UAV payload module camera assembly and retraction mechanism

US11554879B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11554879-B2
Application numberUS-202017060071-A
CountryUS
Kind codeB2
Filing dateSep 30, 2020
Priority dateJun 29, 2010
Publication dateJan 17, 2023
Grant dateJan 17, 2023

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.

In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by the winch to retract the payload within the housing.

First claim

Opening claim text (preview).

What is claimed is: 1. A method in a UAV comprising: a) applying a biasing force to a payload to bias a payload out of the UAV; b) retaining the payload within the UAV using a flexible retraction mechanism; c) extending the payload from the UAV using the flexible retraction mechanism; and d) retracting the payload using a flexible retraction mechanism so as to cause the payload to retract into the UAV from the deployed position while biasing the payload out of the UAV. 2. The method of claim 1 , wherein extending the payload comprises extending the payload from the fuselage. 3. The method of claim 2 further comprising: a) launching the UAV; b) landing the UAV without using landing gear; and c) wherein extending the payload comprises extending the payload after launching and before landing the UAV. 4. The method of claim 1 further comprising: a) launching the UAV and extending the payload from the UAV; and b) landing the UAV without using landing gear. 5. The method of claim 4 , wherein landing the UAV comprises landing the UAV on water. 6. The method of claim 4 , wherein landing the UAV comprises landing the UAV on land. 7. The method of claim 4 , wherein launching the UAV comprises launching the UAV by hand. 8. The method of claim 4 , wherein landing comprises using a skid pad. 9. The method of claim 1 further comprising: a) launching the UAV by hand; and b) landing the UAV on water. 10. The method of claim 1 further comprising: a) launching the UAV by hand; and b) landing the UAV on land.

Assignees

Inventors

Classifications

  • Equipment for handling freight; Equipment for facilitating passenger embarkation or the like · CPC title

  • for imaging, photography or videography · CPC title

  • B64D47/08Primary

    Arrangements of cameras · CPC title

  • using steam or spring force (jet aircraft B64D27/16) · CPC title

  • Operations & Transport · mapped topic

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 US11554879B2 cover?
In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by th…
Who is the assignee on this patent?
Aerovironment Inc
What technology area does this patent fall under?
Primary CPC classification B64D47/08. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jan 17 2023 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 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).