The invention provides a double-rotor helicopter and fixed wing combined integrated manned aircraft, and relates to the field of aircraft design and manufacturing. The double-rotor helicopter and fixed wing combined integrated manned aircraft comprises an aircraft body, the aircraft body comprises a cockpit, wings are symmetrically arranged on the two sides of the cockpit, and power devices are arranged on the wings; each power device comprises a periodic variable-pitch propeller, the center line of the periodic variable-pitch propeller is parallel to the center line of the cockpit, empennages are arranged at the end, away from blades of the periodic variable-pitch propeller, of the periodic variable-pitch propeller, the empennages comprise vertical empennages perpendicular to the periodic variable-pitch propeller, and horizontal empennages are arranged between the vertical empennages; the vertical empennages comprise first empennages and second empennages, and the horizontal empennages are located at the ends, away from the periodic variable-pitch propeller, of the two first empennages. The aircraft can carry out horizontal flight and vertical flight by adjusting the flight attitude, and dependence on a runway is reduced.
本发明提出了一种双旋翼直升机与固定翼结合一体化载人飞行器,涉及飞行器设计及其制造领域。一种双旋翼直升机与固定翼结合一体化载人飞行器,包括飞行器主体,飞行器主体包括驾驶舱,驾驶舱两侧对称设置有机翼,机翼上均设置有动力装置;动力装置包括周期变距螺旋桨,周期变距螺旋桨的中心线与驾驶舱的中心线相互平行,周期变距螺旋桨远离其叶片的一端设置有尾翼,尾翼包括垂直于周期变距螺旋桨的垂直尾翼,垂直尾翼之间设置有水平尾翼;垂直尾翼包括第一尾翼和第二尾翼,水平尾翼位于两个第一尾翼远离周期变距螺旋桨的一端。其能够通过调节飞行姿态,实现水平飞行和竖直飞行,降低对跑道的依赖。
Double-rotor helicopter and fixed wing combined integrated manned aircraft
一种双旋翼直升机与固定翼结合一体化载人飞行器
2021-11-30
Patent
Electronic Resource
Chinese
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