Method for detecting fiber bragg grating acoustic emission of helicopter bearing fault

An acoustic emission detection and fiber grating technology, which is used in mechanical bearing testing, material analysis using acoustic emission technology, etc., can solve problems such as failure to effectively find faults, and achieve simple installation and operation, easy to distinguish, and low spectral noise. Effect

Inactive Publication Date: 2013-10-09
CHINESE PEOPLES LIBERATION ARMY AVIATION COLLEGE +1
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Problems solved by technology

At present, most of the original detection methods such as visual inspection and hand-touch temperature judgment or vibration-based detection methods cannot effectively detect faults (especially early faults)

Method used

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  • Method for detecting fiber bragg grating acoustic emission of helicopter bearing fault
  • Method for detecting fiber bragg grating acoustic emission of helicopter bearing fault
  • Method for detecting fiber bragg grating acoustic emission of helicopter bearing fault

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Embodiment Construction

[0020] Specific embodiments of the present invention will be described below in conjunction with the accompanying drawings, so as to better understand the present invention. It should be noted that in the following description, when detailed descriptions of known functions and designs may dilute the main content of the present invention, these descriptions will be omitted here.

[0021] Such as figure 1 As shown, the FBG acoustic emission detection method for helicopter bearing faults of the present invention includes three parts: sensor installation, signal sensing and demodulation; wherein, sensor installation includes mounting of grating sensors (packaged or unpackaged); The sensing adopts single fiber grating sensing method; the demodulation part includes photoelectric conversion, amplification, acquisition, resonance demodulation processing, etc. The specific implementation is as follows: the narrowband optical signal 4 is generated by a narrowband tunable laser, and its...

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Abstract

The invention provides a method for detecting fiber bragg grating acoustic emission of a helicopter bearing fault in order to detect an early-time state of the fault of rolling bearings on a helicopter, enhance the capacity for recognizing the fault of the bearings of the helicopter and prolong the service life of the bearings of the helicopter. The detecting method includes the steps of sensor installation, signal sensing and demodulation, wherein the sensor installation includes pasting-installation of a grating sensor (packaged or non-packaged), the single-fiber-bragg-grating sensing method is adopted for the sensing, and the demodulation includes photoelectric conversion, amplification, acquiring, resonance demodulation processing and the like. The method for detecting fiber bragg grating acoustic emission of the helicopter bearing fault is mainly used for detecting the fault of the bearings of the helicopter and faults of bearings of other rotating machines at the home position and on line. Compared with traditional detecting methods (eye observing, vibration, magnetic powder and the like), the method for detecting fiber bragg grating acoustic emission of the helicopter bearing fault can effectively detect the early-time state of the faults and accurately judge the fault type and the fault severity order, and the method has great significance for on-condition maintenance and service life prolonging of the helicopter.

Description

technical field [0001] The invention belongs to the technical field of acoustic emission detection, and in particular relates to a fiber grating acoustic emission detection method for bearing faults such as a support bearing of a helicopter tail drive shaft. Background technique [0002] The tail drive shaft of the helicopter mainly transmits the torque of the main reducer to the tail rotor. It is installed in the tail beam and is a high-speed rotating part, and the support bearing of the tail drive shaft is a key component. At present, most of the original detection methods such as visual inspection and hand-touch temperature judgment or vibration-based detection methods cannot effectively detect faults (especially early faults). Bearing faults (cracks, wear, pitting, peeling, loosening, etc.) have to go through a slow expansion process. This stage is not enough to cause obvious vibration of the bearing, but the acoustic emission signal is more obvious. Therefore, acoustic ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M13/04G01N29/14
Inventor 李宁魏鹏梅盛开涂万里杨而蒙高煊孔莉莎
Owner CHINESE PEOPLES LIBERATION ARMY AVIATION COLLEGE
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