Gas turbine engine having outlet guide vanes
US-2024418094-A1 · Dec 19, 2024 · US
US10400672B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10400672-B2 |
| Application number | US-201415029503-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 31, 2014 |
| Priority date | Nov 4, 2013 |
| Publication date | Sep 3, 2019 |
| Grant date | Sep 3, 2019 |
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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.
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.
Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title
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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