Method for joining two components using a magnetic forming method, use of same and resulting assembly

The method involves forming form-fit geometry (15) by two components (1, 2) i.e. rotor and impeller, where the components are fixed to each other and one of components is made of a non-weldable material such as titanium aluminide. A portion of one of the components is in the form-fitting geometry wh...

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Bibliographische Detailangaben
Hauptverfasser:	Burghardt, Andreas, Matic, Mario, Ramsayer, Reiner
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	The method involves forming form-fit geometry (15) by two components (1, 2) i.e. rotor and impeller, where the components are fixed to each other and one of components is made of a non-weldable material such as titanium aluminide. A portion of one of the components is in the form-fitting geometry when the components are completely separated. One of the components is subjected, before or during the joining process to temperature treatment such as heating treatment. The two components are circular in cross section and concentrically arranged with each other. An independent claim is also included for a components composite.