Invention Grant
- Patent Title: Preferential cooling of gas turbine nozzles
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Application No.: US12719674Application Date: 2010-03-08
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Publication No.: US10337404B2Publication Date: 2019-07-02
- Inventor: Kevin Weston McMahan , Joseph V. Citeno
- Applicant: Kevin Weston McMahan , Joseph V. Citeno
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Fletcher Yoder, P.C.
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D9/04 ; F01D25/08 ; F02C7/12

Abstract:
Turbine nozzle assemblies include a plurality of circumferentially spaced first components and second components, which are designed to provide different amounts of cooling. The second components, which are generally aligned with an opening of transition pieces, are designed to provide more cooling than the first components, which are generally aligned with interfaces between the transition pieces.
Public/Granted literature
- US20110217159A1 PREFERENTIAL COOLING OF GAS TURBINE NOZZLES Public/Granted day:2011-09-08
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