Virtual test architecture for aero-engine high-altitude simulation test

An aero-engine and virtual test technology, applied in the field of virtual test framework, can solve problems such as complex working conditions of test subjects, increased difficulty in engine development, and a large number of equipment, so as to meet the needs of construction and development, enrich the amount of effective data, and shorten the test period. Effect

Active Publication Date: 2022-03-08
AECC SICHUAN GAS TURBINE RES INST
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  • Application Information

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Problems solved by technology

[0002] The high-altitude simulation test of aero-engine is an important means of aero-engine design verification and an insurmountable important link in the development process. The traditional high-altitude simulation test mode requires a lot of equipment, high test risks, and the test subjects are complicated and costly. In the future, The difficulty of engine development has increased significantly, and the test technology is bound to face new developments
At present, physical tests are still used in China to evaluate the performance of aero-engines. Simulation technology has only been widely used in the process of engine design, and it is still in its infancy in the field of high-altitude simulation tests, which cannot meet the development needs of new test technologies.
[0003] At present, the aero-engine test technology system is not perfect, and there is a considerable gap compared with foreign countries. In particular, the real-time approaches, methods, and technical solutions adopted for virtual test technology are still unclear. , prototype construction, application verification and other aspects of research is very lacking

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Embodiment Construction

[0023] Embodiments of the present application will be described in detail below in conjunction with the accompanying drawings.

[0024] Embodiments of the present application are described below through specific examples, and those skilled in the art can easily understand other advantages and effects of the present application from the content disclosed in this specification. Apparently, the described embodiments are only some of the embodiments of this application, not all of them. The present application can also be implemented or applied through other different specific implementation modes, and various modifications or changes can be made to the details in this specification based on different viewpoints and applications without departing from the spirit of the present application. It should be noted that, in the case of no conflict, the following embodiments and features in the embodiments can be combined with each other. Based on the embodiments in this application, all...

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Abstract

The invention provides a virtual test architecture for an aero-engine high-altitude simulation test, and belongs to the technical field of aero-engine tests, and the virtual test architecture comprises a demand analysis layer which is used for carrying out the demand analysis of a high-altitude platform virtual test for the aero-engine high-altitude simulation test, and determining the needed key technology and research range; the technical support layer is used for carrying out modeling and simulation in sequence according to an analysis result of the demand analysis layer, and determining a virtual test platform technology and a virtual test prototype technology; the engineering verification layer is used for building a virtual prototype and performing function rehearsal and verification of the high-altitude platform under the condition that the physical system is connected to the virtual test prototype; and the application layer is used for performing test capability and testable range evaluation, test scheme pre-optimization, test layout and test layout optimization and test data validity evaluation after function rehearsal and verification. By means of the processing scheme, the test simulation degree is improved, the test period is shortened, and high-altitude platform test technology progress is promoted.

Description

technical field [0001] The present application relates to the technical field of aero-engine testing, in particular to a virtual test framework for high-altitude simulation tests of aero-engines. Background technique [0002] The high-altitude simulation test of aero-engine is an important means of aero-engine design verification and an insurmountable important link in the development process. The traditional high-altitude simulation test mode requires a lot of equipment, high test risks, and the test subjects are complicated and costly. In the future, The difficulty of engine development has increased significantly, and the test technology will inevitably face new developments. At present, physical tests are still used in China to evaluate the performance of aero-engines. Simulation technology has only been widely used in the engine design process, and it is still in its infancy in the field of high-altitude simulation tests, which cannot meet the development needs of new t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G06F30/28G06F30/15
CPCG06F30/20G06F30/28G06F30/15Y02T90/00
Inventor 冷林涛吴锋冯旭栋杨彩琼徐倩楠乔彦平刘涛张韦雅
Owner AECC SICHUAN GAS TURBINE RES INST
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