Invention Grant
- Patent Title: Gas turbine blade and manufacturing method
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Application No.: US15397810Application Date: 2017-01-04
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Publication No.: US10669858B2Publication Date: 2020-06-02
- Inventor: Alexey Mozharov , Andreas Bauer , Dominic Graf
- Applicant: General Electric Technology GmbH
- Applicant Address: CH Baden
- Assignee: General Electric Technology GmbH
- Current Assignee: General Electric Technology GmbH
- Current Assignee Address: CH Baden
- Agency: Fletcher Yoder, P.C.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@4c52c094
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
A blade for a gas turbine is described, the blade comprising a trailing edge and a trailing edge cooling channel extending from a first upstream end to a second downstream end, in which the width of the trailing edge cooling channel in the direction perpendicular to the camber line of the blade varies and the narrowest width in the trailing edge cooling channel is at the first upstream end, so as to provide a blade where the trailing edge can be removed with a minimal change or no change in the cooling flow capacity through the trailing edge cooling channel. Related methods are also described.
Public/Granted literature
- US20170204729A1 GAS TURBINE BLADE AND MANUFACTURING METHOD Public/Granted day:2017-07-20
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