Invention Grant
- Patent Title: Nozzle guide vane with cooled platform for a gas turbine
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Application No.: US13809963Application Date: 2011-06-17
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Publication No.: US09856747B2Publication Date: 2018-01-02
- Inventor: Anthony Davis , Paul Mathew Walker
- Applicant: Anthony Davis , Paul Mathew Walker
- Applicant Address: DE Münich
- Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee Address: DE Münich
- Priority: EP10007335 20100715
- International Application: PCT/EP2011/060144 WO 20110617
- International Announcement: WO2012/007250 WO 20120119
- Main IPC: F01D25/12
- IPC: F01D25/12 ; F01D9/04

Abstract:
A platform for supporting a nozzle guide vane for a gas turbine is provided. The platform has a gas passage surface arranged to be in contact with a streaming operation gas, and a cooling channel for guiding a cooling fluid within the cooling channel formed in an inside of the platform. A cooling portion of an inner surface of the cooling channel is in thermal contact with the gas passage surface. The platform is an integrally formed part representing a segment in a circumferential direction of the gas turbine. The cooling channel has a first cooling channel portion and a second cooling channel portion arranged downstream of the first cooling channel portion with respect to a streaming direction of the operation gas. The first cooling channel portion and the second cooling channel portion are interconnected.
Public/Granted literature
- US20130209231A1 NOZZLE GUIDE VANE WITH COOLED PLATFORM FOR A GAS TURBINE Public/Granted day:2013-08-15
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