Anchoring element and mooring device for an aircraft

US8925858B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8925858-B2
Application numberUS-201113308902-A
CountryUS
Kind codeB2
Filing dateDec 1, 2011
Priority dateDec 16, 2010
Publication dateJan 6, 2015
Grant dateJan 6, 2015

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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.

An anchoring element ( 2 ) intended to be fixed on at least one external anchor point ( 4 ) of an aircraft's fuselage, comprising a fixing area ( 5 ) for ensuring the fixing of the anchoring element ( 2 ) on the external anchor point ( 4 ) and said anchoring element ( 2 ) comprising an anchor means for the connection to attaching means, characterized in that the fixing area ( 5 ) comprises means for fixing the anchoring element ( 2 ) also to a additional external anchor point ( 6 ) of the aircraft's fuselage and said fixing area ( 5 ) comprising an extension area ( 7 ) on which is located the anchor means.

First claim

Opening claim text (preview).

What is claimed is: 1. An anchoring element fixably coupled to an aircraft's fuselage above a sliding path of an upper side of an aircraft door, said anchoring element comprising: a fixing area for ensuring the fixing of the anchoring element on the aircraft fuselage; and an extension area including an anchor means for connection to an attaching means, wherein the fixing area comprises a first connection point fixed to a first external anchor point of the aircraft's fuselage a…

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Classifications

  • B64F1/125Primary

    Operations & Transport · mapped topic

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Frequently asked questions

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What does patent US8925858B2 cover?
An anchoring element ( 2 ) intended to be fixed on at least one external anchor point ( 4 ) of an aircraft's fuselage, comprising a fixing area ( 5 ) for ensuring the fixing of the anchoring element ( 2 ) on the external anchor point ( 4 ) and said anchoring element ( 2 ) comprising an anchor means for the connection to attaching means, characterized in that the fixing area ( 5 ) comprises mean…
Who is the assignee on this patent?
Spiral Fabien, Airbus Helicopters Deutschland GmbH
What technology area does this patent fall under?
Primary CPC classification B64F1/125. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jan 06 2015 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).