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
- Patent Title: Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air
- Patent Title (中): 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
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Application No.: US11152234Application Date: 2005-06-15
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Publication No.: US07707835B2Publication Date: 2010-05-04
- Inventor: John Joseph Lipinski , Thomas Edward Johnson , Robert Paul Ziegler , Mark Stewart Schroder
- Applicant: John Joseph Lipinski , Thomas Edward Johnson , Robert Paul Ziegler , Mark Stewart Schroder
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Nixon & Vanderhye, P.C.
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F02G3/00

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.
Public/Granted literature
- US20060283189A1 Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air Public/Granted day:2006-12-21
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