JP2017515703A5 - - Google Patents

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Publication number
JP2017515703A5
JP2017515703A5 JP2016564577A JP2016564577A JP2017515703A5 JP 2017515703 A5 JP2017515703 A5 JP 2017515703A5 JP 2016564577 A JP2016564577 A JP 2016564577A JP 2016564577 A JP2016564577 A JP 2016564577A JP 2017515703 A5 JP2017515703 A5 JP 2017515703A5
Authority
JP
Japan
Prior art keywords
section
composite
adhesive
tapered
adhesive layers
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
JP2016564577A
Other languages
English (en)
Japanese (ja)
Other versions
JP2017515703A (ja
JP6587635B2 (ja
Filing date
Publication date
Priority claimed from US14/267,220 external-priority patent/US9492975B2/en
Application filed filed Critical
Priority claimed from PCT/US2015/012897 external-priority patent/WO2015167630A1/en
Publication of JP2017515703A publication Critical patent/JP2017515703A/ja
Publication of JP2017515703A5 publication Critical patent/JP2017515703A5/ja
Application granted granted Critical
Publication of JP6587635B2 publication Critical patent/JP6587635B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2016564577A 2014-05-01 2015-01-26 テーパ状の接着設計を有する構造的な接合パッチ Active JP6587635B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US14/267,220 2014-05-01
US14/267,220 US9492975B2 (en) 2009-03-09 2014-05-01 Structural bonded patch with tapered adhesive design
PCT/US2015/012897 WO2015167630A1 (en) 2014-05-01 2015-01-26 Structural bonded patch with tapered adhesive design

Publications (3)

Publication Number Publication Date
JP2017515703A JP2017515703A (ja) 2017-06-15
JP2017515703A5 true JP2017515703A5 (https=) 2018-03-01
JP6587635B2 JP6587635B2 (ja) 2019-10-09

Family

ID=52462466

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016564577A Active JP6587635B2 (ja) 2014-05-01 2015-01-26 テーパ状の接着設計を有する構造的な接合パッチ

Country Status (5)

Country Link
EP (1) EP3137288B1 (https=)
JP (1) JP6587635B2 (https=)
CN (1) CN106794645B (https=)
ES (1) ES2770020T3 (https=)
WO (1) WO2015167630A1 (https=)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016125468A1 (de) * 2016-12-22 2018-06-28 Rheinmetall Man Military Vehicles Gmbh Befestigungsvorrichtung
JP7065052B2 (ja) * 2019-03-14 2022-05-11 三菱重工業株式会社 フィッティング方法及び修理方法
CN109838435B (zh) * 2019-04-02 2023-09-05 苏州鑫本智能科技有限公司 一体化定位贴片机构
US11376812B2 (en) 2020-02-11 2022-07-05 Helicoid Industries Inc. Shock and impact resistant structures
US12275227B2 (en) 2020-02-11 2025-04-15 Helicoid Industries, Inc. Composite materials and structures
CN113187788A (zh) * 2021-04-16 2021-07-30 辽宁忠旺铝合金精深加工有限公司 一种提高粘接可靠性的刚性支撑
US11346499B1 (en) 2021-06-01 2022-05-31 Helicoid Industries Inc. Containers and methods for protecting pressure vessels
US11852297B2 (en) 2021-06-01 2023-12-26 Helicoid Industries Inc. Containers and methods for protecting pressure vessels
CN114211785B (zh) * 2021-12-13 2024-03-29 沈阳航空航天大学 一种飞机蒙皮破洞型损伤的复合材料修复工艺
CN115042458B (zh) * 2022-06-22 2024-06-18 沈阳飞机工业（集团）有限公司 一种可用于飞机盒段结构复合材料构件的胶接修补工艺
WO2024006078A1 (en) 2022-06-27 2024-01-04 Helicoid Industries Inc. High impact-resistant, reinforced fiber for leading edge protection of aerodynamic structures

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5207541A (en) * 1988-12-13 1993-05-04 The Boeing Company Scarfing apparatus
US5626934A (en) * 1995-10-20 1997-05-06 United States Of America Enhancing damage tolerance of adhesive bonds
US7628879B2 (en) * 2007-08-23 2009-12-08 The Boeing Company Conductive scrim embedded structural adhesive films
GB0721546D0 (en) * 2007-11-01 2007-12-12 Rolls Royce Plc Composite material repair
US8617694B1 (en) * 2009-03-09 2013-12-31 The Boeing Company Discretely tailored multi-zone bondline for fail-safe structural repair
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
US8524356B1 (en) * 2009-03-09 2013-09-03 The Boeing Company Bonded patch having multiple zones of fracture toughness

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