Vertical/Short Take-Off and Landing Aircraft

作者: Gert Lundgren

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摘要: A vertical/short take-off and landing aircraft with a single proprotor assembly that has pair of inline counter-rotating rotors. Two engines are directly connected to the One engine is shut down in horizontal flight improve efficiency. Gimbal mounting permits thrust be directed forward back left right control pitch roll when hovering. Varying relative speeds controls yaw. The adaptable as an unmanned vehicle.

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