METHOD FOR ADJUSTING HIGHLY-DEFORMABLE TITANIUM AND TITANIUM-ALLOY INTEGRATED FASTENER AND FASTENER ADJUSTED THEREBY

PROBLEM TO BE SOLVED: To solve a problem that there exists a need in a technology for an integrated fastener reduced in the complexity of installation which may be installed in a short time while providing strength characteristics which are at least equivalent to conventional two-piece fasteners.SOL...

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Bibliographische Detailangaben
1. Verfasser:	KEENER STEVEN G
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ENGINEERING ELEMENTS AND UNITS FORGE FURNACES FORGING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HAMMERING HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL PERFORMING OPERATIONS PRESSING METAL PUNCHING METAL RIVETING THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To solve a problem that there exists a need in a technology for an integrated fastener reduced in the complexity of installation which may be installed in a short time while providing strength characteristics which are at least equivalent to conventional two-piece fasteners.SOLUTION: A fastener 200 has a cold-worked head 204, a cold-worked shank 212, and a ductile shank 214 extending from the cold-worked shank 212 to a tail end 210 of the fastener 200.