MULTIFRAME BLADE TIP WELDING FIXTURE

A system includes a stand having a first axis, a first arm, and a second arm. The first arm and the second arm extend from the axis. The first arm is configured to rotate about the axis and the second arm is configured to rotate about the axis. The system includes a first can coupled to the first ar...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	GONTARSKI, Tomasz, MIEKUS, Marek, POLTORAK, Grzegorz, KOWALCZYK, Michal, STECKOWICZ, Piotr
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT COMBINED OPERATIONS DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINE TOOLS MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OTHER WORKING OF METAL PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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Beschreibung
Zusammenfassung:	A system includes a stand having a first axis, a first arm, and a second arm. The first arm and the second arm extend from the axis. The first arm is configured to rotate about the axis and the second arm is configured to rotate about the axis. The system includes a first can coupled to the first arm. The first can is configured to be disposed around a first tip of a first airfoil, the first can is configured to receive a first gas flow, and the first can is configured to distribute the first gas flow to a first work cavity around the first tip of the first airfoil. The system further includes a second can coupled to the second arm. The second can is configured to be disposed around a second tip of a second airfoil, the second can is configured to receive a second gas flow, and the second can is configured to distribute the second gas flow to a second work cavity of the second airfoil.