Combustion equipment

Patent metadata

Field	Value
Publication number	US-10208664-B2
Application number	US-201615061150-A
Country	US
Kind code	B2
Filing date	Mar 4, 2016
Priority date	Mar 31, 2015
Publication date	Feb 19, 2019
Grant date	Feb 19, 2019

Abstract

Combustion equipment includes annular combustion chamber having an annular upstream wall structure. Annular outer casing surrounds and is spaced from annular combustion chamber and annular inner casing is within and spaced from annular combustion chamber. Ogee shaped annular cowl is positioned upstream of annular upstream wall structure and a stage of compressor outlet guide vanes is positioned upstream of annular cowl. Pre-diffuser extends in downstream direction from stage of compressor outlet guide vanes, pre-diffuser is positioned upstream of cowl. Stage of compressor outlet guide vanes is connected to outer and inner casing. Outer fairing extends radially inwardly from outer casing such that annular outer casing, outer fairing and pre-diffuser define annular outer cavity and outer fairing is spaced from cowl or inner fairing extends radially outwardly from inner casing such that annular inner casing, inner fairing and pre-diffuser define an annular inner cavity and inner fairing is spaced from cowl.

First claim

The invention claimed is:

1. Combustion equipment comprising:
an annular combustion chamber that includes an annular upstream wall structure, an annular outer casing surrounding and spaced from the annular combustion chamber, and an annular inner casing within and spaced from the annular combustion chamber,
an annular cowl positioned upstream of the annular upstream wall structure, the annular cowl having an upstream end and a downstream end,
a stage of compressor outlet guide vanes positioned upstream of the annular cowl, the stage of compressor outlet guide vanes being connected to the outer casing and the inner casing,
a pre-diffuser that extends in a downstream direction from the stage of compressor outlet guide vanes, the pre-diffuser being positioned upstream of the cowl,
an outer fairing that extends radially inwardly from the outer casing such that the annular outer casing, the outer fairing and the pre-diffuser define an annular outer cavity, the outer fairing being spaced from the cowl,
the outer fairing comprising a concave first portion extending from the outer casing radially inwardly and in an upstream direction to a position upstream of the downstream end of the cowl and a second portion extending from the first portion radially outwardly to the outer casing, the first portion of the outer fairing extending to a position at or downstream of the upstream end of the cowl, and

an inner fairing that extends radially outwardly from the inner casing such that the annular inner casing, the inner fairing and the pre-diffuser define an annular inner cavity, the inner fairing being spaced from the cowl,
the inner fairing comprising a concave first portion extending from the inner casing radially outwardly and in an upstream direction to a position upstream of the downstream end of the cowl and a second portion extending from the first portion to the inner casing, the first portion of the inner fairing extending to a position downstream of the upstream end of the cowl,

wherein the annular cowl is ogee in cross-sectional profile and an apex of the cowl is arranged at the upstream end of the cowl.

2. The combustion equipment as claimed in claim 1 , wherein the first and the second portions of the outer fairing and the outer casing form a triangle.

3. The combustion equipment as claimed in claim 1 , wherein the first and second portions of the inner fairing and the inner casing form a triangle.

4. The combustion equipment as claimed in claim 1 , wherein the apex of the cowl is arcuate.

5. The combustion equipment as claimed in claim 1 , wherein the pre-diffuser comprises an inner annular wall and an outer annular wall defining an annular passage, the inner annular wall and the outer annular wall being arcuate in cross-section such that the annular passage has a greater cross-sectional area at its downstream end than its upstream end.

6. The combustion equipment as claimed in claim 5 , wherein the inner annular wall and the outer annular wall are cubic curves.

7. The combustion equipment as claimed in claim 1 , wherein the annular outer cavity is defined by the the second portion of the outer fairing and an annular wall extending from the outer casing to the stage of compressor outlet guide vanes.

8. The combustion equipment as claimed in claim 1 , wherein the annular inner cavity is defined by the second portion of the inner fairing.

9. The combustion equipment as claimed in claim 1 , wherein the second portion of the outer fairing is positioned downstream of a downstream end of the pre-diffuser.

10. The combustion equipment as claimed in claim 1 , wherein the second portion of the inner fairing is positioned downstream of the downstream end of the pre-diffuser.

11. The combustion equipment as claimed in claim 1 , wherein:
an inlet to the annular outer cavity is defined between a downstream end of the pre-diffuser and a junction between the first and second portions of the outer fairing, and
an inlet to the annular inner cavity is defined between the downstream end of the pre-diffuser and a junction between the first and second portions of the inner fairing.

Assignees

• Rolls Royce Plc

Inventors

• Armit Christopher
• Aurifeille Emmanuel
• Shahpar Shahrokh
• Denman Paul
• Ford Christopher

Classifications

• F23R3/10 Primary

  for primary air (F23R3/06, F23R3/045 take precedence) · CPC title

• F02C3/04 Primary

  having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title

• F23R3/26

  Controlling the air flow · CPC title

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title