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Aero-engine starting simulation model correction method based on test data

An aero-engine and simulation model technology, applied in design optimization/simulation, electrical digital data processing, CAD numerical modeling, etc., can solve few problems, meet engineering accuracy requirements, and improve the effect of start-up simulation accuracy

Active Publication Date: 2022-01-04
AECC SHENYANG ENGINE RES INST
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Problems solved by technology

In the published literature, there is no specific guidance method to improve the accuracy of the start-up simulation, and there are very few correction techniques for the start-up simulation model based on test data. Therefore, it is necessary to carry out a general start-up model correction based on test data Method research, improve the simulation accuracy of the starting simulation model, and provide tool support for the forward design of starting performance

Method used

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  • Aero-engine starting simulation model correction method based on test data
  • Aero-engine starting simulation model correction method based on test data
  • Aero-engine starting simulation model correction method based on test data

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Embodiment Construction

[0027] In order to make the objectives, technical solutions and advantages of the implementation of the application clearer, the technical solutions in the implementation modes of the application will be described in more detail below with reference to the drawings in the implementation modes of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the present application. The embodiments described below by referring to the figures are exemplary and are intended to explain the present application, and should not be construed as limiting the present application. Based on the implementation manners in this application, all other implementation manners obtained by persons of ordinary skill in the art without creative efforts fall within the scope of protection of this application. Embodiments of the pr...

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Abstract

The invention belongs to the field of aero-engine design, and particularly relates to an aero-engine starting simulation model correction method based on test data, and the method comprises the steps: calculating a correction value under a preset condition, and carrying out the simulation calculation of the calculated correction value to obtain a simulation correction value under a target condition, and calculating the rotating speed under the target condition through the obtained correction value. By adopting the method, the starting simulation precision can be greatly improved, the maximum error of high-voltage and low-voltage rotating speed simulation and actual comparison is within 6.9%, and the engineering precision requirement is met.

Description

technical field [0001] The application belongs to the field of aero-engine design, in particular to an aero-engine starting simulation model correction method based on test data. Background technique [0002] Numerical simulation of aero-engine starting is an important method for the study of engine starting process, and it is very necessary to establish a simulation model for engine starting. Starting simulation is an important means to promote the change of aero-engine starting performance design from "traditional design" to "predictive design". The repetition of physical tests shortens the development cycle, reduces development costs, and effectively accelerates the independent innovation and development of my country's aero-engines. [0003] The starting simulation model can calculate the starting characteristics of the engine within the entire starting envelope range with a certain accuracy, and can be used for starting simulation and starting performance design within ...

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Application Information

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IPC IPC(8): G06F30/17G06F30/28G06F111/10G06F113/08G06F119/14G06F119/08
CPCG06F30/17G06F30/28G06F2111/10G06F2113/08G06F2119/14G06F2119/08
Inventor 唐兰郭海红于涵韩文俊刘亚君
Owner AECC SHENYANG ENGINE RES INST
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