Small unmanned aerial vehicle (SUAV) shipboard recovery system
US-10046864-B2 · Aug 14, 2018 · US
US10479526B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10479526-B2 |
| Application number | US-201816036604-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 16, 2018 |
| Priority date | Apr 29, 2014 |
| Publication date | Nov 19, 2019 |
| Grant date | Nov 19, 2019 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
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.
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.
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
Related publications grouped by family.
Answers are generated from the same data shown on this page.