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Title: Turbine airfoil to shroud attachment method

Abstract

Bi-casting a platform (50) onto an end portion (42) of a turbine airfoil (31) after forming a coating of a fugitive material (56) on the end portion. After bi-casting the platform, the coating is dissolved and removed to relieve differential thermal shrinkage stress between the airfoil and platform. The thickness of the coating is varied around the end portion in proportion to varying amounts of local differential process shrinkage. The coating may be sprayed (76A, 76B) onto the end portion in opposite directions parallel to a chord line (41) of the airfoil or parallel to a mid-platform length (80) of the platform to form respective layers tapering in thickness from the leading (32) and trailing (34) edges along the suction side (36) of the airfoil.

Inventors:
; ; ; ;
Issue Date:
Research Org.:
Siemens Energy, Inc., Orlando, FL (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1166020
Patent Number(s):
8,914,976
Application Number:
13/195,959
Assignee:
Siemens Energy, Inc. (Orlando, FL) NETL
DOE Contract Number:  
FC26-05NT42644
Resource Type:
Patent
Resource Relation:
Patent File Date: 2011 Aug 02
Country of Publication:
United States
Language:
English
Subject:
36 MATERIALS SCIENCE; 17 WIND ENERGY

Citation Formats

Campbell, Christian X, Kulkarni, Anand A, James, Allister W, Wessell, Brian J, and Gear, Paul J. Turbine airfoil to shroud attachment method. United States: N. p., 2014. Web.
Campbell, Christian X, Kulkarni, Anand A, James, Allister W, Wessell, Brian J, & Gear, Paul J. Turbine airfoil to shroud attachment method. United States.
Campbell, Christian X, Kulkarni, Anand A, James, Allister W, Wessell, Brian J, and Gear, Paul J. Tue . "Turbine airfoil to shroud attachment method". United States. https://www.osti.gov/servlets/purl/1166020.
@article{osti_1166020,
title = {Turbine airfoil to shroud attachment method},
author = {Campbell, Christian X and Kulkarni, Anand A and James, Allister W and Wessell, Brian J and Gear, Paul J},
abstractNote = {Bi-casting a platform (50) onto an end portion (42) of a turbine airfoil (31) after forming a coating of a fugitive material (56) on the end portion. After bi-casting the platform, the coating is dissolved and removed to relieve differential thermal shrinkage stress between the airfoil and platform. The thickness of the coating is varied around the end portion in proportion to varying amounts of local differential process shrinkage. The coating may be sprayed (76A, 76B) onto the end portion in opposite directions parallel to a chord line (41) of the airfoil or parallel to a mid-platform length (80) of the platform to form respective layers tapering in thickness from the leading (32) and trailing (34) edges along the suction side (36) of the airfoil.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2014},
month = {12}
}

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