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Aircraft engine blade nondestructive flaw detection device

An aircraft engine, non-destructive testing technology, applied in the direction of measuring device, testing of mechanical components, testing of machine/structural components, etc., can solve the problems of low work efficiency, detail parts cannot be detected, etc., to achieve the effect of high work efficiency

Active Publication Date: 2022-05-13
CIVIL AVIATION FLIGHT UNIV OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, when the current aircraft engine blades are in use, the surface will be hindered by wind force, and there will be deep scratches on the surface, while the commonly used non-destructive testing devices can only detect large scratches or depressions on aircraft engine blades. The details cannot be detected, and the overall work efficiency is low. Therefore, we propose a non-destructive testing device for aircraft engine blades

Method used

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Embodiment Construction

[0032] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. 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.

[0033] Refer to the attached Figure 1-5, a non-destructive testing device for aircraft engine blades, including a cleaning mechanism 3 and a detection mechanism 4, the cleaning mechanism 3 includes an airbag telescopic rod 302, the top of the airbag telescopic rod 302 is inserted with a push rod frame 304, one side of the push rod frame 304 A fixed block frame 303 is clamped, and the surface of the fixed block frame 303 is provided with multiple groups of cle...

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Abstract

The invention discloses an aircraft engine blade nondestructive flaw detection device, and particularly relates to the field of aircraft engine blades, the aircraft engine blade nondestructive flaw detection device comprises a cleaning mechanism and a detection mechanism, the cleaning mechanism comprises an air bag telescopic rod, a push rod frame is inserted into the top end of the air bag telescopic rod, and a fixed clamping block frame is clamped to one side of the push rod frame; a plurality of groups of movable cleaning brush plates are arranged on the surface of the fixed clamping block frame, mounting holes for insertion are formed in the centers of the inner sides of the movable cleaning brush plates, and deflection rods are clamped to the two sides of the movable cleaning brush plates. And the other side of the cleaning movable brush plate moves towards the outer side by cleaning the limit on the inner side of the cleaning movable brush plate, so that the cleaning movable brush plate is attached to the concave part of the machine sheet, and the surface of the machine sheet is fully washed, so that the influence of impurities on later detection is avoided while workers are replaced to clean the surface of the machine sheet by themselves.

Description

technical field [0001] The invention relates to the field of aircraft engine blades, and more specifically, the invention relates to a non-destructive testing device for aircraft engine blades. Background technique [0002] An aircraft engine is a highly complex and sophisticated thermodynamic mechanism that provides the aircraft with the power required for flight. As the heart of an aircraft, it is known as the "Flower of Industry". It directly affects the performance, reliability and economy of an aircraft. It is an important manifestation of a country's technology, industry and national defense strength. The characteristic of engine research and development is technical difficulty. Large, costly, and long-term, the engine has a decisive impact on the performance of the aircraft and the success or failure and progress of aircraft development, and the engine technology has good dual-use characteristics for military and civilian use, which is of great significance to nationa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/00B08B1/00
CPCG01M13/00B08B1/12Y02E10/72
Inventor 魏武国杨琦
Owner CIVIL AVIATION FLIGHT UNIV OF CHINA
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