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Adjusting device for aircraft wing assembly

A technology for adjusting devices and wings, which is applied in aircraft assembly and other directions, can solve problems such as damaged aircraft wing structures, potential safety hazards in aircraft, and large differences in wing volume and height, so as to achieve fast and efficient operation and reduce handling The number of times, the effect of facilitating transportation and transfer

Active Publication Date: 2021-07-02
XIAN AERONAUTICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The volume and height of the wings of these aircraft are quite different. When transferring and assembling the wings, it is easy to damage the wing structure of the aircraft due to improper operation, resulting in potential safety hazards for the aircraft.

Method used

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  • Adjusting device for aircraft wing assembly
  • Adjusting device for aircraft wing assembly
  • Adjusting device for aircraft wing assembly

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0044] Such as Figure 1-4 As shown, a kind of adjusting device for aircraft wing assembly comprises a mounting frame base plate 1 and a lifting frame base plate 2, the top of the mounting frame base plate 1 is provided with an operating platform 4 through a support column 3, and the bottom of the operating platform 4 is provided with There is a motor frame 7, the motor frame 7 is provided with a motor 6, the top of the operating platform 4 is provided with a base 5, the lower symmetrical center of the base 5 is fixedly connected with one end of the output shaft of the motor 6, and is controlled by the motor 6 The base 5 rotates to adjust the direction of the adjusting device when the aircraft wing is assembled. The upper end of the base 5 is sleeved with an operation panel 10, and at least three groups of mutually symmetrical hydraulic cylinders 11 are arranged between the operation panel 10 and the base 5. By adjusting the lifting of the hydraulic cylinders 11, the aircraft ...

Embodiment 2

[0055] Such as Figure 1-4 As shown, a kind of adjusting device for aircraft wing assembly comprises a mounting frame base plate 1 and a lifting frame base plate 2, the top of the mounting frame base plate 1 is provided with an operating platform 4 through a support column 3, and the bottom of the operating platform 4 is provided with There is a motor frame 7, the motor frame 7 is provided with a motor 6, the top of the operating platform 4 is provided with a base 5, the lower symmetrical center of the base 5 is fixedly connected with one end of the output shaft of the motor 6, and is controlled by the motor 6 The base 5 rotates to adjust the direction of the aircraft wing; the upper end of the base 5 is sleeved with an operating panel 10, and at least three groups of mutually symmetrical hydraulic cylinders 11 are arranged between the operating panel 10 and the base 5. Adjust the hydraulic cylinder 11 to realize the adjustment of the angle of inclination of the aircraft wing;...

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PUM

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Abstract

The invention discloses an adjustment device for aircraft wing assembly, which comprises a bottom plate of a mounting frame and a bottom plate of a lifting frame, an operating platform is arranged above the bottom plate of the mounting frame through a support column, and a motor frame is arranged below the operating platform, so that The motor frame is provided with a motor, and the device can directly transport the aircraft wing to the operating platform of the installation frame by using the transport vehicle through the lifting frame, reducing the number of handling of the aircraft wing, reducing the probability of damage, and realizing the maintenance of the aircraft wing. The whole operation process is fast and efficient; the aircraft wing on the operation panel is kept stable; the installation frame and the lifting frame are connected by a lock, which is convenient for disassembly and assembly, and is conducive to the transportation and transfer of the device.

Description

technical field [0001] The invention belongs to the technical field of tooling for assembling wings, and in particular relates to an adjusting device for assembling aircraft wings. Background technique [0002] The aircraft wing is one of the important parts of the aircraft and is installed on the fuselage. Its main function is to generate lift. At the same time, ammunition warehouses and fuel tanks can be arranged in the wings, and the landing gear can be stored during flight. In addition, flaps to improve take-off and landing performance and ailerons for lateral manipulation of the aircraft are installed on the wings, and some devices are also equipped with slats and other lift-increasing devices on the leading edge of the wings. [0003] During the assembly process of the aircraft wing, it is necessary to strictly ensure the installation connection size and tolerance range of each component between the aircraft wing and the fuselage. However, due to the large number of ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor 赵东平郭温张建华侯伟
Owner XIAN AERONAUTICAL UNIV
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