The invention discloses a rotor aircraft capable of vertically taking off and landing. The rotor aircraft comprises a fuselage, wings, a propeller, rotors, an empennage and an undercarriage, wherein the front part of the fuselage is a closed cockpit; a power device, a luggage compartment, a transmission system, a control system and the like are arranged in the fuselage; the tail of the fuselage isprovided with a tail beam; the empennage is installed at the tail end of the tail beam; the wings are located on the left side and the right side of the middle of the fuselage and provide an installation point for the propeller and can also provide considerable lift force when the aircraft flies horizontally; one side of each wing is provided with an aileron and a flap, the ailerons provide rolling torque, and the flaps provide lift force. The rotor aircraft combines the advantages of a helicopter, a fixed-wing aircraft and a gyrocopter, has the vertical take-off and landing and ultralow-altitude flight capacity of the helicopter, also has the high-speed flight capacity of the fixed-wing aircraft, and further has the characteristics of high safety and low energy consumption of the gyrocopter, thereby meeting wider use requirements, and being beneficial to popularization and application.
本发明公开了一种可垂直起降的旋翼航空器,包括机身、机翼、螺旋桨、旋翼、尾翼与起落架,所述机身的前部是封闭式驾驶舱,所述机身的内部设置有动力装置、行李舱、传动系统,操控系统等,所述机身的尾部是尾梁,尾梁末端安装有尾翼,所述机翼位于机身的中部左右两侧,为螺旋桨提供安装点,也可以在航空器水平飞行时提供可观的升力,所述机翼的一侧设置有副襟翼,其中副翼提供滚转力矩,襟翼提供升力。本发明结合了直升机,固定翼飞机及自转旋翼机的优点,具备直升机的垂直起降和超低空飞行能力,也具备固定翼飞机的高速飞行能力,还具备自转旋翼机安全性高和能耗低的特点,满足了更广泛的使用需求,有利于推广使用。
Rotor aircraft capable of vertically taking off and landing
一种可垂直起降的旋翼航空器
2020-10-13
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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