A kind of aircraft special-shaped parts clamping auxiliary device and clamping method

An auxiliary device and special-shaped technology, which is applied to metal processing mechanical parts, positioning devices, clamping and other directions, can solve the problems of difficult clamping and processing, affecting processing accuracy, low processing efficiency, etc., to improve cutting accuracy, extend the Service life, the effect of stable overall structure

Active Publication Date: 2022-08-09
四川仨川航空科技股份有限公司
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Problems solved by technology

[0002] At present, in the machining of small-volume special-shaped parts of aircraft, special-shaped special-shaped parts that are difficult to clamp are generally processed by custom-made special tooling, multiple clamping through three-axis CNC equipment, or high-end CNC machine tools such as five-axis. For parts with special shapes that are difficult to clamp, different sizes, and thin wall thickness, the difficulty of clamping and processing is often greater, the processing cycle is long, and the technical requirements are high. A little carelessness will affect the processing accuracy or even be scrapped. parts, resulting in increased costs and inefficient processing

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  • A kind of aircraft special-shaped parts clamping auxiliary device and clamping method

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[0033] The specific embodiments of the present invention are described below to facilitate those skilled in the art to understand the present invention, but it should be clear that the present invention is not limited to the scope of the specific embodiments. For those skilled in the art, as long as various changes Such changes are obvious within the spirit and scope of the present invention as defined and determined by the appended claims, and all inventions and creations utilizing the inventive concept are within the scope of protection.

[0034] like figure 1 As shown, the aircraft special-shaped parts clamping auxiliary device of this scheme includes a cylindrical rotating body 4, and the two ends of the rotating body 4 are respectively provided with cylindrical clamping ends 15 and fixed ends 10. The clamping end 15 and the fixed end 10 It is coaxial with the rotary body 4; the clamping end 15 is fixed on the chuck 1 of the machine tool, and the fixed end 10 is mounted on...

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Abstract

The invention discloses an auxiliary device for clamping special-shaped parts of an aircraft and a clamping method thereof, which comprises a cylindrical rotating body, two ends of the rotating body are respectively provided with cylindrical clamping ends and fixed ends; The surface on one side of the end is provided with two planes. The two planes are symmetrical with the axis of the revolving body. The clamping surface is provided with several screw holes, and both ends of the clamping surface are provided with fixed bosses. Two bolt holes are provided on the fixed boss, and pin holes are set between the two bolt holes. The clamping method includes steps S1-S14. By designing different stations on the same rotary body, the invention can assist CNC machine tools to process aircraft special-shaped and difficult-to-machine parts, avoid multiple clamping and the use of special tooling in the processing process, improve processing efficiency, and ensure the size of the parts. Accuracy and Geometric Accuracy.

Description

technical field [0001] The invention relates to the technical field of aircraft special-shaped parts processing, in particular to an aircraft special-shaped part clamping auxiliary device and a clamping method thereof. Background technique [0002] At present, in the machining of small-volume special-shaped parts of aircraft, customized special tooling is generally used for special-shaped parts that are difficult to clamp, and three-axis CNC equipment is used for multiple clamping, or high-end CNC machine tools such as five-axis are used for processing: and For special-shaped parts that are difficult to clamp, different in size, and thin in wall thickness, the clamping difficulty and processing difficulty are often greater, the processing cycle is long, and the technical requirements are high. A little carelessness will affect the processing accuracy or even scrap it parts, resulting in rising costs and inefficiencies in processing. SUMMARY OF THE INVENTION [0003] In vi...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23Q3/06
CPCB23Q3/062Y02T50/40
Inventor 郭仕华徐飞何博涛冉从德徐攀
Owner 四川仨川航空科技股份有限公司
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