CN219384604U - Auxiliary device convenient to spatial structure is assembled aloft - Google Patents
Auxiliary device convenient to spatial structure is assembled aloft Download PDFInfo
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- CN219384604U CN219384604U CN202320317368.5U CN202320317368U CN219384604U CN 219384604 U CN219384604 U CN 219384604U CN 202320317368 U CN202320317368 U CN 202320317368U CN 219384604 U CN219384604 U CN 219384604U
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Abstract
The utility model relates to the technical field of building construction, and discloses an auxiliary device convenient for assembling a space structure at high altitude, which comprises a stabilizing mechanism, wherein a hoisting mechanism is arranged outside the stabilizing mechanism; the stabilizing mechanism comprises a movable framework beam, a framework connecting plate is connected to the inner side of the movable framework beam through bolts, and an installation seat is arranged on the side face of the movable framework beam. This auxiliary device convenient to spatial structure high altitude is assembled, link the board concatenation through the bolt with removing skeleton crossbeam and skeleton and assemble, install the mount pad in removing the skeleton crossbeam outside through positioning bolt, promote through electric putter and move the fixture block and slide, move the fixture block and decide the fixture block joint and be fixed in the spatial structure outside of preinstallation, fix the fixture block and lock in the spatial structure outside through four groups, thereby make and remove skeleton crossbeam and skeleton and link the board stable fixed, link board to supporting seat and hoist engine stable support through the skeleton, remove the skeleton crossbeam and support branch stable support, branch to fixed pulley stable support.
Description
Technical Field
The utility model relates to the technical field of building construction, in particular to an auxiliary device convenient for assembling a space structure at high altitude.
Background
The space structure is a hall room with large area and volume in the hall type plane combination, such as a spectator hall of a theatre, a competition hall of a gymnasium and the like, and the coverage and enclosure problems are the key of the arrangement of the hall type plane combination structure, so that the novel space structure is rapidly developed, the coverage problem of the space is effectively solved, and meanwhile, the rich and colorful building image is also created. The space structure can adopt a large amount of steel structures during construction, is widely applied to the field of space structure buildings such as large-scale factory buildings, venues and super high-rise buildings because the self weight of the space structure is light, and is convenient to construct, and the installation of large-scale H-shaped steel beams such as crane beams, frame beams or roof beams can be frequently encountered in the current steel structure installation process in construction.
In the prior art, the steel structure of the space structure is mainly installed by a crane or a tower crane. The tower crane has large volume, high space requirement and large construction engineering quantity, and the crane is used for hoisting, so that the construction site is limited and is not suitable for complex construction sites.
Therefore, we propose an auxiliary device for facilitating the high-altitude assembly of the space structure to solve the above-mentioned problems in the background.
Disclosure of Invention
The utility model aims to provide an auxiliary device for facilitating high-altitude assembly of a space structure, so as to solve the problems in the background art.
In order to solve the technical problems, the utility model provides the following technical scheme:
an auxiliary device convenient for assembling a space structure at high altitude comprises a stabilizing mechanism, wherein a hoisting mechanism is arranged outside the stabilizing mechanism;
the stabilizing mechanism comprises a movable framework cross beam, a framework connecting plate is connected to the inner side of the movable framework cross beam through bolts, an installation seat is arranged on the side face of the movable framework cross beam, a positioning bolt is installed between the installation seat and the movable framework cross beam, a fixed clamping block is fixedly connected to the bottom of one end of the installation seat, a movable clamping block is arranged on the inner side of the fixed clamping block, and an electric push rod is installed on the outer side of the movable clamping block;
the hoisting mechanism comprises a supporting seat, a hoist is arranged at the upper end of the supporting seat, a steel wire rope is wound on the surface of the hoist, a fixed pulley is arranged on the outer side of the steel wire rope, a supporting rod is arranged on the outer side of the fixed pulley, and a hoisting lock hook is fixedly connected with the other end of the steel wire rope.
According to the technical scheme, the movable framework cross beam and the framework connecting plate are spliced and assembled through the bolts, the mounting seat is mounted on the outer side of the movable framework cross beam through the positioning bolts, the movable clamping block is pushed to slide through the electric push rod, the movable clamping block and the fixed clamping block are clamped and fixed on the outer part of the pre-installed space structure, and the four groups of fixed clamping blocks and the movable clamping block are locked on the outer part of the space structure, so that the movable framework cross beam and the framework connecting plate are stably fixed, the movable framework cross beam stably supports the supporting seat and the winch through the framework connecting plate, the supporting rod stably supports the supporting rod, the supporting rod stably supports the fixed pulley, so that the upper hoisting mechanism is kept stable, the hoisting mechanism is used for hoisting materials installed on the space structure, so that the space structure is convenient to assemble at high altitude, the structure is light in weight, small in size, convenient to assemble and use place, convenient to operate, and convenient to assist the space structure to assemble at high altitude;
the hoist is stably supported through the supporting seat, the steel wire rope is driven to be wound and unwound through the supporting seat, the fixed pulley is stably supported through the supporting rod, the fixed pulley guides the steel wire rope, meanwhile, the fixed pulley rotates to enable the winding and unwinding of the steel wire rope to be smooth, the steel wire rope is used for hoisting the pre-installation component through the hoisting lock hook, high-altitude conveying of space structure installation materials is facilitated, and the working efficiency of high-altitude assembly of the space structure is improved.
Preferably, the support rod is obliquely arranged, and the lower end of the support rod is connected with the movable framework cross beam through a bolt.
Through above-mentioned technical scheme, branch slope installation to upper portion fixed pulley steady support makes hoist and mount mechanism stable, branch lower extreme and removal skeleton crossbeam bolted connection, the dismouting of being convenient for.
Preferably, the number of the supporting rods is two, the two supporting rods are respectively arranged on two sides of the fixed pulley, and reinforcing ribs are connected between the movable framework cross beam and the supporting rods through bolts.
Through above-mentioned technical scheme, through two spinal branch poles to the steady rest in fixed pulley both ends, make branch more stable through the strengthening rib.
Preferably, the number of the movable framework cross beams is two, and the two movable framework cross beams are respectively connected with two ends of the framework connecting plate through bolts.
Through above-mentioned technical scheme, two movable frame crossbeams and two skeleton link board bolted connection constitute I-shaped structure, stable in structure and be convenient for dismouting.
Preferably, two framework connecting plates are arranged on the inner side of the movable framework cross beam, and the supporting seat is arranged on the upper portion of each framework connecting plate.
Preferably, two mounting seats are respectively arranged at two ends of the outer side of the movable framework beam, and two positioning bolts are arranged on the movable framework beam and the mounting seats.
Through above-mentioned technical scheme, fixed fixture block and the movable fixture block through both ends mount pad bottom are fixed with spatial structure main part, make the movable skeleton crossbeam fix on spatial structure main part upper portion, when fixed fixture block and movable fixture block do not chucking, the movable skeleton crossbeam can be in spatial structure main part upper portion sliding adjustment mounted position, and it is more convenient to use.
Preferably, the movable clamping block is slidably connected to the bottom of the mounting seat, and a plurality of equally distributed threaded holes are formed in the outer side of the movable framework beam.
Through above-mentioned technical scheme, move fixture block sliding connection in the mount pad bottom, make to move the fixture block stable in sliding, when fixed fixture block and move the fixture block and be fixed in the space structure main part outside, the structure is more stable, guarantees the security of device.
Compared with the prior art, the utility model has the following beneficial effects:
according to the utility model, the movable framework cross beam and the framework connecting plate are spliced and assembled through the bolts, the mounting seat is mounted on the outer side of the movable framework cross beam through the positioning bolts, the movable clamping block is pushed to slide through the electric push rod, the movable clamping block and the fixed clamping block are clamped and fixed on the outer part of a pre-mounted space structure, and are locked on the outer part of the space structure through the four groups of fixed clamping blocks and the movable clamping block, so that the movable framework cross beam and the framework connecting plate are stably fixed, the supporting seat and the winch are stably supported through the framework connecting plate, the movable framework cross beam stably supports the supporting rod, the supporting rod stably supports the fixed pulley, so that the upper hoisting mechanism is kept stable, the hoisting mechanism is used for hoisting materials mounted on the space structure, so that the space structure is convenient to assemble the space structure at high altitude.
The second, the utility model supports the hoist engine steadily through the supporting seat, drive the steel wire rope to receive and release through the supporting seat, support the fixed pulley steadily through the fulcrum, the fixed pulley guides the steel wire rope, the fixed pulley rotates and makes the steel wire rope receive and release smoothly at the same time, the steel wire rope hoists the preinstalled component through the hoist and mount latch hook, facilitate the overhead transport of the space structure mounting material, raise the work efficiency that the space structure is assembled aloft.
Drawings
FIG. 1 is a schematic view of the external structure of the present utility model;
FIG. 2 is a schematic side view of the present utility model;
FIG. 3 is a schematic top view of the present utility model;
fig. 4 is a schematic view of a hoist mounting structure of the present utility model.
Wherein: 101. moving the skeleton cross beam; 102. a framework connecting plate; 103. a mounting base; 104. positioning bolts; 105. a fixed clamping block; 106. a movable clamping block; 107. an electric push rod; 201. a support base; 202. a hoist; 203. a wire rope; 204. a fixed pulley; 205. a support rod; 206. and hoisting the lock hook.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to figures 1-4 of the drawings,
an auxiliary device convenient for assembling a space structure at high altitude comprises a stabilizing mechanism, wherein a hoisting mechanism is arranged outside the stabilizing mechanism;
the stabilizing mechanism comprises a movable framework cross beam 101, a framework connecting plate 102 is connected to the inner side of the movable framework cross beam 101 through bolts, an installation seat 103 is arranged on the side face of the movable framework cross beam 101, a positioning bolt 104 is installed between the installation seat 103 and the movable framework cross beam 101, a fixed clamping block 105 is fixedly connected to the bottom of one end of the installation seat 103, a movable clamping block 106 is arranged on the inner side of the fixed clamping block 105, and an electric push rod 107 is installed on the outer side of the movable clamping block 106;
the hoisting mechanism comprises a supporting seat 201, a winch 202 is installed at the upper end of the supporting seat 201, a steel wire rope 203 is wound on the surface of the winch 202, a fixed pulley 204 is installed on the outer side of the steel wire rope 203, a supporting rod 205 is installed on the outer side of the fixed pulley 204, and a hoisting lock hook 206 is fixedly connected with the other end of the steel wire rope 203.
According to the technical scheme, the movable framework cross beam 101 and the framework connecting plate 102 are spliced and assembled through the bolts, the mounting seat 103 is mounted on the outer side of the movable framework cross beam 101 through the positioning bolts 104, the movable clamping block 106 is pushed to slide through the electric push rod 107, the movable clamping block 106 and the fixed clamping block 105 are clamped and fixed outside a pre-mounted space structure, the four groups of the fixed clamping blocks 105 and the movable clamping blocks 106 are locked outside the space structure, so that the movable framework cross beam 101 and the framework connecting plate 102 are stably fixed, the supporting seat 201 and the winch 202 are stably supported through the framework connecting plate 102, the movable framework cross beam 101 is stably supported on the supporting rod 205, the supporting rod 205 is stably supported on the fixed pulley 204, therefore, the upper hoisting mechanism is kept stable, the material mounted on the space structure is hoisted through the hoisting mechanism, the space structure is convenient to assemble at high altitude, the space structure is light in weight compared with the existing crane and tower crane, the structure is convenient to assemble and use at high altitude, the place is flexible and convenient to operate, and the auxiliary space structure is convenient to assemble at high altitude;
the winch 202 is stably supported through the supporting seat 201, the steel wire rope 203 is driven to be retracted and released through the supporting seat 201, the fixed pulley 204 is stably supported through the supporting rod 205, the fixed pulley 204 guides the steel wire rope 203, meanwhile, the fixed pulley 204 rotates to enable the retraction and the release of the steel wire rope 203 to be smooth, the steel wire rope 203 is used for hoisting the pre-installation components through the hoisting lock hooks 206, high-altitude conveying of space structure installation materials is facilitated, and the working efficiency of high-altitude assembly of the space structure is improved.
Specifically, the supporting rod 205 is obliquely installed, and the lower end of the supporting rod 205 is connected with the movable framework cross beam 101 through bolts.
Through above-mentioned technical scheme, branch 205 slope installation to upper portion fixed pulley 204 steady support makes hoist and mount mechanism stable, branch 205 lower extreme and removal skeleton crossbeam 101 bolted connection, the dismouting of being convenient for.
Specifically, there are two struts 205, and two struts 205 are set up respectively in the fixed pulley 204 both sides, and the bolt connection has the strengthening rib between movable skeleton crossbeam 101 and the strut 205.
Through above-mentioned technical scheme, through two branches 205 to the steady rest of fixed pulley 204 both ends, make branch 205 more stable through the strengthening rib.
Specifically, the number of the movable skeleton beams 101 is two, and the two movable skeleton beams 101 are respectively connected to two ends of the skeleton connecting plate 102 by bolts.
Through above-mentioned technical scheme, two movable skeleton crossbeams 101 and two skeleton link plates 102 bolted connection constitute the I-shaped structure, stable in structure and be convenient for dismouting.
Specifically, two frame connecting plates 102 are installed on the inner side of the movable frame cross beam 101, and a supporting seat 201 is installed on the upper portion of the frame connecting plates 102.
Specifically, two mounting seats 103 are respectively arranged at two ends of the outer side of the movable framework cross beam 101, and two positioning bolts 104 are arranged on the movable framework cross beam 101 and the mounting seats 103.
Through above-mentioned technical scheme, fixed fixture block 105 and the movable fixture block 106 through both ends mount pad 103 bottom are fixed with spatial structure main part, make the movable skeleton crossbeam 101 fix on spatial structure main part upper portion, when fixed fixture block 105 and movable fixture block 106 do not chucking, the movable skeleton crossbeam 101 can be in spatial structure main part upper portion sliding adjustment mounted position, and it is more convenient to use.
Specifically, the movable clamping block 106 is slidably connected to the bottom of the mounting seat 103, and a plurality of equally spaced threaded holes are formed in the outer side of the movable skeleton beam 101.
Through above-mentioned technical scheme, move fixture block 106 sliding connection in mount pad 103 bottom, make and move fixture block 106 slip stability, when fixed fixture block 105 and move fixture block 106 block and be fixed in the space structure main part outside, the structure is more stable, guarantees the security of device.
When the movable framework cross beam 101 and the framework connecting plate 102 are spliced and assembled through bolts, the mounting seat 103 is mounted on the outer side of the movable framework cross beam 101 through the positioning bolts 104, the movable clamping block 106 is pushed to slide through the electric push rod 107, the movable clamping block 106 and the fixed clamping block 105 are clamped and fixed on the outer part of a pre-mounted space structure, the movable framework cross beam 101 and the framework connecting plate 102 are locked on the outer part of the space structure through four groups of the fixed clamping blocks 105 and the movable clamping blocks 106, the support seat 201 and the winch 202 are stably supported through the framework connecting plate 102, the movable framework cross beam 101 is stably supported on the support rod 205, the support rod 205 is stably supported on the fixed pulley 204, so that a hoisting mechanism at the upper part is kept stable, materials mounted on the space structure are hoisted through the hoisting mechanism, the space structure is convenient to assemble the space structure at high altitude, the space structure is light in weight compared with the existing crane and tower crane, the space structure is small in size, the space structure is convenient to assemble and use at high altitude, the use place is flexible, the operation is convenient, and the auxiliary space structure is assembled at high altitude;
the winch 202 is stably supported through the supporting seat 201, the steel wire rope 203 is driven to be retracted and released through the supporting seat 201, the fixed pulley 204 is stably supported through the supporting rod 205, the fixed pulley 204 guides the steel wire rope 203, meanwhile, the fixed pulley 204 rotates to enable the retraction and the release of the steel wire rope 203 to be smooth, the steel wire rope 203 is used for hoisting the pre-installation components through the hoisting lock hooks 206, high-altitude conveying of space structure installation materials is facilitated, and the working efficiency of high-altitude assembly of the space structure is improved.
Although particular embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations may be made therein without departing from the principles and spirit thereof, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. Auxiliary device convenient to spatial structure high altitude is assembled, including stabilizing mean, its characterized in that: a hoisting mechanism is arranged outside the stabilizing mechanism;
the stabilizing mechanism comprises a movable framework cross beam (101), a framework connecting plate (102) is connected to the inner side of the movable framework cross beam (101) through bolts, an installation seat (103) is arranged on the side face of the movable framework cross beam (101), a positioning bolt (104) is arranged between the installation seat (103) and the movable framework cross beam (101), a fixed clamping block (105) is fixedly connected to the bottom of one end of the installation seat (103), a movable clamping block (106) is arranged on the inner side of the fixed clamping block (105), and an electric push rod (107) is arranged on the outer side of the movable clamping block (106);
the hoisting mechanism comprises a supporting seat (201), a hoist (202) is arranged at the upper end of the supporting seat (201), a steel wire rope (203) is wound on the surface of the hoist (202), a fixed pulley (204) is arranged on the outer side of the steel wire rope (203), a supporting rod (205) is arranged on the outer side of the fixed pulley (204), and a hoisting lock hook (206) is fixedly connected with the other end of the steel wire rope (203).
2. An auxiliary device for facilitating high-altitude assembly of a space structure according to claim 1, wherein: the support rod (205) is obliquely arranged, and the lower end of the support rod (205) is connected with the movable framework cross beam (101) through bolts.
3. An auxiliary device for facilitating high-altitude assembly of a space structure according to claim 1, wherein: the two support rods (205) are arranged, the two support rods (205) are respectively arranged on two sides of the fixed pulley (204), and reinforcing ribs are connected between the movable framework cross beam (101) and the support rods (205) through bolts.
4. An auxiliary device for facilitating high-altitude assembly of a space structure according to claim 1, wherein: the movable framework cross beams (101) are two, and the two movable framework cross beams (101) are respectively connected to two ends of the framework connecting plate (102) through bolts.
5. An auxiliary device for facilitating high-altitude assembly of a space structure according to claim 1, wherein: two skeleton connecting plates (102) are arranged on the inner side of the movable skeleton cross beam (101), and the supporting seat (201) is arranged on the upper portion of the skeleton connecting plates (102).
6. An auxiliary device for facilitating high-altitude assembly of a space structure according to claim 1, wherein: two mounting seats (103) are respectively arranged at two ends of the outer side of the movable framework cross beam (101), and two positioning bolts (104) are arranged on the movable framework cross beam (101) and the mounting seats (103).
7. An auxiliary device for facilitating high-altitude assembly of a space structure according to claim 1, wherein: the movable clamping blocks (106) are slidably connected to the bottoms of the mounting seats (103), and a plurality of equally distributed threaded holes are formed in the outer side of the movable framework cross beam (101).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320317368.5U CN219384604U (en) | 2023-02-27 | 2023-02-27 | Auxiliary device convenient to spatial structure is assembled aloft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320317368.5U CN219384604U (en) | 2023-02-27 | 2023-02-27 | Auxiliary device convenient to spatial structure is assembled aloft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219384604U true CN219384604U (en) | 2023-07-21 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320317368.5U Active CN219384604U (en) | 2023-02-27 | 2023-02-27 | Auxiliary device convenient to spatial structure is assembled aloft |
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| Country | Link |
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| CN (1) | CN219384604U (en) |
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- 2023-02-27 CN CN202320317368.5U patent/CN219384604U/en active Active
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