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Device for measuring the eccentric position of the aero-engine bearing holder

A technology for aero-engines and bearing housings, applied in measuring devices, electric devices, jet engine testing, etc., can solve problems such as high ambient temperature of bearings, inability to apply sensors and measurement methods, etc.

Active Publication Date: 2017-02-15
CHINA PRECISION ENG INST FOR AIRCRAFT IND AVIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The temperature of the high-temperature gas in the gas channel can reach 500-700°C, and the heat will also be transferred to the bearing cavity through conduction, heat radiation, etc., resulting in a high ambient temperature of the bearing. Such a harsh working environment makes many conventional sensors and measurement methods cannot be applied

Method used

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  • Device for measuring the eccentric position of the aero-engine bearing holder
  • Device for measuring the eccentric position of the aero-engine bearing holder
  • Device for measuring the eccentric position of the aero-engine bearing holder

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Embodiment Construction

[0019] The technical scheme of the present invention will be described in further detail below in conjunction with accompanying drawing and embodiment:

[0020] See attached Figure 1~3 As shown, the device for measuring the eccentric displacement of the aero-engine bearing seat includes:

[0021] A cylindrical capacitive displacement sensor 1, the capacitive displacement sensor 1 can withstand a high temperature of 400-600 ° C, and can accurately measure the displacement in the direction of its own axis;

[0022] A low-expansion rod body 2 capable of withstanding a high temperature of 400-600°C. The low-expansion rod body 2 is a hollow cylindrical structure, which can be made of ceramic material or Invar material with a low expansion coefficient. The low-expansion rod 2 is between 400-600 The axial expansion at ℃ ambient temperature is smaller than the resolution of the capacitive displacement sensor 1;

[0023] Fix the capacitive displacement sensor 1 on one end of the low...

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Abstract

The invention provides a device for measuring the eccentric position of the aero-engine bearing holder, which achieves the real time monitoring of the running state of an engine's main shaft through the measurement of the eccentric position of the engine bearing holder. In the implementation, a high temperature withstanding capacitance displacement sensor is mounted on the force bearing support plate of a casing through a rod body made from low expansion materials. When eccentric displacement occurs in the bearing holder, the output of the capacitance displacement sensor is made to change. This leads to the measurement of the eccentric displacement of the bearing holder. In an aero-engine, the rotor system, through the main shaft bearing, is supported and positioned; and the main shaft bearing is just fixedly arranged in the bearing holder of the casing. Therefore, the eccentric displacement of the bearing holder can destroy the coaxiality of the rotor system, and undermines the normal running of the engine. The device for measuring the eccentric position of engine bearing holder works with a simple principle, is very adaptive, and can be conveniently used. The device can also carry out precise measurement to the magnitude and the direction of the eccentric displacement of bearing holder in the vehicle testing process so as to avoid grave consequences caused by large eccentric displacement.

Description

technical field [0001] The invention relates to a device for measuring the eccentric displacement of an aeroengine bearing seat, which belongs to the technical field of measurement. Background technique [0002] In an aero-engine, the casing (3) is the main load-bearing component, and is usually composed of an outer wall, a bearing cavity (4) and several radial load-bearing support plates (6). Among them, the bearing seat (5) of the engine is installed in the bearing cavity (4), and the bearing cavity (4) is connected with the outer wall of the casing (3) through the bearing support plate (6) distributed symmetrically along the circumference. This constitutes a hub-and-spoke frame structure. The main shaft bearing of the engine rotor system is fixed in the bearing seat (5), so once the eccentric displacement occurs in the bearing seat (5) during the working process of the engine, the coaxiality of the rotor system will be destroyed, affecting the normal operation of the eng...

Claims

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Application Information

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IPC IPC(8): G01M15/14G01B7/00
CPCG01B7/00G01M15/14
Inventor 毕超戴长军徐昌语郭霞赵世迁
Owner CHINA PRECISION ENG INST FOR AIRCRAFT IND AVIC
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