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Full working condition sealing test device

A technology of sealing test and full working conditions, which is applied in the direction of measuring devices, testing of mechanical parts, testing of machine/structural parts, etc., can solve the problem that the sealing test device cannot simultaneously simulate the working conditions of the sealing device of the aeroengine, and cannot truly reflect the sealing The actual situation of the device and other issues

Active Publication Date: 2016-04-20
CHINA AVIATION POWER MACHINE INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a full working condition sealing test device to solve the technical problem that the sealing test device in the prior art cannot simulate the working conditions of the aeroengine sealing device at the same time, and the test results cannot truly reflect the actual situation of the sealing device

Method used

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  • Full working condition sealing test device
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Embodiment Construction

[0024] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in many different ways defined and covered by the claims.

[0025] see figure 1 , a preferred embodiment of the present invention provides a test bench, including a rotor 7, a bearing 10 for supporting the rotor 7, a bearing seat 8 and a support 9; Chamber 13 communicates with air outlet chamber 15 and exhaust duct 11 respectively; the channel connected between high pressure chamber 13 and air outlet chamber 15 is the placement position of the sealed test piece, which is used to place the test piece for testing, and the high pressure chamber 13 is connected with exhaust duct 11 The channel is the place where the accompanying test piece is placed, and is used to place the accompanying test piece. The exhaust channel 11 communicates with the cold air passage, and a hot air sealing ring 12 is provided between ...

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Abstract

The invention discloses a testing rack and an all-condition sealing testing device. The testing rack comprises a rotor, a bearing used for bearing the rotor, a bearing base and a supporting base. A high-pressure cavity is formed inside the testing rack, the high-pressure cavity is communicated with an air exhaust cavity and an air exhaust channel respectively, the air exhaust channel is communicated with a cold air channel, and a hot air sealing ring is arranged between the air exhaust channel and the rotor for isolation. High-temperature high-pressure air can be led into the testing rack, real-time working conditions of an aero-engine sealing device can be simulated, normal operation of parts such as the rotor can be guaranteed, the actual situations of the sealing device can be really reflected and correct judgment of the probability, the reliability and the durability of use of the sealing device on an aero-engine can be made.

Description

technical field [0001] The invention relates to a test device, in particular to a test bench and a full working condition sealing test device. Background technique [0002] At present, the sealing devices commonly used in aero-engines are usually designed based on experience, verified by static and dynamic tests, and necessary modifications are made to their structures according to the test results. For the design of some new sealing devices, they are based on new theories, and a large number of experiments are needed to verify whether the theoretical analysis and design are correct. Whether the test result is correct or not is directly related to the success or failure of the design of the sealing device. [0003] With the improvement of the performance of the aero-engine, the cycle parameters (pressure, temperature) increase, the rotor speed increases, the working conditions of the seal are deteriorating day by day, and the problems caused by the sealing device are becomi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M13/00
Inventor 力宁彭最花贺玲周坤李齐飞谭键
Owner CHINA AVIATION POWER MACHINE INST
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