Invention Application
- Patent Title: Turbine Blade Platform Undercut
- Patent Title (中): 涡轮叶片平台底切
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Application No.: US13078664Application Date: 2011-04-01
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Publication No.: US20120251331A1Publication Date: 2012-10-04
- Inventor: Douglas James Dietrich , Stephen Wayne Fiebiger , Gregory Edwin Vogel
- Applicant: Douglas James Dietrich , Stephen Wayne Fiebiger , Gregory Edwin Vogel
- Applicant Address: CH Baden
- Assignee: ALSTOM TECHNOLOGY LTD.
- Current Assignee: ALSTOM TECHNOLOGY LTD.
- Current Assignee Address: CH Baden
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
A system and method of extending the useable life of a gas turbine blade is disclosed in which the gas turbine blade includes an undercut configuration designed to relieve mechanical and thermal stress imparted into the pedestal region of the airfoil trailing edge. The embodiments of the present invention include turbine blade configurations having different trailing edge undercut configurations as well as additional cooling supplied to the internal passages of the trailing edge region of the turbine blade.
Public/Granted literature
- US08550783B2 Turbine blade platform undercut Public/Granted day:2013-10-08
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