CPC B64C 29/0016 (2013.01) [B64C 39/001 (2013.01)] | 22 Claims |
1. A vertical take-off and landing vehicle, comprising:
an airframe having an upper surface, a side surface and a lower surface and a central vertical axis;
a first plurality of axially oriented fans, each axially oriented fan in a channel extending from the upper surface to the lower surface of the airframe, the first plurality of axially oriented fans arranged in a circular pattern in an arc defined by a first radius r1 from the central vertical axis;
a second plurality of axially oriented fans, each axially oriented fan in a channel extending from the upper surface to the lower surface of the airframe, the second plurality of axially oriented fans arranged in a circular pattern in an arc defined by a second radius r2 from the central vertical axis;
a first intake channel extending from a front of the airframe to a rear of the airframe and comprising an upper level duct and a lower lever duct;
a first laterally-oriented fan in the upper level duct of the first intake channel;
a first lateral channel extending from and in fluid communication with the upper level duct of the first intake channel;
a second intake channel extending from the front of the airframe to the rear of the airframe and comprising an upper level duct and a lower level duct;
a second laterally-oriented fan in the upper level duct of the second intake channel;
a second lateral channel extending from and in fluid communication with the upper level duct of the second intake channel;
a third laterally-oriented fan in the first lateral channel and a fourth laterally-oriented fan in the second lateral channel; and
a plenum chamber in fluid communication with the upper level ducts of the first intake channel and the second intake channel; and
an annular inlet in the upper surface in fluid communication with the plenum chamber.
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