Manufacturing turbine engine components using a masking member

A method for masking at least one turbine engine component (30) wherein the method includes providing at least one masking member (31), securing each masking member to the at least one turbine engine component, and applying a metal coating to the at least one turbine engine component. The masking me...

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Bibliographische Detailangaben
Hauptverfasser:	PHILIP ROBERT HAWTIN, MICHAEL SMITH
Format:	Patent
Sprache:	eng
Schlagworte:	CHEMICAL SURFACE TREATMENT CHEMISTRY COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATIONOR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY IONIMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL COATING MATERIAL WITH METALLIC MATERIAL COATING METALLIC MATERIAL DIFFUSION TREATMENT OF METALLIC MATERIAL INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION INGENERAL METALLURGY SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THESURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION
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Beschreibung
Zusammenfassung:	A method for masking at least one turbine engine component (30) wherein the method includes providing at least one masking member (31), securing each masking member to the at least one turbine engine component, and applying a metal coating to the at least one turbine engine component. The masking member extends between adjacent seal teeth of the turbine engine component. The masking member may be subsequently removed.