Invention Grant
US07707835B2 Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air 有权
用于涡轮机燃烧器的轴流套筒和引入流动套管空气的方法

Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air
Abstract:
A combustor has a flow sleeve and a flow liner defining a generally axial flow direction of compressor discharge air toward combustor burners. A casing is secured to the forward end of the flow sleeve defining an annular plenum along the interior of the flow sleeve. Openings through the flow sleeve supply compressor discharge air into the plenum where the air changes direction for flow through apertures into and generally coaxially with the free air stream. The axial injection minimizes or eliminates energy losses due to cross flow injection within the axial air stream while continuing to cool the liner.
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