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Effect of Dynamic Variations in Engine-Inlet Pressure on the Compressor System of a Twin- Spool Turbofan Engine

机译：发动机进气压力动态变化对双滑轮涡扇发动机压气系统的影响

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作者
Mc Aulay, J. E.;
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年度 1970
页码 1-3
总页数 3
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Compressor efficiency ; Inlet pressure ; Pressure oscillations ; Turbofan engines ; Engine failure ; Fluid dynamics;

机译：压缩机效率;进口压力;压力振荡;涡轮风扇发动机;发动机故障;流体动力学;

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专利

1. Qualification Approach of a High-Pressure Compressor Drum of a Military Turbofan Engine for Structural Integrity and Life [J] . R. K. Mishra, L. Prakash, S. N. Mistry Journal of Failure Analysis and Prevention . 2015,第4期

机译：军用涡扇发动机高压压气机鼓轮结构完整性和寿命的鉴定方法
2. Impacts of low-pressure (LP) compressor's deterioration of a turbofan engine upon fuel-usage of a military aircraft [J] . M. Naeem The Aeronautical Journal . 2008,第1127期

机译：低压（LP）压缩机涡扇发动机的退化对军用飞机燃料使用的影响
3. Finite-Time Regulation of Two-Spool Turbofan Engines With One Shaft Speed Control [J] . Wang Jiqiang, Dimirovski Georgi, Yue Hong Journal of Dynamic Systems, Measurement, and Control . 2016,第8期

机译：一轴转速控制的双阀芯涡扇发动机的有限时间调节
4. Design of an Additive Manufactured Compressor Vane with Multi-Hole Pressure Probes for the Application in a Twin-Spool Turbofan Engine [C] . Felix Kern, Stefan Bindl, Martin Strasser, AIAA/SAE/ASEE joint propulsion conference;AIAA propulsion and energy forum . 2016

机译：用于双阀芯涡扇发动机的带有多孔压力探头的增材制造的压缩机叶片的设计
5. Aerothermodynamic cycle analysis of a dual-spool, separate-exhaust turbofan engine with an interstage turbine burner. [D] . Liew, Ka Heng. 2006

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6. Descriptions of Entropy with Fractal Dynamics and Their Applications to the Flow Pressure of Centrifugal Compressor [O] . Yan Liu, Dongxiao Ding, Kai Ma, 2019

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7. Use of the Nonlinear Dynamical System Theory to Study Cycle-to-Cycle Variations from Spark Ignition Engine Pressure Data [O] . C. Letellier, S. Meunier-Guttin-Cluzel, G. Gouesbet, 1997

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Effect of Dynamic Variations in Engine-Inlet Pressure on the Compressor System of a Twin- Spool Turbofan Engine

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