The invention relates to a vertical take-off and landing aircraft configuration and a vertical take-off and landing aircraft, belongs to the technical field of aircrafts, solves the problems existing in the current vertical take-off and landing aircraft configuration, comprises a fuselage provided with at least one propelling device, and is characterized in that a front fixed wing is arranged at the front end of the fuselage, and a rear fixed wing is arranged at the tail end of the fuselage; the front fixed wings and the rear fixed wings are arranged in a staggered mode, the rear fixed wings are higher than the front fixed wings, the front fixed wing parts on the two sides of the fuselage are connected with at least one rotor wing mechanism, each rotor wing mechanism comprises a longitudinal arm fixed to the corresponding front fixed wing, the longitudinal arms are fixed to the rear fixed wings through vertical wings, and each longitudinal arm is provided with at least one lifting device. By the adoption of the structure, the occupied space of the vertical take-off and landing aircraft is reduced, and the applicability is higher.
本发明涉及一种垂直起降飞行器构型及垂直起降飞行器,属于飞行器技术领域,解决了当前垂直起降飞行器构型存在的问题,包括机身,机身设有至少一个推进装置,其特征在于,机身前端设有前固定翼,尾端设有后固定翼,沿竖直方向,前固定翼和后固定翼错开设置,后固定翼的高度高于前固定翼的高度,机身两侧的前固定翼部分与至少一个旋翼机构连接,旋翼机构包括与前固定翼固定的纵臂,纵臂通过垂翼与后固定翼固定,纵臂设有至少一个提升装置,采用本发明的构型减少了垂直起降飞行器的占用空间,适用性更强。
Vertical take-off and landing aircraft configuration and vertical take-off and landing aircraft
一种垂直起降飞行器构型及垂直起降飞行器
2025-02-18
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Variable-configuration vertical take-off and landing aircraft
European Patent Office | 2023
|