A triphibian cross-medium transverse tilting double-rotor aircraft comprises a fuselage, wings and tilting rotor mechanisms, the wings are symmetrically arranged on the left side and the right side of the fuselage, rotor mechanism mounting holes are formed in the middles of the wings, and the tilting rotor mechanisms are arranged in the rotor mechanism mounting holes; a ventral fin is arranged below the rear part of the fuselage, a V tail is arranged above the rear part of the fuselage, and a control surface is arranged on the V tail; an upper reverse winglet and a lower reverse winglet are respectively arranged at the tip of the wing, and an aileron is arranged at the rear edge of the wing; a water tank is arranged in the root of the wing, a vent hole is formed in the top of the water tank, a waterproof vent valve is arranged at the vent hole, a water through hole is formed in the lower part of the water tank, and a throttle valve is arranged at the water through hole; a water pumping opening in one end of the bidirectional water pump is communicated with the water through hole of the water tank through a water conveying pipeline; a water changing hole is formed in the bottom of the machine body, a water pumping opening in the other end of the two-way water pump communicates with the water changing hole through a water conveying pipeline. The aircraft disclosed by the invention has the capabilities of flying in the air, sailing on the water surface and sneaking underwater, and all modes can be freely switched.
一种三栖跨介质横列倾转双旋翼飞行器,包括机身、机翼及倾转旋翼机构;机翼对称设在机身左右两侧,机翼中部设有旋翼机构安装孔,倾转旋翼机构设在旋翼机构安装孔内;机身后部下方设有腹鳍,机身后部上方设有V尾,V尾上设有舵面;机翼翼尖处分别设有上反小翼和下反小翼,机翼后缘处设有副翼;机翼翼根处内部设有水箱,水箱顶部设有通气孔,通气孔处设有防水透气阀,水箱下部设有通水孔,通水孔处设有节流阀;机身内部设有双向水泵,双向水泵的一端泵水口通过输水管道与水箱通水孔相连通;机身底部设有换水孔,双向水泵的另一端泵水口通过输水管道与换水孔相连通。本发明的飞行器具备在空中飞行、水面航行及水下潜行的能力,各模式间可自由切换。
Triphibian cross-medium transverse tilting double-rotor aircraft
一种三栖跨介质横列倾转双旋翼飞行器
08.02.2022
Patent
Elektronische Ressource
Chinesisch