海军航空工程学院学报2012，Vol.27Issue(2)：121-126,6.
应用电磁弹射器的舰载机起飞性能分析
Performance Analysis of Catapult Take-Off Process of Carrier-Based Aircraft Using Electromagnetic Aircraft Launch System
李静 1左斌 2路翠华3
作者信息
- 1. 海军航空工程学院7系,264001／北京图形研究所,北京100029
- 2. 海军航空工程学院控制工程系,山东烟台264001
- 3. 北京图形研究所,北京100029
- 折叠
摘要
Abstract
Taking into consideration the thrust force of electromagnetic launch system,the nose gear fast-extension force and the ship motion process,a mathematical model of a carrier-based aircraft using electromagnetic launch system during the catapult takeoff process was built.Based on the proposed model,the influence of the above factors on catapult take-off safety was analyzed.Moreover,the scales of several take-off factors which accord with the catapult take-off safety were computed.The results indicated that properly increasing the thrust force of electromagnetic launch system and enhancing the nose gear fast-extension force could help to decrease the flight path sinkage and guarantee the catapult take-off safety of the carrier-based aircraft under the condition of atrocious weather.关键词
舰载机/弹射起飞/电磁弹射器/安全准则/起飞性能/突伸力Key words
carrier-based aircraft/catapult take-off/electromagnetic launch system/safety criteria/take-off performance/fast-extension force分类
航空航天引用本文复制引用
李静,左斌,路翠华..应用电磁弹射器的舰载机起飞性能分析[J].海军航空工程学院学报,2012,27(2):121-126,6.
