Tilt rotor aircraft adopting parallel coaxial dual rotors
A coaxial dual-rotor and tilt-rotor technology, which can be used in rotorcraft, aircraft, motor vehicles, etc., and can solve problems such as small footprint
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[0036] See figure 1 , figure 2 , image 3 , Figure 4 , Figure 5 , Figure 6 , as shown, its specific implementation is as follows:
[0037] The present invention adopts the tilt rotor aircraft of parallel coaxial double rotors, adopts the design of conventional aerodynamic layout; it is composed of fuselage 1, wing 2, horizontal stabilizer 7 of empennage, elevator 8, vertical stabilizer 14, Rudder 15, pitch control tail rotor system 6 (including tail rotor blade 16, tail rotor hub 17, tail rotor shaft 18, tail rotor pitch change mechanism 19), wingtip small wheel 11, landing gear 12, power system (engine ) 24 and fuel system 25, clutch 26 of transmission system, gear box 27, transmission shaft 28, rotor system 9 (including rotor blade 20, rotor hub 21, rotor shaft 22, rotor pitch change mechanism 23), rotor nacelle 10. The tilting system 29 is composed; the wing 2 is installed in the middle section of the fuselage 1, the empennage and the pitch control tail rotor syst...
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