METHOD FOR MANUFACTURING A PRESSURE VESSEL

Abstract

A method for manufacturing a pressure vessel (2), which is preferably provided for use in bladder accumulators, comprising the following manufacturing steps:providing a support structure (22), more particularly in the form of a liner;applying a fibrous material (24) to the support structure (22) to form a base structure (20);placing the base structure (20) in a heatable mold apparatus (4, 6, 10); andintroducing a matrix between the mold apparatus (4, 6, 10) and the base structure (20), which partially penetrates the fibrous material (24).

Claims

1. A method for manufacturing a pressure vessel (2), which is provided preferably for use in bladder accumulators, having the following manufacturing steps: providing a support structure (22), in particular, in the form of a liner; applying a fibrous material (24) to the support structure (22) to form a base structure (20); introducing the base structure (20) into a heatable mold apparatus (4, 6, 10); and introducing a matrix between the mold apparatus (4, 6, 10) and the base structure (20), which at least partially penetrates the fibrous material (24).

2. The method according to claim 1, characterized in that the fibrous material (24) is applied dry to the support structure (22) and takes place in the form of a wrapping or braiding.

3. The method according to claim 1, characterized in that the support structure (22) is wrapped with the fibrous material (24) in an axial and tangential direction in such a way that the fibrous material (24) is substantially subjected to tensile loads.

4. The method according to claim 1, characterized in that reactive resin systems; reactive polyamide, preferably caprolactam; or polyurethane systems (PU) are used as a matrix.

5. The method according to claim 1, characterized in that the matrix is injected into the mold apparatus (4, 6, 10) by means of a resin injection method, preferably under a pressure of 30 bar to 40 bar.

6. The method according to claim 1, characterized in that the matrix, together with at least one solvent, preferably in the form of isocyanate, is introduced into the mold apparatus (4, 6, 10) in such a way that the solvent-containing, fluidic matrix saturates the fibrous material (24) of the support structure (22) and the matrix in the cured state protectively encloses the fibrous material (24).

7. The method according to claim 1, characterized in that the matrix, fully cured after removal from the mold apparatus (4, 6, 10), is manufactured as a solid protective sheath body (32) in a non-porous manner

8. The method according to claim 1, characterized in that a negative pressure is applied to the mold apparatus (4, 6, 10) during the introduction of the solvent-containing matrix and/or the interior pressure of the support structure (22) is increased, preferably by introducing a non-reactive, compressible or incompressible pressure medium, such as nitrogen gas, or water or oil.

9. The method according to claim 1, characterized in that the molding temperature selected is below 100 C. and the mold time is less than 10 minutes, preferably approximately 8 minutes.

10. The method according to claim 1, characterized in that the support structure used is a liner (22) made of steel materials or a liner (22) constructed from plastic materials, either of which is designed as a hollow body provided with a through-opening (42) at its opposite ends.

11. A pressure vessel, in particular, manufactured by a method according to claim 1, consisting of at least one support structure (22), which is surrounded by a fibrous sheath (24), which is saturated with a matrix, which encloses the fibrous sheath (24) at least partly toward the outside as a protective sheath body (32).

Description

[0018] The invention is explained in detail below with reference to the appended drawings, in which:

[0019] FIG. 1 shows in longitudinal section and in schematically greatly simplified and basic representation a mold apparatus for carrying out the method according to the invention, wherein a vessel base structure is inserted into the mold apparatus as a semi-finished product of a pressure vessel to be manufactured;

[0020] FIG. 2 a longitudinal section of the pressure vessel manufactured by the method according to the invention; and

[0021] FIG. 3 an enlarged delineated detail of the area identified by III in FIG. 2.

[0022] FIG. 1 shows a schematically simplified representation of a mold apparatus, by means of which a pressure vessel may be manufactured by the method according to the invention, as it is shown in FIG. 2 and identified there in its entirety by reference numeral 2. The mold apparatus includes two mold parts 4 and 6 as mold halves, which are movable perpendicular to a longitudinal axis 8 toward one another and away from one another. In FIG. 1, the mold parts 4, 6 are shown brought together in the position corresponding to the closed state of the mold. The mold may be closed at its upper end in FIG. 1 by a moveable top part 10, which is depicted in the closed position. The inner mold walls of the mold parts 4, 6, which define the external shape of the finished pressure vessel, include for each molded part 4, 6 a center semi-cylindrical main part 12, which forms the cylindrical part 14 of the finished pressure vessel 2, and curved end parts 16 attached to the main part 12, which form the polar caps 18 at the ends in the finished pressure vessel 2. The mold parts 4, 6 and the top part 10 are heatable. Heating devices of state-of-the-art design, which may be formed, for example, by imbedded electrical heat conductors or ducts for the passage of a heating medium, such as steam, are not depicted in FIG. 1.

[0023] The vessel base structure 20 is inserted as the semi-finished product in the opening mold apparatus (FIG. 1) and is appropriately fixed therein (not depicted), after which the mold apparatus is closed, as is shown in FIG. 1. The base structure 20 consists of the liner 22 forming the support structure or the vessel core, on which the fiber reinforcement 24 is situated. During prefabrication of the base structure 20, the liner 22 is manufactured in a manner known per se from a metallic material, such as steel or aluminum, or from a plastic, such as polyamide or polyethylene, wherein a blow molding method or rotational sintering is suitable in this case.

[0024] The fiber reinforcement 24 is applied during prefabrication of the base structure 20 by wrapping or braiding the liner 22 with the dry fibrous material. The material used may be fibers made of carbon, aramid, glass, boron or textile fibers, hybrid yarns or natural fibers, such as basalt, flax, hemp or cotton bamboo or the like, may also be considered. The dry application of the fibrous material takes place in the form of a wrapping or a braiding the of liner 22 in axial and tangential winding directions, wherein in the axially extending winding areas, the orientation of the winding direction when wrapping the cylindrical part 14 is preferably 0 to 25 relative to the cylindrical axis and the axial wrapping also extends uniformly over the pole caps 18. Tangential wrappings as an alternative to axial wrappings take place beforehand or subsequently, wherein the structuring of the winding takes place in such a way that the fibrous material is preferably subjected to tensile loads.

[0025] As shown in FIG. 1, an intermediate space 26 is formed in the closed mold apparatus between the inner mold walls of the mold parts 4, 6 and the outer side of the fiber reinforcement 24, and which completely surrounds the outer side of the fiber reinforcement 24 between the open end 28 of the base structure 20 situated above in FIG. 1 down to the bottom end closed by a closure part 30. In this intermediate space 26, a matrix is introduced, which saturates the dry fiber reinforcement 24, from which, after it has fully cured, a solid protective sheath body 32 is formed, see FIGS. 2 and 3. To introduce the matrix in a consistency suitable for an injection process, an inlet opening 34 is provided on the top part 10 of the mold apparatus, which opens into the intermediate space 26.

[0026] Reactive resin systems, reactive polyamides, preferably caprolactam, or polyurethane systems (PU) are used as the matrix, wherein a solvent, such as isocyanate, is preferably added in order to facilitate the saturation of the fibrous material. The air displaced during the injection is discharged via a suction connection 36 provided on mold part 16 located below in FIG. 1, at which a negative pressure is present for boosting the injection process. To carry out a resin injection method (RTM), the matrix is injected under pressure at a temperature of the mold apparatus, which is in the range of 70 C. to 90 C. or even higher. To avoid a deformation of the base structure 20 as a result of the injection pressure, an overpressure is built up in the interior of the liner 22 during the injection process. For this purpose, the top part 10 includes a pressure connection 38, via which supporting air, such as nitrogen gas, is fed. However, the support structure or the liner 22 is preferably filled with an incompressible fluid, water or oil.

[0027] Following a reaction time of less than 10 minutes, preferably of approximately 8 minutes, the mold apparatus is opened and the pressure vessel 2 with its protective sheath body 32 is removed, which is formed from the fibrous material impregnated with the matrix and which is non-porous in the fully cured state. After removal of the closure part 30, the pressure vessel 2 formed may be provided at both opposite ends with a connection fitting common for such vessels.

[0028] FIGS. 2 and 3 shows the finished pressure vessel 2 with connection fittings, each of which is formed by a pipe socket 42 in the form of a so-called standardized SAE flange. FIG. 3 shows in an enlarged representation further details of the identically designed pipe socket 42 on both ends of the vessel. As is apparent, said pipe socket includes a collar 44 at its inner end, which forms a shoulder surface 46 as a contact surface for a half-ring 48. The half-ring 48, together with an identically designed second half-ring 40 (FIG. 2), forms an annular body surrounding the pipe socket 42. Each half-ring 48, 50 includes a retaining ring 52 protruding axially in the direction of the vessel interior with a radially protruding end edge 54. The latter forms a type of securing hook, which secures by hooking said retaining ring by engaging in a slotted opening of a ring disc 56.

[0029] Mounted outside the half-rings 48, 50 on the outer side of the pipe socket 42 is a compression ring 58, which is supported at the open end 28 on the liner 22. A nut 60, which is seated on an outer thread 62 of the pipe socket 42, abuts the outer side of compression ring 58. Tightening the nut 60, which is supported on the liner 22 via the compression ring 58, creates a tensile force in the pipe socket 42 directed from the vessel interior outwardly, which is transferred via the shoulder surface 46 on the collar 44 to the half-rings 48, 50. In this way, the elastomer ring disk 56 is braced against the inner side of the liner 22 via the retaining ring 52 with the radially protruding end edge 52, and forms a seal. A further seal is provided by an O-ring 64 on the inner side of the end section of the liner 22.

[0030] Further details of the method according to the invention may be gleaned from the example indicated below.

Example

[0031] A liner provided for a composite pressure vessel is manufactured in a conventional manner with a material weight of 864 g. A vessel base structure is formed by wrapping the liner with fibrous material, the weight of which is 250 g, wherein the wrapping takes place in axial and tangential winding directions to form a fiber reinforcement. The fibrous material used is a high-performance carbon fiber, manufactured by Toho Tenax with the product designation HTS45 E23 12k with a yarn count of 800 tex.

[0032] The wrapped base structure is inserted into a mold apparatus, the basic structure of which is shown in FIG. 1 and which includes the heatable mold parts. To carry out a resin injection method (RTM), a matrix is injected into the intermediate mold space between the fiber reinforcement and the adjoining mold walls at an interior mold temperature of the mold parts of 87 C. and an exterior temperature of the mold parts of 77 C., wherein a vacuum of 200 mbar is present at the intermediate mold space and a supporting pressure of 15 bar is generated in the interior of the liner by means of nitrogen gas.

[0033] A matrix in the form of a polyurethane system (PU) is injected, which includes Elastolit R8819/104/LT of BASF, Ludwigshafen, Germany, as one mixing component, Polyol A.4.D.22.6/196-R1 (tradename Elastolit R8819/104 of BASF) as the second mixing component, and Isocyanate IsoMNDI 92052 as the solvent additive. Also provided is an additive of Indrosil 2000 of Indroma Chemikalien, Bad Soden, Germany as a release agent, which facilitates the separation process between the mold and the manufactured mold body when the mold apparatus is opened.

[0034] The base structure with the fiber reinforcement saturated by the matrix remains in the closed mold apparatus for a reaction period of 8 minutes. After the mold apparatus is opened, the removed pressure vessel has a fully cured solid, protective sheath body that is non-porous.