Manufacturing a titanium alloy part, which is useful in aeronautical industry, comprises performing N-successive treatment cycles of hot forging treatment at a specified temperature until the part obtains a uniform temperature

The process comprises performing N-successive treatment cycles of hot forging treatment at a specified temperature (T n) until the part obtains a uniform temperature. The piece is maintained at room temperature before carrying out the forging treatment. The total number of treatment cycles is 2, in...

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Bibliographische Detailangaben

Hauptverfasser:	BARUSSAUD ANNE, MONS CLAUDE MARCEL
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	ALLOYS CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS ANDNON-FERROUS ALLOYS CHEMISTRY FERROUS OR NON-FERROUS ALLOYS FORGE FURNACES FORGING HAMMERING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL METALLURGY PERFORMING OPERATIONS PRESSING METAL PUNCHING METAL RIVETING TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS
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