CA2328573A1 - Jonction composite pour le montage d'au moins un organe exterieur sur un panneau sandwich, et panneau integrant au moins une telle jonction - Google Patents
Jonction composite pour le montage d'au moins un organe exterieur sur un panneau sandwich, et panneau integrant au moins une telle jonction Download PDFInfo
- Publication number
- CA2328573A1 CA2328573A1 CA002328573A CA2328573A CA2328573A1 CA 2328573 A1 CA2328573 A1 CA 2328573A1 CA 002328573 A CA002328573 A CA 002328573A CA 2328573 A CA2328573 A CA 2328573A CA 2328573 A1 CA2328573 A1 CA 2328573A1
- Authority
- CA
- Canada
- Prior art keywords
- junction
- panel
- cells
- composite
- sandwich panel
- 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
- 239000002131 composite material Substances 0.000 title abstract 3
- 230000001413 cellular effect Effects 0.000 abstract 1
- 239000000835 fiber Substances 0.000 abstract 1
- 239000011347 resin Substances 0.000 abstract 1
- 229920005989 resin Polymers 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
Abstract
Jonction composite pour le montage d'au moins un organe extérieur sur un panneau sandwich, et panneau intégrant au moins une telle jonction. Pour permettre la transmission des efforts statiques et/ou dynamiques entre au moins un organe extérieur et un panneau sandwich, on intègre dans ce panneau au moins une jonction composite (10). Cette jonction comprend une pluralité de cellules tubulaires élémentaires (12) juxtaposées, orientées dans le sens de l'épaisseur du panneau, ainsi qu'au moins une cellule d'introduction d'efforts (12a), dans laquelle est montée une pièce rigide (14) destinée à la fixation de l'organe extérieur. Les cellules tubulaires (12) comprennent des parois composites, formées de mèches de fibres tressées et de résine.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE9900817A BE1013181A5 (fr) | 1999-12-17 | 1999-12-17 | Jonction composite pour le montage d'au moins un organe exterieur sur un panneau sandwich, et panneau integrant au moins une telle jonction. |
BE09900817 | 1999-12-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2328573A1 true CA2328573A1 (fr) | 2001-06-17 |
CA2328573C CA2328573C (fr) | 2008-07-29 |
Family
ID=3892202
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002328573A Expired - Fee Related CA2328573C (fr) | 1999-12-17 | 2000-12-14 | Jonction composite pour le montage d'au moins un organe exterieur sur un panneau sandwich, et panneau integrant au moins une telle jonction |
Country Status (7)
Country | Link |
---|---|
US (1) | US6668515B2 (fr) |
EP (1) | EP1108896B1 (fr) |
AT (1) | ATE261551T1 (fr) |
BE (1) | BE1013181A5 (fr) |
CA (1) | CA2328573C (fr) |
DE (1) | DE60008841T2 (fr) |
ES (1) | ES2215591T3 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7291373B2 (en) * | 2005-05-05 | 2007-11-06 | Northrop Grumman Corporation | Thermally insulated structure—full depth sandwich joint concept |
US20080276557A1 (en) * | 2007-05-09 | 2008-11-13 | Antonio Rapaz | Construction panel |
US8464490B2 (en) * | 2007-05-09 | 2013-06-18 | Antonio Rapaz | Construction panel |
US9010060B2 (en) | 2007-05-09 | 2015-04-21 | Antonio Rapaz | Construction panel |
US8136328B2 (en) * | 2008-05-28 | 2012-03-20 | The Boeing Company | Fastener receptacle for a panel |
CA2786737C (fr) | 2010-02-04 | 2016-04-19 | Bell Helicopter Textron Inc. | Noyau composite et procede de fabrication associe |
EP2960567B1 (fr) * | 2013-02-20 | 2019-09-25 | Toray Industries, Inc. | Structure de renfort pour corps structurel ayant des sections de fixation |
FR3003233B1 (fr) * | 2013-03-18 | 2016-05-06 | Airbus Operations Sas | Panneau de voilure pour aeronef |
US9981446B2 (en) * | 2013-09-03 | 2018-05-29 | The Boeing Company | Structural inserts for honeycomb structures |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1132264A (fr) | 1955-09-24 | 1957-03-07 | Citroen Sa Andre | Dispositif de transmission amortisseur de vibrations |
GB876106A (en) | 1959-11-11 | 1961-08-30 | Frederick William Rohe | An improved nut fastener for use with sandwich-type panels |
US3579942A (en) * | 1969-12-05 | 1971-05-25 | Thomas & Betts Corp | Fastener anchored in honeycomb panel |
US3742663A (en) * | 1971-08-02 | 1973-07-03 | Mc Donnell Douglas Corp | Panel blocking |
US3977146A (en) * | 1974-12-18 | 1976-08-31 | Standard Pressed Steel Co. | Fastener bushing |
DE2911058C3 (de) | 1979-03-21 | 1981-11-05 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Einbauelement für Schichtverbundplatten |
GB8627819D0 (en) * | 1986-11-20 | 1986-12-17 | Dunlop Ltd | Panels |
US4845915A (en) * | 1988-06-27 | 1989-07-11 | Stageright Corporation | High impact panel corner |
US5116689A (en) * | 1988-11-07 | 1992-05-26 | Rohr Industries, Inc. | Apparatus and method for selectively increasing density and thermal conductivity of honeycomb structures |
US5240543A (en) | 1990-06-11 | 1993-08-31 | Atr International, Inc. | Apparatus for and method of seating a fastener insert in a honeycomb panel |
US5378099A (en) | 1993-07-01 | 1995-01-03 | Gauron; Richard F. | Inset panel fastener with shoulder-engaging floating member |
US6165588A (en) * | 1998-09-02 | 2000-12-26 | Henkel Corporation | Reinforcement of hollow sections using extrusions and a polymer binding layer |
WO1997026958A1 (fr) * | 1996-01-22 | 1997-07-31 | Ride Manufacturing, Inc. | Systeme d'ancrage de fixation |
-
1999
- 1999-12-17 BE BE9900817A patent/BE1013181A5/fr not_active IP Right Cessation
-
2000
- 2000-12-14 EP EP00403524A patent/EP1108896B1/fr not_active Expired - Lifetime
- 2000-12-14 AT AT00403524T patent/ATE261551T1/de not_active IP Right Cessation
- 2000-12-14 DE DE60008841T patent/DE60008841T2/de not_active Expired - Lifetime
- 2000-12-14 ES ES00403524T patent/ES2215591T3/es not_active Expired - Lifetime
- 2000-12-14 CA CA002328573A patent/CA2328573C/fr not_active Expired - Fee Related
- 2000-12-15 US US09/738,476 patent/US6668515B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1108896A1 (fr) | 2001-06-20 |
US20010003888A1 (en) | 2001-06-21 |
EP1108896B1 (fr) | 2004-03-10 |
DE60008841D1 (de) | 2004-04-15 |
BE1013181A5 (fr) | 2001-10-02 |
DE60008841T2 (de) | 2005-02-10 |
ES2215591T3 (es) | 2004-10-16 |
CA2328573C (fr) | 2008-07-29 |
US6668515B2 (en) | 2003-12-30 |
ATE261551T1 (de) | 2004-03-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20191216 |