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航空发动机防喘扩稳构件效能的试验
引用本文:叶巍,乔渭阳,侯敏杰.航空发动机防喘扩稳构件效能的试验[J].航空动力学报,2009,24(8):1747-1751.
作者姓名:叶巍  乔渭阳  侯敏杰
作者单位:西北工业大学动力与能源学院;中国燃气涡轮研究院;
摘    要:为评估和优化发动机防喘系统的效能,采用温度畸变发生器作为逼喘装置,分别给出了某涡扇、涡喷发动机扩稳构件在不同组合方案下的试验结果.比较和讨论了防喘系统不同扩稳构件的扩稳效果.试验结果表明:发动机防喘系统扩稳效果最为显著的是采用短时切断燃油以及导叶、放气等调节手段,但其缺点会带来较大的推力损失和系统的复杂性;而采用切油加导叶调节的手段尽管扩稳效果不如前者明显,但其推力损失较小且系统易于实现.

关 键 词:防喘  扩稳  温度畸变  效能
收稿时间:6/4/2008 12:00:00 AM
修稿时间:2008/9/30 0:00:00

Test investigation of areo-engine's stability enhancement components in anti-surge system
YE Wei,QIAO Wei-yang and HOU Min-jie.Test investigation of areo-engine''s stability enhancement components in anti-surge system[J].Journal of Aerospace Power,2009,24(8):1747-1751.
Authors:YE Wei  QIAO Wei-yang and HOU Min-jie
Institution:1.School of Power and Energy;Northwestern Polytechnical University;Xi'an 710072;China;2.China Gas Turbine Establishment;Chengdu 610500;China
Abstract:To assess and optimize the optimal efficiency of the anti-surge system,this paper adopted the temperature distortion generator as the force-surge system and presented the test results of certain turbojet and turbofan engine's stability enhancement components at different combinatorial projects respectively,compared and discussed the effects of various stability enhancement components of the anti-surge system.The test results show that the most effective anti-surge system is the one using throttle cutting fo...
Keywords:anti-surge  stability enhancement  temperature distortion  efficiency  
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