Invention Grant
- Patent Title: Method of assembling a structure using highly-deformable titanium and titanium-alloy one-piece fasteners
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Application No.: US14569031Application Date: 2014-12-12
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Publication No.: US09649682B2Publication Date: 2017-05-16
- Inventor: Steven G. Keener
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Main IPC: B21K1/60
- IPC: B21K1/60 ; B21J15/02 ; B21K1/58 ; F16B19/06 ; F16B5/04

Abstract:
A method of forming a fastener may include inserting a blank precursor into a bore of a forming die having an enlarged bore portion. The method may further include applying a first axial compression force to the blank precursor, and forming a cold-worked head section and an enlarged shank portion on the blank precursor corresponding to the enlarged bore portion. The enlarged shank portion may have a nominal shank portion extending therefrom. The method may additionally include inserting the nominal shank portion into a bore of a final reduction die, applying a second axial compression force to the enlarged shank portion, and urging the enlarged shank portion into the bore of the final reduction die. The method may also include reducing a cross-sectional area of the enlarged shank portion by approximately 2 to 5 percent to form a cold-worked shank section.
Public/Granted literature
- US20150096166A1 METHOD FOR PREPARING HIGHLY-DEFORMABLE TITANIUM AND TITANIUM-ALLOY ONE-PIECE FASTENERS Public/Granted day:2015-04-09
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