Titanium-Aluminium-Seatslide

A first region (2) is made of a titanium material, a second region (4) is made of aluminum. The two are materially-bonded together by a deep-welding process in the aluminum, in combination with a diffusion process toward the titanium material, which is driven by the heat flux. Heat is supplied by a...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	KREIMEYER, MICHAEL, SCHUMACHER, JOERG, VOLLERTSEN, FRANK, KOCIK, RAINER, KASCHEL, SEBASTIAN
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CLADDING OR PLATING BY SOLDERING OR WELDING COSMONAUTICS CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS SOLDERING OR UNSOLDERING TRANSPORTING WELDING WORKING BY LASER BEAM
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A first region (2) is made of a titanium material, a second region (4) is made of aluminum. The two are materially-bonded together by a deep-welding process in the aluminum, in combination with a diffusion process toward the titanium material, which is driven by the heat flux. Heat is supplied by a de-focused laser beam or an electron beam, under a protective gas atmosphere. An independent claim is included for the corresponding method.