提高WP－11发动机起动高度的研究与实施

推进技术 ›› 1994, Vol. 15 ›› Issue (4): 22-26.

提高WP－11发动机起动高度的研究与实施

冯延光,杨新江

北京航空航天大学;北京航空航天大学

发布日期:2021-08-15

AN INVESTIGATION ON INCREASING STARTING ALTITUDE OF WP-11 TURBINE

Beijing University of Aeronautics and Astronautics, Beijing,100083;Beijing University of Aeronautics and Astronautics, Beijing,100083

Published:2021-08-15

摘要/Abstract

摘要： 研究了ＷＰ－１１发动机点火高度从４０００ｍ提高到８０００ｍ的某些问题。详细讨论了点火高度的理论基础，并为ＷＰ－１１研制了一种可用的空中补氧点火装置，扩大了ＷＰ－１１发动机的使用范围。带着空中补氧点火装置的ＷＰ－１１发动机成功完成了高空舱试验和Ｙ－８飞机带飞实验。

关键词: 涡轮喷气发动机;空中起动;高空飞行;空中点火试验;点火装置;氧气设备

Abstract: The starting altitude of WP-11 turbine engine has been increased from 4000m to 8000m. The basic theory of increasing starting altitude is discussed in details. An air-borne oxygen supply ignition device (AOSID) has been developed to expand the applied range of the engine. High altitude simulating cell tests and flight tests with Y-8 airplane for WP-11 engine equipped with AOSID have also been performed successfully.

Key words: Turbojet engine;Air starting;High altitrude flight;In-flight ignition test;Ignition device;Oxygen equipment

冯延光,杨新江. 提高WP－11发动机起动高度的研究与实施[J]. 推进技术, 1994, 15(4): 22-26.