航空学报 > 2023, Vol. 44 Issue (S1): 727516-727516   doi: 10.7527/S1000-6893.2022.27516

民用飞机高升力系统先进技术及发展

马高杰(), 安刚, 史佑民, 康宁, 孙军帅   

  1. 庆安集团有限公司,西安 710077
  • 收稿日期:2022-05-14 修回日期:2022-06-01 接受日期:2022-07-12 出版日期:2023-06-25 发布日期:2022-07-21
  • 通讯作者: 马高杰 E-mail:magj006@avic.com

Advanced technology and development of high lift system for civil aircraft

Gaojie MA(), Gang AN, Youmin SHI, Ning KANG, Junshuai SUN   

  1. Qing’an Group Co. ,Ltd. ,Xi’an 710077,China
  • Received:2022-05-14 Revised:2022-06-01 Accepted:2022-07-12 Online:2023-06-25 Published:2022-07-21
  • Contact: Gaojie MA E-mail:magj006@avic.com

摘要:

分析了现有飞机高升力系统技术的发展现状、存在的技术问题或技术瓶颈,对新一代典型飞机高升力系统采用的先进技术进行了研究。结合绿色航空理念、利用TRIZ(Theory of Inventive Problem Solving)动态性进化创新理论对未来或下一代民用飞机高升力系统先进技术的发展趋势进行了推演和预测,着重从飞机层级、系统层级、关键部件技术和材料等不同维度开展分析研究工作。获得了未来或下一代民用飞机高升力系统先进技术的发展方向和趋势,所得结论可为后续民用飞机高升力系统先进技术应用提供支持和参考。

关键词: 高升力系统, 智能机翼, 机翼变弯度, 襟翼差动, 电子力矩限制, 自适应翼型

Abstract:

This paper analyzes thedevelopmentstatus, existing technical problems and key technology ofthe conventional aircrafthigh-lift-system, and deduces and predicts the development trend of the high lift system technology for the future and next generation aircraft,based on the research of the advanced technology adopted by the high-lift-system for the typical aircraft of the latest generation, and combining the green aviation concept and the TRIZ (Theory of Inventive Problem Solving) dynamic evolution innovation theory. In particular, we analyze it from different levels such as the aircraft level, the system level, the critical partsand materials. Our conclusionprovidestechnical support and reference for subsequent civil aircraft high lift systems.

Key words: high lift system, intelligent wing, variable camber wing, differential control flap, electronic torque limiter, adaptive airfoil

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