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
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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.)
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Application number
JP2016564577A
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English (en)
Japanese (ja)
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JP6587635B2 (ja
JP2017515703A (ja
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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 (cg-RX-API-DMAC7.html) 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 (cg-RX-API-DMAC7.html)
JP (1) JP6587635B2 (cg-RX-API-DMAC7.html)
CN (1) CN106794645B (cg-RX-API-DMAC7.html)
ES (1) ES2770020T3 (cg-RX-API-DMAC7.html)
WO (1) WO2015167630A1 (cg-RX-API-DMAC7.html)

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
US12275227B2 (en) 2020-02-11 2025-04-15 Helicoid Industries, Inc. Composite materials and structures
US11376812B2 (en) 2020-02-11 2022-07-05 Helicoid Industries Inc. Shock and impact resistant 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
US11852297B2 (en) 2021-06-01 2023-12-26 Helicoid Industries Inc. Containers and methods for protecting pressure vessels
US11346499B1 (en) 2021-06-01 2022-05-31 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
CA3260537A1 (en) 2022-06-27 2024-01-04 Helicoid Industries Inc. Reinforced fiber resistant to significant impacts 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
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

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