Using multirotor lifters to deploy fixed wing aircraft
First Claim
Patent Images
1. A system, comprising:
- an unmanned fixed wing aircraft, including;
a fixed wing;
a thrusting motor and corresponding thrusting propeller;
a payload; and
an engagement receiver to receive an engagement mechanism of an unmanned multirotor lifter;
the unmanned multirotor lifter, including;
a plurality of motors and corresponding propellers of a size sufficient to vertically lift the unmanned fixed wing aircraft and the unmanned multirotor lifter;
the engagement mechanism configured to selectively engage or disengage the engagement receiver of the unmanned fixed wing aircraft; and
a communication component to wirelessly communicate with the unmanned fixed wing aircraft;
a computing system, including;
a processor; and
a memory coupled to the processor and storing program instructions that when executed by the processor cause the processor to at least;
determine that the multirotor lifter is at a desired altitude with the unmanned fixed wing aircraft engaged by the engagement mechanism;
send a disengagement authorization;
confirm that the multirotor lifter has disengaged the engagement mechanism from the engagement receiver of the unmanned fixed wing aircraft; and
confirm that the unmanned fixed wing aircraft has initiated a flight from the desired altitude.
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Abstract
This disclosure describes systems and processes using multirotor lifter to deploy and/or engage fixed wing aircraft. For example, one or more unmanned multirotor lifters may engage an unmanned fixed wing aircraft, aerially navigate the fixed wing aircraft vertically to a desired altitude, and then release the fixed wing aircraft so that the fixed wing aircraft can initiate a flight plan. In some implementations, multirotor lifter may also be configured to engage fixed wing aircraft while both the multirotor lifters and the fixed wing aircraft are in flight.
34 Citations
21 Claims
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1. A system, comprising:
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an unmanned fixed wing aircraft, including; a fixed wing; a thrusting motor and corresponding thrusting propeller; a payload; and an engagement receiver to receive an engagement mechanism of an unmanned multirotor lifter; the unmanned multirotor lifter, including; a plurality of motors and corresponding propellers of a size sufficient to vertically lift the unmanned fixed wing aircraft and the unmanned multirotor lifter; the engagement mechanism configured to selectively engage or disengage the engagement receiver of the unmanned fixed wing aircraft; and a communication component to wirelessly communicate with the unmanned fixed wing aircraft; a computing system, including; a processor; and a memory coupled to the processor and storing program instructions that when executed by the processor cause the processor to at least; determine that the multirotor lifter is at a desired altitude with the unmanned fixed wing aircraft engaged by the engagement mechanism; send a disengagement authorization; confirm that the multirotor lifter has disengaged the engagement mechanism from the engagement receiver of the unmanned fixed wing aircraft; and confirm that the unmanned fixed wing aircraft has initiated a flight from the desired altitude. - View Dependent Claims (2, 3, 4, 5)
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6. A multirotor lifter to selectively engage or disengage a fixed wing aircraft, the multirotor lifter comprising:
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a plurality of lifting propulsion components to aerially lift the multirotor lifter and at least a portion of the fixed wing aircraft; an engagement mechanism to engage or disengage the fixed wing aircraft; and a control system configured to at least; cause the multirotor lifter to aerially lift the fixed wing aircraft to a determined altitude; and disengage, at the determined altitude, the fixed wing aircraft such that the fixed wing aircraft can initiate flight without aid from the multirotor lifter. - View Dependent Claims (7, 8, 9, 10, 11, 12, 13, 14)
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15. A method, comprising:
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engaging, at a first altitude and with a multirotor lifter, a fixed wing aircraft; lifting the fixed wing aircraft from the first altitude to a second altitude; and releasing, at the second altitude and from the multirotor lifter, the fixed wing aircraft such that the fixed wing aircraft can initiate a flight without aid from the multirotor lifter. - View Dependent Claims (16, 17, 18, 19, 20, 21)
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Specification