面向适航的航空发动机非线性气动热力建模方法综述

张曙光; 魏志远; 夏双枝

doi:10.13224/j.cnki.jasp.2018.12.009

面向适航的航空发动机非线性气动热力建模方法综述

doi: 10.13224/j.cnki.jasp.2018.12.009

1.
北京航空航天大学交通科学与工程学院，北京 100191；北京航空航天大学飞机/发动机综合系统安全性北京市重点实验室，北京 100191；先进航空发动机协同创新中心，北京 100191
2.
北京航空航天大学交通科学与工程学院，北京 100191；北京航空航天大学飞机/发动机综合系统安全性北京市重点实验室，北京 100191
3.
中国保利集团有限公司新时代工程咨询有限公司，北京 100088

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出版历程
- 收稿日期: 2017-11-13
- 刊出日期: 2018-12-28

Review on methods of aircraft engine nonlinear aerothermal-dynamic modeling for airworthiness requirement

摘要

摘要: 对适航规章关注的喘振和吸雨、吸雹等特殊运行环境安全问题中，航空发动机非线性气动热力模型建立方法开展需求分析及其进展综述。在分析发动机动态特性和过渡态仿真方法基础上，提炼了民用大型航空发动机喘振、吸雨和吸雹仿真的气动热力建模要素。分析认为:相对于容积动力学和传热动力学，转子动力学是发动机最重要的动态特性；流量法仿真精度更高，容积法更适宜于描述发动机高频特性；符合性验证仿真建模可在基于部件匹配的气动热力模型基础上，纳入喘振、吸雨、吸雹的模型要素。分析结果可支持基于试验数据和服役数据进行仿真工具的开发。
- 航空发动机适航 /
- 符合性验证 /
- 气动热力建模 /
- 喘振 /
- 吸雨 /
- 吸雹
Abstract: The requirement and progress of aircraft engine nonlinear aerothermal-dynamic modeling technique for the surge phenomenon and rain and hail ingestion effects in special operating conditions were reviewed pursuant to airworthiness regulation. Key modeling elements for the model with the simulation capability of surge, rain ingestion and hail ingestion were proposed based on the analysis of aero-engine dynamic characteristics and transient simulation methods. Result showed that, rotor dynamics was the most important compared with volume dynamics and thermal effect. Constant flow method had high accuracy and inter-component volume method was suitable for description of the engine high frequency dynamics. Compliance demonstration model should incorporate surge, rain ingestion and hail ingestion elements based on the component-matching aerothermal-dynamic model. The analysis can support the simulation tools development based on test data and service data.
- aircraft engine airworthiness /
- compliance demonstration /
- aerothermal-dynamic modeling /
- surge /
- rain ingestion /
- hail ingestion

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