Vertical take-off and landing (VTOL) aircraft with distributed thrust and control
First Claim
1. A vertical take-off and landing (VTOL) aircraft, comprising a fuselage;
- a forward and an aft wing on each side of the fuselage, a plurality of spars on at least one side of the fuselage;
each spar having one end attached to one of the forward wings and the other end of each spar attached to at least one of the aft wings, a plurality of vertical take-off and landing (VTOL) cells attached directly to, and in a spaced relationship along each of said spars, each of said VTOL cells further comprising a motor, a motor controller, and a low inertia fixed pitched two blade propeller;
at least one forward thruster;
at least one power source connected to each VTOL cell motor and to said at least one forward thruster;
wherein the VTOL cells are retractable within the spars in order to take on an aerodynamic configuration.
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Abstract
An aircraft having a vertical take-off and landing (VTOL) propulsion system. The aircraft includes a fuselage, the VTOL propulsion system, at least one forward thruster, a power source used for both the VTOL propulsion system and forward thruster, fore and aft wings and a plurality of spars attached to and spanning the space between the two wings. The VTOL propulsion system includes a plurality of VTOL cells (including a motor, motor controller, and propeller) attached in a spaced relation along each spar. The VTOL cells are used exclusively for vertical flight or hovering and are powered down as the aircraft develops forward flight velocity and corresponding wing lift. During forward flight the VTOL propellers are articulated to allow the aircraft to take on a low drag configuration. The present invention is suitable for use in manned or un-manned aircraft of any scale.
127 Citations
48 Claims
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1. A vertical take-off and landing (VTOL) aircraft, comprising a fuselage;
- a forward and an aft wing on each side of the fuselage, a plurality of spars on at least one side of the fuselage;
each spar having one end attached to one of the forward wings and the other end of each spar attached to at least one of the aft wings, a plurality of vertical take-off and landing (VTOL) cells attached directly to, and in a spaced relationship along each of said spars, each of said VTOL cells further comprising a motor, a motor controller, and a low inertia fixed pitched two blade propeller;
at least one forward thruster;
at least one power source connected to each VTOL cell motor and to said at least one forward thruster;
wherein the VTOL cells are retractable within the spars in order to take on an aerodynamic configuration. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47, 48)
- a forward and an aft wing on each side of the fuselage, a plurality of spars on at least one side of the fuselage;
Specification