Invention Grant
- Patent Title: Turbomachinery blade having a platform relief hole
- Patent Title (中): 涡轮机叶片具有平台释放孔
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Application No.: US11383988Application Date: 2006-05-18
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Publication No.: US07862300B2Publication Date: 2011-01-04
- Inventor: Gregory M. Nadvit , Andrew D. Williams , Leone J. Tessarini , Michel P. Arnal
- Applicant: Gregory M. Nadvit , Andrew D. Williams , Leone J. Tessarini , Michel P. Arnal
- Applicant Address: CH Neuenhof
- Assignee: Wood Group Heavy Industrial Turbines AG
- Current Assignee: Wood Group Heavy Industrial Turbines AG
- Current Assignee Address: CH Neuenhof
- Agency: Baker Botts L.L.P.
- Main IPC: F01D5/12
- IPC: F01D5/12

Abstract:
A turbomachinery blade having a relief hole in its platform and a method of limiting the formation and/or propagation of cracks in the trailing edge of the blade are provided. The relief hole may be formed in the concave side of the platform proximate the trailing edge along its mean camber line. The relief hole may be circular in cross-section and is blind, i.e., does not exit on any other face of the platform. The relief hole prevents the formation of cracks in the trailing edge of the blade and also slows the propagation of any cracks which may have formed in this region of the blade.
Public/Granted literature
- US20070269313A1 TURBOMACHINERY BLADE HAVING A PLATFORM RELIEF HOLE Public/Granted day:2007-11-22
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