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Distributed Electric Propulsion Modular Wing Aircraft with Blown Wing and Extreme Flaps for VTOL and/or STOL Flight

机译:分布式电动推进模块化翼飞机与吹翼和vtol和/或stol飞行的极端襟翼

摘要

An aircraft wing configuration for a vertical or a short take-off and landing aircraft having a plurality of propeller-blown wings mounted at different longitudinal locations along a fuselage of the vertical take-off and landing aircraft, producing two or more lifting surfaces, fixed at a predetermined acute wing angle greater than 0° and substantially less than 90° relative to a horizontal plane, and having a plurality of flaps disposed behind the wings. The configuration has a plurality of propellers distributed in front of the plurality of wings producing two or more lifting surfaces and mounted such that the wings are externally blown by forced airstreams from the propellers. The propellers produce distributed thrust components, and the plurality of flaps are in the forced airstreams of the propellers when one or more of the flaps is in an extended position.
机译:用于垂直或短起飞和着陆飞机的飞机翼配置,该飞机具有沿着垂直起飞和着陆飞机的机身安装在不同的纵向位置处的多个螺旋桨吹式机翼,产生两个或更多个提升表面,固定 在预定的急性翼角,相对于水平面的大于0°并且基本上小于90°,并且具有设置在翼后面的多个襟翼。 该构造具有多个螺旋桨分布在多个翼的前面,产生两个或更多个升降表面并安装成使得翅膀由来自螺旋桨的强制气流外部吹来。 螺旋桨产生分布式推力部件,当一个或多个襟翼处于伸出位置时,多个襟翼处于螺旋桨的强制气流中。

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