Aero-engine conduit conical surface coloring detection device and detection method

An aero-engine and detection method technology, applied in the direction of mechanical measuring devices, measuring devices, mechanical devices, etc., can solve problems such as incomplete fit, low qualified rate of pipe end cone surface coloring inspection, and large influence of human factors, etc., to achieve Improve the pass rate, ensure the effect of coloring inspection and pass rate, and the effect of accurate coloring effect

Inactive Publication Date: 2020-09-08
AECC AERO SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

This method is greatly affected by human factors
At the same time, after the cone surface is formed, there is a small amount of springback. Under the action of a relatively small manual gripping force, the angle of the cone surface of the pipe end and the taper of the coloring gauge cannot be completely fitted, resulting in a low pass rate of the pipe end cone surface coloring inspection.

Method used

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  • Aero-engine conduit conical surface coloring detection device and detection method
  • Aero-engine conduit conical surface coloring detection device and detection method

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Embodiment

[0023] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. The components of the embodiments of the invention generally described and illustrated in the figures herein may be arranged and designed in a variety of different configurations.

[0024] Accordingly, the following detailed description of the embodiments of the invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely represents selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art wi...

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Abstract

The invention discloses an aero-engine conduit conical surface coloring detection device and detection method, wherein the detection device comprises a workload gauge, a detection conical surface arranged at the front end of the workload gauge, a clamping part arranged at the rear end of the workload gauge, a detection thread arranged on the workload gauge and located between the detection conicalsurface and the clamping part, and a detection gauge matched with the workload gauge; the detection conical surface is the same as a detected part in terms of conicity. The coloring detection deviceis convenient to operate and good in reliability, and effectively solves the coloring inspection problem of the sealing conical surface of the pipe end. The coloring inspection effect and the percentof pass of a pipe end sealing conical surface are guaranteed, powerful verification is provided for the sealing performance of the guide pipe assembly, and high use value is achieved.

Description

technical field [0001] The invention relates to the field of Hankong engines, in particular to an aeroengine duct tapered surface coloring detection device and detection method. Background technique [0002] The engine ducts are all over the engine body, conveying various fluids, known as the engine "vessels". Therefore, the sealing performance of the pipe end is extremely important. After the tapered surface of the pipe end seal is formed, coloring inspection must be carried out on the tapered surface to verify the forming quality of the tapered surface. The structure of the traditional cone coloring gauge is a 74° outer cone head structure. The colorant is evenly applied to the outer cone surface, and the parts and the coloring gauge are manually held to inspect the cone surface by hand. This method is greatly affected by human factors. At the same time, after the cone surface is formed, there is a small amount of springback. Under the action of a relatively small manua...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B5/00G01B5/02G01B5/20
CPCG01B5/003G01B5/025G01B5/20
Inventor 李强陈海筠任相杰陈立牟青杜爽
Owner AECC AERO SCI & TECH CO LTD
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