Winged multi-rotor flying craft with payload accomodating shifting structure and automatic payload delivery
First Claim
1. A vertical takeoff/landing capable flying multi-engine aircraft without elevator or rudder surfaces, comprising:
- at least one lifting airfoil without elevator or rudder surfaces;
first and second strut apertures disposed in the airfoil, opposite each other from a vertical bisecting plane of the airfoil;
struts disposed through the strut apertures, first and second ends of each of the struts disposed on opposite vertical sides of the airfoil, wherein the struts are adjustably attached to the airfoil,wherein the strut apertures are adapted to accommodate vertical translation and horizontal translation of the airfoil in reference to the struts disposed through the strut apertures;
a first plurality of engines attached to the first end of the struts, wherein an attachment position of the first plurality of engines to the struts is horizontally adjustable;
a second plurality of engines attached to the opposite second end of the struts, wherein an attachment position of the second plurality of engines to the struts is horizontally adjustable; and
a computerized engine controller, controlling respective thrusts of the first and second plurality of engines to enable the aircraft to vertically lift off/land and re-orient the aircraft to horizontally fly, and perform thrust-initiated elevator and rudder emulating flight.
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Accused Products
Abstract
A vertical takeoff/landing capable, multi-engine aircraft with an airfoil without elevator or rudder surfaces is provided. Strut apertures accommodate vertical and horizontal translation of the airfoil in reference to engine supporting struts which are disposed through the apertures, opposite ends of the struts extending to opposite sides of the airfoil, wherein the struts are adjustably attached to the airfoil. A first and second plurality of engines are attached to ends of the struts, an attachment position of the plurality of engines to the struts is horizontally adjustable. A computerized engine controller, controls thrusts of the engines, to enable the aircraft to vertically lift off/land and re-orient itself to horizontally fly, and perform thrust-initiated elevator and rudder emulating flight. An external payload-to-delivery mating mechanism is attached to the bottom of the payload, which mates to a pole leading to the payload receptacle. Transceivers facilitate precise transfer of the payload.
79 Citations
20 Claims
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1. A vertical takeoff/landing capable flying multi-engine aircraft without elevator or rudder surfaces, comprising:
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at least one lifting airfoil without elevator or rudder surfaces; first and second strut apertures disposed in the airfoil, opposite each other from a vertical bisecting plane of the airfoil; struts disposed through the strut apertures, first and second ends of each of the struts disposed on opposite vertical sides of the airfoil, wherein the struts are adjustably attached to the airfoil, wherein the strut apertures are adapted to accommodate vertical translation and horizontal translation of the airfoil in reference to the struts disposed through the strut apertures; a first plurality of engines attached to the first end of the struts, wherein an attachment position of the first plurality of engines to the struts is horizontally adjustable; a second plurality of engines attached to the opposite second end of the struts, wherein an attachment position of the second plurality of engines to the struts is horizontally adjustable; and a computerized engine controller, controlling respective thrusts of the first and second plurality of engines to enable the aircraft to vertically lift off/land and re-orient the aircraft to horizontally fly, and perform thrust-initiated elevator and rudder emulating flight. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. An automatic payload delivery system, comprising:
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a vertical takeoff/landing capable flying multi-engine aircraft without elevator or rudder surfaces, comprising; at least one lifting airfoil without elevator or rudder surfaces; first and second strut apertures disposed in the airfoil, opposite each other from a vertical bisecting plane of the airfoil; struts disposed through the strut apertures, first and second ends of each of the struts disposed on opposite vertical sides of the airfoil, wherein the struts are adjustably attached to the airfoil, wherein the strut apertures are adapted to accommodate vertical translation and horizontal translation of the airfoil in reference to the struts disposed through the strut apertures; a first plurality of engines attached to the first end of the struts, wherein an attachment position of the first plurality of engines to the struts is horizontally adjustable; a second plurality of engines attached to the opposite second end of the struts, wherein an attachment position of the second plurality of engines to the struts is horizontally adjustable; and a computerized engine controller, controlling respective thrusts of the first and second plurality of engines to enable the aircraft to vertically lift off/land and re-orient the aircraft to horizontally fly, and perform thrust-initiated elevator and rudder emulating flight; a payload, attached to a bottom and center portion of the airfoil; an external payload-to-receiver system transfer mating mechanism, attached to a bottom of the payload; a location assistance receiver in the aircraft, adapted to provide location accuracy and docking precision for the aircraft when transferring the payload to a receiver system. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification