Distributed propulsion system for vertical take off and landing closed wing aircraft
AssigneeTextron Innovations Inc.
InventorsCarlos Alexander Fenny, Rohn Lee Olson, Andrew James Zahasky
Life of this patent
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AssigneeTextron Innovations Inc.
InventorsCarlos Alexander Fenny, Rohn Lee Olson, Andrew James Zahasky
Estimating the term…
An aircraft comprises a fuselage, first and second wing segments each having a leading edge and a trailing edge, a plurality of spokes coupling the fuselage to the first and second wing segments, one or more motors disposed within or attached to the plurality of spokes, and three or more propellers proximate to a leading edge of the plurality of spokes, distributed along the plurality of spokes, and operably connected to the motors to provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight and provide thrust whenever the aircraft is in forward flight. When the aircraft is in vertical takeoff and landing and stationary flight, the fuselage is approximately vertical. When the aircraft is in forward flight, the fuselage is approximately in the direction of the forward flight and extends forward beyond the leading edges of the first wing segment and the second wing segment.
An aircraft capable of vertical takeoff and landing, stationary flight and forward flight, the aircraft comprising:
An aircraft capable of vertical takeoff and landing, stationary flight and forward flight, the aircraft comprising:
An aircraft capable of vertical takeoff and landing, stationary flight and forward flight, the aircraft comprising:
Dependencies are inferred from the claim text.