Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor

• US 8,459,042 B2
• Filed: 01/19/2012
• Issued: 06/11/2013
• Est. Priority Date: 12/27/2007
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Lohmueller, Steven Joseph
• Primary Examiner(s): NGUYEN, ANDREW H
• Application Number:
  US13/353,414
• Publication Number:
  US 20120114478A1
• Time in Patent Office: 509 Days
• Field of Search: 60796-797, 60799-800, 607/37, 607/40, 60746-748, 607/52, 60754-760, 60/398.21
• US Class Current: 60/800
• CPC Class Codes: F23R 3/04 Air inlet arrangements
• CPC Class Codes: F23R 3/26 Controlling the air flow
• CPC Class Codes: F23R 3/283 Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

In a gas turbine engine combustor and method for delivering purge gas thereto, a ferrule is generally coupled to the housing and moveable relative thereto. The ferrule has a primary opening through which a combustor component extends into a combustion chamber of the combustor. The ferrule further has a plurality of purge gas openings separate from and in transversely spaced relationship with the primary opening to allow purge gas to flow through the ferrule. In a first position of the ferrule at least one purge gas opening is blocked against the flow of purge gas therethrough and at least one other purge gas opening is unblocked against purge gas flow. In a second position of the ferrule at least one of the blocked purge gas openings of the first ferrule position is unblocked to permit the flow of purge gas therethrough.

Claims

1. A ferrule assembly for mounting a combustor component on a combustor housing of a gas turbine engine, the combustor housing at least in part defining an internal combustion chamber of the combustor, the ferrule assembly comprising:

a ferrule mount secured to the housing to remain generally stationery relative thereto during operation of the gas turbine engine; and

a ferrule mounted on the ferrule mount for transverse sliding movement relative thereto between a first transverse ferrule position and a second transverse ferrule position, the ferrule having a primary opening for receiving the combustor component therethrough for conjoint transverse movement with the ferrule relative to the ferrule mount, said ferrule further having a plurality of purge gas openings formed therein separate from and uniformly spaced transversely from the primary opening a first distance, a plurality of second purge gas openings uniformly spaced transversely from the primary opening a second distance greater than said first distance, and a plurality of third purge gas openings uniformly spaced transversely from the primary opening a third distance greater than said second distance, in the first ferrule position at least one of the second purge gas openings and at least one of the third purge gas openings being blocked by the ferrule mount against the flow of purge gas therethrough, at least one of said blocked second purge gas openings and at least one of said blocked third purge gas openings being unblocked by the ferrule mount in the second ferrule position to permit the flow of purge gas therethrough into the combustion chamber.

2. The ferrule assembly set forth in claim 1, wherein the ferrule is moveable through a maximum range of transverse movement relative to said ferrule mount, the ferrule mount being configured to limit transverse movement of the ferrule relative thereto to said maximum range of transverse movement.

3. The ferrule assembly set forth in claim 2, wherein at least one of said first, second, or third purge gas openings remains unblocked at every position of the ferrule throughout said maximum range of transverse movement of said ferrule relative to said ferrule mount.

4. The ferrule assembly set forth in claim 1, wherein in the second position of the ferrule relative to the ferrule mount at least one of the unblocked purge gas openings of the first ferrule position is blocked by said ferrule mount against the flow of purge gas into the combustion chamber.

5. The ferrule assembly set forth in claim 1, wherein all of the third purge gas openings are blocked against the flow of purge gas therethrough in the first position of the ferrule.