FR2616198A1 - System for assembling a metal end-fitting and a high-pressure composite material tube and applications particularly to equipment in the petrochemical field - Google Patents
System for assembling a metal end-fitting and a high-pressure composite material tube and applications particularly to equipment in the petrochemical field Download PDFInfo
- Publication number
- FR2616198A1 FR2616198A1 FR8707722A FR8707722A FR2616198A1 FR 2616198 A1 FR2616198 A1 FR 2616198A1 FR 8707722 A FR8707722 A FR 8707722A FR 8707722 A FR8707722 A FR 8707722A FR 2616198 A1 FR2616198 A1 FR 2616198A1
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- FR
- France
- Prior art keywords
- composite material
- tube
- high pressure
- composite
- metal
- 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
-
- 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
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L47/00—Connecting arrangements or other fittings specially adapted to be made of plastics or to be used with pipes made of plastics
- F16L47/20—Connecting arrangements or other fittings specially adapted to be made of plastics or to be used with pipes made of plastics based principally on specific properties of plastics
- F16L47/24—Connecting arrangements or other fittings specially adapted to be made of plastics or to be used with pipes made of plastics based principally on specific properties of plastics for joints between metal and plastics pipes
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N9/00—Investigating density or specific gravity of materials; Analysing materials by determining density or specific gravity
- G01N9/24—Investigating density or specific gravity of materials; Analysing materials by determining density or specific gravity by observing the transmission of wave or particle radiation through the material
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Health & Medical Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Health & Medical Sciences (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
Abstract
Description
La présente invention se rapporte à un système d'assemblage matériau composite/métal permettant d'utiliser les matériaux composites dans le transport de fluides corrosifs et/ou abrasifs sous des pressions statiques pouvant atteindre 150 MPa.The present invention relates to a composite material / metal assembly system making it possible to use the composite materials in the transport of corrosive and / or abrasive fluids under static pressures up to 150 MPa.
L'invention permet notamment d'intercaler entre les conduits métalliques, ou circule un fluide sous très haute pression, un élément de tube composite qui peut notamment faire partie d'un capteur destiné à mesurer diverses propriétés du fluide (viscosité, débit, densité, etc...)
Un des problèmes connus de l'art antérieur consiste en la difficulté de réaliser des raccords matériau composite/métal capables de résister durant une longue période à de très hautes pressions. L'invention résoud ce problème.The invention makes it possible in particular to interpose between the metal conduits, or a fluid circulating under very high pressure, a composite tube element which can in particular form part of a sensor intended to measure various properties of the fluid (viscosity, flow rate, density, etc ...)
One of the known problems of the prior art consists in the difficulty of producing composite material / metal connections capable of withstanding very high pressures for a long time. The invention solves this problem.
Une application particulièrement importante réside dans l'application aux capteurs de l'industrie pétrolière et parapétrolière qui doivent mesurer comme on le sait des propriétés (viscosité, densité, paramètres rhéologiques, etc...) de fluides circulant sous de très hautes pressions, et qui peuvent être corrosifs (acides) et/ou fortement abrasifs (laitiers de ciment). A particularly important application lies in the application to sensors of the petroleum and parapetroleum industry which must measure, as we know, the properties (viscosity, density, rheological parameters, etc.) of fluids circulating under very high pressures, and which can be corrosive (acids) and / or highly abrasive (cement slag).
Selon l'invention, on dispose entre le matériau composite et le tube métallique un embout métallique comportant un épaulement en saillie à son extrémité en contact avec le matériau composite et un raccord haute pression à son autre extrémité.According to the invention, there is between the composite material and the metal tube a metal end piece comprising a projecting shoulder at its end in contact with the composite material and a high pressure connection at its other end.
Les figures 1 et 2 annexées représentent un mode de réalisation préféré de l'invention, non limitatif, en vue en coupe longituginale dans un plan parallèle à l'axe de conduit.Figures 1 and 2 attached show a preferred embodiment of the invention, without limitation, in longitudinal section view in a plane parallel to the axis of conduit.
L'une des caractéristiques essentielles de l'invention réside dans l'épaulement en saillie 2 autour duquel sont déposés par bobinage, de manière connue, les différents plis de matériau composite.One of the essential characteristics of the invention resides in the projecting shoulder 2 around which the various plies of composite material are deposited by winding, in known manner.
L'avantage de cette structure est de permettre un bobinage normal du matériau composite tout en assurant pour la première fois dans l'industrie la tenue aux contraintes de traction et de torsion entre le tube métallique (et l'embout métallique) d'une part, et le tube composite d'autre part.The advantage of this structure is that it allows normal winding of the composite material while ensuring, for the first time in the industry, the resistance to tensile and torsional stresses between the metal tube (and the metal end piece) on the one hand. , and the composite tube on the other hand.
On élimine ainsi les risques de déformation, fuites et ruptures qui sont courants dans les tentatives de l'art antérieur.This eliminates the risks of deformation, leaks and ruptures which are common in attempts in the prior art.
Etant données les pressions de travail, on voit que cet avantage est tout à fait déterminant. Given the work pressures, we see that this advantage is absolutely decisive.
Dans l'industrie pétrolière et parapétrolière, les inconvénients de l'art antérieur ont des conséquences encore plus graves (toute interruption du travail sur une ligne entraine un risque grave mauvais traitement du puits, mauvais placement du ciment, avec des conséquences quelquefois irrémédiables).In the petroleum and parapetroleum industry, the drawbacks of the prior art have even more serious consequences (any interruption of work on a line entails a serious risk of poor treatment of the well, poor placement of cement, with sometimes irreversible consequences).
Les références ont la signification suivante 1 . Matériau composite bobiné 2 . Epaulement sur embout métallique 3 . Embout métallique 4 . Fibres circonférentielles de matériau composite 5 . Fibres longituginales du matériau composite
P . Pression exercée par le fluide pompé à l'intérieur du
conduit.References have the following meaning 1. Wound composite material 2. Shoulder on metal tip 3. Metal tip 4. Circumferential fibers of composite material 5. Longitugin fibers of the composite material
P. Pressure exerted by the pumped fluid inside the
drove.
S . Section du conduit
F . Efforts de tension longitudinaux dus à la pression
R . Rayon sur épaulement AH. Angles des plans inclinés sur épaulement 6 . Manchon anti-abrasion/anti-corrosion 7 . Système d'assemblage type Weco avec un tube métallique
haute pression non représenté 8 . Joint haute pression 9 . Bague de protection 10. Joints toriques
La figure 3 représente une réalisation d'un capteur (11) de mesure de propriétés du fluide, mesures faites à travers le matériau composite constitutif du conduit (1).S. Duct section
F. Longitudinal tension forces due to pressure
R. Radius on shoulder AH. Angles of the inclined planes on the shoulder 6. Anti-abrasion / anti-corrosion sleeve 7. Weco type assembly system with a metal tube
high pressure not shown 8. High pressure seal 9. Protection ring 10. O-rings
FIG. 3 represents an embodiment of a sensor (11) for measuring properties of the fluid, measurements made through the composite material constituting the conduit (1).
La figure 4 représente un tube très haute pression en matériau composite, raccordable aux deux bouts, grâce à l'application de l'invention.FIG. 4 represents a very high pressure tube made of composite material, connectable at both ends, thanks to the application of the invention.
La figure 1 illustre de facon détaillée le principe de fonctionnement de l'invention.Figure 1 illustrates in detail the operating principle of the invention.
Lorsqu'unie pression importante P est appliquée à l'intérieur du conduit, elle crée une forte tension F =PxS au sein du matériau constitutif du conduit. When a high pressure P is applied inside the pipe, it creates a high tension F = PxS within the material of the pipe.
Les fibres longitudinales (5) du matériau composite reprennent en partie cet effort. Dans la zone de raccordement entre le tube en composite et l'embout métallique 3, les efforts de cisaillement à l'interface entre les deux matériaux atteignent des valeurs telles qu'aucune colle ne peut suffir à maintenir l'ensemble.The longitudinal fibers (5) of the composite material partially take up this force. In the connection zone between the composite tube and the metal end piece 3, the shear forces at the interface between the two materials reach values such that no adhesive can be sufficient to hold the assembly together.
C'est à ce point que les réalisations de l'art antérieur sont fragiles. Dans la présente invention le tube en matériau composite est bobiné autour d'un épaulement (2) en saillie sur l'embout métallique. It is at this point that the achievements of the prior art are fragile. In the present invention, the tube made of composite material is wound around a shoulder (2) projecting from the metal end piece.
Lorsque l'on exerce un effort de traction sur le tube, tout glissement doit se traduire par une augmentation du diamètre d'une partie des spires de la couche de fibres circonférentielles (4) du matériau composite.When a tensile force is exerted on the tube, any slippage must result in an increase in the diameter of part of the turns of the layer of circumferential fibers (4) of the composite material.
Or ces fibres sont constituées de matériau à module d'Young très élevé, c'est notamment le cas pour les fibres de verre, de carbone ou d'aramide. Il est par conséquent très difficile, voire impossible de faire glisser l'assemblage, que ce soit en traction ou en compression grâce à la forme de l'épaulement 2 qui présente deux plans inclinés aux angles A, B.However, these fibers are made of material with a very high Young's modulus, this is particularly the case for glass, carbon or aramid fibers. It is therefore very difficult, if not impossible, to slide the assembly, either in tension or in compression, thanks to the shape of the shoulder 2 which has two planes inclined at the angles A, B.
Pour éviter de casser par amorce de rupture les fibres longitudinales on prendra la précaution de définir des rayons R bien choisis au niveau de l'épaulement.To avoid breaking the longitudinal fibers by breaking off, we will take the precaution of defining well-chosen radii R at the shoulder.
En définitive, la forme de l'épaulement peut etre choisie de diverses manières mais comportera de préférence un profil tel que les changements de diamètres ne soient pas trop "brutaux".Ultimately, the shape of the shoulder can be chosen in various ways but will preferably include a profile such that the diameter changes are not too "abrupt".
Dans un autre mode de bobinage préféré, les fibres du matériau composite seront bobinées selon deux spirales symétriques (l'une gauche, l'autre droite) dont l'angle des fibres par rapport à l'axe du conduit sera de l'ordre de 50 à 600. On sait en effet qu'un tuyau constitué de fibres bobinées en spirales a un angle de Arctg(2) env. 54,730 est virtuellement inexpansible sous l'effet des forces de pression. In another preferred winding mode, the fibers of the composite material will be wound in two symmetrical spirals (one left, the other right), the angle of the fibers relative to the axis of the conduit will be of the order of 50 to 600. We know that a pipe made of fibers wound in a spiral has an angle of Arctg (2) approx. 54,730 is virtually inexpansible under the effect of pressure forces.
On peut enfin, envisager la réalisation de l'invention avec une combinaison de plus de 2 couches de fibres avec des orientations choisies parmi les exemples cités.Finally, it is possible to envisage carrying out the invention with a combination of more than 2 layers of fibers with orientations chosen from the examples cited.
La figure 2 précise la réalisation de l'invention. Un manchon 6 en matériau résistant aux fluides pompés (corrosifs ou abrasifs), pouvant être notamment du polyuréthane ou du polytétrafluoroéthylène, a pour fonction de protéger le matériau composite contre l'attaque chimique. On sait en effet que les résines liant les fibres de renfort du matériau peuvent etre dissoutes par certains fluides, par ailleurs les fibres de verre sont attaquées par l'acide fluorhydrique.Figure 2 specifies the embodiment of the invention. A sleeve 6 made of a material resistant to pumped fluids (corrosive or abrasive), which can in particular be polyurethane or polytetrafluoroethylene, has the function of protecting the composite material against chemical attack. It is known in fact that the resins binding the reinforcing fibers of the material can be dissolved by certain fluids, moreover the glass fibers are attacked by hydrofluoric acid.
Le manchon 6 peut être mis à profit pour faciliter la fabrication du tube. En effet il peut etre utilisé pour servir de guide, au bobinage du matériau composite par dessus l'embout métallique 2. The sleeve 6 can be used to facilitate the manufacture of the tube. In fact, it can be used as a guide for winding the composite material over the metal end piece 2.
La pièce métallique 9 associée au joint 8 permettent de protéger l'extrémité du manchon 6 contre l'abrasion. Les joints toriques 10 assurent une étanchéité totale et évitent ainsi la pénétration sous l'effet de la pression des fluides agressifs entre la pièce 9 et le manchon 6.The metal part 9 associated with the joint 8 makes it possible to protect the end of the sleeve 6 against abrasion. The O-rings 10 ensure total sealing and thus prevent penetration under the effect of the pressure of aggressive fluids between the part 9 and the sleeve 6.
Dans cet exemple, on a fait figurer l'extrémité 7 d'une connexion haute pression type Ueco femelle. Le système d'assemblage WECO est bien connu, notamment dans l'industrie pétrolière et parapétrolière. On pourra cependant le remplacer par tout autre système connu de l'homme du métier capable de résister aux très hautes pressions mentionnées ici.In this example, the end 7 of a high pressure female Ueco type connection has been shown. The WECO assembly system is well known, especially in the petroleum and oil services industry. It can however be replaced by any other system known to those skilled in the art capable of withstanding the very high pressures mentioned here.
La figure 3 illustre l'application de l'invention à la réalisation de capteurs raccordables à des lignes haute pression.FIG. 3 illustrates the application of the invention to the production of sensors connectable to high pressure lines.
Dans ce mode d'application le capteur (11) mesure une ou plusieurs propriétés du fluide circulant dans le conduit composite 1. Le capteur sera notamment un débitmètre, un densitomètre, un capteur de mesure de conductivité, de type connu et qu'il est inutile de décrire ici en détail. In this mode of application, the sensor (11) measures one or more properties of the fluid flowing in the composite conduit 1. The sensor will in particular be a flow meter, a densitometer, a conductivity measurement sensor, of known type and that it is needless to describe here in detail.
Enfin la figure 4 représente un tuyau très haute pression ayant à chaque extrémité un raccord type Weco male et femelle (respectivement) reliés au tuyau en matériau composite grâce à l'invention.Finally, FIG. 4 represents a very high pressure pipe having at each end a Weco male and female type connection (respectively) connected to the pipe made of composite material thanks to the invention.
L'intéret de l'utilisation des matériaux composites à base de polymères pour les tuyaux haute pression, résident surtout dans le gain important de poids, permettant une manutention plus aisée et le transport d'un plus grand nombre de tuyaux par camion. Pour l'industrie, notamment pétrolière et parapétrolière, cet avantage revêt une extrème importance. The advantage of using polymer-based composite materials for high-pressure hoses lies above all in the significant weight gain, allowing easier handling and the transport of a greater number of hoses by truck. For the industry, notably the oil and oil industry, this advantage is extremely important.
Claims (9)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8707722A FR2616198B1 (en) | 1987-06-02 | 1987-06-02 | SYSTEM FOR ASSEMBLING A METAL END PIECE AND A TUBE IN HIGH PRESSURE COMPOSITE MATERIAL AND APPLICATIONS IN PARTICULAR TO EQUIPMENT IN THE OIL FIELD |
EP87201852A EP0266810B1 (en) | 1986-10-24 | 1987-09-28 | System for the assembly of a metal joining-piece and a high-pressure composite material tube - notably applications for equipment used in the oil industry |
DE8787201852T DE3776270D1 (en) | 1986-10-24 | 1987-09-28 | SYSTEM FOR CONNECTING A METAL CONNECTING PIECE AND A HIGH PRESSURE PIPE MADE OF COMPOSITE MATERIAL, IN PARTICULAR FOR APPLICATION TO DEVICES IN THE PETROLEUM INDUSTRY. |
US07/111,841 US4974245A (en) | 1986-10-24 | 1987-10-21 | System for the assembly of a metal joining piece and a high pressure composite material tube notably applications for equipment used in the oil industry |
NO874430A NO874430L (en) | 1986-10-24 | 1987-10-23 | SYSTEM FOR COMPOSITION OF A METAL SHIPPING PIPE AND A HIGH PRESSURE BEAM OF COMPOSITION MATERIAL SPECIFIC TO EQUIPMENT USED IN THE OIL INDUSTRY. |
CA000550071A CA1314244C (en) | 1986-10-24 | 1987-10-23 | System for the assembly of a metal joining piece and a high pressure composite material tube - notably applications for equipment used in the oil industry |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8707722A FR2616198B1 (en) | 1987-06-02 | 1987-06-02 | SYSTEM FOR ASSEMBLING A METAL END PIECE AND A TUBE IN HIGH PRESSURE COMPOSITE MATERIAL AND APPLICATIONS IN PARTICULAR TO EQUIPMENT IN THE OIL FIELD |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2616198A1 true FR2616198A1 (en) | 1988-12-09 |
FR2616198B1 FR2616198B1 (en) | 1989-09-15 |
Family
ID=9351683
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8707722A Expired FR2616198B1 (en) | 1986-10-24 | 1987-06-02 | SYSTEM FOR ASSEMBLING A METAL END PIECE AND A TUBE IN HIGH PRESSURE COMPOSITE MATERIAL AND APPLICATIONS IN PARTICULAR TO EQUIPMENT IN THE OIL FIELD |
Country Status (1)
Country | Link |
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FR (1) | FR2616198B1 (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2219047A (en) * | 1939-01-12 | 1940-10-22 | Goodrich Co B F | Hose and coupling structure |
US2854030A (en) * | 1956-09-13 | 1958-09-30 | Schulthess Ernest | Oil hose |
DE1932448U (en) * | 1961-07-22 | 1966-02-10 | Heinrich Dr Ing Klein | PRESSURE RESISTANT TUBE MADE OF THERMOPLASTIC PLASTIC. |
AT320362B (en) * | 1972-09-18 | 1975-02-10 | Schwarz Walter | Pipe connection |
GB2009875A (en) * | 1977-12-06 | 1979-06-20 | Bridgestone Tire Co Ltd | Reinforced rubber hose |
US4313629A (en) * | 1980-07-14 | 1982-02-02 | Champion Spark Plug Company | Hose connector |
-
1987
- 1987-06-02 FR FR8707722A patent/FR2616198B1/en not_active Expired
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2219047A (en) * | 1939-01-12 | 1940-10-22 | Goodrich Co B F | Hose and coupling structure |
US2854030A (en) * | 1956-09-13 | 1958-09-30 | Schulthess Ernest | Oil hose |
DE1932448U (en) * | 1961-07-22 | 1966-02-10 | Heinrich Dr Ing Klein | PRESSURE RESISTANT TUBE MADE OF THERMOPLASTIC PLASTIC. |
AT320362B (en) * | 1972-09-18 | 1975-02-10 | Schwarz Walter | Pipe connection |
GB2009875A (en) * | 1977-12-06 | 1979-06-20 | Bridgestone Tire Co Ltd | Reinforced rubber hose |
US4313629A (en) * | 1980-07-14 | 1982-02-02 | Champion Spark Plug Company | Hose connector |
Also Published As
Publication number | Publication date |
---|---|
FR2616198B1 (en) | 1989-09-15 |
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