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    • 8. 发明授权
    • Three wing, six tilt-propulsion units, VTOL aircraft
    • 三翼,六倾斜推进装置,垂直起落飞机
    • US08616492B2
    • 2013-12-31
    • US12900790
    • 2010-10-08
    • Richard David Oliver
    • Richard David Oliver
    • B64C29/00
    • B64D27/12B64C29/0033B64C29/0075B64C39/08B64D27/06Y02T50/44
    • A vertical takeoff and landing aircraft having a fuselage with three wings and six synchronously tilt-able propulsion units, each one mounted above, below, or on each half of the aforementioned three wings. The propulsion units are vertical for vertical flight, and horizontal for forward flight. The aircraft wings are placed such that the rear wing is above the middle wing which is placed above the front wing. The placement of each of the propulsion units relative to the center of gravity of the aircraft about the vertical axis inherently assures continued stability in vertical flight mode, following the loss of thrust from any one propulsion unit. The placement of the propulsion units, viewing the aircraft from the front, is such that each propulsion units' thrust wake does not materially disturb the propulsion unit to its rear. When engine driven propellers or rotors are utilized, flapped wing panels are attached outboard of the forward and/or rearward propulsion units to provide yaw control during vertical flight.
    • 垂直起飞和着陆飞机具有机身三翼和六个同步倾斜的推进单元,每个都安装在上述三翼的每一半的上方,下方或上方。 推进单元垂直垂直,垂直方向垂直。 飞机机翼被放置成使后翼位于放置在前翼上方的中间翼的上方。 随着从任何一个推进单元的推力损失,每个推进单元相对于飞机围绕垂直轴的重心的位置固有地确保垂直飞行模式的持续稳定性。 从前方观察飞行器的推进装置的放置使得每个推进装置的推力尾流不会将推进装置重大地打扰到其后部。 当使用发动机驱动的螺旋桨或转子时,翼板翼板被安装在前部和/或后部推进单元的外侧,以在垂直飞行期间提供偏航控制。