Gas turbine engine internal compartment structure having egress feature

US8998569B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8998569-B2
Application numberUS-201113211404-A
CountryUS
Kind codeB2
Filing dateAug 17, 2011
Priority dateAug 17, 2011
Publication dateApr 7, 2015
Grant dateApr 7, 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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Abstract

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A gas turbine engine includes a gas turbine engine internal compartment structure having an integral passageway. Wiring is routed through the integral passageway of the gas turbine engine internal compartment structure.

First claim

Opening claim text (preview).

What is claimed is: 1. A gas turbine engine, comprising: a gas turbine engine internal compartment structure having an integral passageway; wiring routed through said integral passageway and along a downstream wall of said gas turbine engine internal compartment structure; and wherein said gas turbine engine internal compartment structure includes a radially inner portion, a radially outer portion and a flange that extends between said radially inner portion and said radially…

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What does patent US8998569B2 cover?
A gas turbine engine includes a gas turbine engine internal compartment structure having an integral passageway. Wiring is routed through the integral passageway of the gas turbine engine internal compartment structure.
Who is the assignee on this patent?
Witlicki Russell B, United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D25/162. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 07 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).