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Device for improving magnetic testing sensitivity of aviation engine blade

An aero-engine and sensitivity technology, which is applied in the direction of material magnetic variables, can solve the problems of low longitudinal magnetization sensitivity, high magnetic field strength, and low magnetic detection efficiency, and achieve the effects of reducing the difficulty of demagnetization, low magnetic field strength, and improving efficiency

Active Publication Date: 2014-01-22
CHENGDU ENGINE GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In view of the problems existing in the existing magnetic detection of blades, the purpose of the present invention is to provide a device for improving the sensitivity of magnetic detection of aircraft engine blades, so as to solve the problem of low longitudinal magnetization sensitivity in the existing magnetic detection technology. Magnetic inspection of blades requires high magnetic field strength and difficult demagnetization. Large-scale demagnetization equipment needs to be used for repeated demagnetization. The efficiency of magnetic inspection is low, and there are few types of applicable blades.

Method used

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  • Device for improving magnetic testing sensitivity of aviation engine blade
  • Device for improving magnetic testing sensitivity of aviation engine blade

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Embodiment 1

[0023] The device for improving the magnetic detection sensitivity of aeroengine blades in this embodiment has a structure such as figure 1 and figure 2 As shown, its composition is mainly composed of a fixed base plate 1 for placing the device on the bed body of the magnetic detection equipment, a tenon holding joint 3 placed on the fixed base plate for holding one end of the tenon of the blade under test, and a tenon holding joint 3 for holding the measured blade. The blade tip holding joint 2 at one end of the blade tip, and the extension plate 4 arranged on the tenon holding joint for increasing the magnetic detection aspect ratio of the measured blade is composed of the installation direction of the extension plate is opposite to the installation direction of the measured blade. The tenon holding joint and the blade tip holding joint are arranged oppositely. The tenon holding joint is a rotatable tenon holding joint, and its holding structure is a connection structure f...

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Abstract

The invention discloses a device for improving magnetic testing sensitivity of an aviation engine blade. The device mainly comprises a fixing bottom plate for arranging a tool device on a magnetic testing equipment bed, a tenon holding head which is arranged on the fixing bottom plate and which is used for holding one end of a tenon of the tested blade, a blade tip holding head for holding one end of the tested blade, and an extended plate which is arranged on the tenon holding head and which is used for increasing the length-diameter ratio of the tested blade, wherein the mounting direction of the extended plate is opposite to the mounting direction of the tested blade; the tenon holding head and the blade tip holding head are arranged oppositely; at least one of the tenon holding head and the blade tip holding head is a rotary holding head which can hold the tested blade to rotate; and at least one of the tenon holding head and the blade tip holding head is a movable holding head which can move and adjust the mounting position relative to the other one. The device has the characteristics that the longitudinal magnetization sensitivity is high, the length-diameter ratio is smaller than blade magnetic testing magnetic field intensity, demagnetization can be easily achieved without using large-size demagnetization equipment to carry out repeated demagnetization, the magnetic testing efficiency is high, and the device is applicable to various blades.

Description

technical field [0001] The invention relates to the magnetic detection technology of aero-engine blades, and more specifically relates to a tooling device used for magnetic detection equipment to improve the magnetic detection sensitivity of aero-engine blades. Background technique [0002] Aeroengine blades are very important parts of aeroengines. Magnetic particle testing (magnetic inspection) is required piece by piece before assembly, and demagnetization is required after magnetic inspection to ensure the safe operation of aeroengines. The magnetic particle inspection of aero-engine blades is a special inspection, and the defects that can be detected include cracks, inclusions, hairlines, folds, etc. In order to ensure the reliability of magnetic inspection and prevent accidents due to defects after parts are installed, it is necessary to carry out magnetic inspection and demagnetization in strict accordance with the magnetic inspection procedures and standards. Magneti...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N27/84
Inventor 李凌朱建伟刘素平周先火
Owner CHENGDU ENGINE GROUP
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