WO2006096647A3 - Procede destine a fabriquer un cadran de numerotation - Google Patents
Procede destine a fabriquer un cadran de numerotation Download PDFInfo
- Publication number
- WO2006096647A3 WO2006096647A3 PCT/US2006/007930 US2006007930W WO2006096647A3 WO 2006096647 A3 WO2006096647 A3 WO 2006096647A3 US 2006007930 W US2006007930 W US 2006007930W WO 2006096647 A3 WO2006096647 A3 WO 2006096647A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- layout
- caul plate
- composite
- resin
- composite layout
- 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.)
- Ceased
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
- 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
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47B—TABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
- A47B96/00—Details of cabinets, racks or shelf units not covered by a single one of groups A47B43/00 - A47B95/00; General details of furniture
- A47B96/18—Tops specially designed for working on
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/36—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and impregnating by casting, e.g. vacuum casting
-
- 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
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/546—Measures for feeding or distributing the matrix material in the reinforcing structure
- B29C70/548—Measures for feeding or distributing the matrix material in the reinforcing structure using distribution constructions, e.g. channels incorporated in or associated with the mould
-
- 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
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
L'invention concerne un procédé destiné à fabriquer un cadran de numérotation. Une conception en mousse est placée entre un ensemble de base et un ensemble supérieur afin de former une conception composite. L'ensemble de base comprend une première conception en fibre de carbone segmentée et l'ensemble supérieur comprend un seconde conception en fibre de carbone segmentée. Une plaque d'acier inoxydable est ensuite placée à proximité de la conception composite. La plaque d'acier inoxydable comprend plusieurs ouvertures. Un vide est ensuite généré à proximité de la conception composite. Une résine est étirée à travers les ouvertures au moyen du vide généré jusqu'à ce que la conception composite soit infusée de résine. La plaque d'acier inoxydable est retirée et la conception composite infusée de résine est cuite au four. Le cadran de numérotation est ainsi fabriqué.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US65926205P | 2005-03-07 | 2005-03-07 | |
| US60/659,262 | 2005-03-07 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2006096647A2 WO2006096647A2 (fr) | 2006-09-14 |
| WO2006096647A3 true WO2006096647A3 (fr) | 2009-04-09 |
Family
ID=36953934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/US2006/007930 Ceased WO2006096647A2 (fr) | 2005-03-07 | 2006-03-06 | Procede destine a fabriquer un cadran de numerotation |
Country Status (1)
| Country | Link |
|---|---|
| WO (1) | WO2006096647A2 (fr) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2949710B1 (fr) * | 2009-09-04 | 2011-11-25 | Lorraine Construction Aeronautique | Dispositif de moulage destine a recevoir des fibres et une resine par injection. |
| US8940213B2 (en) * | 2010-06-25 | 2015-01-27 | The Boeing Company | Resin infusion of composite parts using a perforated caul sheet |
| US9682514B2 (en) | 2010-06-25 | 2017-06-20 | The Boeing Company | Method of manufacturing resin infused composite parts using a perforated caul sheet |
| US8636252B2 (en) | 2010-06-25 | 2014-01-28 | The Boeing Company | Composite structures having integrated stiffeners with smooth runouts and method of making the same |
| US8628717B2 (en) | 2010-06-25 | 2014-01-14 | The Boeing Company | Composite structures having integrated stiffeners and method of making the same |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3484335A (en) * | 1965-07-19 | 1969-12-16 | Ppg Industries Inc | Laminated articles containing oxidatively cured non-rubbery interpolymers and method for making |
| US4090537A (en) * | 1977-02-16 | 1978-05-23 | Bollman Clifford J | Unitary, composite, multi-layer work area |
| US4279957A (en) * | 1978-08-31 | 1981-07-21 | Mitsui Petrochemical Industries, Ltd. | Laminated film or sheet structure and process for production thereof |
| US4526421A (en) * | 1982-09-30 | 1985-07-02 | Ptc Aerospace Inc. | Multi-passenger aircraft seat having composite panel frame |
| US6605343B1 (en) * | 1999-02-22 | 2003-08-12 | Sekisui Chemical Co., Ltd. | Composite material and synthetic sleeper using the composite material |
| US20040200392A1 (en) * | 2003-04-11 | 2004-10-14 | Sun Isle Inc. | Table top and process of making the same |
-
2006
- 2006-03-06 WO PCT/US2006/007930 patent/WO2006096647A2/fr not_active Ceased
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3484335A (en) * | 1965-07-19 | 1969-12-16 | Ppg Industries Inc | Laminated articles containing oxidatively cured non-rubbery interpolymers and method for making |
| US4090537A (en) * | 1977-02-16 | 1978-05-23 | Bollman Clifford J | Unitary, composite, multi-layer work area |
| US4279957A (en) * | 1978-08-31 | 1981-07-21 | Mitsui Petrochemical Industries, Ltd. | Laminated film or sheet structure and process for production thereof |
| US4526421A (en) * | 1982-09-30 | 1985-07-02 | Ptc Aerospace Inc. | Multi-passenger aircraft seat having composite panel frame |
| US6605343B1 (en) * | 1999-02-22 | 2003-08-12 | Sekisui Chemical Co., Ltd. | Composite material and synthetic sleeper using the composite material |
| US20040200392A1 (en) * | 2003-04-11 | 2004-10-14 | Sun Isle Inc. | Table top and process of making the same |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2006096647A2 (fr) | 2006-09-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
| NENP | Non-entry into the national phase |
Ref country code: DE |
|
| NENP | Non-entry into the national phase |
Ref country code: RU |
|
| 32PN | Ep: public notification in the ep bulletin as address of the adressee cannot be established |
Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1)EPC DATED 04-03-2008 |
|
| 122 | Ep: pct application non-entry in european phase |
Ref document number: 06737145 Country of ref document: EP Kind code of ref document: A2 |