CN221027551U - Operation workbench for aircraft assembly - Google Patents
Operation workbench for aircraft assembly Download PDFInfo
- Publication number
- CN221027551U CN221027551U CN202322876456.1U CN202322876456U CN221027551U CN 221027551 U CN221027551 U CN 221027551U CN 202322876456 U CN202322876456 U CN 202322876456U CN 221027551 U CN221027551 U CN 221027551U
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- fixed
- assembly
- aircraft
- console
- lifting adjusting
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- 230000005540 biological transmission Effects 0.000 claims abstract description 32
- 230000007547 defect Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model relates to the technical field of aircraft assembly, and discloses an operation workbench for aircraft assembly, which comprises a movable supporting component, a lifting adjusting component, a control console, a platform fixing component and a protection rod, wherein the lifting adjusting component is arranged at the top of the movable supporting component, the control console is arranged at the top of the lifting adjusting component, and the platform fixing component is arranged at the other end of the top of the lifting adjusting component. This operation workstation is used in aircraft assembly drives through driving motor through the transmission of transmission supporting seat and rotates the screw rod to let the movable block remove outside rotating the screw rod, drive the clamp plate and go up and down, press from both sides the anchor clamps to the object, thereby ensure that the device removes under the condition of going up and down, can not take place to remove the problem that drops, improve the security, set up flutedly through the top of fixed box, can place aircraft assembly through the recess and need instrument and small-size spare part, avoid dropping the lift mesa and lead to assembly efficiency to reduce.
Description
Technical Field
The utility model relates to the technical field of aircraft assembly, in particular to an operation workbench for aircraft assembly.
Background
The operation workbench is one of important equipment in the aircraft assembly process, an operator finishes the assembly work of all parts and components of the aircraft on the workbench, and the types and the sizes of the workbench are different from each other according to the differences of all the parts and components, and some of the workbench is assembled on all the parts of the aircraft by the operator standing on the workbench.
According to the operation workstation for aircraft assembly of authorized publication number CN213895124U, including workstation main part and the base of setting in workstation main part below, the top edge of workstation main part is fixed to be provided with the guardrail, and still is provided with the access & exit on the guardrail, the scissors rotating stand that alternately rotates the setting is installed in the top rotation of base, the equal fixed mounting in bottom both ends of workstation main part has the runing rest, and the top of scissors rotating stand rotates with the bottom of runing rest and be connected. The operating workbench for aircraft assembly is convenient for people to adjust the height and move according to actual needs, avoids the defect that the existing operating workbench for aircraft assembly is inconvenient for people to adjust the height and move according to actual needs because of a relatively fixed structure, has a simple structure, is convenient for people to operate and use, and is convenient for operators to use.
However, the device still has the defects that the moving wheels and the rotating frame move and lift, so that the condition that the operation workbench can move is met, but under the condition of moving and lifting, the moving falling condition of parts and assembly parts placed on the operation workbench possibly exists, so that the safety risk is caused, and the problem of low assembly efficiency is also caused.
Disclosure of utility model
The utility model aims to provide an operation workbench for aircraft assembly, which solves the problems in the prior art.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an aircraft assembly is with operation workstation, includes removal supporting component, lift adjustment subassembly, control cabinet, platform fixed subassembly and guard bar, lift adjustment subassembly sets up in the top of removing the supporting component, the control cabinet sets up in the top of lift adjustment subassembly, the fixed subassembly of platform sets up in the other end at lift adjustment subassembly top, the guard bar sets up in the outside at lift adjustment subassembly top.
The platform fixed subassembly includes fixed box, transmission supporting seat, driving motor, rotation screw rod, movable block and clamp plate, fixed box fixed connection is in the inside bottom of fixed box, driving motor screw connection is in the one end at transmission supporting seat top, the rotation screw rod rotates the other end of being connected at transmission supporting seat top, movable block threaded connection is in the outside of rotation screw rod, clamp plate fixed connection is in the one end of movable block, and driving motor drives the rotation screw rod through the transmission of transmission supporting seat to let the movable block remove outside the rotation screw rod, drive the clamp plate and go up and down, press from both sides the clamp to the object, thereby ensure that the device removes under the condition of going up and down, can not take place to remove the problem that drops, improve the security.
Preferably, the transmission supporting seat comprises a shell, a first rotating rod, a second rotating rod and a transmission belt, wherein the shell is fixedly connected to the bottom inside the fixed box, the first rotating rod is rotationally connected to one end inside the shell, the second rotating rod is rotationally connected to the other end inside the shell, the transmission belt is rotationally connected to the outside of the first rotating rod and the second rotating rod, an output shaft of the driving motor penetrates through the shell and is fixedly connected with the first rotating rod, and the bottom of the rotating screw rod penetrates through the shell and is fixedly connected with the second rotating rod, so that the driving motor can drive the rotating screw rod to rotate through the transmission supporting seat.
Preferably, the movable support assembly comprises a mounting plate, movable wheels, a fixed block and a hydraulic support column, the movable wheels are rotationally connected to one side of the mounting plate, the fixed blocks are fixedly connected to two sides of the mounting plate, the hydraulic support column is fixedly connected to the inside of the fixed blocks, the device can be moved through the movable wheels, the device can be fixed through the hydraulic support column, and stability in lifting is guaranteed.
Preferably, the lifting adjusting assembly comprises a fixing frame, a telescopic frame, a hydraulic telescopic rod, a lifting table top and an air cylinder, wherein the fixing frame is fixedly connected to the top of the mounting plate, the telescopic frame is movably connected to the inner side of the fixing frame, the lifting table top is movably connected to the top of the hydraulic telescopic rod, the air cylinder is fixedly connected to one end of the fixing frame, the hydraulic telescopic rod is arranged in the telescopic frame, and the hydraulic telescopic rod is driven to operate through the air cylinder, so that the telescopic frame is unfolded, the lifting table top is driven to lift, the lifting height of the operation table is controlled, and the aircraft assembly is facilitated.
Preferably, a chute is formed in one side of the fixed box, the moving block is slidably connected to the inside of the chute, and the moving block is convenient to lift through the chute.
Preferably, the bottom of clamp plate is provided with the rubber pad, increases the frictional force with the assembly part through the rubber pad, ensures to push down the centre gripping firm, and secondly the rubber pad plays the guard action, prevents to cause the damage to the assembly part.
Preferably, the top of fixed case is seted up flutedly, can place aircraft assembly through the recess and need instrument and small-size spare part, avoids dropping the lift mesa and leads to assembly efficiency to reduce.
Compared with the prior art, the utility model has the beneficial effects that:
1. This operation workstation is used in aircraft assembly drives the rotation screw through the transmission of driving motor through transmission supporting seat to let the movable block remove outside the rotation screw, drive the clamp plate and go up and down, press from both sides the solid to the object, thereby ensure that the device removes under the condition of going up and down, can not take place to remove the problem that drops, improve the security.
2. This aircraft is operation workstation for assembly sets up flutedly through the top of fixed case, can place aircraft assembly through the recess and need instrument and small-size spare part, avoids dropping the lift mesa and leads to assembly efficiency to reduce.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of a platform securing assembly according to the present utility model;
FIG. 3 is a schematic view of a structure of the present practical transmission support seat;
FIG. 4 is a schematic view of a mobile support assembly according to the present utility model;
Fig. 5 is a schematic structural view of the lifting adjusting assembly of the present utility model.
In the figure: 1. a moving support assembly; 2. a lifting adjusting component; 3. a console; 4. a platform fixing assembly; 5. a protective rod; 101. a mounting plate; 102. a moving wheel; 103. a fixed block; 104. a hydraulic support column; 201. a fixing frame; 202. a telescopic frame; 203. a hydraulic telescopic rod; 204. lifting the table top; 205. a cylinder; 401. a fixed box; 402. a groove; 403. a transmission support seat; 404. a driving motor; 405. rotating the screw; 406. a moving block; 407. a pressing plate; 410. a housing; 411. a first rotating lever; 412. a second rotating rod; 413. a driving belt.
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 fig. 1-5, the present utility model provides a technical solution: the utility model provides an aircraft assembly is with operation workstation, includes removal supporting component 1, lift adjusting component 2, control cabinet 3, platform fixed subassembly 4 and guard bar 5, and lift adjusting component 2 sets up in the top of removing supporting component 1, and control cabinet 3 sets up in the top of lift adjusting component 2, and platform fixed subassembly 4 sets up in the other end at lift adjusting component 2 top, and guard bar 5 sets up in the outside at lift adjusting component 2 top.
The movable support assembly 1 comprises a mounting plate 101, a movable wheel 102, a fixed block 103 and a hydraulic support column 104, wherein the movable wheel 102 is rotatably connected to one side of the mounting plate 101, the fixed block 103 is fixedly connected to two sides of the mounting plate 101, the hydraulic support column 104 is fixedly connected to the inside of the fixed block 103, the device can be moved through the movable wheel 102, the device can be fixed through the hydraulic support column 104, and stability in lifting is ensured.
The lifting adjusting assembly 2 comprises a fixing frame 201, a telescopic frame 202, a hydraulic telescopic rod 203, a lifting table top 204 and an air cylinder 205, wherein the fixing frame 201 is fixedly connected to the top of the mounting plate 101, the telescopic frame 202 is movably connected to the inner side of the fixing frame 201, the lifting table top 204 is movably connected to the top of the hydraulic telescopic rod 203, the air cylinder 205 is fixedly connected to one end of the fixing frame 201, the hydraulic telescopic rod 203 is arranged in the telescopic frame 202, the hydraulic telescopic rod 203 is driven to operate through the air cylinder 205, the telescopic frame 202 is unfolded, the lifting table top 204 is driven to lift, the lifting height of the operation table is controlled, and aircraft assembly is facilitated.
The platform fixed subassembly 4 includes fixed box 401, transmission supporting seat 403, driving motor 404, rotating screw 405, movable block 406 and clamp plate 407, fixed box 401 fixed connection is in the inside bottom of fixed box 401, driving motor 404 screw connection is in the one end at transmission supporting seat 403 top, rotating screw 405 rotates the other end of being connected at transmission supporting seat 403 top, movable block 406 threaded connection is in the outside of rotating screw 405, clamp plate 407 fixed connection is in the one end of movable block 406, driving motor 404 passes through the transmission of transmission supporting seat 403, drive rotating screw 405 rotates, thereby let movable block 406 remove outside rotating screw 405, drive clamp plate 407 goes up and down, press from both sides the clamp plate to the object, thereby ensure that the problem that the removal dropped can not take place under the circumstances that the device goes up and down, improve the security, the spout has been seted up to one side of fixed box 401, movable block 406 sliding connection is in the inside of spout, be convenient for movable block 406 goes up and down through the spout, the bottom of clamp plate 407 is provided with the rubber pad, increase the frictional force with the assembly member through the rubber pad, ensure to push down the centre gripping, the rubber pad guard action, prevent to cause damage to the assembly member, top of fixed box 401 has been seted up the recess, can avoid the mesa 204 to drop down through the tool 402, the required to put down the assembly efficiency of tool 204 is avoided.
The transmission supporting seat 403 comprises a shell 410, a first rotating rod 411, a second rotating rod 412 and a transmission belt 413, wherein the shell 410 is fixedly connected to the bottom inside the fixed box 401, the first rotating rod 411 is rotationally connected to one end inside the shell 410, the second rotating rod 412 is rotationally connected to the other end inside the shell 410, the transmission belt 413 is rotationally connected to the outer parts of the first rotating rod 411 and the second rotating rod 412, an output shaft of the driving motor 404 penetrates through the shell 410 and is fixedly connected with the first rotating rod 411, and the bottom of the rotating screw 405 penetrates through the shell 410 and is fixedly connected with the second rotating rod 412, so that the driving motor 404 can drive the rotating screw 405 to rotate through the transmission supporting seat 403.
When the aircraft assembly device is used, an assembly part is placed on the lifting table top 204, the driving motor 404 starts to operate, the rotating screw rod 405 is driven to rotate through the transmission of the transmission supporting seat 403, the moving block 406 ascends and descends along the rotating screw rod 405, the pressing plate 407 is driven to fix the assembly part, then the assembly part is moved to a proper position through the moving wheel 102, the hydraulic supporting column 104 is used for fixing the assembly part, the air cylinder 205 drives the hydraulic telescopic rod 203 to ascend and descend, the lifting table top 204 is adjusted to a proper position, and aircraft assembly starts.
Although 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 can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an aircraft is operation workstation for assembly, includes removal supporting component (1), lift adjustment subassembly (2), control cabinet (3), platform fixed subassembly (4) and guard bar (5), its characterized in that: the lifting adjusting assembly (2) is arranged at the top of the movable supporting assembly (1), the control console (3) is arranged at the top of the lifting adjusting assembly (2), the platform fixing assembly (4) is arranged at the other end of the top of the lifting adjusting assembly (2), and the protection rod (5) is arranged at the outer side of the top of the lifting adjusting assembly (2);
The platform fixed subassembly (4) is including fixed case (401), transmission supporting seat (403), driving motor (404), rotation screw (405), movable block (406) and clamp plate (407), fixed case (401) fixed connection is in the inside bottom of fixed case (401), driving motor (404) screw connection is in the one end at transmission supporting seat (403) top, rotation screw (405) rotate the other end of being connected in transmission supporting seat (403) top, movable block (406) threaded connection is in the outside of rotating screw (405), clamp plate (407) fixed connection is in the one end of movable block (406).
2. An aircraft-assembling console as set forth in claim 1, wherein: the transmission supporting seat (403) comprises a shell (410), a first rotating rod (411), a second rotating rod (412) and a transmission belt (413), wherein the shell (410) is fixedly connected to the bottom of the inside of the fixed box (401), the first rotating rod (411) is rotationally connected to one end of the inside of the shell (410), the second rotating rod (412) is rotationally connected to the other end of the inside of the shell (410), and the transmission belt (413) is rotationally connected to the outside of the first rotating rod (411) and the second rotating rod (412).
3. An aircraft-assembling console as set forth in claim 1, wherein: the movable supporting assembly (1) comprises a mounting plate (101), a movable wheel (102), a fixed block (103) and a hydraulic supporting column (104), wherein the movable wheel (102) is rotatably connected to one side of the mounting plate (101), the fixed block (103) is fixedly connected to two sides of the mounting plate (101), and the hydraulic supporting column (104) is fixedly connected to the inside of the fixed block (103).
4. An aircraft-assembling console as set forth in claim 1, wherein: lifting adjustment subassembly (2) are including mount (201), expansion bracket (202), hydraulic telescoping rod (203), lift mesa (204) and cylinder (205), mount (201) fixed connection is in the top of mounting panel (101), expansion bracket (202) swing joint is in the inboard of mount (201), lift mesa (204) swing joint is in the top of hydraulic telescoping rod (203), cylinder (205) fixed connection is in the one end of mount (201), hydraulic telescoping rod (203) set up in the inside of expansion bracket (202).
5. An aircraft-assembling console as set forth in claim 1, wherein: a chute is formed in one side of the fixed box (401), and the moving block (406) is connected to the inside of the chute in a sliding mode.
6. An aircraft-assembling console as set forth in claim 1, wherein: the bottom of the pressing plate (407) is provided with a rubber pad.
7. An aircraft-assembling console as set forth in claim 1, wherein: a groove (402) is formed in the top of the fixed box (401).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322876456.1U CN221027551U (en) | 2023-10-26 | 2023-10-26 | Operation workbench for aircraft assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322876456.1U CN221027551U (en) | 2023-10-26 | 2023-10-26 | Operation workbench for aircraft assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221027551U true CN221027551U (en) | 2024-05-28 |
Family
ID=91171592
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322876456.1U Active CN221027551U (en) | 2023-10-26 | 2023-10-26 | Operation workbench for aircraft assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221027551U (en) |
-
2023
- 2023-10-26 CN CN202322876456.1U patent/CN221027551U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |