Connector for an aircraft fuel pipe

US9506587B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9506587-B2
Application numberUS-200913002773-A
CountryUS
Kind codeB2
Filing dateJul 6, 2009
Priority dateJul 10, 2008
Publication dateNov 29, 2016
Grant dateNov 29, 2016

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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.

A connector for connecting a pipe, such as a fuel pipe, to another fuel pipe or pipe terminal, having a first connector element including a first female sub-element and a concentric second female sub-element, a first seal seat positioned within the first female sub-element, a second seal seat positioned in the concentric second female sub-element, a first seal retained within the first seal seat, a second seal retained the second seal seat, and a second connector element providing a connection for a pipe at one end and connection to the first connector element at a second end.

First claim

Opening claim text (preview).

The invention claimed is: 1. A pipe connector, comprising: a first connector element comprising a generally cylindrical body member having a central axis and providing a connection for a pipe at one end, said first connector element having a first female sub-element including a first opening and a second opening defining a first passageway therebetween, and a concentric second female sub-element including a third opening and a fourth opening defining a second passageway therebetwe…

Assignees

Inventors

Classifications

  • Operations & Transport · mapped topic

  • Operations & Transport · mapped topic

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • F16L27/044Primary

    Mechanical Engineering · mapped topic

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Frequently asked questions

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What does patent US9506587B2 cover?
A connector for connecting a pipe, such as a fuel pipe, to another fuel pipe or pipe terminal, having a first connector element including a first female sub-element and a concentric second female sub-element, a first seal seat positioned within the first female sub-element, a second seal seat positioned in the concentric second female sub-element, a first seal retained within the first seal sea…
Who is the assignee on this patent?
Petit David, Airbus Operations Ltd
What technology area does this patent fall under?
Primary CPC classification F16L27/044. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 29 2016 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).