基于倾斜尾桨垂直起降鸭式改型三旋翼机的试制

The Proceedings of The 8th International Conference on Intelligent Systems and Image Processing 2021 Pub Date : 1900-01-01 DOI:10.12792/icisip2021.035

K. Hayama, Tomohiro Kudou, H. Irie

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引用次数: 0

摘要

在倾斜尾桨三旋翼直升机的基础上，进行了新型鸭式垂直起降(VTOL)概念机的试制，用于空中、观测和研究。从垂直飞行到水平飞行的连续过渡可以通过倾斜由鸭翼支撑的尾桨来完成。水平飞行时机翼的升力支撑着飞机的重量，降低了飞机的动力消耗，扩大了飞机的飞行面积。

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Trial Production of Modified Tricopter Based Vertical Take-off Landing Canard Aircraft with Tilt Tail Rotor

The trial production of a new concept vertical take-off and landing (VTOL) canard aircraft based on the modified tricopter with tilt tail rotor was carried out for aerial, observation and research. Continuous transition from vertical to horizontal flight can be done by tilting the tail rotor supported with canard wing. The lift of wing during horizontal flight supported the weight of the aircraft, and its causes the reduction of power consumption and extend the flight area.

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The Proceedings of The 8th International Conference on Intelligent Systems and Image Processing 2021

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