Methods and system for reducing pressure losses in gas...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S039370, C060S752000, C060S757000, C060S760000

Reexamination Certificate

active

07571611

ABSTRACT:
A method of assembling a combustor assembly is provided, wherein the method includes providing a combustor liner having a centerline axis and defining a combustion chamber therein, and coupling an annular flowsleeve radially outward from the combustor liner such that an annular flow path is defined substantially circumferentially between the flowsleeve and the combustor liner. The method also includes orienting the flowsleeve such that a plurality of inlets formed within the flowsleeve are positioned to inject cooling air in a substantially axial direction into the annular flow path to facilitate cooling the combustor liner.

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