Development and application of strength design technology of advanced carrier-based aircraft

被引:0
|
作者
Cao, Qikai [1 ]
Wang, Yan [1 ]
Yao, Niankui [1 ]
He, Gang [1 ]
Chen, Zhongming [1 ]
Zhang, Guijiang [1 ]
Tian, Zhiliang [1 ]
Wu, Xinyue [1 ]
机构
[1] AVIC Shenyang Aircraft Design and Research Institute, Shenyang,110031, China
关键词
Landing gear (aircraft) - Lift - Aircraft manufacture - Drag - Fighter aircraft - Wings - Airframes - Loads (forces);
D O I
暂无
中图分类号
学科分类号
摘要
Carrier-based aircraft is the main weapon in aircraft carrier. In order to meet the requirements of taking off, landing and parking, the design of the carrier aircraft must be centered around characteristic structures such as the landing gear system, arresting hook system, and wing folding system. The impact energy of the advanced carrier aircraft is more than 6 times that that of the land-based aircraft, and the horizontal load brought by interception is 15 times higher than that of the land-based aircraft. Therefore, high load on the characteristic structures presents higher requirements on the strength design. This paper details the design work around the characteristic structures and characteristic loads of the carrier aircraft, including calculation of characteristic loads, i.e. landing gear load, barrage load and folding load; strength design and test verification of characteristic structures including dynamic simulation of the landing gear system, barrage system and wing folding system, static/fatigue strength analysis, flutter analysis of folding wing surface, and post-test analysis of the impact of drag force on the body structure strength; analysis of dynamic response of landing on ship and influence of the combined action of landing load and barrage load on the strength of the aircraft structure; discussion of the test verification methods reflecting the strength characteristics of the characteristic structures of the carrier aircraft. The above research results have been successfully applied to the design of advanced carrier aircraft. © 2021, Beihang University Aerospace Knowledge Press. All right reserved.
引用
收藏
相关论文
共 50 条
  • [21] Carrier-based aircraft approach power compensator system design based on fuzzy logic techniques
    Man, Cuifang
    Jiang, Ju
    Wang, Xinhua
    Zheng, Sheng
    Qiu, Haijun
    Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 2010, 42 (05): : 656 - 660
  • [22] Match characteristics of aircraft-carrier parameters during catapult takeoff of carrier-based aircraft
    Liu, Xingyu
    Xu, Dongsong
    Wang, Lixin
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (01): : 102 - 108
  • [23] The Application of Ship Motion Prediction for Ensuring the Safety of Takeoff and Landing of Carrier-Based Aircraft
    Tkachenko, O. I.
    Kovtun, S. A.
    Dubov, Y. B.
    2019 26TH SAINT PETERSBURG INTERNATIONAL CONFERENCE ON INTEGRATED NAVIGATION SYSTEMS (ICINS), 2019,
  • [24] Research progress in guidance and control of automatic carrier landing of carrier-based aircraft
    College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
    210016, China
    Hangkong Xuebao, 2
  • [25] DYNAMIC RESPONSE ANALYSIS OF CARRIER-BASED AIRCRAFT DURING LANDING
    段萍萍
    聂宏
    魏小辉
    Transactions of Nanjing University of Aeronautics and Astronautics, 2013, (04) : 306 - 316
  • [26] Dynamic response analysis of carrier-based aircraft during landing
    Duan, Pingping
    Nie, Hong
    Wei, Xiaohui
    Transactions of Nanjing University of Aeronautics and Astronautics, 2013, 30 (04) : 306 - 316
  • [27] Parameter suitability envelope for safety bolter of a carrier-based aircraft
    Lin J.
    Wu G.
    Wang L.
    Liu H.
    Wang Y.
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 45 (09): : 1777 - 1786
  • [29] Dynamic modeling and analysis of carrier-based aircraft and arresting hook
    Ding, Zhishen
    Ouyang, Bin
    Liu, Yong
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2024, 46 (05): : 131 - 140
  • [30] Numerical simulation on the RCS of carrier-based electronic warfare aircraft
    Yue, Kui-Zhi
    Jia, Zhong-Hu
    Ji, Jin-Zu
    Su, Min
    Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2014, 36 (05): : 852 - 858