Unmanned aerial vehicle

US9630710B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9630710-B2
Application numberUS-201414527674-A
CountryUS
Kind codeB2
Filing dateOct 29, 2014
Priority dateOct 29, 2014
Publication dateApr 25, 2017
Grant dateApr 25, 2017

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

Unmanned aerial vehicles and methods for providing the same are disclosed. The unmanned aerial vehicles may have various configurations related to a support frame. The unmanned aerial vehicles may have various configurations with a continuous track for ground propulsion. The unmanned aerial vehicles may have various configurations related to payload clamps.

First claim

Opening claim text (preview).

The invention claimed is: 1. An unmanned aerial vehicle comprising: a frame portion; one or more air propulsion devices mounted on the frame portion, wherein the one or more air propulsion devices are configured to propel the frame portion through the air; one or more ground propulsion devices mounted on the frame portion, wherein the one or more ground propulsion devices are configured to propel the frame portion along ground; a first payload interface extends from a first side of the frame portion, wherein the first payload interface is configured to engage a first object on the first side of the frame portion; and a second payload interface extends from a second side of the frame portion, wherein the second payload interface is configured to engage a second object on the second side of the frame portion, wherein the first object and the second object are separate from the frame portion, and the first side and the second side face different directions. 2. The unmanned aerial vehicle of claim 1 , wherein the first side of the frame portion is a bottom side of the frame portion, as the one or more ground propulsion devices propel the frame portion along the ground. 3. The unmanned aerial vehicle of claim 2 , wherein the unmanned aerial vehicle is configured to engage the first object by maneuvering over the first object using the one or more ground propulsion devices, so that the first payload interface is aligned over the first object. 4. The unmanned aerial vehicle of claim 1 , wherein the first payload interface comprises articulating fingers configured to grip a rim of the first object. 5. The unmanned aerial vehicle of claim 1 , wherein the first payload interface comprises a tab for aligning an end of the first object with an end of the first payload interface. 6. The unmanned aerial vehicle of claim 1 , wherein the first payload interface comprises an indentation on a bottom portion of the first payload interface, and wherein the indentation is configured to receive a protrusion of the first object when the first payload interface is aligned in a predefined position over the first object. 7. The unmanned aerial vehicle of claim 6 , wherein the indentation is configured to receive the protrusion of the first object when an electrical connector provided on the bottom portion of the first payload interface is aligned in the predefined position over an electrical connector on the top portion of the first object. 8. The unmanned aerial vehicle of claim 1 , wherein the first payload interface comprises electrical connectors on a bottom portion of the first payload interface, and wherein electrical connectors on a top portion of the first object form electrical connections with the electrical connectors on the bottom portion of the first payload interface when the first payload interface engages the first object. 9. The unmanned aerial vehicle of claim 8 , wherein an electronic component in the unmanned aerial vehicle transfers data signals to the first object using the electrical connections formed when the first payload interface engages the first object. 10. The unmanned aerial vehicle of claim 8 , wherein an electronic component in the unmanned aerial vehicle transfers electrical power to the first object using the electrical connections formed when the first payload interface engages the first object. 11. The unmanned aerial vehicle of claim 1 , wherein the first payload interface is configured to engage the first object by gripping a surface of the first object. 12. The unmanned aerial vehicle of claim 11 , wherein the first payload interface comprises articulating fingers configured to engage the first object by gripping a surface of the first object. 13. The unmanned aerial vehicle of claim 12 , wherein the first payload interface is configured to lift the first object upwards after the articulating fingers have gripped the surface of the first object. 14. The unmanned aerial vehicle of claim 13 , wherein the first payload interface is configured to lift the first object upwards a sufficient distance so that the unmanned aerial vehicle may move along a ground surface without the first object striking the ground surface while the first object is engaged by the first payload interface. 15. The unmanned aerial vehicle of claim 12 , wherein the articulating fingers are configured to continue gripping the surface of the first object so that the unmanned aerial vehicle is able to perform aerial flight while engaging the first object. 16. The unmanned aerial vehicle of claim 1 , wherein the first payload interface is disposed on a bottom side of the frame portion, and wherein the second payload interface is disposed on a top side of the frame portion. 17. The unmanned aerial vehicle of claim 1 , wherein the first side of the frame portion and the second side of the frame portion face opposite directions. 18. The unmanned aerial vehicle of claim 1 , wherein the second payload interface is configured to engage the second object by gripping a surface of the second object. 19. The unmanned aerial vehicle of claim 18 , wherein the second payload interface comprises articulating fingers configured to engage the second object by gripping the surface of the second object. 20. The unmanned aerial vehicle of claim 19 , wherein the second payload interface is configured to pull the second object downwards after the articulating fingers have gripped the surface of the second object. 21. The unmanned aerial vehicle of claim 19 , wherein the articulating fingers are configured to continue gripping the surface of the second object so that the unmanned aerial vehicle is able to perform aerial flight while engaging the second object. 22. The unmanned aerial vehicle of claim 1 , wherein: the first payload interface is configured to pull the first object toward the unmanned aerial vehicle in a first direction toward the first side; the second payload interface is configured to pull the second object toward the unmanned aerial vehicle in a second direction toward the second side; and the first direction and the second direction are opposite directions. 23. The unmanned aerial vehicle of clam 1 , wherein: the one or more ground propulsion devices comprise at least one continuous track that defines a first track segment having a first surface and a second track segment having a second surface; the first surface faces a first direction with respect to the frame portion; the second surface faces a second direction with respect to the frame portion; and the first direction and the second direction are different directions. 24. The unmanned aerial vehicle of claim 23 , wherein the first surface and the second surface are opposite-facing surfaces. 25. The unmanned aerial vehicle of claim 23 , wherein one of the first surface or the second surface contacts the ground as the one or more ground propulsion devices propel the frame portion along the ground. 26. The unmanned aerial vehicle of claim 1 , wherein the first payload interface and the second payload interface are supported by the frame portion at a center of mass of the unmanned aerial vehicle. 27. A method of manufacturing an unmanned aerial vehicle, the method comprising: providing a frame portion; providing one or more air propulsion devices mounted on the frame portion, wh

Assignees

Inventors

Classifications

  • for transporting passengers; for transporting goods other than weapons · CPC title

  • ducted or shrouded · CPC title

  • Operations & Transport · mapped topic

  • Taking-up articles from earth's surface · CPC title

  • B64C37/00Primary

    Convertible aircraft · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9630710B2 cover?
Unmanned aerial vehicles and methods for providing the same are disclosed. The unmanned aerial vehicles may have various configurations related to a support frame. The unmanned aerial vehicles may have various configurations with a continuous track for ground propulsion. The unmanned aerial vehicles may have various configurations related to payload clamps.
Who is the assignee on this patent?
Qualcomm Inc
What technology area does this patent fall under?
Primary CPC classification B64C37/00. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 25 2017 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).