A hybrid aircraft (1) of the unmanned type is described, the aircraft being configured for combined and optimized use of aerostatic and aerodynamic forces, the aircraft comprising an inflatable body (10) comprising an outer shell (11) and a load bearing structure (20) inside said outer shell (11), the inflatable body (10) is adapted to adopt a closed wing operating configuration.
描述了一种无人驾驶型的混合动力飞行器(1),该飞行器被构造成用于将空气静力和空气动力结合且经优化地进行使用,该飞行器包括可充气本体(10),该可充气本体(10)包括外壳体(11)和在所述外壳体(11)内部的载荷支承结构(20),所述可充气本体(10)适于采用闭合翼操作构型。
Unmanned hybrid inflatable aircraft
无人驾驶型混合动力可充气飞行器
2023-09-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |