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Fixing device for detection lever of engine borescope

A fixed device and hole detector technology, which is applied to measuring devices, instruments, measuring instrument components, etc., can solve the problems of inconsistent hole detector probe positions, reduce the engine safety factor, affect the blade detection results, etc., to improve the detection efficiency. , reduce labor costs and improve accuracy

Active Publication Date: 2019-12-03
AECC AVIATION POWER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the instability of the manual hand-held method, the position of the borescope probe is inconsistent during the detection process, which affects the detection results of the blade and reduces the safety factor of the engine
At the same time, the hand-held fixing method of the hole probe rod increases the labor cost in the detection process and reduces the detection efficiency

Method used

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  • Fixing device for detection lever of engine borescope
  • Fixing device for detection lever of engine borescope
  • Fixing device for detection lever of engine borescope

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Embodiment Construction

[0046] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Obviously, the described embodiments are part of the embodiments of the present invention, not all of them. the embodiment. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0047] Such as figure 1 and figure 2 As shown, as a preferred embodiment of the present invention, a fixing device for a probe rod of an engine borescope includes a probe rod fixing sleeve 1, a first screw sleeve 2, a top lock 3, a fixing sleeve limit pin 4, The second screw sleeve 5 and the clamping mechanism 6, the fixed sleeve 1 of the probe rod, the first screw sleeve 2 and th...

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PUM

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Abstract

The invention discloses a fixing device for a detection lever of an engine borescope, thereby effectively solveing problems existing in existing aero-engine borescope detection. The fixing device hasadvantages of small tool number and simple structure; and the labor cost in the detection process can be effective saved and the detection efficiency can be improved. A first threaded sleeve and a second threaded sleeve rotate to clamp each other; a first clamping plate and a second clamping plate clamp a detection lever; and three groups of jacking locks adjust the position of the detection leverslightly. While the fixation of the detection lever is ensured, the operation difficulty is reduced. With the clamp, the engine detection efficiency can be improved, the labor cost in the detection process can be lowered, and the economic benefit can be increased.

Description

technical field [0001] The invention belongs to the technical field of engine borescope, and in particular relates to a fixing device for a probe rod of an engine borescope. Background technique [0002] With the development of aviation technology, the internal structure of the engine has become more and more complex and precise. In order to ensure safe flight, the non-destructive testing technology of the engine is becoming more and more important. At present, in the in-situ non-destructive testing of engines assisted by a borescope, the control of the probe rod of the borescope is fixed manually. Due to the instability of the manual hand-holding method, the position of the borescope probe is inconsistent during the detection process, which affects the detection results of the blade and reduces the safety factor of the engine. At the same time, the hand-held fixing method of the hole probe probe increases the labor cost in the detection process and reduces the detection ef...

Claims

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Application Information

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IPC IPC(8): G01D11/30
CPCG01D11/30
Inventor 侯飞龙张新冬李晨许立君张义德刘金凤蒲海龙杜家燕
Owner AECC AVIATION POWER CO LTD
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