首页|射流预冷不同因素对涡扇发动机性能的影响

射流预冷不同因素对涡扇发动机性能的影响

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为了研究射流预冷下涡扇发动机的性能以及稳定性表现,分别考虑射流预冷导致的进气道掺混换热、截面工质热物理性质的修正以及部件特性修正这三种因素,对涡扇发动机的稳态性能进行了数值模拟.计算结果表明:射流预冷下发动机推力的大幅增长来自于进气流量的增加,其中掺混换热是引起进气流量增加的直接因素,而工质热物理性质和部件特性的变化则导致发动机的推力下降,高水气比下,受进气流量增加的影响,射流预冷仍能大范围的提高发动机的推力水平.进气道掺混换热使得风扇更为逼近喘振点,而随着水气比的增加,风扇和高压压气机的稳定性均有所回升.
Effects of different influencing factors under mass injection and pre-compressor cooling on turbofan engine performance
In order to study the performance and stability of turbofan engine under mass injection and pre-compressor cooling(MIPCC),the steady-state performance of turbofan engine was numerically simulated by considering three factors:inlet mixing heat exchange,modification of thermophysical properties of working fluid and modification of component characteristics.The calculation results showed that the thrust of engine under MIPCC greatly increased due to the increase of intake flow,in which the inlet mixing heat exchange is the direct factor contributing to the increase of intake flow,while the changes of thermophysical properties of working fluid and component characteristics lead to the decrease of the thrust of engine.Even if with high water-air ratio,the thrust level can still be greatly enhanced by intake flow.Inlet mixing heat exchange can make fan work closer to the surge point,however,with the increase of water-air ratio,the stability of fan and high-pressure compressor both rose.

mass injection and pre-compressor cooling(MIPCC)mixing heat exchangethermophysicalpropertiescomponentcharacteristicsthrustsurgemargin

王佳美、郭迎清、于华锋

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西北工业大学动力与能源学院,西安 710072

射流预冷(MIPCC) 掺混换热 工质热物理性质 部件特性 推力 喘振裕度

国家科技重大专项基础研究项目

J2019-V-0003

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(1)
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