Turbine engine combustor heat shield with multi-height rails

Patent metadata

Field	Value
Publication number	US-10240790-B2
Application number	US-201415031908-A
Country	US
Kind code	B2
Filing date	Oct 31, 2014
Priority date	Nov 4, 2013
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall, which includes a shell and a heat shield. The heat shield includes a base and a plurality of panel rails. The panel rails are connected to the base and extend vertically to the shell. The panel rails include first and second rails. A vertical height of the first rail at a first location is less than a vertical height of the second rail at a second location.

First claim

What is claimed is:

1. An assembly for a turbine engine, the assembly comprising:
a combustor wall including a shell and a heat shield, the heat shield including a base and a plurality of panel rails connected to the base and extending vertically to the shell, the plurality of panel rails including first and second rails;
wherein a vertical height of the first rail at a first location is less than a vertical height of the second rail at a second location; and
wherein the vertical height of the first rail varies as the first rail extends longitudinally along the base.

2. The assembly of claim 1 , wherein the first rail is parallel to the second rail.

3. The assembly of claim 1 , wherein the combustor wall extends along a combustor axis, and the first location is longitudinally aligned with the second location relative to the combustor axis.

4. The assembly of claim 1 , wherein the first location comprises a longitudinal midpoint of the first rail.

5. The assembly of claim 1 , wherein
the plurality of panel rails includes a third rail, and the first rail is arranged between the second rail and the third rail.

6. The assembly of claim 5 , wherein the vertical height of the first rail at the first location is less than a vertical height of the third rail at a third location.

7. The assembly of claim 1 , wherein the first and the second rails comprise circumferentially extending rails.

8. The assembly of claim 1 , wherein the vertical height of at least a portion of the first rail is constant.

9. The assembly of claim 1 , further comprising:
a plurality of mechanical attachments attaching the base to the shell,
wherein the first rail is located between the plurality of mechanical attachments and the second rail.

10. The assembly of claim 1 , wherein
first and second cooling cavities extend between the shell and the heat shield, and the first rail defines an aperture which fluidly couples the first cooling cavity with the second cooling cavity.

11. The assembly of claim 1 , wherein
the heat shield includes a plurality of panels arranged circumferentially around a centerline, and the base, the first rail and the second rail are included in one of the plurality of panels.

12. An assembly for a turbine engine, the assembly comprising:
a combustor wall including a shell and a heat shield, the heat shield including a base and a plurality of panel rails connected to the base and extending vertically to the shell, the plurality of panel rails including first and second rails:
a mechanical attachment attaching the base to the shell; and
a plurality of protrusions arranged around the mechanical attachment and connected to the base;
wherein a vertical height of the first rail at a first location is less than a vertical height of the second rail at a second location, and
wherein a vertical height of one of the plurality of protrusions is equal to the vertical height of the first rail at the first location.

13. An assembly for a turbine engine, the assembly comprising:
a combustor wall including a shell and a heat shield, the heat shield including a base and a plurality of panel rails connected to the base and extending vertically to the shell, the plurality of panel rails including first and second rails;
wherein a vertical height of the first rail at a first location is less than a vertical height of the second rail at a second location; and
wherein the plurality of panel rails includes a third rail and a fourth rail, and the first rail and the second rail extend between the third rail and the fourth rail.

14. A combustor wall for a turbine engine, the combustor wall comprising:
a combustor shell; and
a combustor heat shield panel including a plurality of panel rails that extend vertically to the combustor shell, the plurality of panel rails including an intermediate rail arranged between first and second end rails,
wherein a mean vertical height of the intermediate rail is less than a mean vertical height of the first end rail; and
wherein the mean vertical height of the first end rail is less than a mean vertical height of the second end rail.

15. The combustor wall of claim 14 , further comprising:
a mechanical attachment attaching the combustor heat shield panel to the combustor shell; and
a plurality of protrusions arranged around the mechanical attachment and connected to a base of the heat shield panel;
wherein a vertical height of one of the plurality of protrusions is equal to a vertical height of the first rail at a first location.

Assignees

• United Technologies Corp

Inventors

• Eastwood Jonathan J
• Moura Dennis M

Classifications

• F23R3/002 Primary

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

• F23R3/06

  Arrangement of apertures along the flame tube · CPC title

• F23R3/04

  Air inlet arrangements · CPC title

• F23R3/02

  characterised by the air-flow or gas-flow configuration (reverse- flow combustion chambers F23R3/54; cyclone or vortex type combustion chambers F23R3/58) · CPC title