Active purge mechanism with backflow preventer for gas turbine fuel injectors

US9638422B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9638422-B2
Application numberUS-201213530731-A
CountryUS
Kind codeB2
Filing dateJun 22, 2012
Priority dateJun 22, 2012
Publication dateMay 2, 2017
Grant dateMay 2, 2017

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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 fuel injector for a gas turbine engine includes an injector body having a feed arm with a nozzle body mounted thereto. A fuel conduit fluidly connects a fuel inlet portion of the feed arm to a fuel circuit in the nozzle body to form a fuel path through the injector body and an insulative gap is defined between the fuel conduit and an inside of the feed arm wall to thermally insulate the fuel path of the injector body. An aperture through the feed arm wall provides fluid communication between the insulative gap and ambient conditions existing on an outside of the feed arm wall.

First claim

Opening claim text (preview).

What is claimed is: 1. A fuel injector for a gas turbine engine, comprising: an injector body having a feed arm with a nozzle body connected thereto, the feed arm having a feed arm wall bounding a cavity within the feed arm and supporting the nozzle body; a single-piece fuel conduit disposed within the feed arm cavity and fluidly connecting a fuel inlet portion of the feed arm to a fuel circuit in the nozzle body to form a fuel path through the injector body; a feed arm insulative gap bounded by an outer surface of the single-piece fuel conduit and an interior surface of the feed arm wall to thermally insulate the fuel path of the injector body; an aperture formed through the feed arm wall and in fluid communication with an outlet of the nozzle body through the feed arm insulative gap that provides fluid communication between the feed arm insulative gap and ambient conditions existing on an outside of the feed arm wall; a nozzle body insulative gap disposed radially outward of the fuel circuit in the nozzle body and extending about the fuel circuit in the nozzle body, the nozzle body insulative gap being in fluid communication with the feed arm insulative gap; a helical passage disposed within the feed arm insulative gap with an inlet and an outlet, the aperture being in fluid communication with the feed arm insulative gap serially through both the inlet and the outlet of the helical passage; and a reed valve disposed within the insulative gap and fluidly interposed between the outlet of the helical passage and the feed arm insulative gap, wherein the outlet of the helical passage is disposed axially along the feed arm on a side of the aperture opposite the nozzle body to promote fuel coking within the helical passage. 2. The fuel injector as recited in claim 1 , wherein the feed arm wall has a downstream side facing a direction common with an outlet of the nozzle body, and an upstream side facing an opposite direction of the downstream side, wherein the aperture is defined in the feed arm wall on the downstream side. 3. The fuel injector as recited in claim 1 , wherein the feed arm wall has a downstream side facing a direction common with an outlet of the nozzle body, and an upstream side facing an opposite direction of the downstream side, wherein the aperture is defined in the feed arm wall on the upstream side. 4. The fuel injector as recited in claim 1 , wherein the feed arm wall has a downstream side facing a direction common with an outlet of the nozzle body, and an upstream side facing an opposite direction of the downstream side, wherein the aperture is defined in the feed arm wall between the upstream side and the downstream side. 5. The fuel injector as recited in claim 1 , further comprising: a tortuous path formed relative to an inside of the feed arm wall fluidly coupling the aperture to the feed arm insulative gap, wherein the tortuous path is configured and adapted to allow fluid flow through the aperture into the feed arm insulative gap, and to inhibit fluid flow from the feed arm insulative gap through the aperture to form a blockage in the tortuous path. 6. The fuel injector as recited in claim 5 , wherein the tortuous path is a helical passage serially interposed between the aperture and the feed arm insulative gap, wherein the tortuous path includes a single passage extending circumferentially about the single-piece fuel conduit two or more times. 7. The fuel injector as recited in claim 5 , wherein the fuel conduit is in fluid communication with the tortuous path through the feed arm insulative gap, and further including a coke deposit occluding the tortuous path. 8. The fuel injector as recited in claim 5 , wherein the fluid flow through the aperture into the feed arm insulative gap is a gas flow, and the fluid flow from the feed arm insulative gap through the aperture is a fuel flow. 9. The fuel injector as recited in claim 1 , wherein the nozzle body includes an insulative gap to provide thermal insulation for fuel within the fuel circuit, wherein the insulative gap is fluidly isolated from the feed arm insulative gap. 10. The fuel injector as recited in claim 1 , wherein the nozzle body includes an insulative gap to provide thermal insulation for fuel within the fuel circuit, wherein the insulative gap is in fluid communication with the feed arm insulative gap. 11. The fuel injector as recited in claim 1 , wherein an outlet of the nozzle body is in fluid communication with the feed arm insulative gap through an insulative gap defined within the nozzle body. 12. The fuel injector as recited in claim 1 , wherein the nozzle body is an air blast nozzle body.

Assignees

Inventors

Classifications

  • F23R3/283Primary

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

  • Means for compensating clearance or thermal expansion · CPC title

  • Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title

  • with a ball shaped valve member · CPC title

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What does patent US9638422B2 cover?
A fuel injector for a gas turbine engine includes an injector body having a feed arm with a nozzle body mounted thereto. A fuel conduit fluidly connects a fuel inlet portion of the feed arm to a fuel circuit in the nozzle body to form a fuel path through the injector body and an insulative gap is defined between the fuel conduit and an inside of the feed arm wall to thermally insulate the fuel …
Who is the assignee on this patent?
Hall Troy, Caples Mark Alan, Delavan Inc
What technology area does this patent fall under?
Primary CPC classification F23R3/283. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 02 2017 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).