CN207513223U - A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint - Google Patents

A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint Download PDF

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Publication number
CN207513223U
CN207513223U CN201721582540.0U CN201721582540U CN207513223U CN 207513223 U CN207513223 U CN 207513223U CN 201721582540 U CN201721582540 U CN 201721582540U CN 207513223 U CN207513223 U CN 207513223U
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CN
China
Prior art keywords
frame
longitudinal direction
column
cfrp
self
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Expired - Fee Related
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CN201721582540.0U
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Chinese (zh)
Inventor
李镇川
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Individual
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Individual
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Priority to CN201721582540.0U priority Critical patent/CN207513223U/en
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Publication of CN207513223U publication Critical patent/CN207513223U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of self-locking carbon cloth indirect strengthening concrete frame interior joints, include frame column and frame beam plate, frame column pastes one layer of column longitudinal direction L-type CFRP band on along the longitudinal direction, column longitudinal direction L-type CFRP bands are anchored using the CFRP cloth hoop of closing, on frame beam plate one layer of beam slab longitudinal direction L-type CFRP band is pasted in longitudinal direction, beam slab longitudinal direction L-type CFRP bands are self-locking in by U-shaped cloth hoop on the parallel gate bar at beam slab inner corner trim, parallel gate bar is fixed on by hollow movable joint screw rod below the edge of a wing of frame beam plate, hollow movable joint screw rod, which passes through the frame beam plate edge of a wing and passes through the nut of upper end, is fixed on frame beam plate top surface;The reinforcing joint of the utility model, the shear resistance of joint cores can be effectively improved, beam column end is avoided to reinforce the failure of stripping in advance of fiber, while the ductility factor and energy dissipation capacity of joint cores can be improved, so as to further improve the anti-seismic performance of joint cores.

Description

A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint
Technical field
The utility model is related to a kind of frame structure, more particularly to a kind of self-locking carbon cloth indirect strengthening concrete frame Interior joint.
Background technology
Node is a very important position in concrete frame structure, and force-bearing situation is complicated more than beam column component, Under geological process, the horizontal shear born is generally 4-6 times of column shearing, is fallen once destroying and would potentially result in total It collapses destruction, it is therefore proposed that reliable and effective node seismic strengthening technology and corresponding design method have important engineering reality Meaning.Existing reinforcing joint, which exists, does not form joint cores effective anchoring, and there are carbon fiber reinforced plastics It is too early that material (CFRP) cloth hoop coheres glass, coheres glassbreak so as to generate, reduces the anti-seismic performance of node.
Utility model content
The purpose of the utility model is to overcome the defects of the prior art, provide a kind of self-locking carbon cloth indirect strengthening to mix Solidifying soil Frames Joints, the technical solution of the self-locking carbon cloth indirect strengthening concrete frame interior joint are realized in 's:
A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint, including frame column and frame beam plate, the frame Plate of setting a roof beam in place is the T-shaped composite structure being made of Vierendeel girder and plate, and the frame column pastes one layer of column longitudinal direction L on along the longitudinal direction Type CFRP bands, and the column longitudinal direction L-type CFRP bands are anchored using the CFRP cloth hoop of closing, on the frame beam plate One layer of beam slab longitudinal direction L-type CFRP band is pasted in longitudinal direction, the beam slab longitudinal direction L-type CFRP bands pass through U-shaped cloth hoop self-locking On parallel gate bar at beam slab inner corner trim, the parallel gate bar is fixed on by hollow movable joint screw rod under the edge of a wing of frame beam plate Side, the hollow movable joint screw rod, which passes through the frame beam plate edge of a wing and passes through the nut of upper end, is fixed on frame beam plate top surface, the sky Beam slab longitudinal direction L-type CFRP bands are fixed on frame beam plate top surface by section screw rod of being indecisive and changeable by being arranged on the lateral steel plate strip of back.
Further, the U-shaped cloth hoop is CFRP item hoops.
Further, structure glue is coated between longitudinal direction CFRP bands and frame column and the frame beam plate.
Further, the column longitudinal direction L-type CFRP bands of the frame column paste in ranging from column top/bottom latitude 350~ 400mm ranges, the beam slab longitudinal direction L-type CFRP bands of the frame beam plate paste ranging from 600~700mm of beam-ends both sides.
Further, the parallel gate bar is formed by 2 round steel spot welding.
The reinforcing joint of the utility model, on Vierendeel girder direction using longitudinal L-type CFRP bands and CFRP cloth hoop into The closing of styletable is anchored;To beam-ends, terminate U-shaped cloth hoop being self-locking in putting down at beam slab inner corner trim around self-locking is tied using CFRP cloth end On row grid bar, then by wearing the wing hollow movable joint screw rod the lateral steel plate strip of parallel gate bar and top surface of the beam is fastenedly connected, forms envelope The CFRP cloth hoops closed overcome the defects of U-shaped CFRP cloth hoop that beam-ends is just being put is difficult to pass through the plate edge of a wing, and to beam-ends L-type longitudinal direction CFRP bands form reliable anchoring constraint, effectively prevent reinforcing the premature bonding stripping failure of fiber.
The reinforcing joint of the utility model can effectively improve the shear resistance of joint cores, and beam column end is avoided to reinforce The failure of stripping in advance of fiber, while the ductility factor and energy dissipation capacity of joint cores can be improved, so as to further improve The anti-seismic performance of joint cores.
Description of the drawings
Fig. 1 is the utility model overall structure diagram;
Fig. 2 reinforces schematic diagram for the utility model node beam-ends self-locking CFRP;
Fig. 3 is the utility model CFRP bands in parallel gate bar self-locking full-page proof schematic diagram.
Reference numeral:1- frame columns, 2- frame beam plates, 3-CFRP cloth hoops, 4- columns longitudinal direction L-type CFRP bands, 5- beam slabs are indulged To L-type CFRP bands, 6-U type cloth hoops, the hollow movable joint screw rods of 7-, 8- parallel gate bars, 9- transverse direction steel plate strips, 10- nuts.
Specific embodiment
The utility model is described in further detail in the following with reference to the drawings and specific embodiments.
As shown in Figures 1 to 3, a kind of self-locking carbon cloth indirect strengthening concrete frame interior joint, including frame column 1 and frame It sets a roof beam in place plate 2, the frame beam plate 2 is the T-shaped composite structure being made of Vierendeel girder and plate, and the frame column 1 is along the longitudinal direction On paste one layer of column longitudinal direction L-type CFRP band 4, and using closing CFRP cloth hoop 3 to the column longitudinal direction L-type CFRP bands 4 into Row anchors, and one layer of beam slab longitudinal direction L-type CFRP band 5, beam slab longitudinal direction L-type are pasted in longitudinal direction on the frame beam plate 2 CFRP bands 5 are self-locking in by U-shaped cloth hoop 6 on the parallel gate bar 8 at beam slab inner corner trim, and the parallel gate bar 8 passes through hollow movable joint Screw rod 7 is fixed below the edge of a wing of frame beam plate 2, and the hollow movable joint screw rod 7 passes through 2 edge of a wing of frame beam plate and passes through upper end Nut 10 is fixed on 2 top surface of frame beam plate, and the hollow movable joint screw rod 7 is by being arranged on the lateral steel plate strip 9 of back by beam slab Longitudinal L-type CFRP bands 5 are fixed on 2 top surface of frame beam plate.
When it is implemented, the U-shaped cloth hoop 6 is CFRP item hoops.
When it is implemented, the column longitudinal direction L-type CFRP bands 4 and beam slab longitudinal direction L-type CFRP bands 5 and frame column 1 and frame It sets a roof beam in place and structure glue is coated between plate 2.
When it is implemented, the column longitudinal direction L-type CFRP bands 4 of the frame column 1 paste 350 in ranging from column top/bottom latitude ~400mm ranges, the beam slab longitudinal direction L-type CFRP bands 5 of the frame beam plate 2 paste ranging from 600~700mm of beam-ends both sides.
When it is implemented, the parallel gate bar 8 is formed by 2 round steel spot welding.
The technology contents and technical characteristic of the utility model have revealed that as above those skilled in the art still may base The replacement and modification without departing substantially from the utility model in essence are made in the teaching of the utility model, therefore, the utility model protection Range is not limited to the revealed content of embodiment, also including various replacements and modification without departing substantially from the utility model in essence.

Claims (5)

1. a kind of self-locking carbon cloth indirect strengthening concrete frame interior joint, it is characterised in that:Including frame column and Vierendeel girder Plate, the frame beam plate are the T-shaped composite structure being made of Vierendeel girder and plate, and the frame column pastes one on along the longitudinal direction Layer column longitudinal direction L-type CFRP bands, and the column longitudinal direction L-type CFRP bands are anchored using the CFRP cloth hoop of closing, it is described One layer of beam slab longitudinal direction L-type CFRP band is pasted in longitudinal direction on frame beam plate, the beam slab longitudinal direction L-type CFRP bands pass through U Type cloth hoop is self-locking on the parallel gate bar at beam slab inner corner trim, and the parallel gate bar is fixed on frame beam plate by hollow movable joint screw rod The edge of a wing below, the hollow movable joint screw rod, which passes through the frame beam plate edge of a wing and passes through the nut of upper end, is fixed on frame beam plate top Beam slab longitudinal direction L-type CFRP bands are fixed on frame by face, the hollow movable joint screw rod by being arranged on the lateral steel plate strip of back Beam slab top surface.
2. self-locking carbon cloth indirect strengthening concrete frame interior joint according to claim 1, it is characterised in that:It is described U-shaped cloth hoop is CFRP item hoops.
3. self-locking carbon cloth indirect strengthening concrete frame interior joint according to claim 1, it is characterised in that:It is described Structure glue is coated between longitudinal CFRP bands and frame column and frame beam plate.
4. self-locking carbon cloth indirect strengthening concrete frame interior joint according to claim 1, it is characterised in that:It is described The column longitudinal direction L-type CFRP bands of frame column paste 350~400mm ranges in ranging from column top/bottom latitude, the frame beam plate Beam slab longitudinal direction L-type CFRP bands paste ranging from 600~700mm of beam-ends both sides.
5. self-locking carbon cloth indirect strengthening concrete frame interior joint according to claim 1, it is characterised in that:It is described Parallel gate bar is formed by 2 round steel spot welding.
CN201721582540.0U 2017-11-23 2017-11-23 A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint Expired - Fee Related CN207513223U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721582540.0U CN207513223U (en) 2017-11-23 2017-11-23 A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721582540.0U CN207513223U (en) 2017-11-23 2017-11-23 A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint

Publications (1)

Publication Number Publication Date
CN207513223U true CN207513223U (en) 2018-06-19

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Application Number Title Priority Date Filing Date
CN201721582540.0U Expired - Fee Related CN207513223U (en) 2017-11-23 2017-11-23 A kind of self-locking carbon cloth indirect strengthening concrete frame interior joint

Country Status (1)

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CN (1) CN207513223U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108724502A (en) * 2018-06-20 2018-11-02 五冶集团上海有限公司 A kind of the plane bracing means and stone material reinforcement means of stone material
CN114876059A (en) * 2022-05-19 2022-08-09 上海师范大学 Multilayer anchoring connection structure for fiber reinforced concrete beam column joints

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108724502A (en) * 2018-06-20 2018-11-02 五冶集团上海有限公司 A kind of the plane bracing means and stone material reinforcement means of stone material
CN114876059A (en) * 2022-05-19 2022-08-09 上海师范大学 Multilayer anchoring connection structure for fiber reinforced concrete beam column joints

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CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20180619

Termination date: 20181123