The Development of TJE500FH Small Turbojet Engine

摘要：

This paper describes the design and construction of a small turbojet engine with designed static thrust of 500 N at sea level standards. The main components of this small jet engine are single stage radial tipped vanes centrifugal compressor, annular combustion chamber and single stage axial turbine. This engine uses liquid fuel during its operation while gas fuel is used to start and accelerate the engine to its idle condition. The designed speed is 73,000 rpm. The air mass flow and compressor pressure ratio at its designed speed is 0.88 kg/s and 4.07 respectively. After its construction, the engine will be tested to find out its performance.

关键词： turbojet engine small turbojet model turbojet

作者: Firman Hartono

作者单位: Aeronautics Astronautics Study Program, Faculty of Mechanical and Aerospace Engineering, Institute of Technology Bandung, Bandung, Indonesia

会议类型: 国际会议

会议名称: The 7th International Conference on Fluid and Thermal Energy Conversion(第七届流动技术与热能转化国际会议 FTEC 2011)

会议地点: 郑州

会议语种:英文

页码: 357-364

在线出版日期: 2011-09-24（万方平台首次上网日期，不代表论文的发表时间）