CN104787300B - 确定复合结构的完整性的方法和设备 - Google Patents

确定复合结构的完整性的方法和设备 Download PDF

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Publication number
CN104787300B
CN104787300B CN201410837469.0A CN201410837469A CN104787300B CN 104787300 B CN104787300 B CN 104787300B CN 201410837469 A CN201410837469 A CN 201410837469A CN 104787300 B CN104787300 B CN 104787300B
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China
Prior art keywords
composite construction
drop
contact angle
dimensional contact
bond strength
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Expired - Fee Related
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CN201410837469.0A
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English (en)
Chinese (zh)
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CN104787300A (zh
Inventor
E·A·丹于姆博
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Boeing Co
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Boeing Co
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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N13/00—Investigating surface or boundary effects, e.g. wetting power; Investigating diffusion effects; Analysing materials by determining surface, boundary, or diffusion effects
    • G01N13/02—Investigating surface tension of liquids
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0016—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of aircraft wings or blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N13/00—Investigating surface or boundary effects, e.g. wetting power; Investigating diffusion effects; Analysing materials by determining surface, boundary, or diffusion effects
    • G01N13/02—Investigating surface tension of liquids
    • G01N2013/0208—Investigating surface tension of liquids by measuring contact angle

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
  • Moulding By Coating Moulds (AREA)
CN201410837469.0A 2014-01-16 2014-12-29 确定复合结构的完整性的方法和设备 Expired - Fee Related CN104787300B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/157,211 US9518907B2 (en) 2014-01-16 2014-01-16 Methods and apparatus to determine integrity of composite structures
US14/157,211 2014-01-16

Publications (2)

Publication Number Publication Date
CN104787300A CN104787300A (zh) 2015-07-22
CN104787300B true CN104787300B (zh) 2018-12-11

Family

ID=52103220

Family Applications (1)

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CN201410837469.0A Expired - Fee Related CN104787300B (zh) 2014-01-16 2014-12-29 确定复合结构的完整性的方法和设备

Country Status (7)

Country Link
US (1) US9518907B2 (https=)
EP (1) EP2896954B1 (https=)
JP (1) JP6677447B2 (https=)
KR (1) KR102201552B1 (https=)
CN (1) CN104787300B (https=)
BR (1) BR102014023719B1 (https=)
CA (1) CA2859212C (https=)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9518907B2 (en) 2014-01-16 2016-12-13 The Boeing Company Methods and apparatus to determine integrity of composite structures
US11519840B2 (en) * 2019-01-22 2022-12-06 Ford Global Technologies, Llc Hydrophobic coating characterization
CN117195639B (zh) * 2023-09-12 2024-09-13 中航成飞民用飞机有限责任公司 基于能量耗散途径的结构抗鸟撞性能评估方法

Citations (5)

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US5216799A (en) * 1990-11-09 1993-06-08 British Aerospace Public Limited Company Carbon fibre composite wing manufacture
CN101370642A (zh) * 2006-01-11 2009-02-18 空中客车德国有限公司 元件粘合方法和装置
CN101384478A (zh) * 2006-02-17 2009-03-11 空中客车德国有限公司 免蒸压粘接飞行器用部件的方法
US8386194B1 (en) * 2010-06-24 2013-02-26 The Boeing Company Determining bond surface condition in composite structures
US8616050B1 (en) * 2011-02-09 2013-12-31 The Boeing Company Bond surface testing apparatus and method

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US4788235A (en) * 1987-11-23 1988-11-29 Minnesota Mining And Manufacturing Company Phosphite modified epoxy resin
JP2000258328A (ja) * 1999-03-08 2000-09-22 Hitachi Ltd 表面張力による実空間座標値圧力評価関数からの液体の形状予測方法
JP2005114615A (ja) * 2003-10-09 2005-04-28 Canon Inc 固体表面のぬれ性測定方法及び測定装置
WO2009126862A1 (en) * 2008-04-11 2009-10-15 3M Innovative Properties Company One-part epoxy-based structural adhesive
US8409384B2 (en) 2009-03-09 2013-04-02 The Boeing Company Predictable bonded rework of composite structures
US8617694B1 (en) 2009-03-09 2013-12-31 The Boeing Company Discretely tailored multi-zone bondline for fail-safe structural repair
US8449703B2 (en) 2009-03-09 2013-05-28 The Boeing Company Predictable bonded rework of composite structures using tailored patches
US8524356B1 (en) 2009-03-09 2013-09-03 The Boeing Company Bonded patch having multiple zones of fracture toughness
US8540909B2 (en) 2009-03-09 2013-09-24 The Boeing Company Method of reworking an area of a composite structure containing an inconsistency
JP5548494B2 (ja) * 2010-03-19 2014-07-16 東京応化工業株式会社 表面改質材料、レジストパターン形成方法及びパターン形成方法
JP2011257259A (ja) * 2010-06-09 2011-12-22 Seiko Epson Corp 接合膜の評価方法および接合膜の評価装置
JP5891482B2 (ja) * 2011-03-30 2016-03-23 ＳＡＷ＆ＳＰＲ−Ｔｅｃｈ有限会社 固体表面の接触角測定方法及びその装置
JP6218241B2 (ja) * 2011-07-29 2017-10-25 ウィスコンシン・アルムナイ・リサーチ・ファウンデーションＷｉｓｃｏｎｓｉｎ Ａｌｕｍｎｉ Ｒｅｓｅａｒｃｈ Ｆｏｕｎｄａｔｉｏｎ 薄膜の誘導組織化用ブロック共重合体物質を調製する方法並びにブロック共重合体を有する組成物および構造物
JP2013156239A (ja) * 2012-01-27 2013-08-15 Kohei Kosaka 単眼拡大鏡用接触角値換算スケール板
US9676028B2 (en) 2012-07-06 2017-06-13 Pcc Structurals, Inc. Method for processing castings
US9518907B2 (en) 2014-01-16 2016-12-13 The Boeing Company Methods and apparatus to determine integrity of composite structures

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5216799A (en) * 1990-11-09 1993-06-08 British Aerospace Public Limited Company Carbon fibre composite wing manufacture
CN101370642A (zh) * 2006-01-11 2009-02-18 空中客车德国有限公司 元件粘合方法和装置
CN101384478A (zh) * 2006-02-17 2009-03-11 空中客车德国有限公司 免蒸压粘接飞行器用部件的方法
US8386194B1 (en) * 2010-06-24 2013-02-26 The Boeing Company Determining bond surface condition in composite structures
US8616050B1 (en) * 2011-02-09 2013-12-31 The Boeing Company Bond surface testing apparatus and method

Also Published As

Publication number Publication date
BR102014023719B1 (pt) 2021-12-14
US20150198514A1 (en) 2015-07-16
JP6677447B2 (ja) 2020-04-08
CN104787300A (zh) 2015-07-22
CA2859212A1 (en) 2015-07-16
US9518907B2 (en) 2016-12-13
JP2015148603A (ja) 2015-08-20
KR20150085770A (ko) 2015-07-24
BR102014023719A2 (pt) 2015-10-06
EP2896954A1 (en) 2015-07-22
CA2859212C (en) 2018-11-06
EP2896954B1 (en) 2021-04-14
KR102201552B1 (ko) 2021-01-12

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Granted publication date: 20181211