Cooled fuel injector system for a gas turbine engine

US10400672B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10400672-B2
Application numberUS-201415029503-A
CountryUS
Kind codeB2
Filing dateOct 31, 2014
Priority dateNov 4, 2013
Publication dateSep 3, 2019
Grant dateSep 3, 2019

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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 cooling system for a fuel injector system of a gas turbine engine has a heat exchanger for cooling a portion of diffuser case air and then routing the cooled diffuser case air through a sleeve that surrounds a fuel injector conduit located in at least the diffuser case plenum for minimizing fuel heat-up rates in the conduit. By minimizing fuel temperatures within the injector conduit, coking accumulation is thereby eliminated or reduced.

First claim

Opening claim text (preview).

What is claimed is: 1. A cooling system for a fuel injector system of a combustor section of a gas turbine engine, the cooling system comprising: a heat exchanger for cooling hot diffuser case air; a cooling fluid sleeve surrounding at least in part a fuel conduit of a fuel injector and extending to about a tip of the fuel injector of the fuel injector system; an outlet of the sleeve proximate to the tip; an inlet of the sleeve for receiving cooled diffuser case air; and a distribution apparatus constructed and arranged to receive the cooled diffuser case air from the outlet and direct the cooled diffuser case air onto a backside of at least one heat shield of a bulkhead assembly of the combustor section. 2. The cooling system of claim 1 , wherein the distribution apparatus has a plurality of tubes spaced circumferentially from one another and about the tip. 3. The cooling system of claim 1 , wherein the distribution apparatus has an expansion joint for connection to the cooling fluid sleeve. 4. The cooling system of claim 1 , wherein the heat exchanger is configured for conditioning the cooled diffuser case air. 5. The cooling system of claim 4 wherein the heat exchanger is constructed and arranged to receive bypass air of the gas turbine engine for cooling of the diffuser case air.

Assignees

Inventors

Classifications

  • Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

  • F02C7/14Primary

    of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · CPC title

  • Preventing heat transfer · CPC title

  • Fuel flow conduits, e.g. manifolds · CPC title

  • in gas turbines · CPC title

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What does patent US10400672B2 cover?
A cooling system for a fuel injector system of a gas turbine engine has a heat exchanger for cooling a portion of diffuser case air and then routing the cooled diffuser case air through a sleeve that surrounds a fuel injector conduit located in at least the diffuser case plenum for minimizing fuel heat-up rates in the conduit. By minimizing fuel temperatures within the injector conduit, coking …
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F02C7/14. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 03 2019 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).