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    • 20. 发明授权
    • Hybrid flying wing
    • 混合飞翼
    • US06860449B1
    • 2005-03-01
    • US10197358
    • 2002-07-16
    • Zhuo Chen
    • Zhuo Chen
    • B64B1/06B64B1/32B64B1/34B64C29/00
    • B64B1/32B64B1/06B64B1/34B64B2201/00B64C29/0025B64D2211/00Y02T50/55
    • An aircraft has a flying wing and two wingtip hulls installed on the wingtips of the flying wing. Both of the wingtip hulls contain lighter-than-air gas to generate static lift. These wingtip hulls not only contribute to lift-generating but also help the aircraft achieve roll stability and control. Forward propulsion systems are installed at the upper-front positions of the flying wing. When vertical and/or short take-off and landing (V/STOL) capability is required, one or more lift-fan propulsion systems can be installed on the flying wing. The lift-fan propulsion systems can either be driven by their own engines or by the power transmitted from the forward propulsion systems. Payload can be carried inside the flying wing or be hung under or held above the flying wing.
    • 一架飞机有一个飞翼和两个翼尖船体安装在飞翼的翼尖上。 两个翼尖外壳都含有比空气中的气体产生静电提升。 这些翼尖不仅有助于提升发电,还有助于飞机实现滚筒的稳定性和控制。 前进推进系统安装在飞翼的上前位置。 当需要垂直和/或短起飞和着陆(V / STOL)能力时,可以在飞翼上安装一个或多个升降机推进系统。 电梯风扇推进系统可以由自己的发动机或从前进推进系统传递的动力驱动。 有效载荷可以在飞行翼内进行,或者悬挂在飞翼下面或者悬挂在飞翼上。