Feature analysis on US military aircraft engine advanced technology programs

被引:0
作者
Liang, Chun-Hua [1 ]
Sun, Ming-Xia [1 ]
Liu, Hong-Xia [1 ]
机构
[1] Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China
来源
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2014年 / 29卷 / 07期
关键词
Advanced technology program; Aircraft engine; Military aircraft engine; Multi-discipline development; Technology corporation; Technology verification;
D O I
10.13224/j.cnki.jasp.2014.07.025
中图分类号
学科分类号
摘要
US military aircraft engine advanced technology programs were overviewed and analyzed from light weight gas generator (LWGG) program initiated in 1960s through integrated high performance turbine engine technology (IHPTET) program started in 1980s, then to versatile affordable advanced turbine engine (VAATE) program. Some features and trends were summarized and concluded by literature statistics method, such as teams based on closely corporation among government, industries and academics, goals oriented with national defence strategies and weapon system development requirements, engineering manufacture and development including all relative disciplines and areas, verification measured by technology readiness level, the application extending to military aircraft engine, civilian engine, gas turbine and space vehicle, etc. The experience and lessons obtained can provide reference and guide for technology research and engineering manufacture and development of military aircraft engines in the world.
引用
收藏
页码:1701 / 1709
页数:8
相关论文
共 15 条
[1]  
Hong W.S., Collopy P.D., Technology for jet engines: a case study in science and technology development, (2004)
[2]  
Liang C., Key features of versatile affordable advanced turbine engine program, Aeroengine, 37, 5, pp. 58-62, (2011)
[3]  
Liang C., Technology program of European Union high bypass ratio aeroengine, Aeroengine, 33, 2, pp. 57-58, (2007)
[4]  
Liang C., Advance of IHPTET, International Aviation, 2, pp. 58-60, (2004)
[5]  
Wu D., New version IHPTET program: important role of base technology and demonstrator in aircraft engine development, Aeroengine, 29, 2, pp. 1-4, (2003)
[6]  
Hill R.J., The purpose and status of IHPTET, (1996)
[7]  
Dadd G.J., Multivariable control of military engines, (1996)
[8]  
Stricker J.M., Advanced turbine engine concepts and their impact on the next millennium, (1997)
[9]  
Chamis C.C., Technology insertion benefits assessment in engines and aircraft, (1997)
[10]  
Dunbar L.W., Turbine configuration impact on advanced IHPTET engine system mission capabilities, (1990)