期刊文献+

自适应变循环发动机性能优势评价方法 被引量:3

Performance Advantage Evaluation Method of Adaptive Variable Cycle Engine
下载PDF
导出
摘要 为了综合评价自适应变循环发动机相比常规涡扇发动机的性能优势,提出了从发动机耗油率降低和质量增加2个维度以及从发动机耗油率、飞机燃油消耗量和燃油效率之间关系的角度来评价自适应变循环发动机性能的2种方法。结果表明:发动机耗油率降低和质量增加之间存在某个平衡点,只有质量增加幅度小于耗油率降低幅度时,才能体现自适应变循环发动机的性能优势,并且飞机航程越长,越能体现自适应变循环发动机耗油率降低带来的优势;发动机耗油率、飞机燃油消耗量和燃油效率之间呈指数关系变化,当假设飞机巡航航程为3500 km、飞机升阻比为10.5时,自适应变循环发动机巡航耗油率相比常规涡扇发动机的降低1%,可使飞机燃油消耗量减少约1.9%,飞机燃油效率提高约2.4%。 In order to comprehensively evaluate the performance advantages of adaptive variable cycle engines compared with conventional turbofan engines,two methods for evaluating the performance of adaptive variable cycle engines were proposed from two dimensions of engine specific fuel consumption reduction and mass increase and the perspective of the relationship between engine specific fuel consumption,aircraft fuel consumption and fuel efficiency.The results show that there is a balance point between the decrease of engine specific fuel consumption and the increase of engine mass.Only when the increase of mass is less than the decrease of specific fuel consumption can the performance advantages of adaptive variable cycle engine be reflected.The longer the flight,the better the advantages of the reduced specific fuel consumption of the adaptive variable cycle engine.The relationship between engine specific fuel consumption and aircraft fuel consumption and fuel efficiency is exponential.Assuming that the aircraft cruise range is 3500 km and the lift-to-drag ratio is 10.5,the cruise specific fuel consumption of adaptive variable cycle engine can be reduced by 1%compared with that of the conventional turbofan engine,which can reduce the aircraft fuel consumption by about 1.9%and increase the aircraft fuel efficiency by about 2.4%.
作者 李瑞军 王靖凯 吴濛 LI Rui-jun;WANG Jing-kai;WU-Meng(AECC Shenyang Engine Research Institute,Shenyang 110015,China)
出处 《航空发动机》 北大核心 2021年第2期17-21,共5页 Aeroengine
基金 航空动力基础研究项目资助。
关键词 自适应变循环发动机 燃油消耗量 燃油效率 耗油率 性能优势 评价方法 adaptive variable cycle engine fuel consumption fuel efficiency specific fuel consumption performance advantages evaluation method
  • 相关文献

参考文献7

二级参考文献29

  • 1方昌德.变循环发动机[J].燃气涡轮试验与研究,2004,17(3):1-5. 被引量:71
  • 2郭琦,李兆庆,卢传义.第四代战斗机的动力装置[J].燃气涡轮试验与研究,2005,18(2):58-62. 被引量:6
  • 3梁春华.未来的航空涡扇发动机技术[J].航空发动机,2005,31(4):54-58. 被引量:29
  • 4VAATE BAA III Adaptive Versatile Engine Technology (ADVENT), Broad Agency Announcement Number 07-01-PRK,Call 01 ,Air Force Research Laboratory,Propulsion Directorate [J].Wright-Patterson AFB, OH, 2007.
  • 5H Miyagi,H Kirnura,K Kishi,etc.Combined cycle engine research in japanese HYPR program [ J ].AIAA 1998-3278.
  • 6James E.Johnson,Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle:US, Patent 580303[P], 1998.
  • 7Rollin G.Giffin,III,James E Johnson,David W.Crall,et al Turbofan engine with a core driven supercharged bypass duet: US, Patent 5809772[ P ], 1998.
  • 8E.Carrera, A.Rodriguez, J.Talamantes.Measurement of residua stresses in cast aluminium engine block, [J].Jourmal of Materials Processing Teehn- ology, 2007 (1):206-210.
  • 9J.E.Wyatt,J.T.Berry,A.R.Williams.Residual stresses in aluminum castings [J]. Jourrnal of Materials Processing Technology, 2007( 8 ) : 170-173.
  • 10Marco A, Pericles P. The selective bleed variable cycle engine. ASME 91-GT -388.

共引文献99

同被引文献30

引证文献3

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部