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小涵道比涡扇发动机吞鸟能力仿真评估与验证

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军用航空发动机的吞鸟能力须满足国军标和适航相关规定,可靠的发动机吞鸟能力评估方法是开展吞鸟试验的基础,可降低试验风险、提高试验成功率.以国内某涡扇发动机研制中的吞鸟能力仿真与验证项目为基础,提出基于仿真分析、动量类比法和接触应力类比法的发动机吞鸟能力评估方法.根据相关标准规范,确定试验要求,开展整机吞鸟试验验证,通过4次整机吞鸟试验,验证了本文提出的发动机吞鸟能力评估方法的准确性,获得了发动机吞鸟能力底数.试验结果和评估方法可为其他涡扇发动机型号研制提供参考.
Simulation evaluation and verification of bird ingestion ability of turbofan engine
The bird-swallowing ability of engine must meet the requirements of the national military standard and airworthiness.It is necessary to propose a reliable method to assess the bird-swallowing ability of the engine before bird-swallowing tests,the test risk can be reduced and the test success rate can be increased.Based on the bird-swallowing capability simulation and verification project of a turbofan,a method for evaluating the bird-swallowing capability of an engine is proposed in this paper based on simulation analysis,momentum analogy and contact stress analogy.According to the relevant standards and specifications,the test requirements are determined,and the bird-swallowing test is carried out for four times.It is verified that the method is accurate.The test results and assess-ment methods can provide reference for the development of other turbofan models.

turbofan enginebird ingestionsimulation analysismomentum analogycontact stress analogy

贾超、范杰、江通通、陈倩

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中国航发贵阳发动机设计研究所 总体性能研究部,贵阳 550081

清华大学 航空发动机研究院,北京 100084

涡扇发动机 吞鸟 仿真分析 动量类比法 接触应力类比法

2024

航空工程进展
中国航空学会 西北工业大学

航空工程进展

CSTPCD
影响因子:0.207
ISSN:1674-8190
年,卷(期):2024.15(2)
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