Modular unmanned aerial system with multi-mode propulsion
First Claim
1. A modular Unmanned Aerial System (UAS) having a vertical takeoff and landing (VTOL) configuration and a forward-flight configuration, the UAS comprising:
- a plurality of Unmanned Aerial Vehicle (UAV) modules each having;
a main wing coupled to a corresponding fuselage and having a uniform tip chord length across the plurality of UAV modules;
a pair of booms extending orthogonally from the main wing;
a first pair of propellers, each of which is connected to the main wing via a corresponding arm and selectively stowable within a respective one of the booms in the forward-flight configuration, the corresponding arm being configured to pivot with respect to the main wing;
a second pair of propellers, each of which is connected to a respective one of the booms via a corresponding articulating motor mount and tiltable with respect to the booms via operation of the corresponding articulating motor mount, wherein the first and second pairs of propellers rotate in parallel horizontal planes in the VTOL configuration, and the second pair of propellers rotates in a vertical plane in the forward-flight configuration; and
wingtip docking mechanisms;
wherein the UAS is configured to selectively couple the UAV modules to each other, wingtip-to-wingtip, in both the VTOL and forward-flight configurations using the wingtip docking mechanisms, and is further configured to selectively uncouple the UAV modules from each other via the wingtip docking mechanisms in an independent flight configuration of the UAS.
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Abstract
A modular Unmanned Aerial System (UAS) includes an Unmanned Aerial Vehicle (UAV) parent module and UAV child modules. A main wing extends from a respective fuselage of the modules. The UAS includes docking mechanisms coupled to wingtips of the main wings. The child modules dock with the wingtips of the parent or an adjacent child module. Docking forms a linked-flight configuration, with undocking and separation from the parent or adjacent child module achieving an independent-flight configuration. The modules have booms arranged transverse to the main wings and parallel to the longitudinal axis, as well as front and rear rotors/propellers. The front and rear propellers have axes of rotation that are normal to a plane of the longitudinal axis in a vertical takeoff and landing (VTOL) configuration, with the axis of rotation of the rear propellers parallel to the longitudinal axis in a forward-flight configuration.
44 Citations
20 Claims
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1. A modular Unmanned Aerial System (UAS) having a vertical takeoff and landing (VTOL) configuration and a forward-flight configuration, the UAS comprising:
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a plurality of Unmanned Aerial Vehicle (UAV) modules each having; a main wing coupled to a corresponding fuselage and having a uniform tip chord length across the plurality of UAV modules; a pair of booms extending orthogonally from the main wing; a first pair of propellers, each of which is connected to the main wing via a corresponding arm and selectively stowable within a respective one of the booms in the forward-flight configuration, the corresponding arm being configured to pivot with respect to the main wing; a second pair of propellers, each of which is connected to a respective one of the booms via a corresponding articulating motor mount and tiltable with respect to the booms via operation of the corresponding articulating motor mount, wherein the first and second pairs of propellers rotate in parallel horizontal planes in the VTOL configuration, and the second pair of propellers rotates in a vertical plane in the forward-flight configuration; and wingtip docking mechanisms; wherein the UAS is configured to selectively couple the UAV modules to each other, wingtip-to-wingtip, in both the VTOL and forward-flight configurations using the wingtip docking mechanisms, and is further configured to selectively uncouple the UAV modules from each other via the wingtip docking mechanisms in an independent flight configuration of the UAS. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A method for controlling a modular Unmanned Aerial System (UAS) having vertical takeoff and landing (VTOL) and forward-flight configurations, the method comprising:
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docking an Unmanned Aerial Vehicle (UAV) parent module to a plurality of UAV child modules using a plurality of wingtip docking mechanisms to form the UAS, the UAV parent module and UAV child modules each having a corresponding fuselage with a longitudinal axis and main wing extending orthogonally from the corresponding fuselage; launching the UAS in the VTOL configuration, including powering a first pair of propellers each connected to a respective boom and arranged forward of a respective one of the main wings, and a second pair of propellers positioned aft of a respective one of the main wings, wherein each propeller of the first and second pairs of propellers has a corresponding axis of rotation that is normal to a plane of the longitudinal axis when the UAS is in the VTOL configuration; transitioning the UAS to the forward-flight configuration at a predetermined altitude of the UAS, including, for the UAV parent module and each of the UAV child modules, articulating the first pair of propellers with respect to a respective one of the main wings, stowing the first pair of propellers within a respective one of the booms, and tilting the second pair of propellers until the axes of rotation of the second pair of propellers are parallel to a longitudinal axis of the fuselage; flying the UAS to a rendezvous point in the forward-flight configuration; undocking some or all of the UAV child modules from the UAV parent module upon reaching the rendezvous point; and independently flying the UAV parent module and the UAV child modules in the forward-flight configuration to a corresponding destination using the second pair of propellers. - View Dependent Claims (13, 14, 15, 16, 17)
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18. An Unmanned Aerial Vehicle (UAV) having vertical takeoff and landing (VTOL) and forward-flight configurations, the UAV comprising:
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a fuselage having a longitudinal axis; a main wing having first and second wing sections connected to the fuselage and orthogonal to the longitudinal axis; first and second booms connected to and extending from the main wing; a first pair of propellers connected proximate a leading edge of the main wing via a corresponding boom; a second pair of propellers positioned aft of a trailing edge of the main wing, each propeller of the second pair of propellers having an axis of rotation that is normal to a plane of the longitudinal axis of the fuselage when the UAV is in the VTOL flight configuration, and that is parallel to the longitudinal axis when the UAV is in the forward-flight configuration; wherein the propellers of the first pair of propellers are selectively stowable within a respective one of the first and second booms when the UAV is in the forward-flight configuration. - View Dependent Claims (19, 20)
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Specification