Towards Smaller Turbo Machinery for Aerospace Propulsion and Power

摘要：

1. Introduction Demands of small power source are recently of rapid increase for micro air vehicles, robots, mobile electric devices, and so on. Batteries are the most commonly used power source for such devices, despite its shortcoming of insufficient duration time. Ultra micro gas turbine including Power MEMS has been suggested as a candidate for such small power source.1, 2 In general, heat engine can achieve higher power and energy density, yielding more compact and durable system than batteries.

作者: Koji OKAMOTO

作者单位: Department of Aeronautics and Astronautics, School of Engineering, University of Tokyo 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, JAPAN

会议类型: 国际会议

会议名称: 2008 National Academic Symposium for Ph. D. Candidates and Tri-University Workshop on Aero-Structural Mechanics & Aerospace Engineering(NASPCTUWMAE2008)(2008年国际航天航空工程会议暨2008年博士生学术会议(力学))

会议地点: 北京

会议语种:英文

页码: 1-4

在线出版日期: 2008-10-23（万方平台首次上网日期，不代表论文的发表时间）