| 叶代勇，滕 健，郭 捷，贾东兵，王飞鸣.短距起飞/垂直降落战斗机发动机[J].航空发动机,2013,39(1):74-78 |
| 短距起飞/垂直降落战斗机发动机 |
| Analysis of Development and Key Technique for Short Takeoff and Vertical Landing (STOVL) Fighter Engin |
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| DOI： |
| 中文关键词: 短距起飞/垂直降落战斗机 航空发动机 升力风扇 3轴承偏转喷管 机械系统 |
| 英文关键词:fighter aeroengine liftfan 3-bearing deflection nozzle mechanical system |
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| 中文摘要: |
| 短距起飞/垂直降落战斗机具有独特的技术特点和较好的环境适应性，生存力强，推进系统尤其带升力风扇的发动机是其关键技术之一。综合分析了短距起飞/垂直降落战斗机发动机的发展历程，总结了升力风扇+常规发动机型短距起飞/垂直降落战斗机发动机的4项主要关键技术：发动机总体设计技术、升力风扇设计技术、3轴承偏转喷管设计技术和升力风扇机械系统设计技术。经分析认为，通过一定技术途径突破上述4项关键技术是掌握短距起飞/垂直降落战斗机发动机技术的关键。 |
| 英文摘要: |
| fighter has unique technique, better accommodation and survivable. The propulsion system is one of key technique, especially in the engine with liftfan. The development course of STOVL version engine was comprehensively analyzed. Many key techniques of STOVL fighter engine composed with liftfan and conventional engine were analyzed, which involved engine, liftfan, 3-bearing deflection nozzle, mechanical system of liftfan design technique. The four techniques are key of mastering the techniques of STOVL fighter engine |
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