Manufacturing method of high-strength alloy cold-drawn wire for aircraft fastener

The invention relates to a manufacturing method of a high-strength alloy cold-drawn wire for an aircraft fastener. The manufacturing method comprises the following steps: taking return steel, chromium metal, a nickel plate, pure iron, manganese metal, molybdenum metal, pure titanium, aluminum metal,...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHANG LING, PEI BINGHONG, WANG RUI, FENG XU, CHEN PANQUAN, HE YUNHUA
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	ALLOYS AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKINGWITHOUT ESSENTIALLY REMOVING MATERIAL CHEMISTRY FERROUS OR NON-FERROUS ALLOYS GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUSMETALS OR ALLOYS MAKING METAL MALLEABLE BY DECARBURISATION, TEMPERING OR OTHERTREATMENTS MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES,OTHERWISE THAN BY ROLLING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL METALLURGY METALLURGY OF IRON MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS PERFORMING OPERATIONS PUNCHING METAL TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS
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