CN214194943U - Composite assembled roof board and assembled building - Google Patents

Composite assembled roof board and assembled building Download PDF

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Publication number
CN214194943U
CN214194943U CN202022858677.2U CN202022858677U CN214194943U CN 214194943 U CN214194943 U CN 214194943U CN 202022858677 U CN202022858677 U CN 202022858677U CN 214194943 U CN214194943 U CN 214194943U
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China
Prior art keywords
fixing device
building body
assembly building
assembly
wall body
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CN202022858677.2U
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Chinese (zh)
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李大波
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Hubei Heyifang Prefabricated Construction Technology Co ltd
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Hubei Heyifang Prefabricated Construction Technology Co ltd
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Priority to CN202022858677.2U priority Critical patent/CN214194943U/en
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Abstract

The utility model relates to a building and building materials technical field just discloses a compound assembled roof boarding and assembly building body, install in the assembly building body of wall body side including wall body and correspondence, assembly building body side-mounting has fixing device, and fixing device inside groove both ends fixed mounting has L shape support, and the channel has been seted up to assembly building body both sides. This compound assembled roof boarding and assembly building body through installing fixing device on wall body side, roofing top surface and bottom surface, utilizes fixing device to assemble building body fixed mounting, then will assemble the channel joint that building body side was seted up on fixing device for the assembly is simple and convenient, and the mode of assembling the installation makes the effect that the scene can not cause rubbish.

Description

Composite assembled roof board and assembled building
Technical Field
The utility model relates to a building and building materials technical field specifically is a compound assembled roof boarding and assembly building body.
Background
The existing roof structure is a main reinforced concrete prefabricated roof panel or a cast-in-place roof panel structure. Currently, such structures have been widely used in building construction.
However, the roof panel structures currently in use also have a series of disadvantages: firstly, the cement concrete has larger volume weight (2400kg/m3), so that the roof panel is heavier, the field construction is also more complicated, particularly, the roof load is increased in a steel structure building, the size of the whole structure is influenced to be larger, and the manufacturing cost is increased; secondly, wet operation is more during construction, so that the whole construction site is dirty and bad and pollution is serious; and thirdly, a special template is needed in the production process, the cost is increased, a release agent needs to be added for demolding, the construction period is long, and the construction procedures are increased.
In view of this, the present invention is proposed to solve the above technical problems.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides a not enough to prior art, the utility model provides a compound assembled roof boarding and assembly building body possesses the assembly portably, can not cause too many rubbish to the scene, and the current building mode of relative ratio, and the above-mentioned technical problem has been solved to advantages such as the quality is slim and graceful.
(II) technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a compound assembled roof boarding and assembly building body, includes the wall body and corresponds the assembly building body of installing in the wall body side, assembly building body side-mounting has fixing device, and fixing device inside groove both ends fixed mounting have L shape support, the channel has been seted up to assembly building body both sides.
Preferably, the assembly building body is fixedly installed on the side face of the wall body through a fixing device, and the channels are formed in the two side faces of the assembly building body.
Through above-mentioned technical scheme, fixing device joint is inside the channel that assembly building body side was seted up, and fixing device installs in the wall body side, will assemble the installation that building body can be stable on the wall body through fixed screw etc..
Preferably, the fixing device comprises a screw hole formed in the upper end and the lower end and a bolt installed inside the screw hole.
Through above-mentioned technical scheme, seted up a plurality of screws in the fixing device, squeeze into the bolt through the screw is inside and can install fixing device on the wall body.
Preferably, the screw holes are formed in two ends of the inner portion of the fixing device, and the bolts are fixedly installed in the side face of the wall body corresponding to the screw holes.
Through above-mentioned technical scheme, the bolt can penetrate fixing device and squeeze into inside the wall body, then assemble building body and be fixed in on fixing device.
Preferably, the L-shaped supports are arranged at two ends inside the fixing device, the L-shaped supports are fixedly arranged inside a wall body penetrating through the fixing device through bolts, and the number of the L-shaped supports is two.
Through above-mentioned technical scheme, there is L shape support fixing device both ends through bolt fixed mounting, and L shape support can be connected in the roofing top surface for strengthen the holistic stability of assembly building body, L shape support is equipped with two, connects in roofing top surface and ground, and all can fix with current gim peg.
Preferably, the U-shaped framework is fixedly installed inside a channel which is formed in one side, far away from the wall body, of the assembly building body, a hole is formed inside the U-shaped framework, an airplane expansion bolt is installed inside the hole, the hole is formed in the joint of the assembly building body, and the U-shaped framework is fixedly installed inside the channel which is formed in the side face of the assembly building body through the airplane expansion bolt.
Through above-mentioned technical scheme, the channel has all been seted up to assembly building body both sides, and the channel on assembly building body both sides equals, do not divide installing of positive and negative, the U-shaped skeleton joint is keeping away from wall body one side in assembly building body, through having seted up the hole for assembly building body junction, and the hole can utilize the electric drill to carry out the trompil according to the place of oneself needs, then squeeze into the hole with the aircraft expansion bolt inside, then cup joint the U-shaped skeleton with next assembly building body and connect.
Compared with the prior art, the utility model provides a compound assembled roof boarding and assembly building body possesses following beneficial effect:
1. this compound assembled roof boarding and assembly building body through installing fixing device on wall body side, roofing top surface and bottom surface, utilizes fixing device to assemble building body fixed mounting, then will assemble the channel joint that building body side was seted up on fixing device for the assembly is simple and convenient, and the mode of assembling the installation makes the effect that the scene can not cause rubbish.
2. This compound assembled roof boarding and assembly building body, current construction will mix earth and template and construct synthetically, and weight is super serious to go out, utilizes assembly building body later stage to carry out fixed mounting, can change the design according to the topography, can not be equipped with the limitation in the later stage fitment, and reaches the light effect of quality.
Drawings
FIG. 1 is a schematic view of the whole structure of the present invention;
FIG. 2 is a schematic view of the structure-assembled building body of the present invention;
FIG. 3 is a schematic view of the structure fixing device and the L-shaped bracket of the present invention;
FIG. 4 is a schematic view of the U-shaped frame of the present invention;
fig. 5 is the structural schematic view of the aircraft expansion bolt of the present invention.
Wherein: 1. a wall body; 2. assembling a building body; 3. a fixing device; 4. an L-shaped bracket; 5. a channel; 6. a U-shaped framework; 301. a screw hole; 302. a bolt; 601. a hole; 602. an aircraft expansion bolt.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-5, a composite assembly type roof panel and an assembly building body include a wall 1 and an assembly building body 2 correspondingly installed on a side surface of the wall 1, and are characterized in that: the side surface of the assembly building body 2 is provided with a fixing device 3, two ends of an inner groove of the fixing device 3 are fixedly provided with L-shaped supports 4, and two sides of the assembly building body 2 are provided with channels 5.
Specifically, assembly building body 2 passes through 3 fixed mounting of fixing device in 1 side of wall body, and channel 5 is seted up at assembly building body 2 both sides face, and the advantage is that 3 joints of fixing device are inside 5 channels of seting up in assembly building body 2 side, and fixing device 3 installs in 1 side of wall body, will assemble building body 2 can be stable through fixed screw etc. and install on 1 of wall body.
Specifically, the fixing device 3 comprises a screw hole 301 formed in the upper end and the lower end and a bolt 302 installed inside the screw hole 301, and the fixing device 3 has the advantages that the plurality of screw holes 301 are formed in the fixing device 3, and the bolt 302 is driven into the screw hole 301 to install the fixing device 3 on the wall 1.
Specifically, screw holes 301 are formed in two ends of the inside of the fixing device 3, and bolts 302 are fixedly installed in the side face of the wall body 1 corresponding to the screw holes 301, so that the advantages that the bolts 302 can penetrate through the fixing device 3 to be driven into the inside of the wall body 1, and then the assembled building body 2 is fixed on the fixing device 3 are achieved.
Specifically, L shape support 4 is installed in 3 inside both ends of fixing device, L shape support 4 passes through bolt 302 fixed mounting inside 1 wall body that runs through fixing device 3, L shape support 4 quantity is two, the advantage is that 3 both ends of fixing device have L shape support 4 through bolt 302 fixed mounting, L shape support 4 can be connected in the roofing top surface, make strengthen the holistic stability of assembly building body 2, L shape support 4 is equipped with two, connect in roofing top surface and ground, and all can fix with current gim peg.
Specifically, a U-shaped framework 6 is fixedly installed inside a channel 5 which is arranged on one side of an assembly building body 2 far away from a wall body 1, a hole 601 is installed inside the U-shaped framework 6, an airplane expansion bolt 602 is installed inside the hole 601, the hole 601 is arranged at the joint of the assembly building body 2, the U-shaped framework 6 is fixedly installed inside the channel 5 which is arranged on the side of the assembly building body 2 by the airplane expansion bolt 602, the advantages are that the channel 5 is arranged on both sides of the assembly building body 2, the channels 5 on both sides of the assembly building body 2 are equal, the installation is not divided into the front side and the back side, the U-shaped framework 6 is clamped in one side of the assembly building body 2 far away from the wall body 1, the hole 601 is arranged at the joint of the assembly building body 2, the hole 601 can be drilled by an electric drill according to the required place, and then the airplane expansion bolt 602 is driven into the hole 601, and then the next assembled building body 2 is sleeved with the U-shaped framework 6 for connection.
When the fixing device is used, the L-shaped supports 4 are installed at the two ends of the fixing device 3, then the fixing device is fixedly installed on the wall body 1 through the bolts 302, the back channels 5 are formed in the two sides of the assembly building body 2, the channels 5 are clamped on the surface of the fixing device 3, then the L-shaped supports 4 are sleeved inside the channels 5 far away from one side of the wall body 1, and the L-shaped supports are fixedly installed inside the holes 601 through the airplane expansion bolts 602.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides a compound assembled roof boarding and assembly building body, includes wall body (1) and corresponds and install in assembly building body (2) of wall body (1) side, its characterized in that: the side surface of the assembly building body (2) is provided with a fixing device (3), two ends of an inner groove of the fixing device (3) are fixedly provided with an L-shaped support (4), and two sides of the assembly building body (2) are provided with channels (5).
2. A composite fabricated roof panel and fabricated building according to claim 1, wherein: the assembly building body (2) is fixedly arranged on the side face of the wall body (1) through the fixing device (3), and the channels (5) are arranged on the two side faces of the assembly building body (2).
3. A composite fabricated roof panel and fabricated building according to claim 1, wherein: the fixing device (3) comprises a screw hole (301) formed in the upper end and the lower end and a bolt (302) installed inside the screw hole (301).
4. A composite fabricated roof panel and fabricated building according to claim 3, wherein: screw hole (301) are seted up at the inside both ends of fixing device (3), bolt (302) correspond screw hole (301) fixed mounting in wall body (1) side.
5. A composite fabricated roof panel and fabricated building according to claim 1 or 4, wherein: the L-shaped supports (4) are arranged at two ends inside the fixing device (3), the L-shaped supports (4) are fixedly arranged inside the wall body (1) penetrating through the fixing device (3) through bolts (302), and the number of the L-shaped supports (4) is two.
6. A composite fabricated roof panel and fabricated building according to claim 1, wherein: assembly building body (2) keep away from channel (5) internally mounted fixed mounting that wall body (1) one side was seted up has U-shaped skeleton (6), U-shaped skeleton (6) internally mounted has hole (601), hole (601) internally mounted has aircraft expansion bolts (602), hole (601) are seted up in assembly building body (2) junction, aircraft expansion bolts (602) are inside with U-shaped skeleton (6) fixed mounting in channel (5) that assembly building body (2) side was seted up.
CN202022858677.2U 2020-12-01 2020-12-01 Composite assembled roof board and assembled building Active CN214194943U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022858677.2U CN214194943U (en) 2020-12-01 2020-12-01 Composite assembled roof board and assembled building

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022858677.2U CN214194943U (en) 2020-12-01 2020-12-01 Composite assembled roof board and assembled building

Publications (1)

Publication Number Publication Date
CN214194943U true CN214194943U (en) 2021-09-14

Family

ID=77649520

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202022858677.2U Active CN214194943U (en) 2020-12-01 2020-12-01 Composite assembled roof board and assembled building

Country Status (1)

Country Link
CN (1) CN214194943U (en)

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