Research on the Application of Integrated Design on Micro Turbojet Engine

Abstract

There are no detailed design criteria and methods for the integrated design of micro turbojet engine.The size and weight design and evaluation method for turbojet engines are used to perform the integrated design of several 9~80 kgf micro turbojet engines and evaluate the engines'data.The integrated design parameters database of micro turbojet engine is established,and the integrated design criterion of micro turbojet engine is extracted.Using this criterion,the integrated design of 16 kgf micro turbojet engine is completed.The results show that,using the integrated design method for the micro turbojet engine,the obtained design criteria is highly reliable,and can perform the overall scheme design of the micro turbojet engine.

Keywords

• micro turbojet engine
• size
• weight
• integrated design
• database
• design criteria