The invention discloses a small unmanned aerial vehicle load fairing which is of a split type structure and comprises an upper fairing body (1) and a lower fairing body (2), the upper fairing body (1) and the lower fairing body (2) are of a thin shell structure and are in shape follow-up design with a load (3), the load (3) is wrapped, the upper fairing body (1) is located above the load (3) and connected with a support of the load (3), and the lower fairing body (2) is located behind the load (3) and connected with a support of the load (3). And the machine body structure (4) is connected. The pneumatic rectification valve has high pneumatic rectification performance, production and machining are easy, and the product cost is reduced.
本发明公开了一种小型无人机载荷整流罩,采用分体式结构,包括上整流罩(1)、下整流罩(2),所述上整流罩(1)、下整流罩(2)采用薄壳结构,与载荷(3)随形设计,将所述载荷(3)包裹,所述上整流罩(1)位于载荷(3)上方,并与载荷(3)支架连接,所述下整流罩(2)位于载荷(3)后方,与机体结构(4)连接。本发明具有较高的气动整流性能,生产加工简单,降低了产品成本。
Small unmanned aerial vehicle load fairing
一种小型无人机载荷整流罩
2023-05-05
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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