Hybrid power dual coaxial ipsilateral reversal tilt-rotor aircraft

• Main Authors: ZHAO XINXIN, LI HONGMIAO, ZHANG BING, CHENG JING, ZENG RUI, TANG YUNXIAO, XIONG JUN
• Format: Patent
• Language: Chinese; English
• Published: 06.02.2018
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention discloses a hybrid power dual coaxial ipsilateral reversal tilt-rotor aircraft. The hybrid power dual coaxial ipsilateral reversal tilt-rotor aircraft comprises a fuselage, a tilt spindle arranged on the fuselage, a tilt wing arranged on the tilt spindle and rotor wing nacelles arranged at the two ends of the tilt spindle, wherein each rotor wing nacelle comprises a first rotor wingand a second rotor wing which are coaxially arranged and opposite in rotation directions, and the first rotor wing and the second rotor wing are arranged at the same end of the rotor wing nacelle. Thehybrid power dual coaxial ipsilateral reversal tilt-rotor aircraft disclosed by the invention adopts dual rotor wing layout, pneumatic pulling force on each rotor wing is relatively obviously increased and is increased by about 18-20% in each state, and flight performance is improved. 本发明公开了种混合动力双共轴同侧反转倾转旋翼飞行器，包括机身、设置于机身上的倾转主轴、设置于倾转主轴上的可倾转机翼和设置于倾转主轴两端的旋翼短舱，所述旋翼短舱包括同轴设置且转动方向相反的第旋翼和第二旋翼，第旋翼和第二旋翼位于旋翼短舱的同端。本发明的混合动力双共轴同侧反转倾转旋翼