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Core engine test performance correction method

A test performance and core machine technology, applied in the direction of nuclear power generation, jet engine testing, gas turbine engine testing, etc., can solve the problems of poor evaluation accuracy and low implementation efficiency, reduce test costs, improve evaluation accuracy, and improve test performance. efficiency effect

Pending Publication Date: 2022-06-03
AECC SHENYANG ENGINE RES INST
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  • Application Information

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Problems solved by technology

[0006] The purpose of this application is to provide a core machine test performance correction method to solve the problems of low implementation efficiency and poor evaluation accuracy caused by the need for multiple nozzles when performing tests at different typical state points in the prior art

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Embodiment Construction

[0022] In order to make the implementation purpose, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the accompanying drawings in the embodiments of the present application.

[0023] A core machine test performance correction method, by obtaining the relationship between the nozzle flow coefficient ratio and the core machine characteristic data, and correcting the core machine test results by the correction amount, so as to improve the accuracy and efficiency of the core machine test evaluation. It includes two major modules, namely: the determination method of the nozzle flow coefficient ratio; the correction method of the core machine circulation work, the total pressure ratio and the total temperature ratio.

[0024] Specific methods include:

[0025] 1. Determination method of nozzle flow coefficient ratio

[0026] Step S100:...

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Abstract

The invention belongs to the field of core engine tests, and relates to a core engine test performance correction method, which comprises the following steps of: before a core engine test is carried out, carrying out a pretreatment test, and measuring a flow parameter of a reference spray pipe and a spray pipe expansion ratio under the pretreatment test so as to obtain a corresponding relation between a parameter in the test and a reference parameter; according to the proportional relation between the reference parameters and the test parameters, it is determined that different correction coefficients are set corresponding to different core engine performance parameters under different conversion rotating speeds and spraying pipe areas, and in this way, in the actual test, different envelope points are subjected to different envelope point tests; the performance parameters of the core machine under the envelope point can be accurately obtained only through the corresponding correction coefficient; compared with an original test method, tests of different envelope points can be carried out under the condition of the same spray pipe state, the performance condition of the core engine is obtained through the correction method, the test efficiency is improved, the test cost is reduced, the evaluation accuracy is improved, and meanwhile the method is more intelligent.

Description

technical field [0001] The present application belongs to the field of core machine testing, and particularly relates to a method for correcting core machine test performance. Background technique [0002] The core engine is the most important part of the engine, including the components and systems with the highest temperature, highest pressure and highest speed in the engine system. Therefore, the core engine development is also the most important link in the engine development process. During the development of the core machine, a large number of core machine and high-altitude platform tests are required to determine the performance of the core machine at a typical point of the work envelope. The performances that need to be evaluated mainly include the core engine cycle work, total pressure ratio, total temperature ratio, component characteristics, and the matching of the core engine working line, but do not need to be evaluated for accompanying test pieces such as inta...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/14
CPCG01M15/14Y02E30/30
Inventor 王赫王军李兆红
Owner AECC SHENYANG ENGINE RES INST