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Title:
高圧タービンシュラウドの修復方法
Document Type and Number:
Japanese Patent JP4463359
Kind Code:
B2
Abstract:
A method for repairing the shroud surfaces of a gas turbine engine to provide corrosion and oxidation resistance of the shroud segments (10) while also restoring the dimensional integrity of the shroud segments (10) . The method entails removing the oxidation and corrosion products from the shroud segment (10) , removing preexisting coating materials, applying a material compatible with the shroud segment substrate material, machining the surface, applying a corrosion-resistant, oxidation-resistant and rub-compliant material to the shroud segment using a HVOF process, machining the shroud segment (10) to preselected dimensions and applying an aluminide coating for improved oxidation and corrosion resistance of the repaired surfaces.

Inventors:
Warren Davis Groscrows, Juniors
Patricia Ann Charles
Application Number:
JP35582499A
Publication Date:
May 19, 2010
Filing Date:
December 15, 1999
Export Citation:
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Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F01D11/08; F02C7/00; C23C4/00; C23C4/12; C23C10/02; F01D25/00
Domestic Patent References:
JP8284604A
JP5042425A
JP9133006A
JP9195067A
Foreign References:
US5794338
Attorney, Agent or Firm:
Arakawa Satoshi



 
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