CN220518575U - Aircraft hanging beam mounting vehicle - Google Patents
Aircraft hanging beam mounting vehicle Download PDFInfo
- Publication number
- CN220518575U CN220518575U CN202322085065.8U CN202322085065U CN220518575U CN 220518575 U CN220518575 U CN 220518575U CN 202322085065 U CN202322085065 U CN 202322085065U CN 220518575 U CN220518575 U CN 220518575U
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- platform
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- vehicle body
- install
- lifting
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- 230000001105 regulatory effect Effects 0.000 claims abstract description 15
- 238000009434 installation Methods 0.000 description 11
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 210000001503 joint Anatomy 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Abstract
The utility model discloses an aircraft hanging beam mounting vehicle which comprises an AGV moving vehicle body, wherein two pairs of Mecanum wheels are arranged at the lower end of the AGV moving vehicle body, an electric cabinet and a battery box are respectively arranged at the front end and the rear end above the AGV moving vehicle body, a lifting scissor fork is arranged on the AGV moving vehicle body and between the electric cabinet and the battery box, a supporting platform is arranged at the upper end of the lifting scissor fork, a pitching fund regulating platform is arranged on the supporting platform, and a longitudinal fund regulating platform is arranged on the driving end of the pitching fund regulating platform.
Description
Technical Field
The utility model relates to the technical field of aircraft hanging beam installation, in particular to an aircraft hanging beam installation vehicle.
Background
In the process of docking and hanging the external stores of the aircraft, various supporting equipment is required to complete operation tasks, due to different heights of the aircraft, various supporting equipment has limited movable space under the aircraft, but the adjustable range in the required space is large when the various external stores are hung, so that a bullet hanging vehicle with smaller vehicle body occupation is required, and the adjustable range of six degrees of freedom for the external stores are operated in the space is large, so that the bullet hanging vehicle can adapt to the requirements of various external stores hung by the aircraft. Most of the common auxiliary installation devices in the market depend on a large amount of experience, meanwhile, the auxiliary installation devices are required to be installed cooperatively by multiple people, the automation degree is too low, and the manpower and material resources are excessively consumed for installation.
Disclosure of Invention
Aiming at the defects of the prior art, the utility model provides an aircraft hanging beam installation vehicle, which solves the problem that most of the existing installation auxiliary devices are inconvenient to install and use in a cooperation way by multiple persons.
In order to achieve the above purpose, the utility model is realized by the following technical scheme: the utility model provides an aircraft hanging beam installs car, includes the AGV removes the automobile body, the lower extreme that the AGV removed the automobile body is equipped with two pairs of Mecanum's wheel, electric cabinet and battery box are installed respectively at both ends around the AGV removes the automobile body top, the AGV removes on the automobile body and be located install between electric cabinet and the battery box and lift and cut the fork, lift and cut the upper end of fork and install supporting platform, install every single move transfer platform on the supporting platform, install vertical transfer platform on every single move transfer platform's the drive end, install horizontal transfer platform on vertical transfer platform's the drive end, install mounting fixture on horizontal transfer platform's the drive end.
Preferably, a lifting electric cylinder is movably mounted on the AGV moving vehicle body, and the telescopic end of the lifting electric cylinder is movably connected with the lifting scissor fork.
Preferably, a sliding groove is formed in one end of the supporting platform, one side of the upper end of the lifting scissor is slid in the sliding groove, and the other side of the upper end of the lifting scissor is rotatably connected with the other end of the supporting platform.
Advantageous effects
The utility model provides an aircraft hanging beam mounting vehicle, which has the following beneficial effects:
according to the design, the Mecanum wheels are arranged below the AGV moving vehicle body, lifting scissors capable of lifting are arranged above the AGV moving vehicle body, three kinds of pitch angle adjusting platforms capable of adjusting the pitch angle, the horizontal angle and the longitudinal angle are arranged on the lifting scissors, the whole AGV moving vehicle body is enabled to have multi-degree-of-freedom adjusting capability, the control precision is high, and single person operation installation can be achieved.
Drawings
Fig. 1 is a perspective view of the present utility model.
Fig. 2 is a front view of the lifting fork of the present utility model when it is raised.
Fig. 3 is a front view of the lifting fork of the present utility model after being recovered.
Fig. 4 is a front view of an end elevation of a pitch control platform of the present utility model.
Figure 5 is a side elevation view of a pitch control platform of the present utility model raised sideways.
FIG. 6 is a schematic diagram of the adjustment of the longitudinal funding platform of the present utility model.
FIG. 7 is a schematic diagram of the horizontal funding platform adjustment of the present utility model.
In the figure: 1. AGVs move the vehicle body; 2. mecanum wheel; 3. an electric control box; 4. a battery box; 5. lifting the scissor fork; 6. a support platform; 7. a pitching fund adjustment platform; 8. a longitudinal fund adjustment platform; 9. a horizontal financing platform; 10. a fixing clamp; 11. and lifting the electric cylinder.
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. 1-7, the present utility model provides a technical solution: the aircraft hanging beam mounting vehicle comprises an AGV moving vehicle body 1, wherein two pairs of Mecanum wheels 2 are arranged at the lower end of the AGV moving vehicle body 1, an electric cabinet 3 and a battery box 4 are respectively arranged at the front end and the rear end above the AGV moving vehicle body 1, a lifting scissor 5 is arranged between the electric cabinet 3 and the battery box 4 and on the AGV moving vehicle body 1, a supporting platform 6 is arranged at the upper end of the lifting scissor 5, a pitching fund regulating platform 7 is arranged on the supporting platform 6, a longitudinal fund regulating platform 8 is arranged at the driving end of the pitching fund regulating platform 7, a horizontal fund regulating platform 9 is arranged at the driving end of the longitudinal fund regulating platform 8, and a fixing clamp 10 is arranged at the driving end of the horizontal fund regulating platform 9;
pitch funding platform 7 is a platform that can adjust front, back, left, right, depression angle or elevation angle, as shown in fig. 4 and 5;
the longitudinal financing platform 8 is shown in fig. 6, and can adjust the horizontal direction of the upper horizontal financing platform 9;
the horizontal financing platform 9 is shown in fig. 7, and can adjust the position of the upper fixing clamp 10;
the fixing clamp 10 is a conventional mature technology, and has a structure shown in fig. 1, mainly comprises a bottom plate and an L-shaped fixing plate, and is fixed by bolting, so that the specific structure thereof is not described in detail;
the three kinds of financing platforms (longitudinal, horizontal and pitching) are used in the patent, and the adjusting mode belongs to the known technology, so that the specific structure of the three kinds of financing platforms is not described in detail, the three kinds of financing platforms are operated by utilizing the electric cabinet 3, the power source is provided by the battery box 4, and the connecting modes are all electrically controlled connection by leads, and belong to the conventional connecting modes.
Further, a lifting electric cylinder 11 is movably mounted on the AGV moving vehicle body 1, and the telescopic end of the lifting electric cylinder 11 is movably connected with the lifting scissor fork 5.
Further, a chute is formed at one end of the supporting platform 6, one side of the upper end of the lifting scissor 5 slides in the chute, and the other side of the upper end of the lifting scissor is rotatably connected with the other end of the supporting platform 6.
The components in this case are connected in sequence by a person skilled in the art, and specific connection and operation sequence should be referred to the following working principle, and the detailed connection means are known in the art, and the following working principle and process are mainly described.
Examples: when the device is used, firstly, the aircraft hanging beam is hoisted to the fixing clamp 10, then the lifting electric cylinder 11 is controlled, the lifting of the lifting scissor fork 5 is controlled by utilizing the lifting electric cylinder 11, then the fixing clamp 10 at the upper end is adjusted, the aircraft hanging beam is lifted to a certain height, then the elevation angle of the pitching adjustment platform 7 is controlled by the electric cabinet 3, the rotation angle of the longitudinal adjustment platform 8 is controlled, the position of the fixing clamp 10 is adjusted by the horizontal adjustment platform 9, and finally the hanging point butt joint is completed, so that the installation is completed. After the installation is completed, the fixture fixing fixture 10 is loosened, the trolley is withdrawn from the installation area, the completion state is reset, and the whole device can be operated by a single person, so that the device is simple and practical.
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 (3)
1. The utility model provides an aircraft hanging beam installs car, includes AGV mobile vehicle body (1), the lower extreme of AGV mobile vehicle body (1) is equipped with two pairs of Mecanum's wheel (2), electric cabinet (3) and battery box (4) are installed respectively at the front and back both ends of AGV mobile vehicle body (1) top, a serial communication port, AGV mobile vehicle body (1) is last and be located install between electric cabinet (3) and battery box (4) and lift and cut fork (5), lift and cut the upper end of fork (5) and install supporting platform (6), install every single move fund regulating platform (7) on supporting platform (6), install vertical fund regulating platform (8) on every single move the drive end of fund regulating platform (7), install horizontal fund regulating platform (9) on the drive end of vertical fund regulating platform (8), install mounting fixture (10) on the drive end of horizontal fund regulating platform (9).
2. The aircraft hanging beam mounting vehicle according to claim 1, wherein a lifting electric cylinder (11) is movably mounted on the AGV moving vehicle body (1), and a telescopic end of the lifting electric cylinder (11) is movably connected with the lifting scissor fork (5).
3. The aircraft hanging beam mounting vehicle according to claim 1, wherein a chute is formed at one end of the supporting platform (6), one side of the upper end of the lifting scissor (5) slides in the chute, and the other side is rotatably connected with the other end of the supporting platform (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322085065.8U CN220518575U (en) | 2023-08-04 | 2023-08-04 | Aircraft hanging beam mounting vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322085065.8U CN220518575U (en) | 2023-08-04 | 2023-08-04 | Aircraft hanging beam mounting vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220518575U true CN220518575U (en) | 2024-02-23 |
Family
ID=89939610
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322085065.8U Active CN220518575U (en) | 2023-08-04 | 2023-08-04 | Aircraft hanging beam mounting vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220518575U (en) |
-
2023
- 2023-08-04 CN CN202322085065.8U patent/CN220518575U/en active Active
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