基于航空发动机产品需求的压气机技术研究 |
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引用本文: | 程荣辉,张军,王东,张学宝,张少平,曾瑶.基于航空发动机产品需求的压气机技术研究[J].航空发动机,2024,50(2):1-10. |
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作者姓名: | 程荣辉 张军 王东 张学宝 张少平 曾瑶 |
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作者单位: | 1.中国航发沈阳发动机研究所,沈阳 110015; 2.中国航发四川燃气涡轮研究院,成都 610500 |
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摘 要: | 压气机是航空发动机的关键核心部件,随着先进作战飞机对航空发动机需求的不断提高,快速研制全面满足发动机产
品需求的压气机是工程设计人员面临的重大挑战。为保证设计的压气机全面满足发动机产品需求,介绍了先进作战飞机发动机
的典型技术特点以及对压气机全面的技术需求,梳理了压气机满足发动机需求需重点考虑的影响因素,开展了宽转速范围高效率
设计技术、全飞行包线高稳定裕度设计技术、高性能保持能力设计技术、高可靠叶片设计技术、高稳健压气机转子设计技术、高可
靠调节机构设计技术、高安全性以及高环境适应性设计技术研究。结果表明:基于需求的综合设计可以保证压气机的综合性能。
该研究可为设计全面满足发动机产品需求的压气机提供参考和依据。
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关 键 词: | 压气机 需求 性能 可靠性 航空发动机 |
Compressor Research Based on Aeroengine Product Requirements |
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Authors: | CHENG Rong-hui ZHANG Jun WANG Dong ZHANG Xue-bao ZHANG Shao-ping ZENG Yao |
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Abstract: | The compressor is an essential component of an aeroengine. With the increasing requirements of advanced combat aircraft
on aeroengines, it is a major challenge for compressor designers to quickly develop a compressor that fully meets aeroengine product
requirements. To ensure that the compressor can fully satisfy aeroengine product requirements, typical characteristics of advanced combat
aircraft engines and comprehensive technical requirements for compressors are reviewed, and key influencing factors for the compressor to
meet aeroengine product requirements are presented. Research of design methods was conducted, including high efficiency in wide
rotational speed range, high stall margin across the full flight envelope, high performance-retention capability, highly reliable blade, highly
robust compressor rotor, highly reliable blade angle adjusting mechanism, high safety, and high environment adaptability. The research
shows that the requirement-based comprehensive design can ensure the comprehensive performance of the compressor, providing a refer?
ence for the design of a compressor that fully meets aeroengine product requirements. |
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Keywords: | compressor requirement performance reliability aeroengine |
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