110382797A (en) * 2017-02-17 2019-10-25 Sdr技术股份有限公司 The manufacturing method and column beam connected structure of column beam connected structure
CN110528705A (en) * 2019-09-10 2019-12-03 兰州理工大学 A kind of replaceable plasticity hinged joint in honeycomb fashion girder steel end
CN110952666A (en) * 2019-12-27 2020-04-03 西安理工大学 Assembled high-ductility high-strength steel beam column rigid connection node
CN113089825A (en) * 2021-04-19 2021-07-09 重庆恒昇大业建筑科技集团有限公司 Beam-column mixed frame node, and preparation method and construction method of precast concrete beam
US20240140610A1 (en) * 2022-11-02 2024-05-02 The Boeing Company Systems and methods for coupling a strut to a wing of an aircraft

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2478760C2 (en) * 2011-06-09 2013-04-10 Всеволод Эдуардович Глуховцев Metal frame assembly for low-rise building
CN102888929A (en) * 2011-07-18 2013-01-23 湖南邱则有专利战略策划有限公司 Shearing force prefabricated component for assembled-type hollow grid plate floor system structure
CN102888933A (en) * 2011-07-18 2013-01-23 湖南邱则有专利战略策划有限公司 Shearing prefabricated component for assembling type hollow gridding plate floor structure
CN102888930A (en) * 2011-07-18 2013-01-23 湖南邱则有专利战略策划有限公司 Assembled type hollow grid plate floor system
CN102817413A (en) * 2012-07-05 2012-12-12 北京工业大学 Steel frame precast prestressed beam column joint with post-earthquake recovering function
CN102817413B (en) * 2012-07-05 2015-01-14 北京工业大学 Steel frame precast prestressed beam column joint with post-earthquake recovering function and process thereof
CN104386263A (en) * 2014-11-12 2015-03-04 沈阳航空航天大学 Splicing and repairing method of Z-shaped stringer on airplane
CN105332422A (en) * 2015-11-03 2016-02-17 北京工业大学 Vertical outer rib beam-column joint connector applicable to prefabricated steel structural systems
CN105625585B (en) * 2016-02-03 2019-03-29 山东大学 Buckling-restrained steel structure girder column connected node and steel building
CN105625585A (en) * 2016-02-03 2016-06-01 山东大学 Buckling constraint steel structure beam-column connection and steel structure building
CN105839776A (en) * 2016-05-19 2016-08-10 山东大学 Buckling constraint type steel-beam-and-column end-plate connection joint and steel structure building
CN105839776B (en) * 2016-05-19 2019-03-29 山东大学 Buckling-restrained formula beam-column end plate connecting node and steel building
CN110382797A (en) * 2017-02-17 2019-10-25 Sdr技术股份有限公司 The manufacturing method and column beam connected structure of column beam connected structure
CN109972733A (en) * 2019-04-08 2019-07-05 扬州大学 A kind of novel expansion wing T shape energy consumption connection steel structure frame
CN109972733B (en) * 2019-04-08 2021-06-01 扬州大学 Expand wing T shape power consumption and connect steel construction frame
CN110273482A (en) * 2019-06-28 2019-09-24 西安建筑科技大学 A kind of box column connecting joint structure and assembly method
CN110528705A (en) * 2019-09-10 2019-12-03 兰州理工大学 A kind of replaceable plasticity hinged joint in honeycomb fashion girder steel end
CN110952666A (en) * 2019-12-27 2020-04-03 西安理工大学 Assembled high-ductility high-strength steel beam column rigid connection node
CN113089825A (en) * 2021-04-19 2021-07-09 重庆恒昇大业建筑科技集团有限公司 Beam-column mixed frame node, and preparation method and construction method of precast concrete beam
US20240140610A1 (en) * 2022-11-02 2024-05-02 The Boeing Company Systems and methods for coupling a strut to a wing of an aircraft

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20101201

Termination date: 20141016

EXPY Termination of patent right or utility model