Combustion chamber having axially extending and annular coolant manifolds

Patent metadata

Field	Value
Publication number	US-10451278-B2
Application number	US-201614992300-A
Country	US
Kind code	B2
Filing date	Jan 11, 2016
Priority date	Feb 6, 2015
Publication date	Oct 22, 2019
Grant date	Oct 22, 2019

Abstract

A lean burn combustor includes a first wall and a second wall spaced from the first annular wall. Angularly spaced axially extending coolant collection manifolds collect coolant from the space between the first and second walls. A plurality of rows of axially spaced apertures extend through the first wall to supply coolant into the space between the first and second walls and one row of aperture is positioned between each pair of adjacent manifolds. The second wall extends the full length of the combustor. The second wall has a circumferentially extending wall extending towards and contacting the first wall and the wall is spaced from the downstream end of the second wall. An annular supply manifold supplies coolant to the space between the first and second walls downstream of the circumferentially extending wall and the manifolds supply coolant to the manifold. A film of coolant is discharged from the space.

First claim

The invention claimed is:

1. A combustion chamber comprising a first annular wall and a second annular wall spaced radially from the first annular wall,
a plurality of circumferentially spaced axially extending coolant collection manifolds to collect coolant from a space between the first annular wall and the second annular wall, a plurality of apertures extending through the first annular wall to supply coolant into the space between the first annular wall and the second annular wall, at least one aperture being positioned between each pair of circumferentially adjacent axially extending coolant collection manifolds,
the second annular wall extending the full length of the combustion chamber, the second annular wall having a circumferentially extending wall extending towards and contacting the first annular wall, the circumferentially extending wall being positioned adjacent to and spaced from a downstream end of the second annular wall,
an annular supply manifold to supply coolant to a space between the first annular wall and the second annular wall downstream of the circumferentially extending wall, the axially extending coolant collection manifolds being arranged to supply coolant to the annular supply manifold, and
the space between the first annular wall and the second annular wall downstream of the circumferentially extending wall being arranged to discharge a film of coolant from the downstream end of the second annular wall.

2. A combustion chamber as claimed in claim 1 , wherein the plurality of apertures are a plurality of rows of axially spaced apertures extending through the first annular wall to supply coolant into the space between the first annular wall and the second annular wall; and at least one row of axially spaced apertures, including the at least one aperture, being positioned between each pair of circumferentially adjacent axially extending coolant collection manifolds.

3. A combustion chamber as claimed in claim 1 wherein the first annular wall being corrugated and having axially extending grooves and axially extending ridges, the axially extending grooves and axially extending ridges alternating circumferentially around the first annular wall, each axially extending groove in the first annular wall having a plurality of axially spaced apertures extending through the first annular wall to supply coolant into the space between the first annular wall and the second annular wall, each axially extending ridge defining a respective one of the plurality of collection manifolds to collect coolant from the space between the first annular wall and the second annular wall,
the second annular wall having a first surface facing the first annular wall and a second surface facing away from the first annular wall, the circumferentially extending wall of the second annular wall extending from the first surface of the second annular wall towards and contacting the first annular wall, the first annular wall having a circumferentially extending ridge positioned adjacent to and spaced from the downstream end of the first annular wall, the circumferentially extending ridge being positioned downstream of the circumferentially extending wall, the circumferentially extending ridge defining the annular supply manifold to supply the coolant to the space between the first annular wall and the second annular wall downstream of the circumferentially extending wall, the axially extending ridges intersecting the circumferentially extending ridge to supply coolant from the collection manifolds to the annular supply manifold.

4. A combustion chamber as claimed in claim 3 wherein a third annular wall being positioned between the first annular wall and the second annular wall, the third annular wall abutting the first annular wall, the third annular wall having a first plurality of apertures extending through the third annular wall and aligned with a corresponding aperture of the plurality of apertures in the first annular wall to supply coolant into the space between the first annular wall and the second annular wall, the third annular wall defining the collection manifolds with the axially extending ridges of the first annular wall, the third annular wall having a second plurality of apertures to supply coolant from the space between the first annular wall and the second annular wall into the collection manifolds, the third annular wall defining the annular supply manifold with the circumferentially extending ridge of the first annular wall and the third annular wall having a third plurality of apertures to supply coolant from the annular supply manifold to the space between the first annular wall and the second annular wall downstream of the circumferentially extending wall.

5. A combustion chamber as claimed in claim 1 wherein the space between the first annular wall and the second annular wall downstream of the circumferentially extending wall being arranged to discharge a film of coolant from the downstream end of the second annular wall onto a combustion chamber discharge nozzle.

6. A combustion chamber as claimed in claim 1 wherein the second annular wall comprising a plurality of circumferentially arranged tiles and each tile has axially extending edge walls extending from a first surface of the second annular wall towards the first annular wall.

7. A combustion chamber as claimed in claim 6 wherein the axially extending edge walls of each tile being circumferentially aligned with corresponding axially extending ridges on the first annular wall.

8. A combustion chamber as claimed in claim 7 wherein the center of each tile being aligned with an axially extending ridge on the first annular wall.

9. A combustion chamber as claimed in claim 6 wherein each tile having a plurality of studs to secure the tile to the first annular wall.

10. A combustion chamber as claimed in claim 6 wherein the tiles being manufactured by a method selected from the group consisting of casting and additive layer manufacture.

11. A combustion chamber as claimed in claim 6 wherein each tile having apertures at an upstream end of the tile to secure the tile between the upstream end of the first annular wall and an upstream wall of the combustion chamber.

12. A combustion chamber as claimed in claim 11 wherein a downstream end of each tile and the downstream end of the first annular wall locate in an annular slot in a combustion chamber discharge nozzle.

13. A combustion chamber as claimed in claim 1 comprising a plurality of circumferentially arranged segments, each segment comprising a portion of the first annular wall and a portion of the second annular wall, each segment has axially extending edge walls extending radially from the portion of the first annular wall to the portion of the second annular wall, the portion of the first annular wall and the portion of the second annular wall are integral and the segments are secured together.

14. A combustion chamber as claimed in claim 13 wherein the axially extending edge walls of each segment being circumferentially aligned with the centers of corresponding axially extending ridges on the first annular wall to define two collections manifolds in each of the corresponding axially extending ridges.

15. A combustion chamber as claimed in claim 14 wherein the center of each segment being aligned with an axially extending ridge on the first annular wall.

16. A combustion chamber as claimed in claim 14 wherein the axially extending edge walls of each segment extending radially beyond the corresponding axially extending ridges to form axially extending flanges, and the flanges of adjace

Assignees

• Rolls Royce Plc

Inventors

• Pidcock Anthony
• Chandler Paul I

Classifications

• F23R2900/03043

  Convection cooled combustion chamber walls with means for guiding the cooling air flow · CPC title

• F23R2900/03045

  Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling · CPC title

• F23R3/54

  Reverse-flow combustion chambers · CPC title

• F23R2900/03042

  Film cooled combustion chamber walls or domes · CPC title

• F23R3/002 Primary

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