Self-adaption absorptive clamping device of airplane skin

A technology for aircraft skinning and clamping devices, which is applied in the direction of clamping devices, positioning devices, clamping, etc., can solve the problem of unable to adjust the adsorption position adaptively due to skin forming errors, and meet the requirements of low cost and reduced component accuracy , The effect of high adsorption success rate

Active Publication Date: 2015-05-27
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0003] Aiming at the problem that the prior art cannot adaptively adjust the adsorption position according to th

Method used

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  • Self-adaption absorptive clamping device of airplane skin
  • Self-adaption absorptive clamping device of airplane skin
  • Self-adaption absorptive clamping device of airplane skin

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[0035] Specific implementation method

[0036] The present invention will be further described below with reference to the accompanying drawings and embodiments, but the present invention is not limited to the embodiments.

[0037] A skin-adaptive adsorption and clamping device is suitable for clamping the skins of various shapes and sizes of aircraft, and includes a frame A, a bent frame B and an adaptive adsorption column C. like figure 1 The upper and lower beams of the frame are respectively equipped with racks; the bent frame is located between the upper and lower beams, the upper and lower parts of the bent frame are meshed with the rack through corresponding gears, and the upper and lower ends of the bent frame are respectively equipped with driving gears to rotate to drive the bent frame The motor I moves in the horizontal direction on the frame, and the synchronous movement of the two motors I can make the bent frame move along the rack on the frame, and the bent...

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Abstract

The invention discloses a self-adaption absorptive clamping device of an airplane skin. The clamping device is characterized by comprising a frame, bent frames and self-adaption absorptive columns, wherein the upper and lower beams of the frame are provided with racks, and the two ends of each bent frame are arranged on the racks and can move along the racks; each bent frame is internally provided with a linear guide rail in a vertical direction, and each group of bent frames is provided with a certain amount of self-adaption adsorption columns and can move along the linear guide rail respectively; each adsorption column comprises a rotary vacuum chuck, a self-adaption telescopic link and a scale column. According to the clamping provided by the invention, the layout of the bent frames and the self-adaption absorptive columns can be adjusted by aiming at the shape of the skin, the absorption height can be adjusted by the scale columns and the self-adaption telescopic links, and the skin can be absorbed by the vacuum suckers; furthermore, the clamping device is applicable to clamping the skins of various shapes and sizes, the comprehensive cost can be reduced, the frock preparation period and production period can be shortened, and the production efficiency can be improved.

Description

technical field [0001] The invention relates to a clamp, in particular to an aircraft skin clamping device, in particular to an aircraft skin self-adaptive adsorption and clamping device. Background technique [0002] Aircraft skin is the outer part that constitutes the aerodynamic shape of the aircraft. It has large size, many types, complex and diverse shapes, and small batches. It is an important part to ensure the aerodynamic performance of the aircraft. In the process of aircraft manufacturing, it is necessary to carry out various processing on the skin. Due to the poor rigidity and small thickness of the skin, it is easy to deform during processing. The existing skin processing usually adopts a multi-point flexible adsorption clamping system. When the skin is formed, certain errors will occur. The existing multi-point flexible adsorption devices usually use motors or hydraulic pressure to precisely control the adsorption position, and locate the adsorption points accor...

Claims

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Application Information

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IPC IPC(8): B23Q3/08
CPCB23Q3/088B23Q2703/10
Inventor 李迎光郝小忠陈耿祥周鑫
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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