AU2001253370A1 - Non-removable structural fastener assembly and method of forming same - Google Patents

Non-removable structural fastener assembly and method of forming same

Info

Publication number
AU2001253370A1
AU2001253370A1 AU2001253370A AU5337001A AU2001253370A1 AU 2001253370 A1 AU2001253370 A1 AU 2001253370A1 AU 2001253370 A AU2001253370 A AU 2001253370A AU 5337001 A AU5337001 A AU 5337001A AU 2001253370 A1 AU2001253370 A1 AU 2001253370A1
Authority
AU
Australia
Prior art keywords
fastener assembly
forming same
structural fastener
removable structural
removable
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU2001253370A
Inventor
Todd Diamond
John A. Duran
Edward A. Vetisian
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Avibank Mfg Inc
Original Assignee
Avibank Mfg Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Avibank Mfg Inc filed Critical Avibank Mfg Inc
Publication of AU2001253370A1 publication Critical patent/AU2001253370A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B39/00Locking of screws, bolts or nuts
    • F16B39/22Locking of screws, bolts or nuts in which the locking takes place during screwing down or tightening
    • F16B39/28Locking of screws, bolts or nuts in which the locking takes place during screwing down or tightening by special members on, or shape of, the nut or bolt
    • F16B39/30Locking exclusively by special shape of the screw-thread
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/02Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
    • F16B5/0208Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread using panel fasteners, i.e. permanent attachments allowing for quick assembly
AU2001253370A 2000-04-18 2001-04-11 Non-removable structural fastener assembly and method of forming same Abandoned AU2001253370A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/552,474 US6290445B1 (en) 2000-04-18 2000-04-18 Non-removable structural threaded fastener with threads of lesser outer diameter than the shank and method of forming same
US09552474 2000-04-18
PCT/US2001/011814 WO2001079708A2 (en) 2000-04-18 2001-04-11 A reduced weight threaded fastener assembly and method of forming

Publications (1)

Publication Number Publication Date
AU2001253370A1 true AU2001253370A1 (en) 2001-10-30

Family

ID=24205487

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001253370A Abandoned AU2001253370A1 (en) 2000-04-18 2001-04-11 Non-removable structural fastener assembly and method of forming same

Country Status (6)

Country Link
US (6) US6290445B1 (en)
EP (1) EP1274948A4 (en)
JP (1) JP2004510102A (en)
AU (1) AU2001253370A1 (en)
CA (1) CA2406978A1 (en)
WO (1) WO2001079708A2 (en)

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US9440744B2 (en) 2013-10-17 2016-09-13 The Boeing Company Decompression panel assembly and method of equalizing air pressure differential
US10071795B2 (en) * 2013-10-25 2018-09-11 The Boeing Company Clamp device for use with a decompression panel in an aircraft assembly
US9233747B2 (en) 2013-10-25 2016-01-12 The Boeing Company Decompression panel for use in an aircraft assembly
US9499251B2 (en) 2013-10-25 2016-11-22 The Boeing Company Decompression panel for use in an aircraft
US9566759B2 (en) 2013-10-25 2017-02-14 The Boeing Company Decompression panel for use in an aircraft assembly
ES2857194T3 (en) 2014-02-18 2021-09-28 Centrix Inc One-piece screws for, and methods of producing and using, blind side fasteners and systems with free-spinning feature
USD817851S1 (en) 2014-03-28 2018-05-15 The Boeing Company Decompression panel
EP3192737B1 (en) * 2016-01-14 2020-12-02 Safran Landing Systems UK Limited Shock strut
JP7078264B2 (en) 2016-02-26 2022-05-31 セントリックス インク. Finger-type expandable collet body with anti-rotation mechanism, clips, inserts, and system containing them
US10378571B2 (en) 2016-03-17 2019-08-13 Centrix Inc. Removable, single side fastener with ultra-low stack height grip range, components, and methods for making and using the same
DE112017002111B4 (en) 2016-04-20 2021-07-22 Centrix Inc. One-sided, temporary holding device with constant pressure functionality
US10436240B2 (en) * 2016-05-06 2019-10-08 The Boeing Company Fastening system and method
USD802410S1 (en) * 2016-06-03 2017-11-14 Salvador Felix Hex fastener
USD799315S1 (en) * 2016-06-10 2017-10-10 Security Locknut, LLC Locknut
EP3296029A1 (en) * 2016-09-16 2018-03-21 Metso Sweden Ab Hammerless solution
WO2018157082A1 (en) 2017-02-27 2018-08-30 Centrix Aero, LLC Sensor pin
US10920812B2 (en) 2017-03-09 2021-02-16 Centrix Inc. Fastener system with expandable ring
US10589835B2 (en) 2017-03-29 2020-03-17 The Boeing Company Floor panel fastener assembly
US10717515B2 (en) 2017-05-15 2020-07-21 The Boeing Company Offset flange floor panel connection system
US10800509B2 (en) 2017-05-15 2020-10-13 The Boeing Company Aircraft floor panel connection system
US10836463B2 (en) 2017-07-06 2020-11-17 The Boeing Company Aircraft floor panel floating connection system
US11692574B2 (en) 2017-09-14 2023-07-04 Centrix Inc. Fastener system
US11193517B2 (en) 2017-09-14 2021-12-07 Centrix Inc. Fastener system
WO2020158700A1 (en) * 2019-01-29 2020-08-06 株式会社大里 Nut member tightening method and tightening tool
US11204057B2 (en) * 2019-07-16 2021-12-21 Dennis Sherlin Optimized thread profile for joining composite materials
US11566655B2 (en) 2020-02-20 2023-01-31 Caterpillar Inc. Bolt retainer configuration to hold a position of a bolt within a component
CN112013005B (en) * 2020-08-12 2022-03-25 苏州剑派实业有限公司 Hexagonal head slotted nut with self-locking function

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Also Published As

Publication number Publication date
US6440001B1 (en) 2002-08-27
US20020012578A1 (en) 2002-01-31
US6290445B1 (en) 2001-09-18
US20020025242A1 (en) 2002-02-28
US20020015630A1 (en) 2002-02-07
EP1274948A2 (en) 2003-01-15
US6595734B2 (en) 2003-07-22
US20020015631A1 (en) 2002-02-07
US20020144574A1 (en) 2002-10-10
EP1274948A4 (en) 2004-12-15
WO2001079708A2 (en) 2001-10-25
CA2406978A1 (en) 2001-10-25
WO2001079708A3 (en) 2002-05-30
US6499925B2 (en) 2002-12-31
JP2004510102A (en) 2004-04-02

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