关键词: 航空发动机, 起动, 微机

Abstract: In this paper the start process of the aeroengine controlled by the microcomputer was studied.The start fuel supply was controlled according to the relation between corrective start fuel supply and corrective speed for automatic regulation of the start fuel supply under different climatic conditions. In order to guarantee the safety and reliablity of the aeroengine, several parameters of the engine were monitored. The hybird simulation test for the whole start process was carried out and satifactory results were obtained.

Key words: aeroengine, start, microcomputer