Small unmanned aerial vehicle (SUAV) shipboard recovery system

US10479526B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10479526-B2
Application numberUS-201816036604-A
CountryUS
Kind codeB2
Filing dateJul 16, 2018
Priority dateApr 29, 2014
Publication dateNov 19, 2019
Grant dateNov 19, 2019

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

Systems, devices, and methods for impacting, by a small unmanned aerial vehicle (SUAV), a net having at least three sides; and converting the kinetic energy of the SUAV into at least one of: elastic potential energy of one or more tensioned elastic cords connected to at least one corner of the net, gravitational potential energy of a frame member connected to at least one corner of the net, rotational kinetic energy of the frame member connected to at least one corner of the net, and elastic potential energy of the frame member connected to at least one corner of the net.

First claim

Opening claim text (preview).

What is claimed is: 1. A small unmanned aerial vehicle (SUAV) recovery system comprising: a net; a mast connected to the net; and a boom connected to the net; wherein the mast and the boom are connected; wherein energy of an impact of the SUAV into the net is progressively transferred by a gravitational potential energy of the boom and a progressive bending of the boom. 2. The SUAV recovery system of claim 1 wherein energy of the impact of the SUAV is also transferred by deformation of the net. 3. The SUAV recovery system of claim 1 further comprising: one or more tensioned elastic cords attached to the net; wherein energy of the impact of the SUAV is also transferred by deformation of the one or more tensioned elastic cords. 4. The SUAV recovery system of claim 1 further comprising: three or more rings attached to the net; and three or more lines, wherein the net is slidably connected to one of the three or more lines by one or more of the three or more rings. 5. The SUAV recovery system of claim 1 , wherein the mast is oriented perpendicular to the boom, and wherein the mast and the boom are telescopically adjustable in length. 6. The SUAV recovery system of claim 1 , wherein a square mesh size of the net is smaller than a cross-sectional size of a fuselage of the SUAV. 7. The SUAV recovery system of claim 1 further comprising: the SUAV; and one or more barbs disposed on a fuselage of the SUAV, wherein the one or more barbs are sized to detachably entangle in the net after impact. 8. A small unmanned aerial vehicle (SUAV) recovery system comprising: a net; a mast connected to the net; and a boom connected to the net; wherein the mast and the boom are connected; wherein energy of an impact of the SUAV into the net is progressively transferred by a rotational kinetic energy of the boom and a progressive bending of the boom. 9. The SUAV recovery system of claim 8 wherein energy of the impact of the SUAV is also transferred by deformation of the net. 10. The SUAV recovery system of claim 8 further comprising: one or more tensioned elastic cords attached to the net; wherein energy of the impact of the SUAV is also transferred by deformation of the one or more tensioned elastic cords. 11. The SUAV recovery system of claim 8 further comprising: three or more rings attached to the net; and three or more lines, wherein the net is slidably connected to one of the three or more lines by one or more of the three or more rings. 12. The SUAV recovery system of claim 8 , wherein the mast is oriented perpendicular to the boom, and wherein the mast and the boom are telescopically adjustable in length. 13. The SUAV recovery system of claim 8 , wherein a square mesh size of the net is smaller than a cross-sectional size of a fuselage of the SUAV. 14. The SUAV recovery system of claim 8 further comprising: the SUAV; and one or more barbs disposed on a fuselage of the SUAV, wherein the one or more barbs are sized to detachably entangle in the net after impact.

Assignees

Inventors

Classifications

  • Waterborne vehicles · CPC title

  • Nets, slipways or the like, for recovering aircraft from the water · CPC title

  • Vessels parts, details, or accessories, not otherwise provided for {(vehicle fittings for preventing or indicating unauthorised use or theft of vehicles in general B60R25/00; propeller guards, line cutters or other means for protecting propellers or rudders B63H5/165; protection of power legs of outboard propulsion units B63H20/36; locking devices for boats, surfboards or parts or accessories thereof E05B73/007)} · CPC title

  • using decelerating or arresting beds · CPC title

  • Operations & Transport · mapped topic

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Frequently asked questions

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What does patent US10479526B2 cover?
Systems, devices, and methods for impacting, by a small unmanned aerial vehicle (SUAV), a net having at least three sides; and converting the kinetic energy of the SUAV into at least one of: elastic potential energy of one or more tensioned elastic cords connected to at least one corner of the net, gravitational potential energy of a frame member connected to at least one corner of the net, rot…
Who is the assignee on this patent?
Aerovironment Inc
What technology area does this patent fall under?
Primary CPC classification B64F1/02. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Nov 19 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).