BR0108601A - Componente laminado pré-curado, conjunto de junta ligada e método de reforçar um componente laminado pré-curado na região de uma ligação adesiva - Google Patents
Componente laminado pré-curado, conjunto de junta ligada e método de reforçar um componente laminado pré-curado na região de uma ligação adesivaInfo
- Publication number
- BR0108601A BR0108601A BR0108601-4A BR0108601A BR0108601A BR 0108601 A BR0108601 A BR 0108601A BR 0108601 A BR0108601 A BR 0108601A BR 0108601 A BR0108601 A BR 0108601A
- Authority
- BR
- Brazil
- Prior art keywords
- laminated component
- cured laminated
- region
- reinforcing
- bonded joint
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
- B29C65/564—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined hidden in the joint, e.g. dowels or Z-pins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
- B29C66/434—Joining substantially flat articles for forming corner connections, fork connections or cross connections
- B29C66/4344—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces
- B29C66/43441—Joining substantially flat articles for forming fork connections, e.g. for making Y-shaped pieces with two right angles, e.g. for making T-shaped pieces, H-shaped pieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/124—Tongue and groove joints
- B29C66/1244—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue
- B29C66/12441—Tongue and groove joints characterised by the male part, i.e. the part comprising the tongue being a single wall
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/721—Fibre-reinforced materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
- Moulding By Coating Moulds (AREA)
- Connection Of Plates (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
"COMPONENTE LAMINADO PRé-CURADO, CONJUNTO DE JUNTA LIGADA E MéTODO DE REFORçAR UM COMPONENTE LAMINADO PRé-CURADO NA REGIãO DE UMA LIGAçãO ADESIVA". Uma junta ligada (40) compreende primeiro e segundo elementos laminados pré-curados (42, 44) tendo faces de junção opostas (48, 50) e uma camada de adesivo (52) intercalada. Uma pluralidade de pinos (466) se estende através de cada elemento laminado (42, 44) e para o interior da camada adesiva (52). Os pinos (46) reforçam os elementos laminados (42, 44) e aumentam sua resistência à deslaminação na região da junta (40) devido a cargas indutoras de tensão. Os pinos (46) podem ser providos niveladamente com a face de junção (48, 50).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0004148.3A GB0004148D0 (en) | 2000-02-23 | 2000-02-23 | Reinforced joint |
PCT/GB2001/000529 WO2001062474A1 (en) | 2000-02-23 | 2001-02-09 | Reinforced joint |
Publications (2)
Publication Number | Publication Date |
---|---|
BR0108601A true BR0108601A (pt) | 2002-11-12 |
BR0108601B1 BR0108601B1 (pt) | 2009-08-11 |
Family
ID=9886160
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0108601-4A BR0108601B1 (pt) | 2000-02-23 | 2001-02-09 | componente laminado pré-curado, conjunto de junta ligada e método de reforçar um componente laminado pré-curado na região de uma ligação adesiva. |
Country Status (9)
Country | Link |
---|---|
US (1) | US20030012922A1 (pt) |
EP (1) | EP1259369B1 (pt) |
AT (1) | ATE257076T1 (pt) |
AU (1) | AU2001233842A1 (pt) |
BR (1) | BR0108601B1 (pt) |
DE (1) | DE60101675T2 (pt) |
ES (1) | ES2210126T3 (pt) |
GB (1) | GB0004148D0 (pt) |
WO (1) | WO2001062474A1 (pt) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040023581A1 (en) * | 2002-08-05 | 2004-02-05 | Bersuch Larry R. | Z-pin closeout joint and method of assembly |
US7712993B2 (en) | 2007-11-30 | 2010-05-11 | The Boeing Company | Double shear joint for bonding in structural applications |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE69431909T2 (de) * | 1993-04-30 | 2003-11-06 | Foster-Miller, Inc. | Ein verstärktes verbindungselement von verbundstrukturen und verfahren zum verbinden von verbundteilen |
US5980665A (en) * | 1996-05-31 | 1999-11-09 | The Boeing Company | Z-pin reinforced bonds for connecting composite structures |
US5879492A (en) * | 1998-04-17 | 1999-03-09 | Northrop Grumman Corporation | Z-peel sheets |
-
2000
- 2000-02-23 GB GBGB0004148.3A patent/GB0004148D0/en not_active Ceased
-
2001
- 2001-02-09 AU AU2001233842A patent/AU2001233842A1/en not_active Abandoned
- 2001-02-09 AT AT01905870T patent/ATE257076T1/de not_active IP Right Cessation
- 2001-02-09 ES ES01905870T patent/ES2210126T3/es not_active Expired - Lifetime
- 2001-02-09 US US10/203,210 patent/US20030012922A1/en not_active Abandoned
- 2001-02-09 BR BRPI0108601-4A patent/BR0108601B1/pt not_active IP Right Cessation
- 2001-02-09 WO PCT/GB2001/000529 patent/WO2001062474A1/en active IP Right Grant
- 2001-02-09 EP EP01905870A patent/EP1259369B1/en not_active Expired - Lifetime
- 2001-02-09 DE DE60101675T patent/DE60101675T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
ES2210126T3 (es) | 2004-07-01 |
BR0108601B1 (pt) | 2009-08-11 |
ATE257076T1 (de) | 2004-01-15 |
GB0004148D0 (en) | 2000-04-12 |
EP1259369B1 (en) | 2004-01-02 |
AU2001233842A1 (en) | 2001-09-03 |
DE60101675D1 (de) | 2004-02-05 |
DE60101675T2 (de) | 2004-07-29 |
US20030012922A1 (en) | 2003-01-16 |
WO2001062474A1 (en) | 2001-08-30 |
EP1259369A1 (en) | 2002-11-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2491203C2 (ru) | Усиленная панель из композиционного материала, содержащая стрингер и первую и вторую стенки, обшивка воздушного судна и способ изготовления усиленной панели из композиционного материала | |
Roberts et al. | THEORETICAL STUDY OF THE BEHAVIOUR OF REINFORCED CONCRETE BEAMS STRENG-THENED BY EXTERNALLY BONDED STEEL PLATES. | |
Hart-Smith | Design of adhesively bonded joints | |
BR9812823A (pt) | Laminado que compreende duas camadas unidas entre si em relação de face com face | |
EP2778309A1 (en) | Method of forming adhesive connections | |
DE60127411D1 (de) | Selbstklebende prepregaussenfolie für sandwichplatten | |
WO2007001365A3 (en) | Splice joints for composite aircraft fuselages and other structures | |
WO1998010919A3 (en) | Laminates | |
BRPI0613658A2 (pt) | método para conectar pelo menos duas formações semelhantes à folha, especificamente pelo menos duas folhas de metal para uma estrutura leve, assim como conexão e estrutura leve | |
JP5784747B2 (ja) | 積層ストリンガー組立部品の層間剥離のリスクを軽減するためのスキュー角半径充填材 | |
JPH1037483A (ja) | 木材の補強方法 | |
SE0200210D0 (sv) | Process for sealing a joint | |
BR0108601A (pt) | Componente laminado pré-curado, conjunto de junta ligada e método de reforçar um componente laminado pré-curado na região de uma ligação adesiva | |
ATE239156T1 (de) | Verbindung zwischen fügeflächen von zwei paneelen eines fussbodenbelages | |
JP3958450B2 (ja) | 木材の接続構造 | |
ATE387310T1 (de) | Aufbringen von glas auf zu verbindende oberflächen von zusammengesetzten materialien | |
EP1127678A1 (en) | Reinforced joint | |
DE60113971D1 (de) | Verwendung von xylan zur verbesserung der haftfestigkeit | |
SU797949A1 (ru) | Стыковое формованное соединениеСТЕКлОплАСТиКОВ | |
Matous et al. | Prestress of adhesively bonded skin/flange assemblies. | |
Xiang et al. | New Method to Study The Effect of Stacking Sequence on Composite Single-Lap Joint Strength | |
KR100717719B1 (ko) | 복합재료의 접합조인트 | |
Klug | Stress Variation in High Strength Film Adhesive Bondlines for Flush Scarf Bonded Joints | |
ATE336364T1 (de) | Flächiges verbundmaterial | |
JPH0622756Y2 (ja) | 床材の構造 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25A | Requested transfer of rights approved |
Owner name: AIRBUS UK LIMITED (GB) Free format text: TRANSFERIDO DE: BAE SYSTEMS PLC |
|
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 09/02/2001, OBSERVADAS AS CONDICOES LEGAIS. |
|
B25D | Requested change of name of applicant approved |
Owner name: AIRBUS OPERATIONS LIMITED (GB) Free format text: NOME ALTERADO DE: AIRBUS UK LIMITED |
|
B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time |
Free format text: REFERENTE A 16A ANUIDADE. |
|
B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |