Invention Application
- Patent Title: COMBUSTOR TRANSITION PIECE WITH DILUTION SLEEVES AND RELATED METHOD
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Application No.: US12855154Application Date: 2010-08-12
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Publication No.: US20120036859A1Publication Date: 2012-02-16
- Inventor: Richard JOHNSON , Crystal McGee McConnaughhay , Bryan Wesley Romig
- Applicant: Richard JOHNSON , Crystal McGee McConnaughhay , Bryan Wesley Romig
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F02C7/12

Abstract:
A gas turbine transition piece adapted to carry combustion gases in a hot gas path extending between a gas turbine combustion chamber and a first stage of the gas turbine, includes a hollow duct having a forward end adapted for connection to a combustor liner and an aft end adapted for connection to a first stage nozzle. One or more dilution air holes are located proximate the forward end, the dilution holes each fitted with a hollow sleeve penetrating into the hot gas path within the hollow duct, the hollow sleeves adapted to supply cooling air into the hot gas path.
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