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Dynamic calibration method for turboshaft engine test bed

A turboshaft engine, dynamic calibration technology, applied in the direction of internal combustion engine testing, etc., can solve the problems of uncertain factors in the normal operation of aircraft, no test bench for stable state discrimination and stability evaluation, no method, process, project content and quantitative standards. , to achieve the effect of improving the test level, improving stability and measurement accuracy

Active Publication Date: 2015-07-15
CHINA AVIATION POWER MACHINE INST
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Problems solved by technology

[0004] The present invention provides a method for dynamic calibration of a turboshaft engine test bench to solve the existing turboshaft engine test bench, which generally only has qualitative requirements for dynamic calibration of the test bench, without specific methods, processes, project contents and quantitative standards. There is also no method for judging the stable state of the test bench and evaluating the stability, which is prone to a series of use problems and brings uncertain factors to the normal operation of the aircraft.

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  • Dynamic calibration method for turboshaft engine test bed

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Embodiment Construction

[0020] 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 various ways defined and covered.

[0021] figure 1 It is a structural block diagram of a dynamic calibration method for a turboshaft engine test bench in a preferred embodiment of the present invention. Such as figure 1 As shown, the dynamic calibration method of the turboshaft engine test bench of the present embodiment includes the following steps: Step 1, check the stability of the test bench, and adjust the test bench in time by analyzing the test data, so that the stability of the test bench reaches Scheduled requirements; step 2, check the temperature uniformity, and adjust the engine in time by arranging temperature probes evenly at the intake part of the engine, and analyze the temperature data, so as to ensure the stability of the engine intake air field; step 3, repeat Perform the initial per...

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Abstract

The invention discloses a dynamic calibration method for a turboshaft engine test bed. The method includes the following steps that firstly, test bed stability inspection is conducted, and the test bed is adjusted in time by analyzing test data; secondly, temperature uniformity inspection is conducted, temperature probes are uniformly distributed on the engine intake part, and an engine is adjusted in time by analyzing temperature data; thirdly, repeatability inspection is conducted, a primary performance test and a repeatability test are carried out on the engine to obtain test values of the engine at different state points, the test values of the repeatability test are compared to obtain repeatability difference values, and the engine is adjusted in time according to the repeatability difference values; fourthly, intersection calibration inspection is conducted, the engine is placed on a reference test bed and the test bed to be calibrated respectively to be subjected to intersection calibration inspection, and the engine is adjusted in time according to obtained intersection calibration difference value data. Stability and measurement accuracy of the turboshaft engine test bed are remarkably improved, and the turboshaft engine test bed can meet strict airworthiness requirements.

Description

technical field [0001] The invention relates to the field of turboshaft engine ground calibration, in particular to a dynamic calibration method for a turboshaft engine complete machine test bench. Background technique [0002] If the engine fails during the flight, it will cause very serious problems, and may even crash. Therefore, after a certain period of use, the aircraft engine must be disassembled no matter whether it is good or bad, and then sent to the factory for maintenance. So it goes round and round until the life of the engine is terminated. The ground facility for testing aircraft engines is called an engine test bench. [0003] At present, in the construction of the turboshaft engine test bench for turboshaft engines, there are generally only qualitative requirements for the dynamic calibration of the test bench. The method of stability assessment is mostly judged by past test experience or the time of stable work. The dynamic calibration of the test bench ...

Claims

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Application Information

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IPC IPC(8): G01M15/04
Inventor 许明文刘知理程文强邹宝军赵平刘引峰
Owner CHINA AVIATION POWER MACHINE INST
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