CN220786145U - Mobile supporting and positioning device for aircraft component assembly - Google Patents
Mobile supporting and positioning device for aircraft component assembly Download PDFInfo
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- CN220786145U CN220786145U CN202322700892.3U CN202322700892U CN220786145U CN 220786145 U CN220786145 U CN 220786145U CN 202322700892 U CN202322700892 U CN 202322700892U CN 220786145 U CN220786145 U CN 220786145U
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- 238000010586 diagram Methods 0.000 description 1
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- 230000001360 synchronised effect Effects 0.000 description 1
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Abstract
The utility model relates to the technical field of aircraft component assembly, and discloses a movable supporting and positioning device for aircraft component assembly, which comprises a reset spring rod movably arranged on the left side and the right side of the surface of a stop block, a sliding plate is sleeved on the top surface of the reset spring rod in a sliding manner, and a clamping plate is fixedly arranged on the top surface of the sliding plate. According to the utility model, the hydraulic device is started, the arranged hydraulic telescopic rod stretches and moves on the surface of the groove to drive the push plate to synchronously slide, so that the arranged four clamping plates are clamped with the aircraft component placed on the top surface of the positioning plate, meanwhile, the positions of the four clamping plates can be regulated again by the arranged reset spring rod and the sliding plate, the aircraft components with different sizes can be effectively treated, the operation is convenient and simple, the arranged bearing can drive the positioning plate to rotate, the angle of the aircraft component can be conveniently regulated by a worker, the quick installation groove of the aircraft component can be conveniently carried out by the worker, and the operation is convenient and simple.
Description
Technical Field
The utility model relates to the technical field of aircraft component assembly, in particular to a movable supporting and positioning device for aircraft component assembly.
Background
The aircraft is an aircraft which has one or more engines and is provided with a power device for generating forward thrust or pulling force, a fixed wing of the aircraft body generates lifting force, the aircraft flies in the atmosphere and is heavier than air, and when the aircraft material is manufactured into parts for aircraft equipment, the parts to be assembled are often pressed and positioned by using a movable supporting and positioning device for specific processing.
According to the publication number CN214870114U, the movable supporting and positioning device for the assembly of the aircraft parts comprises a movable supporting frame, a positioning shell, a bidirectional threaded rod and a clamping and positioning mechanism, wherein the positioning shell is fixedly embedded at the top of the movable supporting frame, the bidirectional threaded rod is rotated in the positioning shell, the left side and the right side of the bidirectional threaded rod are respectively provided with a clamping and positioning mechanism for clamping and positioning the aircraft parts, and the clamping and positioning mechanism comprises a mechanism shell, a spring, a collision block, a push rod, a chute plate, a driving piece, a clamping plate, a threaded block, a fixed block, an elastic buckle and an elastic rod. According to the utility model, the clamping and positioning mechanism is matched with the bidirectional threaded rod, so that the clamping and positioning mechanism clamps the aircraft parts, thereby avoiding the problem of deformation and damage of the aircraft parts caused by excessive force applied by operating the movable supporting and positioning device, and further improving the practicability of the movable supporting and positioning device.
But still have the problem that can't carry out the removal regulation in position to the support frame, need carry the support frame through the staff, reduce the work efficiency to aircraft parts assembly, and can't adjust according to the size and the size of different aircraft parts, receive the restriction great, need improve this.
Disclosure of utility model
The utility model aims to provide a movable supporting and positioning device for assembling aircraft parts, which solves the problems in the background art.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
The utility model provides an aircraft parts assembly is with removing support positioner, includes backup pad and positioning mechanism, positioning mechanism movable mounting is in backup pad top surface, positioning mechanism includes adjustment unit and clamping unit, just adjustment unit and clamping unit all set up in backup pad top surface left and right sides.
Preferably, the adjusting unit comprises a hydraulic device and a hydraulic telescopic rod, the hydraulic device is fixedly arranged on the left side and the right side of the top surface of the supporting plate, grooves are formed in the left side and the right side of the surface of the supporting plate, and the hydraulic telescopic rod is sleeved inside the grooves in a telescopic manner.
Preferably, the clamping unit comprises a bearing, a positioning plate, a push plate, a stop block, a reset spring rod, a sliding plate and a clamping plate, wherein the bearing is rotationally sleeved at the center position of the top surface of the supporting plate, the positioning plate is fixedly clamped at the top surface of the bearing, the push plate is movably mounted at the left side and the right side of the surface of the positioning plate, the stop block is fixedly mounted at the center position of the surface of the push plate, the reset spring rod is movably mounted at the left side and the right side of the surface of the stop block, the sliding plate is slidingly sleeved at the top surface of the reset spring rod, and the clamping plate is fixedly mounted at the top surface of the sliding plate.
Preferably, the backup pad includes guide rail, driving motor, support column and rotation gear, guide rail fixed mounting is in backup pad bottom surface both sides, rotation gear meshes in the guide rail surface, driving motor fixed mounting is in backup pad bottom surface central point put, support column movable mounting is around the backup pad bottom surface.
Preferably, one side of the surface of the hydraulic telescopic rod is correspondingly connected with the surface position of the set push plate, the hydraulic telescopic rod drives the push plate to slide and clamp to two sides of the surface of the positioning plate through the set hydraulic device, and the set hydraulic telescopic rod can carry out sliding adjustment on the position of the push plate, so that the clamping plate and the aircraft component placed on the surface of the positioning plate are effectively fastened and clamped.
Preferably, the joint board is equipped with four altogether, four the joint board is L shape, four the joint board is through reset spring pole and the slide that sets up and the corresponding joint all around of locating plate surface, just the locating plate rotates at backup pad top surface central point through the bearing that sets up, starts hydraulic means, and the hydraulic telescoping rod that sets up drives the push pedal synchronous sliding at recess surface, makes the aircraft part that four joint boards that set up and locating plate top surface placed carry out the joint, and reset spring pole and the slide that set up can adjust the position of four joint boards again simultaneously, can effectively adjust the aircraft part of equidimension not, convenient operation is simple, and the bearing that sets up can drive the locating plate and rotate, and the staff of being convenient for adjusts aircraft part angle, makes things convenient for the staff to carry out quick mounting groove to aircraft part, convenient for easy operation.
Preferably, the backup pad is through the guide rail and the rotation gear left and right sides slip of setting up at support column top surface, starts driving motor, and the dwang rotates, and then can drive the rotation gear operation, under the tooth effect, can drive the backup pad whole and control the regulation removal on the position at the guide rail top surface, avoids needing the manual whole removal to the backup pad of staff, improves the work efficiency to aircraft parts assembly.
The utility model provides a movable supporting and positioning device for aircraft component assembly, which has the following beneficial effects:
(1) According to the utility model, the push plate can be slidably adjusted in position through the hydraulic telescopic rod, and the clamping plate is effectively fastened and connected with the aircraft component placed on the surface of the positioning plate.
(2) According to the utility model, the hydraulic device is started, the set hydraulic telescopic rod stretches and moves on the surface of the groove to drive the push plate to synchronously slide, so that the set four clamping plates are clamped with the airplane components placed on the top surface of the positioning plate, meanwhile, the set reset spring rod and the slide plate can adjust the positions of the four clamping plates again, the airplane components with different sizes can be effectively treated, the operation is convenient and simple, the set bearing can drive the positioning plate to rotate, the angle of the airplane components can be conveniently adjusted by a worker, the airplane components can be conveniently and rapidly installed by the worker, and the operation is convenient and simple.
(3) According to the utility model, the driving motor is started, the rotating rod rotates, so that the rotating gear can be driven to operate, the whole supporting plate can be driven to adjust and move on the left and right positions on the top surface of the guide rail under the action of the meshing teeth, the phenomenon that a worker manually moves the whole supporting plate is avoided, and the working efficiency of assembling aircraft parts is improved.
Drawings
FIG. 1 is a schematic view of the overall structure of the front face of the present utility model;
FIG. 2 is a schematic view of a positioning mechanism in a top view of the present utility model;
FIG. 3 is a schematic view of the connection structure of the push plate and the hydraulic telescopic rod of the side face of the present utility model;
fig. 4 is a schematic diagram showing the connection structure of the driving motor and the rotating gear according to the present utility model.
In the figure: 1. a support plate; 101. a guide rail; 102. a driving motor; 103. a support column; 104. rotating the gear; 2. a positioning mechanism; 201. a hydraulic device; 202. a bearing; 203. a positioning plate; 204. a push plate; 205. a stop block; 206. a reset spring lever; 207. a slide plate; 208. a clamping plate; 209. a groove; 210. a hydraulic telescopic rod.
Detailed Description
The utility model provides the following technical scheme:
As shown in fig. 1-4, a mobile supporting and positioning device for assembling aircraft components comprises a supporting plate 1 and a positioning mechanism 2, wherein the positioning mechanism 2 is movably mounted on the top surface of the supporting plate 1, the supporting plate 1 slides left and right on the top surface of a supporting column 103 through a guide rail 101 and a rotating gear 104, the positioning mechanism 2 comprises an adjusting unit and a clamping unit, and the adjusting unit and the clamping unit are arranged on the left side and the right side of the top surface of the supporting plate 1.
The adjusting unit comprises a hydraulic device 201 and a hydraulic telescopic rod 210, wherein the hydraulic device 201 is fixedly arranged on the left side and the right side of the top surface of the supporting plate 1, grooves 209 are formed in the left side and the right side of the surface of the supporting plate 1, the hydraulic telescopic rod 210 is telescopically sleeved in the grooves 209, one side of the surface of the hydraulic telescopic rod 210 is correspondingly connected with the surface position of the set push plate 204, and the hydraulic telescopic rod 210 drives the push plate 204 to slide and be clamped to the two sides of the surface of the positioning plate 203 through the set hydraulic device 201.
The clamping unit comprises a bearing 202, a positioning plate 203, a push plate 204, a stop block 205, a reset spring rod 206, a sliding plate 207 and a clamping plate 208, wherein the bearing 202 is rotationally sleeved at the center position of the top surface of the supporting plate 1, the positioning plate 203 is fixedly clamped on the top surface of the bearing 202, the clamping plate 208 is provided with four clamping plates 208 in an L shape, the four clamping plates 208 are correspondingly clamped around the surface of the positioning plate 203 through the set reset spring rod 206 and the sliding plate 207, the positioning plate 203 rotates at the center position of the top surface of the supporting plate 1 through the set bearing 202, the push plate 204 is movably mounted on the left side and the right side of the surface of the positioning plate 203, the stop block 205 is fixedly mounted at the center position of the surface of the push plate 204, the reset spring rod 206 is movably mounted on the left side and the right side of the surface of the stop block 205, the sliding plate 207 is slidingly sleeved on the top surface of the reset spring rod 206, and the clamping plate 208 is fixedly mounted on the top surface of the sliding plate 207.
The support plate 1 comprises a guide rail 101, a driving motor 102, support columns 103 and rotating gears 104, wherein the guide rail 101 is fixedly arranged on two sides of the bottom surface of the support plate 1, the rotating gears 104 are meshed with the surface of the guide rail 101, the driving motor 102 is fixedly arranged at the center of the bottom surface of the support plate 1, and the support columns 103 are movably arranged around the bottom surface of the support plate 1.
According to the utility model, when the hydraulic device 201 is started, the hydraulic telescopic rod 210 is arranged to stretch and retract on the surface of the groove 209 to drive the push plate 204 to synchronously slide, so that the four clamping plates 208 are clamped with the aircraft parts placed on the top surface of the positioning plate 203, meanwhile, the reset spring rod 206 and the sliding plate 207 can be used for adjusting the positions of the four clamping plates 208 again, the aircraft parts with different sizes can be effectively adjusted, the operation is convenient and simple, the positioning plate 203 can be driven by the arranged bearing 202 to rotate, the angle of the aircraft parts can be conveniently adjusted by a worker, the quick installation groove of the aircraft parts can be conveniently and simply carried out by the worker, the sliding adjustment on the position of the push plate 204 can be conveniently and simply carried out by the worker, the clamping plates 208 are effectively clamped with the aircraft parts placed on the surface of the positioning plate 203, the driving motor 102 is started, the rotating rod is rotated, the rotating gear 104 can be further driven to operate, the whole support plate 1 can be driven to be adjusted and moved on the top surface of the guide rail 101 under the action of the meshing teeth, the whole support plate 1 is prevented from being manually moved by the worker, and the work efficiency of assembling the parts is improved.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Claims (7)
1. The utility model provides an aircraft parts assembly is with removing support positioner, includes backup pad (1) and positioning mechanism (2), its characterized in that: the positioning mechanism (2) is movably mounted on the top surface of the supporting plate (1), the positioning mechanism (2) comprises an adjusting unit and a clamping unit, and the adjusting unit and the clamping unit are arranged on the left side and the right side of the top surface of the supporting plate (1).
2. The mobile support positioning device for aircraft component assembly according to claim 1, wherein: the adjusting unit comprises a hydraulic device (201) and a hydraulic telescopic rod (210), wherein the hydraulic device (201) is fixedly arranged on the left side and the right side of the top surface of the supporting plate (1), grooves (209) are formed in the left side and the right side of the surface of the supporting plate (1), and the hydraulic telescopic rod (210) is in telescopic sleeve connection with the inside of the grooves (209).
3. The mobile support positioning device for aircraft component assembly according to claim 1, wherein: the clamping unit comprises a bearing (202), a positioning plate (203), a push plate (204), a stop block (205), a reset spring rod (206), a sliding plate (207) and a clamping plate (208), wherein the bearing (202) is rotationally sleeved on the center position of the top surface of the supporting plate (1), the positioning plate (203) is fixedly clamped on the top surface of the bearing (202), the push plate (204) is movably mounted on the left side and the right side of the surface of the positioning plate (203), the stop block (205) is fixedly mounted on the center position of the surface of the push plate (204), the reset spring rod (206) is movably mounted on the left side and the right side of the surface of the stop block (205), the sliding plate (207) is slidingly sleeved on the top surface of the reset spring rod (206), and the clamping plate (208) is fixedly mounted on the top surface of the sliding plate (207).
4. The mobile support positioning device for aircraft component assembly according to claim 1, wherein: the support plate (1) comprises a guide rail (101), a driving motor (102), support columns (103) and rotating gears (104), wherein the guide rail (101) is fixedly installed on two sides of the bottom surface of the support plate (1), the rotating gears (104) are meshed with the surface of the guide rail (101), the driving motor (102) is fixedly installed at the center position of the bottom surface of the support plate (1), and the support columns (103) are movably installed around the bottom surface of the support plate (1).
5. A mobile support positioning device for the assembly of aircraft components according to claim 2, characterized in that: one side of the surface of the hydraulic telescopic rod (210) is correspondingly connected with the surface position of the push plate (204), and the hydraulic telescopic rod (210) drives the push plate (204) to slide and be clamped to two sides of the surface of the positioning plate (203) through the arranged hydraulic device (201).
6. A mobile support positioning device for the assembly of aircraft components according to claim 3, characterized in that: the four clamping plates (208) are arranged in total, the four clamping plates (208) are L-shaped, the four clamping plates (208) are correspondingly clamped around the surface of the positioning plate (203) through reset spring rods (206) and sliding plates (207) which are arranged, and the positioning plate (203) rotates at the center position of the top surface of the supporting plate (1) through bearings (202) which are arranged.
7. The mobile support positioning device for aircraft component assembly according to claim 4, wherein: the supporting plate (1) slides left and right on the top surface of the supporting column (103) through the arranged guide rail (101) and the rotating gear (104).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322700892.3U CN220786145U (en) | 2023-10-09 | 2023-10-09 | Mobile supporting and positioning device for aircraft component assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322700892.3U CN220786145U (en) | 2023-10-09 | 2023-10-09 | Mobile supporting and positioning device for aircraft component assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220786145U true CN220786145U (en) | 2024-04-16 |
Family
ID=90654362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322700892.3U Active CN220786145U (en) | 2023-10-09 | 2023-10-09 | Mobile supporting and positioning device for aircraft component assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220786145U (en) |
-
2023
- 2023-10-09 CN CN202322700892.3U patent/CN220786145U/en active Active
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