Multi-point power tail supporting vertical takeoff and landing aircraft

A multi-point power tail support vertical takeoff and landing aircraft belongs to the technical field of aircrafts. The utility model provides a multi-point power tail support vertical takeoff and landing aircraft. The multi-point power tail support vertical takeoff and landing aircraft is character...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ZHENG PEIYING, LIU KAI
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:A multi-point power tail support vertical takeoff and landing aircraft belongs to the technical field of aircrafts. The utility model provides a multi-point power tail support vertical takeoff and landing aircraft. The multi-point power tail support vertical takeoff and landing aircraft is characterized by comprising an aircraft body, wings, a power device and a takeoff and landing support frame, the number of the power devices is not less than three; an included angle larger than 45 degrees is formed between the landing support frame supporting face of the landing support frame and an aircraft transverse rolling shaft of the multi-point power tail supporting vertical landing aircraft. The flight attitude of the aircraft can be stably controlled at a low speed, and runway-free takeoff and landing of the fixed-wing aircraft can be realized. 多点动力尾部支撑垂直起落飞机属于飞行器技术领域。本实用新型提供了多点动力尾部支撑垂直起落飞机,其特征在于:所述多点动力尾部支撑垂直起落飞机包括飞机机体、机翼、动力装置、起落支撑架;所述动力装置不少于三具;所述起落支撑架的起落支撑架支撑面与所述多点动力尾部支撑垂直起落飞机的飞机横滚轴形成夹角大于45度。本实用新型可以实现低速时能够稳定控制飞行姿