MULTIFRAME BLADE TIP WELDING FIXTURE

A system (40) includes a stand (42) having a first axis (90), a first arm (44), and a second arm (44). The first arm (44) and the second arm (44) extend from the axis (90). The first arm (44) is configured to rotate about the axis (90) and the second arm (44) is configured to rotate about the axis (...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	GONTARSKI, Tomasz, MIEKUS, Marek, POLTORAK, Grzegorz, KOWALCZYK, Michal, STECKOWICZ, Piotr
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CASTING CLADDING OR PLATING BY SOLDERING OR WELDING COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING MACHINE TOOLS MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS MAKING METALLIC POWDER MANUFACTURE OF ARTICLES FROM METALLIC POWDER METAL-WORKING NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS POWDER METALLURGY SOLDERING OR UNSOLDERING TRANSPORTING WELDING WORKING BY LASER BEAM WORKING METALLIC POWDER
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A system (40) includes a stand (42) having a first axis (90), a first arm (44), and a second arm (44). The first arm (44) and the second arm (44) extend from the axis (90). The first arm (44) is configured to rotate about the axis (90) and the second arm (44) is configured to rotate about the axis (90). The system (40) includes a first can (48) coupled to the first arm (44). The first can (48) is configured to be disposed around a first tip (100) of a first airfoil (80), the first can (48) is configured to receive a first gas flow, and the first can (48) is configured to distribute the first gas flow to a first work cavity (56) around the first tip (100) of the first airfoil (80). The system (40) further includes a second can (48) coupled to the second arm (44). The second can (48) is configured to be disposed around a second tip (100) of a second airfoil (82), the second can (48) is configured to receive a second gas flow, and the second can (48) is configured to distribute the second gas flow to a second work cavity (56) of the second airfoil (82).