CN223989479U - A horizontal support device for aircraft components - Google Patents
A horizontal support device for aircraft componentsInfo
- Publication number
- CN223989479U CN223989479U CN202520150056.9U CN202520150056U CN223989479U CN 223989479 U CN223989479 U CN 223989479U CN 202520150056 U CN202520150056 U CN 202520150056U CN 223989479 U CN223989479 U CN 223989479U
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- Prior art keywords
- limiting
- block
- clamping
- moving
- supporting
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Abstract
本实用新型公开了一种航空器零部件水平支撑装置，包括支撑台和支撑板，支撑板底部设有球头，支撑台上设有球套，球头底部设有支撑杆和铅锤，支撑台上设有多个支撑螺栓，支撑板上对称设有移动槽，移动槽上滑动设有移动块，移动块上设有连接装置和夹持架，连接装置包括连接块，连接块上转动设有卡接块，卡接块上设有限位槽，限位槽上滑动设有限位板和限位杆，连接块上设置有限位孔，通过球头和铅锤连接，在铅锤的重力作用下，带动支撑板处于水平状态，通过支撑螺栓对支撑板进行水平支撑，进而使支撑板对航空器零部件进行水平支撑，通过限位板上的限位杆与连接块上的限位孔配合，固定卡接块的位置，进而对夹持架和移动块进行安装。
This utility model discloses a horizontal support device for aircraft components, including a support platform and a support plate. The support plate has a ball head at its bottom, a ball sleeve on the support platform, a support rod and a plumb bob at the bottom of the ball head, and multiple support bolts on the support platform. The support plate has symmetrically arranged moving grooves, and moving blocks slide on the moving grooves. Each moving block has a connecting device and a clamping frame. The connecting device includes a connecting block, a locking block rotatably mounted on the connecting block, a limiting groove on the locking block, a limiting plate and a limiting rod sliding on the limiting groove, and a limiting hole on the connecting block. The device connects the ball head and the plumb bob. Under the gravity of the plumb bob, the support plate is brought to a horizontal position. The support bolts provide horizontal support for the support plate, thus providing horizontal support for the aircraft components. The limiting rod on the limiting plate engages with the limiting hole on the connecting block to fix the position of the locking block, thereby allowing the clamping frame and the moving block to be installed.
Description
Technical Field
The utility model relates to the technical field of aircrafts, in particular to a horizontal supporting device for parts of an aircraft.
Background
The aviation component manufacturing industry mainly refers to the manufacture of various components of an aviation aircraft, including the manufacture of components of an aircraft body, the manufacture of components of an aircraft engine, the manufacture of instruments, airborne equipment, hydraulic systems, accessories and the like, and does not include the assembly of components, the assembly of the aircraft engine, the assembly of the whole machine and the like, and when the production and the manufacture of the components of the aircraft are carried out, the components are required to be horizontally supported.
In the prior art, the operation panel of part of aircraft spare part processing is inconvenient to carry out leveling support, can lead to the spare part flatness error increase of processing, influence the assembly precision of spare part, if the operation panel straightness is not enough, the hole site of processing, guide rail etc. will not reach the design requirement, influence interchangeability and the functionality of spare part, the operation panel is uneven needs frequent adjustment equipment or relocation, waste a large amount of time, the position of clamping assembly is inconvenient for installation and position adjustment simultaneously, the assembly time of manual operation adjustment has been increased, work efficiency has been reduced.
Disclosure of utility model
(One) solving the technical problems
Aiming at the problems in the prior art, the utility model provides a horizontal supporting device for parts of an aircraft, which aims to solve the technical problems that an operation table is inconvenient to level and a clamping assembly is inconvenient to install and adjust in the prior art.
(II) technical scheme
In order to achieve the purpose, the horizontal supporting device for the aircraft parts comprises a supporting table and a supporting plate, wherein a ball head is arranged at the bottom of the supporting plate, a ball sleeve is arranged on the supporting table, a supporting rod is arranged at the bottom of the ball head, a plumb is arranged at the bottom of the supporting rod, a plurality of supporting bolts are arranged on the supporting table, moving grooves are symmetrically arranged on the supporting plate, moving blocks are slidably arranged on the moving grooves, connecting devices and clamping frames are arranged on the moving blocks, the connecting devices comprise connecting blocks, the connecting blocks are arranged on the moving blocks, clamping blocks are rotatably arranged on the connecting blocks, limiting grooves are formed in the clamping blocks, limiting plates are slidably arranged on the limiting grooves, limiting rods are symmetrically arranged on the limiting plates, and limiting holes matched with the limiting rods are formed in the connecting blocks.
The utility model is further arranged that a plurality of balls are rotatably arranged on the side wall of the ball sleeve, so that the ball head can conveniently rotate in the ball sleeve.
The ball sleeve is further provided with fastening bolts in symmetrical threaded connection, so that the positions of the ball sleeve and the ball head can be conveniently fixed.
The utility model is further characterized in that the supporting rod is provided with a supporting screw rod, the supporting rod is in threaded connection with the ball head through the supporting screw rod, and the supporting rod is conveniently connected with the ball head through the supporting screw rod.
The utility model is further characterized in that a moving screw rod is rotationally arranged in the moving groove, one end of the moving screw rod is provided with a moving motor, the moving screw rod is in threaded connection with the moving block, and the moving motor drives the moving screw rod to rotate so as to drive the moving block and the clamping frame to move.
The clamping cylinders are symmetrically arranged on the clamping frame, the clamping plates are arranged at the output ends of the clamping cylinders, and the clamping plates are driven to move through the clamping cylinders, so that the aircraft parts can be clamped and supported conveniently.
The utility model is further characterized in that the clamping plate is provided with a clamping block, the clamping frame is provided with a clamping groove, and the movement direction of the clamping plate is limited by the cooperation of the clamping block and the clamping groove.
The utility model is further arranged that a limiting spring is arranged between the limiting plate and the limiting groove, and one end of the limiting plate is provided with a limiting handle, so that the position of the limiting plate can be conveniently moved.
(III) beneficial effects
Compared with the prior art, the utility model provides the horizontal supporting device for the parts of the aircraft, which has the following beneficial effects:
1. Through bulb and plumb connection, under the action of the gravity of plumb, drive the backup pad and be in the horizontality, through the relative position of fastening bolt fixed bulb and ball cover, carry out horizontal support to the backup pad through supporting bolt, and then make the backup pad be in horizontal support position, be convenient for carry out horizontal support to aircraft spare part.
2. The movable screw is driven to rotate through the movable motor, the movable block is driven to move in the movable groove, the position of the clamping frame is adjusted, the clamping plate is driven to move through the clamping cylinder, and the aircraft parts are clamped and fixed conveniently.
3. Through the spacing hole cooperation on gag lever post on the limiting plate and the connecting block, the position of fixed joint piece, the position of fixed holder through the joint piece, and then be convenient for connect fixedly movable block and holder, improved the convenience of holder installation and dismantlement.
Drawings
FIG. 1 is a schematic view of the overall structure of a horizontal support device for aircraft parts in accordance with the present utility model;
FIG. 2 is a schematic cross-sectional view of a support table and a support plate according to the present utility model;
FIG. 3 is a schematic diagram of the cooperation structure of the support plate, the moving groove, the moving block and the moving screw in the present utility model;
FIG. 4 is a schematic diagram of the cooperation structure of the clamping frame, the clamping cylinder and the clamping plate in the utility model;
fig. 5 is a schematic cross-sectional view of the connecting device of the present utility model.
The device comprises a supporting table 1, a supporting plate 2, a supporting plate 3, a ball head 4, a ball sleeve 5, a supporting rod 6, a plumb, a 7, a supporting bolt 8, a moving groove 9, a moving block 10, a clamping frame 11, a connecting block 12, a clamping block 13, a limiting groove 14, a limiting plate 15, a limiting rod 16, a limiting hole 17, a ball, 18, a fastening bolt 19, a supporting screw rod 20, a moving screw rod 21, a moving motor 22, a clamping cylinder 23, a clamping plate 24, a clamping block 25, a clamping groove 26, a limiting spring 27 and a limiting handle.
Detailed Description
It should be noted that, without conflict, the embodiments of the present utility model and features of the embodiments may be combined with each other. The utility model will be described in detail below with reference to the drawings in connection with embodiments.
It is noted that all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs unless otherwise indicated.
In the present utility model, unless otherwise indicated, the terms "upper" and "lower" are used generally in the directions shown in the drawings or in the vertical, vertical or gravitational directions, and similarly, for convenience of understanding and description, the terms "left" and "right" are used generally in the directions shown in the drawings, and the terms "inner" and "outer" are used to refer to the inner and outer sides with respect to the outline of each component itself, but the terms of orientation are not intended to limit the present utility model.
Referring to fig. 1-5, a horizontal supporting device for parts of an aircraft comprises a supporting table 1 and a supporting plate 2, wherein a ball head 3 is arranged at the bottom of the supporting plate 2, a ball sleeve 4 is arranged on the supporting table 1, a supporting rod 5 is arranged at the bottom of the ball head 3, a plumb 6 is arranged at the bottom of the supporting rod 5, a plurality of supporting bolts 7 are arranged on the supporting table 1, a moving groove 8 is symmetrically arranged on the supporting plate 2, a moving block 9 is slidably arranged on the moving groove 8, a connecting device and a clamping frame 10 are arranged on the moving block 9, the connecting device comprises a connecting block 11, the connecting block 11 is arranged on the moving block 9, a clamping block 12 is rotatably arranged on the connecting block 11, a limiting groove 13 is arranged on the limiting groove 13, a limiting plate 14 is slidably arranged on the limiting groove, a limiting rod 15 is symmetrically arranged on the connecting block 11, a plurality of balls 17 are rotatably arranged on the side wall of the ball sleeve 4, a fastening bolt 18 is symmetrically and threadedly connected with the supporting rod 5, and the supporting rod 5 is slidably connected with the ball head 3 through the supporting bolt 19.
In this embodiment, when the leveling of the supporting plate 2 is performed, the plumb 6 and the supporting rod 5 are mounted on the ball head 3 through the supporting screw 19, the ball head 3 is driven to rotate in the ball sleeve 4, the rotating convenience is improved through the ball 17, the levelness of the supporting plate 2 is adjusted, after the adjustment is completed, the supporting height of the supporting bolt 7 is adjusted, the supporting plate 2 is at the horizontal height, the relative positions of the ball sleeve 4 and the ball head 3 are fixed through the fastening bolt 18, the clamping frame 10 is mounted on the moving block 9, the clamping frame 10 is sleeved on the connecting block 11, the limiting spring 26 is in a compressed state at this moment, the clamping block 12 is rotated, when the limiting rod 15 on the clamping block 12 is aligned with the limiting hole 16 of the connecting block 11, the limiting plate 14 drives the limiting rod 15 to extend into the limiting hole 16 under the elastic force of the limiting spring 26, the position of the clamping block 12 is fixed, the limiting handle 27 is pulled upwards when the clamping block 10 is dismounted, the limiting handle 27 drives the limiting plate 14 to compress the limiting spring 26, the limiting rod 15 is separated from the limiting hole 16, and the clamping block 12 can be dismounted when the clamping block 12 is aligned with the connecting block 11.
Referring to fig. 3-4, as an embodiment of the clamping frame 10, a moving screw 20 is rotationally arranged in a moving groove 8, a moving motor 21 is arranged at one end of the moving screw 20, the moving screw 20 is in threaded connection with a moving block 9, clamping cylinders 22 are symmetrically arranged on the clamping frame 10, a clamping plate 23 is arranged at the output end of the clamping cylinders 22, a clamping block 24 is arranged on the clamping plate 23, a clamping groove 25 is arranged on the clamping frame 10, a limiting spring 26 is arranged between a limiting plate 14 and the limiting groove 13, and a limiting lifting handle 27 is arranged at one end of the limiting plate 14.
More specifically, when carrying out the centre gripping to aircraft spare part, start movable motor 21, movable motor 21 drives and removes screw rod 20 rotation, and then drives movable block 9 and subtend removal in movable tank 8, adjusts the position of grip block 10, starts clamping cylinder 22, and clamping cylinder 22 drives grip block 23 and carries out the centre gripping fixed to spare part, through the cooperation of grip block 24 and grip slot 25, restricts the direction of movement of grip block 23, has improved the practicality of grip block 23.
In sum, when the whole equipment is used or operated, when the supporting plate 2 is leveled, the plumb 6 and the supporting rod 5 are installed on the ball head 3 through the supporting screw 19, the ball head 3 is driven to rotate in the ball sleeve 4, the rotating convenience is improved through the ball 17, the levelness of the supporting plate 2 is adjusted, after the adjustment is finished, the supporting height of the supporting bolt 7 is adjusted, the supporting plate 2 is at the horizontal height, the relative positions of the ball sleeve 4 and the ball head 3 are fixed through the fastening bolt 18, the clamping frame 10 is installed on the moving block 9, the clamping frame 10 is sleeved on the connecting block 11, the limiting spring 26 is in a compressed state at the moment, the clamping block 12 is rotated, when the limiting rod 15 on the clamping block 12 is aligned with the limiting hole 16 of the connecting block 11, the limiting plate 14 drives the limiting rod 15 to extend into the limiting hole 16 under the elastic force of the limiting spring 26, the position of the clamping block 12 is fixed, the limiting lifting handle 27 is pulled upwards when the clamping block 10 is disassembled, the limiting handle 27 drives the limiting plate 14 to compress the limiting spring 26, and the limiting rod 15 is separated from the limiting hole 16, and the clamping block 12 can be disassembled when the clamping block 10 is aligned with the connecting block 11.
When carrying out the centre gripping to aircraft spare part, start movable motor 21, movable motor 21 drives and removes screw rod 20 rotation, and then drives movable block 9 and move in the opposite direction in movable groove 8, adjusts the position of grip block 10, starts clamping cylinder 22, and clamping cylinder 22 drives grip block 23 and carries out the centre gripping to spare part fixedly, through the cooperation of grip block 24 and grip groove 25, restricts the direction of movement of grip block 23, has improved the practicality of grip block 23.
In all the above mentioned solutions, in which the connection between two components can be chosen according to the actual situation, welding, bolt-and-nut-mating connection, bolt-or-screw connection or other known connection means, which are not described in detail herein, where reference is made to a written fixed connection, the preferred consideration is welding, although embodiments of the 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 principle and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents;
In all the above mentioned schemes, the operation of the electric elements is controlled by the controller if not explicitly described, and because the equipment matched with the controller is common equipment, the control principle and the circuit connection of the equipment belong to the existing known and mature technology, and the electrical connection relation and the specific circuit structure of the equipment are not repeated here;
In all the above mentioned schemes, the motor can be matched with the speed reducer if actually needed, and the connection structure and the working principle between the motor and the speed reducer are the prior known technologies, and the utility model is not repeated.
Claims (8)
1. The utility model provides an aircraft parts horizontal support device, includes brace table (1) and backup pad (2), characterized by backup pad (2) bottom is equipped with bulb (3), be equipped with ball socket (4) on brace table (1), bulb (3) bottom is equipped with bracing piece (5), bracing piece (5) bottom is equipped with plumb (6), be equipped with a plurality of supporting bolts (7) on brace table (1), the symmetry is equipped with movable groove (8) on backup pad (2), the slip is equipped with movable block (9) on movable block (8), be equipped with connecting device and holder (10) on movable block (9), connecting device includes connecting block (11), connecting block (11) set up on movable block (9), the rotation is equipped with joint piece (12) on connecting block (11), be equipped with spacing groove (13) on spacing groove (13) and slide and be equipped with limiting plate (14), be equipped with gag lever post (15) on limiting plate (14), be provided with on connecting block (11) with spacing hole (16) with cooperation.
2. The horizontal support device for aircraft parts according to claim 1, wherein a plurality of balls (17) are rotatably provided on the side wall of the ball sleeve (4).
3. The horizontal support device for aircraft parts according to claim 1, wherein the ball sleeve (4) is symmetrically threaded with fastening bolts (18).
4. The horizontal supporting device for the aircraft parts, as set forth in claim 1, characterized in that the supporting rod (5) is provided with a supporting screw (19), and the supporting rod (5) is connected with the ball head (3) through the supporting screw (19) in a threaded manner.
5. The horizontal supporting device for the aircraft parts according to claim 1, wherein a moving screw (20) is rotatably arranged in the moving groove (8), one end of the moving screw (20) is provided with a moving motor (21), and the moving screw (20) is in threaded connection with the moving block (9).
6. The horizontal supporting device for the aircraft parts according to claim 1, wherein clamping cylinders (22) are symmetrically arranged on the clamping frame (10), and clamping plates (23) are arranged at the output ends of the clamping cylinders (22).
7. The horizontal support device for aircraft parts according to claim 6, wherein the clamping plate (23) is provided with a clamping block (24), and the clamping frame (10) is provided with a clamping groove (25).
8. The horizontal supporting device for the aircraft parts according to claim 1, wherein a limiting spring (26) is arranged between the limiting plate (14) and the limiting groove (13), and a limiting handle (27) is arranged at one end of the limiting plate (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202520150056.9U CN223989479U (en) | 2025-01-22 | 2025-01-22 | A horizontal support device for aircraft components |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202520150056.9U CN223989479U (en) | 2025-01-22 | 2025-01-22 | A horizontal support device for aircraft components |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN223989479U true CN223989479U (en) | 2026-03-13 |
Family
ID=99004672
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202520150056.9U Active CN223989479U (en) | 2025-01-22 | 2025-01-22 | A horizontal support device for aircraft components |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN223989479U (en) |
-
2025
- 2025-01-22 CN CN202520150056.9U patent/CN223989479U/en active Active
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