JP2014528371A5 - - Google Patents

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Publication number
JP2014528371A5
JP2014528371A5 JP2014534561A JP2014534561A JP2014528371A5 JP 2014528371 A5 JP2014528371 A5 JP 2014528371A5 JP 2014534561 A JP2014534561 A JP 2014534561A JP 2014534561 A JP2014534561 A JP 2014534561A JP 2014528371 A5 JP2014528371 A5 JP 2014528371A5
Authority
JP
Japan
Prior art keywords
peel
arms
resistant
resistant mechanism
adhesive
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.)
Granted
Application number
JP2014534561A
Other languages
English (en)
Japanese (ja)
Other versions
JP5954804B2 (ja
JP2014528371A (ja
Filing date
Publication date
Priority claimed from US13/269,062 external-priority patent/US8895130B2/en
Application filed filed Critical
Publication of JP2014528371A publication Critical patent/JP2014528371A/ja
Publication of JP2014528371A5 publication Critical patent/JP2014528371A5/ja
Application granted granted Critical
Publication of JP5954804B2 publication Critical patent/JP5954804B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2014534561A 2011-10-07 2012-07-13 コンポーネントの結合に使用される耐剥離性機構 Expired - Fee Related JP5954804B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/269,062 US8895130B2 (en) 2011-10-07 2011-10-07 Peel-resistant mechanism for use in bonding components
US13/269,062 2011-10-07
PCT/US2012/046781 WO2013052193A1 (en) 2011-10-07 2012-07-13 Peel-resistant mechanism for use in bonding components

Publications (3)

Publication Number Publication Date
JP2014528371A JP2014528371A (ja) 2014-10-27
JP2014528371A5 true JP2014528371A5 (enExample) 2015-07-23
JP5954804B2 JP5954804B2 (ja) 2016-07-20

Family

ID=46724593

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014534561A Expired - Fee Related JP5954804B2 (ja) 2011-10-07 2012-07-13 コンポーネントの結合に使用される耐剥離性機構

Country Status (7)

Country Link
US (2) US8895130B2 (enExample)
EP (1) EP2747988B1 (enExample)
JP (1) JP5954804B2 (enExample)
KR (2) KR102055530B1 (enExample)
CN (1) CN103842163B (enExample)
CA (1) CA2848081C (enExample)
WO (1) WO2013052193A1 (enExample)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170259514A1 (en) * 2014-10-17 2017-09-14 Philmore H. Colburn, II Repair patch for rotor blade
CA3147928C (en) 2021-03-05 2025-09-09 The Boeing Company STRUCTURES AND METHODS FOR REPAIRING COMPOSITE ELEMENTS

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2855014A (en) 1954-04-24 1958-10-07 Stahlgruber Gruber & Co Otto Repair patch for rubber and rubberized articles
GB868380A (en) * 1958-12-17 1961-05-17 Romac Ind Ltd Improvements in or relating to repair patches and plasters
US4978404A (en) * 1986-07-21 1990-12-18 The Boeing Company Method for repairing a hole in a structural wall of composite material
DE3726991A1 (de) * 1987-08-13 1989-02-23 Stahlgruber Gruber & Co Otto Reparaturflicken fuer gummi- und kunststoffgegenstaende
GB9622780D0 (en) * 1996-11-01 1997-01-08 British Aerospace Repair of composite laminates
US10390647B2 (en) * 2004-04-08 2019-08-27 Parallax Group International, Llc Floor matting
US20070264458A1 (en) * 2005-07-16 2007-11-15 Kenneth Luna Patch for boards
US20070014957A1 (en) * 2005-07-16 2007-01-18 Dean Sislin Patch for boards
US8765245B2 (en) * 2008-03-04 2014-07-01 Source One Distributors, Inc. Self adhering fabric patch
CN201291594Y (zh) * 2008-08-26 2009-08-19 励土峰 免锉补胎贴片
US8524356B1 (en) 2009-03-09 2013-09-03 The Boeing Company Bonded patch having multiple zones of fracture toughness
US8409384B2 (en) 2009-03-09 2013-04-02 The Boeing Company Predictable bonded rework of composite structures
US8449703B2 (en) 2009-03-09 2013-05-28 The Boeing Company Predictable bonded rework of composite structures using tailored patches
US8540909B2 (en) 2009-03-09 2013-09-24 The Boeing Company Method of reworking an area of a composite structure containing an inconsistency
US8815132B2 (en) 2010-01-18 2014-08-26 The Boeing Company Method of configuring a patch body

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