aircraft
A technology of aircraft and fuselage, which is applied in the field of aircraft, and can solve problems such as insufficient flexibility of aircraft pitching or steering performance
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[0023] The aircraft of the present invention will be described in detail below in conjunction with the accompanying drawings.
[0024] see Figure 1-9 , respectively show perspective views of the aircraft of the present invention in different implementations and different viewing angles from different angles and assembled states.
[0025] see Figure 1~6 , shows an aircraft 100 according to a first embodiment of the present invention. It is an aircraft in the form of a glider. Its composition includes a fuselage 101 , a main wing 102 , a V-shaped tail 103 , a V-shaped tail rudder 104 and a ducted propeller 114 . The structure of the aircraft 100 is basically the same as that of the existing glider. For example, its main wing 102 is fixed on the front part of the fuselage 101 along its central axis, and the main wing 102 is provided with an aileron 102A. The propeller 114 is suspended vertically below the main wing 102 . The axial direction of the central axis of the fusel...
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