Combustion chamber assembly with an air swirler and a fuel injector having inter-engaging faces

Patent metadata

Field	Value
Publication number	US-10018167-B2
Application number	US-201414534605-A
Country	US
Kind code	B2
Filing date	Nov 6, 2014
Priority date	Dec 2, 2013
Publication date	Jul 10, 2018
Grant date	Jul 10, 2018

Abstract

A combustion chamber includes an upstream end wall having an aperture and a fuel injector. An air swirler is mounted such that the air swirler is movable radially with respect to the aperture. An inner wall of the air swirler has a first portion. A fuel injector head of the fuel injector is arranged coaxially within the air swirler. An outer wall of the fuel injector head has a first portion. The inner diameter of the first portion of the air swirler is less than the outer diameter of the first portion of the fuel injector head. One of the first portions is elastically radially deformable to allow the fuel injector head to be installed and removed from the air swirler. The inner wall and the outer wall have inter-engaging radially and axially extending faces to align the fuel injector head axially and radially within the air swirler.

First claim

The invention claimed is:

1. A combustion chamber assembly comprising a combustion chamber including an upstream end wall having at least one aperture and at least one fuel injector,
an air swirler located within the aperture, the air swirler being mounted in the aperture such that the air swirler is movable radially with respect to the aperture, the air swirler having an annular inner wall, the annular inner wall of the air swirler having a first portion,
the at least one fuel injector comprising a fuel feed arm and a fuel injector head,
the fuel injector head of the at least one fuel injector being arranged coaxially within the air swirler,
the fuel injector head having an annular outer wall, the annular outer wall of the fuel injector head having a first portion,
the inner diameter of the first portion of the annular inner wall of the air swirler being less than the outer diameter of the first portion of the annular outer wall of the fuel injector head, one of the first portion of the annular inner wall of the air swirler and the first portion of the annular outer wall of the fuel injector head being elastically radially deformable to allow the fuel injector head to be installed and removed from the annular inner wall of the air swirler, and
the annular inner wall of the air swirler and the annular outer wall of the fuel injector head each having a radial step, the radial step of the annular inner wall of the air swirler and the radial step of the annular outer wall of the fuel injector head configured to engage to align the fuel injector head within the air swirler.

2. A combustion chamber assembly as claimed in claim 1 wherein the first portion of the annular inner wall has a plurality of circumferentially spaced axially extending slots such that the annular inner wall is elastically radially deformable.

3. A combustion chamber assembly as claimed in claim 1 wherein the air swirler comprises a plurality of swirl vanes extending radially outwardly from the annular inner wall, and the annular inner wall of the air swirler has an upstream end and a downstream end and the swirl vanes are secured to a second portion of the annular inner wall.

4. A combustion chamber assembly as claimed in claim 3 wherein the first portion of the annular inner wall are upstream of the second portion of the annular inner wall.

5. A combustion chamber assembly as claimed in claim 3 wherein the annular inner wall has a third portion in which the inner diameter of the annular inner wall is less than the outer diameter of the first portion of the annular outer wall of the fuel injector head, the third portion of the annular inner wall is downstream of the second portion of the annular inner wall and the inner diameter of the second portion of the annular inner wall is greater than the outer diameter of the first portion of the annular outer wall of the fuel injector head to axially locate the fuel injector head in the air swirler.

6. A combustion chamber assembly as claimed in claim 5 wherein the annular outer wall of the fuel injector head has an upstream end and a downstream end, the annular outer wall having a second portion upstream of the first portion and a third portion downstream of the first portion and the outer diameter of the third portion are substantially the same as the inner diameter of the third portion of the annular inner wall of the air swirler.

7. A combustion chamber assembly as claimed in claim 6 wherein the inner diameter of the second portion of the annular inner wall increases to a maximum diameter from the first portion to define a ramp, and the radial step of the annular inner wall is positioned at the intersection of the second portion and the third portion of the annular inner wall.

8. A combustion chamber assembly as claimed in claim 6 wherein the outer diameter of the first portion of the annular outer wall gradually increases to a maximum diameter from the second portion to form a first ramp and the outer diameter gradually decreases from the maximum diameter to form a second ramp, and the radial step of the annular outer wall is positioned at the intersection of the first portion and the third portion of the annular outer wall.

9. A combustion chamber assembly as claimed in claim 1 wherein the downstream end of the annular inner wall has a conical inner surface and the downstream end of the annular outer wall having a conical inner surface aligned with the conical inner surface of the downstream end of the annular inner wall.

10. A combustion chamber assembly as claimed in claim 1 wherein the annular inner wall of the air swirler has an annular groove on its radially inner surface and the annular groove has a tapered surface at its upstream end and a radial surface at its downstream end and the annular outer wall of the fuel injector head having an annular projection on its radially outer surface and the annular projection has a tapered surface at its upstream end and a tapered surface at its downstream end.

11. A combustion chamber assembly as claimed in claim 1 wherein the fuel injector is a rich burn fuel injector, the fuel injector head having a first air swirler, a first pre-filming surface arranged around the first air swirler and a second air swirler arranged around the first-pre-filming surface.

12. A combustion chamber assembly as claimed in claim 1 wherein the fuel injector is a lean burn fuel injector, the fuel injector head having a first air swirler, a first pre-filming surface arranged around the first air swirler, a second air swirler arranged around the first-pre-filming surface, a third air swirler around the second air swirler and second pre-filming surface arranged around the third air swirler.

13. A combustion chamber assembly as claimed in claim 12 wherein the fuel injector head has a fourth air swirler between the second air swirler and the third air swirler.

14. A combustion chamber assembly as claimed in claim 1 wherein the air swirler has an annular outer wall, the annular outer wall of the air swirler having a radially outwardly extending flange and the flange locating in a radial slot defined in the upstream end wall of the combustion chamber.

15. A combustion chamber assembly as claimed in claim 1 wherein the upstream end of the annular inner wall of the air swirler has an aerodynamically shaped outer surface.

16. A combustion chamber assembly as claimed in claim 1 wherein the upstream end of the annular outer wall of the fuel injector head is shaped and dimensioned so that a radially outer surface of the upstream end is flush with a radially outer surface of the upstream end of the annular inner wall of the air swirler.

17. A combustion chamber assembly as claimed in claim 1 wherein the combustion chamber upstream end wall has a plurality of apertures and a plurality of fuel injectors,
an air swirler being mounted in each aperture such that each air swirler is movable radially with respect to the respective aperture, each air swirler having an annular inner wall, the annular inner wall of each air swirler having a first portion,
each fuel injector comprising a fuel feed arm and a fuel injector head,
the fuel injector head of each fuel injector being arranged coaxially within the air swirler of a corresponding one of the apertures,
each fuel injector head having an annular outer wall, the annular outer wall of each fuel injector head having a first portion,
the inner diameter of the first portion of the annular inner wall of each air swirler being less than the outer diameter of the first portion of the annular outer wall of the

Assignees

• Rolls Royce Plc

Inventors

• Tentorio Luca

Classifications

• F23R3/60

  Support structures; Attaching or mounting means · CPC title

• F02M57/04

  the devices being combustion-air intake or exhaust valves · CPC title

• F02M61/14 Primary

  Arrangements of injectors with respect to engines; Mounting of injectors · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F23R2900/00017

  Assembling combustion chamber liners or subparts · CPC title