The invention is suitable for the field of rotorcrafts, and provides a vertical take-off and landing rotorcraft which comprises a rotorcraft body and further comprises a vertical take-off and landing device installed on one side of the rotorcraft body and used for controlling the rotorcraft body to ascend and descend under the condition that no runway exists; and a horizontal propelling device which is installed on one side of the machine body and used for propelling the machine body in the horizontal direction. The vertical take-off and landing rotorcraft has the advantages that the limitation that a conventional rotorcraft needs to run and take off on a runway is eliminated, and the vertical take-off and landing rotorcraft is suitable for take-off and landing in narrow regions; the vertical take-off and landing rotorcraft can get rid of and avoid dangerous factors caused by the fact that a conventional rotorcraft needs to run on a runway to take off and descend to a certain extent.
本发明适用于旋翼机领域,提供了一种垂直起降旋翼机,包括机身,还包括:垂直起降装置,所述垂直起降装置安装在机身的一侧,用于控制所述机身在无跑道的情况下实现升降;水平推进装置,所述水平推进装置安装在机身的一侧,用于对所述机身进行水平方向的推进动作。本发明优点在于:此垂直起降旋翼机摆脱解决了常规旋翼机需要跑道滑跑起飞的限制,适用于狭小的地域起飞及降落;此垂直起降旋翼机能在一定程度上摆脱避免了常规旋翼机需要跑道滑跑起飞、下降所带来的危险因素。
Vertical take-off and landing rotorcraft
一种垂直起降旋翼机
2021-09-07
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2023
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