“昆仑”发动机的衍生发展

介绍了中国首次按国军标GJB241—1987《航空涡轮喷气和涡轮风扇发动机通用规范》的要求，自行设计研制成功的“昆仑”加力式双转子涡喷发动机的衍生发展。解决了与现役涡喷系列发动机安装互换性的技术难题，发展出“昆仑”A／B／H系列发动机，可满足多型飞机的动力需求；采用先进技术，增大空气流量、提高部件效率、减少压力损失，发展了推力增大型“昆仑Ⅱ”发动机；沿着“航机改燃机”捷径，改进燃气发生器，全新研制双级动力涡轮，发展了QD-128工业燃气轮机，已用于油田发电。

Derivative Development of "Kunlun" Aeroengine

The self-design "Kunlun" two-spool augmented turbojet engine was introduced which was successfully designed and developed according to the requirements of national military standard GJB241-87 "General specification for turbojet and turbofan aeroengine".The technical problems on installation replacements with the turbojet series engines in service have been resolved.The derivative "Kunlun"-A/B/H engines developed could effectively satisfy propulsion requirements of polytype aircrafts.The thrust augmentation ...