综合机载机电及环控系统新技术

王浚; 刘永绩; 董素君

综合机载机电及环控系统新技术

北京航空航天大学航空科学与工程学院, 北京 100083

详细信息

中图分类号: V 245
计量
- 文章访问数: 2816
- HTML全文浏览量: 32
- PDF下载量: 1462
- 被引次数: 0
出版历程
- 收稿日期: 2003-07-13
- 网络出版日期: 2003-11-30

Advanced technologies of the integrated aircraft utility system and ECS

School of Aeronautics Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 首先对美国两种飞机综合机载机电系统发展方案做简单介绍,并进一步介绍了其中公共设备(机载机电)管理系统、多电飞机、"热油箱"燃油热管理系统、组合动力装置和热/能量管理组件等新技术概念内涵与关键问题,最后重点详细介绍了现代军用机先进的环控系统技术.
- 环境控制 /
- 飞机 /
- 机载机电系统 /
- 管理系统
Abstract: Two trends of the aircraft utility system integration technology of USA are introduced. The concepts of its key technologies, such as the integrated utilities management system, more electric aircraft, "hot fuel tank" integrated fuel system, integrated power unit and thermal/energy management module are presented in detail. And the advanced environmental control system(ECS) technologies of the modern military aircraft are emphasized at last.
- environmental control /
- aircraft /
- utility system /
- management system

HTML全文

参考文献(1)

[1] 于敦. 机载机电系统综合化的发展方向[J]. 航空科学技术, 1997, (4):6~8, 33 Yu Dun. Trend of aircraft utility system integration[J]. Aeronautical Science and Technology, 1997, (4):6~8, 33 (in Chinese) [2] Vrable D L, Yerkes K L. A thermal management concept for more electric aircraft power system applications. SAE Aerospace Power Systems Conference. VA, USA:Williamsburg, 1998. 271~277. [3] Yu-Hang Bill Ho, Tsugin Lin, Tibbs G B, et al. Thermal benefits of advanced integrated fuel system using JP-8+100 fuel. 1997 World Aviation Congress. CA, USA:Anaheim, 1997. SAE 975507. [4] Koerner M. Recent developments in aircraft emergency power. 35^th Intersociety Energy Conversion Engineering Conference and Exhibit. NV, USA:Las Vegas, 2000. 12~19. [5] Letlow J T, Jenkins L C. Development of an integrated environmental control system. 28^th International Conference on Environmental Systems. MA, USA:Massachusetts,1998. SAE981544. [6] Baird D, Ferentinos J. Application of MIL-C- -87252 in F-22 liquid cooling system. 28^th International Conference on Environmental Systems. MA, USA:Massachusetts, 1998. SAE981543. [7] Ghanekar M. Vapor cycle system for the F-22 Raptor. 30^th International Conference on Environmental Systems. France:Toulouse, 2000. SAE2000-01-2268. [8] Sprouse James G. F-22 environmental control/thermal management system design optimization for reliability and integrity——A case study. 26^th International Conference on Environmental Systems. CA, USA:Monterey, 1996. SAE961339. [9] Beam J. Heat sink options for a more electric aircraft thermal management system. SAE Aerospace Power Systems Conference. VA, USA:Williamsburg, 1997. SAE971244. [10] 王浚, 余建组, 庄达民, 等. 新兴的人机与环境工程技术科学[J]. 北京航空航天大学学报, 2002, 28(5):504~511 Wang Jun, Yu Jianzu, Zhuang Damin, et al. Newly developed human, machine and environment engineering technology science[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(5):504~511 (in Chinese)

施引文献

资源附件(0)

访问统计