“昆仑”发动机的衍生发展 |
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引用本文: | 严成忠.“昆仑”发动机的衍生发展[J].航空发动机,2009,35(1):11-17. |
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作者姓名: | 严成忠 |
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作者单位: | 沈阳发动机设计研究所,沈阳,110015 |
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摘 要: | 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。
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关 键 词: | “昆仑”发动机 衍生发展 推力增大型 燃气轮机 |
Derivative Development of "Kunlun" Aeroengine |
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Authors: | YAN Cheng-zhong |
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Institution: | Shenyang Aeroengine Research Institute;Shenyang 110015;China |
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Abstract: | 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 ... |
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Keywords: | "Kunlun" aeroengine derivative development thrust augmenta-tion gas turbine |
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