Combustion chamber and a combustion chamber fuel injector seal

Patent metadata

Field	Value
Publication number	US-10704517-B2
Application number	US-201715837446-A
Country	US
Kind code	B2
Filing date	Dec 11, 2017
Priority date	Dec 20, 2016
Publication date	Jul 7, 2020
Grant date	Jul 7, 2020

Abstract

A combustion chamber comprising an upstream end wall, at least one annular wall, at least one fuel injector and at least one seal. The at least one annular wall being secured to the upstream end wall. The upstream end wall having at least one aperture. Each fuel injector being arranged in a corresponding one of the apertures in the upstream end wall and each seal being arranged in a corresponding one of the apertures in the upstream end wall and around the corresponding one of the fuel injectors. Each seal having an inner surface facing the corresponding one of the fuel injectors and an outer surface facing away from the corresponding one of the fuel injectors. Each seal abutting the corresponding one of the fuel injectors. The downstream end of each seal increasing in diameter in a downstream direction and the upstream end of each seal having a radially extending flange. Each seal having a plurality of coolant apertures extending axially through the radially extending flange and/or each seal having a plurality of thermal conductors extending axially from the radially extending flange to the downstream end of the seal.

First claim

The invention claimed is:

1. A combustion chamber comprising an upstream end wall, at least one annular wall, at least one fuel injector and at least one seal,
the at least one annular wall being secured to the upstream end wall,
the upstream end wall having at least one aperture,
each fuel injector being arranged in a corresponding one of the apertures in the upstream end wall,
each seal being arranged in a corresponding one of the apertures in the upstream end wall and around the corresponding one of the fuel injectors, each seal having an inner surface facing the corresponding one of the fuel injectors and an outer surface facing away from the corresponding one of the fuel injectors, each seal abutting the corresponding one of the fuel injectors, the downstream end of each seal increasing in diameter in a downstream direction, the upstream end of each seal having a radially extending flange extending outward of the outer surface, the downstream end of each seal being positioned axially downstream of the upstream end wall, each seal being located in the corresponding one of the apertures in the upstream end wall such that an annular space is formed between the outer surface of the seal and the upstream end wall, each seal having a plurality of thermal conductors extending axially from the radially extending flange to the downstream end of the seal, and wherein each thermal conductor extends radially outwardly from the outer surface of the seal throughout the full axial distance between the radially extending flange and the downstream end of the seal.

2. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein each seal has at least one circumferentially spaced row of the apertures extending axially through the radially extending flange.

3. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein each seal has a plurality of circumferentially spaced rows of the apertures extending axially through the radially extending flange.

4. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein the diameter of the coolant apertures is less than or equal to 3 mm and more than or equal to 0.4 mm.

5. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein the axes of the coolant apertures are angled radially inwardly or angled radially outwardly.

6. The combustion chamber as claimed in claim 5 wherein the coolant apertures are angled radially inwardly at an angle of less than or equal to 60°.

7. The combustion chamber as claimed in claim 5 wherein the coolant apertures are angled radially outwardly at an angle of less than or equal to 60°.

8. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein the coolant apertures extend purely perpendicularly through the radially extending flange.

9. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein the axes of the coolant apertures are angled circumferentially.

10. The combustion chamber as claimed in claim 9 wherein the coolant apertures are angled circumferentially in a direction of swirling fuel and air mixture from the fuel injector.

11. The combustion chamber as claimed in claim 10 wherein the coolant apertures are angled circumferentially at an angle of less than or equal to 60°.

12. The combustion chamber as claimed in claim 9 wherein the coolant apertures are angled circumferentially in an opposite direction of swirling fuel and air mixture from the fuel injector.

13. The combustion chamber as claimed in claim 12 wherein the coolant apertures are angled circumferentially at an angle of less than or equal to 10°.

14. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein the coolant apertures in the radially extending flange are arranged at a radius less than or equal to the radius of the outer surface of the seal+(0.6×(radius of the aperture in the upstream end wall—radius of the outer surface of the seal)) and at a radius more than or equal to the radius of the outer surface of the seal+(0.3×(radius of the aperture in the upstream end wall—radius of the outer surface of the seal)).

15. The combustion chamber as claimed in claim 1 wherein the thermal conductors are hollow.

16. The combustion chamber as claimed in claim 1 wherein each thermal conductor has a radially outer surface remote from the outer surface of the seal and side surfaces extending radially from the radially outer surface to the outer surface of the seal.

17. The combustion chamber as claimed in claim 16 wherein the surface area of the radially outer surface of the thermal conductor divided by twice the surface area of the side surfaces of the thermal conductor is less than 1.

18. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein there are between 1 and 10 coolant apertures extending axially through the radially extending flange positioned between each pair of circumferentially spaced thermal conductors.

19. The combustion chamber as claimed in claim 18 wherein the diameter of the coolant apertures is less than or equal to 3 mm and more than or equal to 0.4 mm.

20. The combustion chamber as claimed in claim 1 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein there are between 1 and 10 coolant apertures extending through the seal from the inner surface to the outer surface positioned between each pair of circumferentially spaced thermal conductors.

21. The combustion chamber as claimed in claim 20 , each seal having a plurality of coolant apertures extending axially through the radially extending flange, wherein the diameter of the coolant apertures is less than or equal to 3 mm and more than or equal to 0.4 mm.

22. The combustion chamber as claimed in claim 1 wherein each seal has a plurality of coolant apertures extending axially through the radially extending flange and each seal has a second plurality of coolant apertures extending there-through, each of the second plurality of coolant aperture has an inlet in the inner surface and an outlet in the outer surface of the seal, the second plurality of coolant apertures being arranged upstream of the downstream end of the seal, the second plurality of coolant apertures extending there-through with axial and radial components, the outlet of each of the second plurality of coolant aperture being axially spaced in a downstream direction from its inlet, the outlet of each of the second plurality of coolant aperture being radially spaced from its inlet.

23. A combustion chamber comprising an upstream end wall, at least one annular wall, at least one fuel injector and at least one seal,
the at least one annular wall being secured to the upstream end wall,
the upstream end wall having at least one aperture,

Assignees

• Rolls Royce Plc

Inventors

• Wilson David P
• Rimmer John E
• Rupp Jochen
• Martin Damian
• Aurifeille Emmanuel V
• Resvanis Kyriakoulis L
• Allitt Michael J

Classifications

• F23R3/283 Primary

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

• F23R2900/00012

  Details of sealing devices · CPC title

• F23R3/50

  Combustion chambers comprising an annular flame tube within an annular casing (toroidal combustion chambers F23R3/52) · CPC title

• F05D2260/22141

  using fins or ribs · CPC title

• F23R3/002

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