Patent ID: 11952151
Assignee: AUTOFLIGHT (KUNSHAN) CO., LTD.
Field: Transport (Mechanical engineering)
Classification: CPC B  H  Y | IPC B

Claim 1:
2. The vertical tail for the composite-wing UAV according to claim 1, characterized in that the shock absorbing component (4) further comprises a cushioning foot (43); wherein the cushioning foot (43) comprises a buffer plate (431) and a connecting frame (432); wherein an end of the buffer plate (431) disposed away from the shock absorber (41) has a curved surface; the connecting frame (432) is hinged with a first end of the shock absorber (41) disposed away from the lower end plate (111); the connecting frame (432) is provided with a plurality of assembly holes (4321), the assembly holes (4321) are suitable for mounting an expansion structure.