FR2836982A1 - Equipment vacuum-forming sealed, composite, fiber-reinforced, tubular supporting structures, employs tubing of crenellated or spiral form - Google Patents
Equipment vacuum-forming sealed, composite, fiber-reinforced, tubular supporting structures, employs tubing of crenellated or spiral form Download PDFInfo
- Publication number
- FR2836982A1 FR2836982A1 FR0202842A FR0202842A FR2836982A1 FR 2836982 A1 FR2836982 A1 FR 2836982A1 FR 0202842 A FR0202842 A FR 0202842A FR 0202842 A FR0202842 A FR 0202842A FR 2836982 A1 FR2836982 A1 FR 2836982A1
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- FR
- France
- Prior art keywords
- crenellated
- tubing
- fiber
- equipment
- version
- 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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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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/542—Placing or positioning the reinforcement in a covering or packaging element before or during moulding, e.g. drawing in a sleeve
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Description
<Desc/Clms Page number 1> <Desc / Clms Page number 1>
La présente invention concerne un dispositif de construction de structures tubulaires porteuses en composites armées, sous vide et sans moule rigide. The present invention relates to a device for constructing load-bearing tubular structures in reinforced composites, under vacuum and without rigid mold.
Le dispositif selon l'invention repose sur l'utilisation de gaines ou de tuyaux plastiques à spirales ou à crénelages, pour leurs caractéristiques mécaniques spécifiques. Utilisés plus particulièrement, dans l'électricité du bâtiment ou dans les travaux public à l'enterrement de conduites, pour un rôle de prétubage de cablage ou de tunel pour des tuyauteries, elles ont pouravantage de résister à l'écrasement par des charges extérieures et au niveau des courbes de conserver leur section. The device according to the invention is based on the use of plastic sheaths or pipes with spirals or notches, for their specific mechanical characteristics. Used more particularly, in building electricity or in public works for the burial of pipes, for a role of pre-tubing of cabling or tunel for pipes, they have the advantage of resisting crushing by external loads and at the curves to keep their section.
Le dispositif rend possible leur utilisation, dans la fabrication de structures tubulaires porteuses, en résines composites statifiées ou matières plastiques armées, sans moule rigide et permet son emploi, dans des formes à rayon écliptique, curvilignes concaves ou convexes, multidimentionnelles et directionnelles. Le dispositif est particulièrement destiné à concevoir des structures porteuses de formes complexes, précontraintes et courbées pour l'architecture, le design, l'ameublement ou l'habitat. The device makes it possible to use them, in the manufacture of load-bearing tubular structures, in statified composite resins or reinforced plastics, without rigid mold and allows its use, in shapes with an ecliptic radius, curved concave or convex, multidimensional and directional. The device is particularly intended to design load-bearing structures of complex shapes, prestressed and curved for architecture, design, furniture or housing.
Les dessins annexés illustrent l'invention. The accompanying drawings illustrate the invention.
La figure 1 représente en coupe le dispositif selon l'invention. Figure 1 shows in section the device according to the invention.
La figure 2 représente en coupe le dispositif dans le positionnement des divers éléments le constituant. Figure 2 shows in section the device in the positioning of the various elements constituting it.
En référence à ces dessins, le dispositif sur la base d'une gaine (1) spiralée ou crènelée, de forme géométrique variable ronde, carré, rectangulaire, ovale ou de toutes autres compatibles sans limites, est remplis d'éléments filamentaires (2) de résistance élevée. Sous une forme préférentielle du type fibre de verre, fil de carbone ou de kévlar. elles sont tirées à l'aide d'un fil (3) de fer ou autre, souvant
Inclus dans les produits commercialisés pour une fonction identique. Le dispositif est équipé pour introduire les fibres et fils de résistance (2) à sec avant ou après la mise en forme désirée, d'un répartiteur (9) dans le cas d'une structure pleine et d'un centreur (8) pour une section centrale vide. Ces éléments de répartition (8) et (9) sont indispensables au dispositif, pour une non ségrégation entre les résines et les éléments filamentaires utilisés, spécialement dans les courbes, les enroulements ou pendant la mise en forme. L'élément (8) à aussi la fonction de centreur du tube (7) With reference to these drawings, the device on the basis of a spiral or crenellated sheath, of variable geometric shape, round, square, rectangular, oval or any other compatible without limits, is filled with filamentary elements (2) high strength. In a preferred form of the glass fiber, carbon or kevlar yarn type. they are drawn using a wire (3) of iron or other, often
Included in products marketed for an identical function. The device is equipped to introduce the fibers and resistance wires (2) dry before or after the desired shaping, a distributor (9) in the case of a solid structure and a centralizer (8) for an empty center section. These distribution elements (8) and (9) are essential to the device, for non-segregation between the resins and the filamentary elements used, especially in curves, windings or during shaping. The element (8) also has the function of centering the tube (7)
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sur des grandes longueurs dans une version à centre vide La phase suivante consiste à boucher la gaine (1) ou la chambre formée par l'intervalle entre la gaine intérieure (7) et (1) extérieure au niveau de ses extrémités opposées à l'aide d'un bouchon (4) avec un mastic étanche. Des raccords (6) installés sur les extrémités ou par internes régulières, sur la paroie du tube (1) suivant la distance entre la zone d'injection et celle de fluage, permettent de réaliser le vide inteme et le remplissage du tubage par les résines (5). Cette disposition des raccords (6) dépend aussi de la valeur du vide réalisé, de la longueurs et formes des sections, en rapport avec la viscosité des résines et colles utilisées. Une fois la stratification et le durcissement du composite réalisé, ces extrémités (4) ou les longueurs de sections désirées sont coupées, pour être raccordées par des unions (10) simples ou à plusieurs jonctions et à divers degrés d'orientation. Une enveloppe (11) thermo. rétractable de recouvrement de finition peut être installée, avant la mise en oeuvre du dispositif sur la gaine (1). over long lengths in a version with empty center The next phase consists in sealing the sheath (1) or the chamber formed by the gap between the inner sheath (7) and (1) outside at its ends opposite to the using a plug (4) with a waterproof sealant. Fittings (6) installed on the ends or by regular internals, on the wall of the tube (1) according to the distance between the injection zone and that of creep, allow to realize the internal vacuum and the filling of the casing with resins (5). This arrangement of the fittings (6) also depends on the value of the vacuum produced, on the lengths and shapes of the sections, in relation to the viscosity of the resins and adhesives used. Once the composite has been laminated and hardened, these ends (4) or the desired lengths of sections are cut, to be connected by simple unions (10) or with several junctions and at various degrees of orientation. A thermo envelope (11). retractable cover can be installed before the implementation of the device on the sheath (1).
Le dispositif et particulièrement destiné à la conception de structures porteuses sous vide, sans moules pour des formes complexes ou à fort rayon de courbures The device and particularly intended for the design of load-bearing structures under vacuum, without molds for complex shapes or with a large radius of curvature
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0202842A FR2836982A1 (en) | 2002-03-06 | 2002-03-06 | Equipment vacuum-forming sealed, composite, fiber-reinforced, tubular supporting structures, employs tubing of crenellated or spiral form |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0202842A FR2836982A1 (en) | 2002-03-06 | 2002-03-06 | Equipment vacuum-forming sealed, composite, fiber-reinforced, tubular supporting structures, employs tubing of crenellated or spiral form |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2836982A1 true FR2836982A1 (en) | 2003-09-12 |
Family
ID=27763590
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0202842A Pending FR2836982A1 (en) | 2002-03-06 | 2002-03-06 | Equipment vacuum-forming sealed, composite, fiber-reinforced, tubular supporting structures, employs tubing of crenellated or spiral form |
Country Status (1)
Country | Link |
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FR (1) | FR2836982A1 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2082872A5 (en) * | 1970-03-31 | 1971-12-10 | Pigeon Daniel | Prefabricated frames - of glass fibre reinforced plastics |
US5405668A (en) * | 1987-12-28 | 1995-04-11 | Sandt; Hartley | Composite structural element |
DE4418809A1 (en) * | 1994-05-30 | 1995-12-07 | Gert Prof Stolz | Light-weight deformable structure mfr. for e.g cycle frames and scaffolding |
DE19512525C1 (en) * | 1995-04-06 | 1996-04-11 | Dornier Gmbh | Lightweight tubular component or hollow section with outer or inner sleeve |
-
2002
- 2002-03-06 FR FR0202842A patent/FR2836982A1/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2082872A5 (en) * | 1970-03-31 | 1971-12-10 | Pigeon Daniel | Prefabricated frames - of glass fibre reinforced plastics |
US5405668A (en) * | 1987-12-28 | 1995-04-11 | Sandt; Hartley | Composite structural element |
DE4418809A1 (en) * | 1994-05-30 | 1995-12-07 | Gert Prof Stolz | Light-weight deformable structure mfr. for e.g cycle frames and scaffolding |
DE19512525C1 (en) * | 1995-04-06 | 1996-04-11 | Dornier Gmbh | Lightweight tubular component or hollow section with outer or inner sleeve |
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