METHOD FOR THE PRODUCTION OF COMPONENTS OF A GAS TURBINE

The invention relates to a method for producing components preferably of a gas turbine, particularly an aircraft engine, by means of powder-metallurgical injection molding. In powder-metallurgical injection molding, a powder metal is first mixed with a binding agent so as to obtain a homogeneous mas...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ANDREES, GERHARD, KRANZEDER, JOSEF, KRAUS, MAX, LACKERMEIER, RAIMUND
Format: Patent
Sprache:eng ; fre ; ger
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