An electric arrangement for acceleration in soil of sustentacao rotor wing aircraft not in flight automatic LED

• 1. 一种具有可变距跷跷板式旋翼头的重型自转旋翼机混合动力跳飞系统 [P] . 中国专利： CN105966609B . 2019.11.26
• 2. 一种具有可变距跷跷板式旋翼头的重型自转旋翼机混合动力跳飞系统 [P] . 中国专利： CN105966609A . 2016-09-28
• 3. Flight regulating arrangement for automatic flying of aircraft e.g. micro aircraft has two regulating device whereby sensor values determines the current flight conditions, which are controlled by actuators [P] . 德国专利： DE102005037091A1 . 2007-02-15

  机译： 用于飞机自动飞行的飞行调节装置，例如微型飞机有两个调节装置，传感器值可以确定当前的飞行状态，并由执行器控制

• 4. Improvements to the rotors of rotary-wing aircraft has blades a folding and automatic installation of electrical connection of the blades [P] . 法国专利： FR2818238B1 . 2003-03-28

  机译： 旋翼飞机旋翼的改进包括叶片的折叠和叶片叶片电连接的自动安装

• 5. Rotary-wing aircraft rotors with automatically folding blades and electrical connection installation for the blades [P] . 美国专利： US6485261B2 . 2002-11-26

  机译： 旋翼飞机旋翼，具有自动折叠的叶片和叶片的电气连接装置

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• 6. Air ambulance flights in northern Norway 2002-2008. Increased number of secondary fixed wing (FW) operations and more use of rotor wing (RW) transports [O] . Jan Norum, Trond M Elsbak 2011
• 7. Trim Strategy, Control Model, and Flight Dynamics Characteristics of Canard Rotor/Wing Aircraft in Transition Mode [O] . Honggang Gao, Zhenghong Gao, Yang Na, 2019
• 8. Flight-Test and Simulation Evaluation of the Longitudinal Final Approach and Landing Performance of an Automatic System for a Light Wing Loading STOL Aircraft Equipped with Wing Spoilers [R] . Brown, S. C., Hardy, G. H., Hindson, W. S. 1984

• 1. Adaptive Kalman Filter of Transfer Alignment with Un-modeled Wing Flexure of Aircraft [J] . 周峰 ,孟秀云 . 北京理工大学学报：英文版 . 2008,第4期
• 2. 固定翼涡桨飞机续航性能影响因素敏感性研究 [C] . Zhang Xiao ,张晓 ,Wang Zhuo . 2017年（第三届）中国航空科学技术大会 . 2017
• 3. 直升机大机动飞行中旋翼非定常空气动力研究 [A] . 徐进 . 2007