The invention discloses a flying device wing and a V-tail flying device, belongs to the technical field of flying devices, and solves the problems that in the prior art, when an empennage is unfolded, the structure is complex, the occupied space is large, and the requirement for a machine body is high. The flight device wing comprises a rotating mechanism and an empennage. The mounting seat is mounted on the machine body. The rotating structure comprises a guide piece and a torsion spring. And the guide piece is mounted on the mounting seat. And the empennage is arranged on the guide piece. One end of the torsion spring abuts against the installation base, the other end of the torsion spring abuts against the empennage, and when the empennage is located at the folding position, the torsion spring has preset torque. The first limiting structure is arranged on the fuselage, is in communication connection with the flight control system and is configured to limit the empennage to be located at the folding position. And the second limiting structure is arranged on the mounting seat and is configured to limit the empennage rotating to the unfolding position. The torsion spring drives the empennage to rotate, the structure is simple, the occupied space is small, and the requirement for the machine body is low.
本申请公开了一种飞行装置机翼及V尾飞行装置,属于飞行装置技术领域,解决了现有技术中尾翼展开时结构复杂、占用空间大以及对机体要求高的问题。该飞行装置机翼包括旋转机构和尾翼。安装座安装在机身上。旋转结构包括导向件和扭力弹簧。导向件安装在安装座上。尾翼设置在导向件上。扭力弹簧的一端与安装座抵接,扭力弹簧的另一端与尾翼抵接,当尾翼处于折叠位置时,扭力弹簧具有预设扭矩。第一限位结构设置在机身上,并与飞控系统通信连接,被配置为限位尾翼处于折叠位置。第二限位结构设置在安装座上,被配置为限位旋转至展开位置的尾翼。本申请通过扭力弹簧带动尾翼旋转,结构简单、占用空间较小且对机体的要求低。
Flying device wing and V-tail flying device
一种飞行装置机翼及V尾飞行装置
2023-11-28
Patent
Electronic Resource
Chinese
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