Combustor heat shield sealing

Patent metadata

Field	Value
Publication number	US-10012385-B2
Application number	US-201414455185-A
Country	US
Kind code	B2
Filing date	Aug 8, 2014
Priority date	Aug 8, 2014
Publication date	Jul 3, 2018
Grant date	Jul 3, 2018

Abstract

A method and an apparatus for reducing airflow leakage between a combustor liner and a rail of a heat shield mounted to an inner surface of the combustor liner. The method comprises locally deforming the combustor liner in sealing engagement with the rail by applying a pressure on the outer surface of the combustor liner over the rail of the heat shield. A tool, such as a sealing clip, may be mounted in pressing engagement with the outer surface of the combustor liner to apply forces locally on the liner over the rail of the heat shield.

First claim

The invention claimed is:

1. A combustor of a gas turbine engine, the combustor comprising: a combustor liner defining a combustion chamber, a heat shield mounted to an inner surface of the combustor liner in the combustion chamber, the heat shield having a rail projecting from a back face of the heat shield, a sealing clip mounted to an outer surface of the combustor liner, the sealing clip having two anchoring points and an elongated body, the elongated body aligned with and positioned over the rail of the heat shield along a length and extending between the two anchoring points, the two anchoring points axially offset and spaced from the elongated body and the rail, each of the two anchoring points defining a respective hole in the sealing clip to facilitate mounting and holding of the elongated body in pressing engagement with the outer surface of the combustor liner, the elongated body redistributing a bolting pressure applied at the two anchoring points, and wherein the elongated body locally deforms the combustor liner in sealing engagement against the rail of the heat shield along the length.

2. The combustor defined in claim 1 , the respective holes in the sealing clip of the two anchoring points receiving respective studs projecting outwardly through respective mounting holes defined in the combustor liner, the respective studs each having a threaded portion for threaded engagement with a respective nut.

3. The combustor defined in claim 2 , wherein the respective studs extend from the back face of the heat shield through the respective mounting holes defined in the combustor liner.

4. The combustor defined in claim 2 , wherein the length the elongated body is aligned with and positioned over the rail of the heat shield generally corresponds to a length of the rail of the heat shield.

5. The combustor defined in claim 2 , the elongated body being pressed against the outer surface of the combustor liner by the respective nuts engaging the respective threaded portions of the respective studs.

6. The combustor defined in claim 2 , wherein each of the two anchoring points comprises a washer portion.

Assignees

• Pratt & Whitney Canada

Inventors

• Hayek Daniel
• Herborth Jason
• Wang Yen-Wen

Classifications

• F23R3/002 Primary

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

• F23R2900/00012

  Details of sealing devices · CPC title

• F23R3/60

  Support structures; Attaching or mounting means · CPC title