Nozzle with insulating air gap and seal to close the gap

Patent metadata

Field	Value
Publication number	US-11085633-B2
Application number	US-201916248002-A
Country	US
Kind code	B2
Filing date	Jan 15, 2019
Priority date	Feb 9, 2018
Publication date	Aug 10, 2021
Grant date	Aug 10, 2021

Abstract

A nozzle for a fuel injector of a gas turbine engine, the nozzle having an insulating air gap adjacent a conduit for carrying fuel, the air gap formed between a pair of concentrically arranged annular walls, wherein the pair of annular walls are arranged to move independently to accommodate differential thermal expansion, the nozzle further including: a channel extending circumferentially around a surface a first of the pair of annular walls, facing a second of the pair of annular walls; and a sealing member received in the channel, to close the insulating gap.

First claim

The invention claimed is:

1. A nozzle for a fuel injector of a gas turbine engine, the nozzle comprising:
an insulating air gap adjacent a fuel conduit, the insulating air gap being formed between a pair of concentrically arranged annular walls, wherein the pair of concentrically arranged annular walls are arranged to move independently to accommodate differential thermal expansion;
a channel extending circumferentially around a surface of a first annular wall of the pair of concentrically arranged annular walls, facing a second annular wall of the pair of concentrically arranged annular walls;
a piston ring sealing member received in the channel, to close the insulating air gap, wherein the piston ring sealing member includes a split extending from an outer-most circumferential edge of the piston ring sealing member to an inner-most circumferential edge of the piston ring sealing member; and
an air swirler concentrically within the fuel conduit,
wherein one of the first annular wall or the second annular wall is adjacent the fuel conduit, and
wherein the other of the first annular wall or the second annular wall includes an aperture extending therethrough, the aperture being located such that the piston ring sealing member is between the aperture and an outlet end of the nozzle, and wherein, during operation of the nozzle, the insulating air gap is configured to receive air from the aperture to form a pressure differential over the piston ring sealing member and the fuel conduit is configured to carry fuel.

2. The nozzle of claim 1 , wherein the piston ring sealing member is biased towards the second annular wall of the pair of concentrically arranged annular walls.

3. The nozzle of claim 1 , including:
an outer wall having a first radial outer face forming an exterior surface of the nozzle and a first radial inner face opposing the outer face, wherein the second annular wall is the outer wall; and
an annular heat shield concentrically within the outer wall, the annular heat shield having a second radial inner face adjacent the fuel conduit and a second radial outer face opposing the second inner face and facing the outer wall, wherein the first annular wall is the annular heat shield,
wherein the insulating air gap is formed between the first radial inner face of the outer wall and the second radial outer face of the annular heat shield.

4. The nozzle of claim 3 , wherein the fuel conduit comprises a radial inner face concentrically within the annular heat shield, the air swirler comprises a radial outer face facing the radial inner face of the fuel conduit, and the nozzle further includes:
a second insulating air gap formed between the radial inner face of the fuel conduit and the radial outer face of the air swirler;
a second channel extending around a surface of one of the radial inner face of the fuel conduit and the radial outer face of the fuel swirler; and
a second sealing member received in the channel, to close the second insulating air gap.

5. The nozzle of claim 1 , wherein the fuel conduit comprises a radial inner face, and the air swirler comprises a radial outer face facing the radial inner face of the fuel conduit, wherein the insulating air gap is formed between the radial inner face of the fuel conduit and the radial outer face of the air swirler.

6. The nozzle of claim 1 , including:
a pair of axially spaced annular circumferential projections extending from the first annular wall of the pair of concentrically arranged annular walls, wherein the channel is formed between the pair of axially spaced annular circumferential projections.

7. The nozzle of claim 1 , including:
a feed arm for supplying fuel to the nozzle; and
a feed arm support housing forming an exterior surface of the feed arm and a rearward portion of the nozzle,
wherein the piston ring sealing member is provided axially forward of the feed arm housing.

8. The nozzle of claim 1 , wherein the pair of concentrically arranged annular walls are formed of a first material, and the piston ring sealing member is formed of a second material, less resistant to wear than the first material.

9. An injector for a gas turbine engine, the injector having the nozzle according to claim 1 .

10. The nozzle of claim 1 , wherein the piston ring sealing member is configured to prevent ingress of fuel or other deposits into the insulating air gap between the pair of concentrically arranged annular walls by contacting the first annular wall of the pair of concentrically arranged annular walls and by contacting the second annular wall of the pair of concentrically arranged annular walls.

11. A nozzle for a fuel injector of a gas turbine engine, the nozzle comprising:
an insulating air gap adjacent a fuel conduit, the insulating air gap being formed between a pair of concentrically arranged annular walls, wherein the pair of concentrically arranged annular walls are arranged to move independently to accommodate differential thermal expansion;
a pair of axially spaced annular circumferential projections extending from a first annular wall of the pair of concentrically arranged annular walls;
a channel extending circumferentially around a surface of the first annular wall of the pair of concentrically arranged annular walls, facing a second annular wall of the pair of annular walls, wherein the channel is formed between the pair of axially spaced annular circumferential projections;
a sealing member received in the channel, to close the insulating air gap, wherein the sealing member includes a split extending from an outer-most circumferential edge of the sealing member to an inner-most circumferential edge of the sealing member; and
an air swirler concentrically within the fuel conduit,
wherein one of the first annular wall or the second annular wall is adjacent the fuel conduit, and
wherein the other of the first annular wall or the second annular wall includes an aperture extending therethrough, the aperture being located such that the sealing member is between the aperture and an outlet end of the nozzle, and wherein, during operation of the nozzle, the insulating air gap is configured to receive air from the aperture to form a pressure differential over the sealing member and the fuel conduit is configured to carry fuel.

12. The nozzle of claim 11 , wherein the sealing member is biased towards the second annular wall of the pair of concentrically arranged annular walls.

13. The nozzle of claim 11 , including:
an outer wall having a radial outer face forming an exterior surface of the nozzle and a radial inner face opposing the radial outer face, wherein the second annular wall is the outer wall; and
an annular heat shield concentrically within the outer wall and having a radial inner face adjacent the fuel conduit and a radial outer face opposing the radial inner face and facing the outer wall, wherein the first annular wall is the annular heat shield,
wherein the insulating air gap is formed between the inner face of the outer wall and the radial outer face of the annular heat shield.

14. The nozzle of claim 11 , including:
a feed arm for supplying fuel to the nozzle; and
a feed arm support housing forming an exterior surface of the feed arm and a rearward portion of the nozzle,
wherein the sealing member is provided axially forward of the feed arm housing.

15. The nozzle of claim 11 , wherein the pair of concentrically arranged annular walls are formed of a first material, and the sealing member is formed of a second material, less resistant to wear than the first material.

16. A nozzle for a fuel in

Assignees

• Rolls Royce Plc

Inventors

• Glover Mark

Classifications

• F23R3/283 Primary

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

• F23R2900/00004

  Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits · CPC title

• F23R2900/00005

  Preventing fatigue failures or reducing mechanical stress in gas turbine components · CPC title

• F23R2900/00012

  Details of sealing devices · CPC title

• F23D14/78

  Cooling burner parts · CPC title