METHOD FOR PRODUCING A METAL BLADED ELEMENT OF AN AIRCRAFT TURBINE ENGINE

A method for producing a metal bladed element of a turbine engine, in particular of an aircraft, includes steps of producing the bladed element, depositing a coating made of wear-proof material on at least one portion of the bladed element and verifying, preferably visually, the conformity of the bl...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Loisel, Bruno Marc-Etienne, Nguyen, Alexandre Thanh Nhan, Pragassam, Carine Thuy-Huong, Evrard, Guillaume Sylvain Frédéric
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES LIGHTING MACHINES OR ENGINES IN GENERAL MEASURING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PHYSICS STEAM ENGINES TESTING WEAPONS
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