Invention Application
- Patent Title: METHOD FOR RECONDITIONING A HOT GAS PATH PART OF A GAS TURBINE
- Patent Title (中): 用于重新燃气涡轮机的热气路径的方法
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Application No.: US14851459Application Date: 2015-09-11
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Publication No.: US20160069185A1Publication Date: 2016-03-10
- Inventor: Alexander STANKOWSKI , Julien Rene Andre Zimmermann , Simone Hoevel , Piero-Daniele Grasso , Sven Olliges , Sophie Betty Claire Duval
- Applicant: ALSTOM Technology Ltd
- Priority: EP13160050.4 20130319
- Main IPC: F01D5/00
- IPC: F01D5/00 ; C23C4/08 ; B23K26/00 ; B23P6/00 ; B23K26/342

Abstract:
A method for reconditioning a hot gas path part of a gas turbine in order to flexibly adapt an operation regime of said gas turbine for subsequent operation intervals is disclosed. The method includes providing a hot gas path part to be reconditioned; removing a predetermined area of said hot gas path part, resulting in a cutout at said hot gas path part; and manufacturing a coupon for being inserted into said cutout to replace said removed area of said hot gas path part. The method further includes inserting said coupon into said cutout; and joining said hot gas path part with said inserted coupon. The coupon is manufactured by a selective laser melting (SLM) method resulting in a fine grain sized material with significantly improved low cycle fatigue (LCF) lifetime. The hot gas path part is coated, at least in an area comprising said inserted coupon, with a metallic overlay with improved thermo-mechanical fatigue (TMF) and oxidation lifetime.
Public/Granted literature
- US09926785B2 Method for reconditioning a hot gas path part of a gas turbine Public/Granted day:2018-03-27
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