Swivel hinge of tail rotor blades for helicopter models

• 1. 直升机旋转式电动直驱变距尾桨总成及直升机 [P] . 中国专利： CN109606646B . 2021.11.19
• 2. 直升机旋转式电动直驱变距尾桨总成及直升机 [P] . 中国专利： CN109606646A . 2019-04-12
• 3. Helicopter with foldable tail beam - has perpendicular hinge near forward end of tail beam and foldable main rotor blades [P] . IT1032070B . 1979-05-30

  机译： 带有可折叠尾梁的直升机-在尾梁的前端附近具有垂直铰链，并且可折叠主旋翼桨叶

• 4. Rotor for model helicopter and aircraft has rotor blades connected to hub via film hinges [P] . 德国专利： DE20314043U1 . 2004-04-15

  机译： 用于模型直升机和飞机的转子具有通过薄膜铰链连接到轮毂的转子叶片

• 5. Rotor for model helicopter and aircraft has rotor blades connected to hub via film hinges [P] . 德国专利： DE20314043U1 . 2004-03-11

  机译： 用于模型直升机和飞机的转子具有通过薄膜铰链连接到轮毂的转子叶片

• 1. Simulation on Helicopter Scissors Tail-Rotor Noise Based on N-S Equations and F1A Formulas [J] . Meng Xiaowei, Xu Guohua, Shi Yongjie, 南京航空航天大学学报（英文版） . 2017,第006期
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• 4. Modeling and Dynamic Analysis for the Foundation of a Blade-Rotor System [J] . Liang Anyang, Huang Guoyuan, Zhang Yuetong, 南京航空航天大学学报（英文版） . 2017,第003期
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• 9. THEORY OF SELF-EXCITED MECHANICAL OSCILLATIONSnOF HELICOPTER ROTORS WITH HINGED BLADES CHAPTER I THEORY OF SELF-EXCITED MECHANICAL OSCILLATIONSnOF HINGED ROTOR BLADES [R] . Robert P. Coleman 1957

• 1. Using of Particle Swarm for Performance Optimization of Helicopter Rotor Blades [J] . Giorgio Guglieri . 应用数学（英文） . 2012,第10期
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• 3. 直升机旋翼-尾桨对建筑物的气动干扰研究 [A] . 程蒙 . 2021