Tilt wing aircraft
A tilt-wing, aircraft technology, applied in the direction of rotorcraft, vertical take-off and landing aircraft, aircraft, etc., can solve problems such as erosion, and achieve the effect of maintaining stability
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[0031] In order to explain in detail the technical content, structural features, achieved goals and effects of the technical solution, the following will be described in detail in conjunction with specific embodiments and accompanying drawings.
[0032] refer to Figure 1-3 , the aircraft with tiltable wings has a fuselage 10, and the cockpit is located under the windshield 11. The tail of the fuselage 10 is provided with a vertical empennage 12, and a rudder 14 is also arranged on the vertical empennage 12. A horizontal stabilizer 16 is also installed on the empennage 12 , and two elevators 18 are provided on the horizontal stabilizer 16 .
[0033]Three inclined wings are mounted on the fuselage 10 : a front wing 20 , a middle wing 22 and a rear wing 24 . Wings 20, 22 and 24 (which are also referred to as main wings) are respectively mounted on and are rotatable about rotational tilt axes 20D, 22D and 24D. Tilt axes 20D, 22D and 24D are transverse to the longitudinal axis ...
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