FIBER-REINFORCED STRUCTURES
20170341318 · 2017-11-30
Assignee
Inventors
Cpc classification
B29C53/822
PERFORMING OPERATIONS; TRANSPORTING
B29C49/44
PERFORMING OPERATIONS; TRANSPORTING
B29C53/566
PERFORMING OPERATIONS; TRANSPORTING
B29C70/446
PERFORMING OPERATIONS; TRANSPORTING
B29K2063/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2105/06
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C70/44
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for manufacturing a fiber reinforced structure includes the following. A mandrel of a first material comprises a hollow interior and an aperture that allows a fluid to enter the interior. A layer of a second material provided on the mandrel includes an uncured resin and fibers. The mandrel and the layer are placed in a mold cavity formed by a mold. A pressurized fluid is introduced into the interior of the mandrel via the aperture to generate a force acting to expand the mandrel outward. The mandrel is heated so that it becomes deformable and expand outward to press the layer against the mold. The layer is heated so that it cures. The mandrel is then heated to a temperature above its melting point of the first material so that it melts, after which it is removed.
Claims
1. A method for manufacturing a structure reinforced by fibers, the method comprises: (i) providing a mandrel of a first material, wherein the mandrel comprises an outside surface, a hollow interior, and an aperture for allowing a fluid to enter the interior, the first material is rigid at room temperature and has a melting temperature at which it melts, and the first material becomes deformable when approaching the melting temperature, (ii) providing a layer of a second material on the outside surface of the mandrel without blocking the aperture, wherein the second material comprises an uncured thermo-setting resin and fibers configured for reinforcing the structure, the second material has a curing temperature below which it is pliable and above which it cures, (iii) placing the mandrel and the layer in a mold cavity formed by a mold, wherein the mold is configured to allow a fluid to reach the aperture of the mandrel, (iv) introducing a pressurized fluid into the interior of the mandrel via the aperture for generating a force acting to expand the mandrel outward, heating the mandrel to a temperature below the melting temperature of the first material for making the mandrel deformable and allowing the mandrel to expand outward and press the layer against the mold, and heating the layer to a temperature above the curing temperature of the second material to cure and form the structure, (v) heating the mandrel to a temperature above the melting point of the first material for melting the mandrel, and (vi) removing the melted mandrel from the structure.
2. The method according to claim 1, wherein the structure is a hollow structure, and in step (ii) the layer is provided to enclose or enfold the mandrel or a portion of the mandrel.
3. The method according to claim 1, wherein the first material is a thermoplastic, the resin comprises an epoxy resin, and/or the fibers comprise carbon fibers.
4. The method according to claim 1, wherein in step (iii), the mold is configured to leave the aperture open to the surroundings of the mold, and the step (iv) further comprises: placing the mold in an autoclave and generating a pressurized and heated atmosphere inside the autoclave for providing the pressurized fluid and for heating the mandrel and the layer.
5. The method according to claim 1, wherein the step (iv) further comprises: connecting the aperture of the mandrel to a pressure source via a pressure conduit, wherein the pressure source provides the pressurized fluid and the pressure conduit conveys the pressurized fluid to the aperture, and the step (iv) further comprises: placing the mold in an oven generating heat for heating the mandrel and the layer.
6. The method according to claim 1, wherein the curing in step (iv) is a first curing, and the method further comprises the step of: (vii) subjecting the layer or structure to a second curing at a temperature that is greater than the temperature of the first curing.
7. The method according to claim 6, wherein the subjecting of the second material to a second curing in step (vii) comprises: heating the layer or structure to a temperature in the range 170-200° C.
8. The method according to claim 1, wherein in step (ii), providing layer of a second material on the outside surface of the mandrel comprises: applying one or more sheets of the second material on the mandrel.
9. The method according to claim 1, wherein the method comprises prior to and/or simultaneous to step (iv): (ix) evacuating air inside the mold cavity between the mandrel and the mold.
10. The method according to claim 1, wherein the step (ii) further comprises: providing the layer with one or more openings, wherein each of the one or more openings is configured to prevent the mandrel from being removed through the one or more openings prior to a melting of the mandrel, and wherein each of the one or more openings is configured to allow the mandrel to be removed through the one or more openings subsequent to a melting of the mandrel.
11. The method according to claim 1, wherein the method is further configured to form an additional structure reinforced by fibers and joined to the structure, and wherein the mold comprises an additional outside surface and a gap for allowing access to the mold cavity outside the mold, and the step (iii) further comprises: providing an additional layer of the second material on the additional outside surface of the mold and joining the additional layer to the layer provided on the outside surface of the mandrel via the gap.
12. A mandrel for being placed in mold cavity of a mold having an opening to allow access to the mold cavity from outside the mold, wherein the mandrel comprises a hollow interior and an aperture for allowing a fluid to enter the interior, wherein the mandrel is configured to allow the aperture to be accessed via the opening when the mandrel is placed in the mold cavity, and wherein the mandrel is of a first material that is rigid at room temperature and has a melting temperature at which it melts, and the first material becomes deformable when approaching the melting temperature.
13. The mandrel according to claim 12, wherein the mandrel comprises a protruding portion on which the aperture is located, and the protruding portion is configured to extend through the opening of the mold for positioning the aperture on the outside of the mold when the mandrel is placed in the mold cavity.
14. A molding system comprising: a mold having a mold cavity and an opening to allow access to the mold cavity from outside the mold, and a mandrel comprising a hollow interior and an aperture for allowing a fluid to enter the interior, wherein the mandrel is configured to allow the aperture to be accessed via the opening when the mandrel is placed in the mold cavity, and wherein the mandrel is of a material that is rigid at room temperature and has a melting temperature at which it melts, and the first material becomes deformable when approaching the melting temperature.
15. The molding system according to claim 14, wherein the mandrel comprises a protruding portion on which the aperture is located, and the protruding portion is configured to extend through the opening of the mold for positioning the aperture on the outside of the mold when the mandrel is placed in the mold cavity.
16. (canceled)
Description
BRIEF DESCRIPTION OF DRAWINGS
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DETAILED DESCRIPTION OF DRAWINGS
[0071] The following detailed description of example embodiments refers to the accompanying drawings. The same reference numbers re used in different drawings to identify the same or similar elements. Also, the detailed description is provided for the purpose of illustration and explanation of the different aspects of the invention. Any of the modifications or functions described above for the different aspects of the invention may be applied to embodiments below, either by replacement of described features, or by addition.
[0072] An embodiment of a method for manufacturing a fiber-reinforced structure is illustrated in
[0073] In a second step, a layer 18 of a second material is provided on the mandrel 10 on the outside surface 12 of the mandrel 10, as is shown in the perspective view of
[0074] In a third step, which is illustrated in
[0075] In a fourth step, which is illustrated in
[0076] In a fifth step, the mandrel 10 is heated to a temperature above the melting point of the first material so that the mandrel 10 melts, which is illustrated in
[0077] The curing in the fourth step, which is described in connection with
[0078] In the fourth step, the mold 20 with the mandrel 10 and layer 18 inside it are placed in an autoclave 26, which is schematically illustrated in
[0079] The fifth to the seventh steps are also performed in the autoclave 26, where the heating element 30 increases the temperature of the atmosphere inside the autoclave 26, thus causing the heating. A pressurized atmosphere is maintained in the autoclave throughout the fourth to seventh steps, which means that an elevated pressure presses the layer 18 against the mold 20 until the vitrification or final curing is complete.
[0080] The mandrel 10 is made of polyethylene, i.e. the first material is a thermoplastic. The polyethylene has a melting temperature about 120-130° C., above which it starts to melt. The layer is composed of carbon fibers fused with an epoxy resin, i.e. the second material has these components. The epoxy resin effectively has a curing temperature of 110° C., above which it cures. After the mold 20 has been placed in the autoclave, with the mandrel 10 and the layer 18 inside it, the heating element 30 uninterruptedly heats the atmosphere inside the autoclave 26 from room temperature to about 170° C. The limited heat transport of the atmosphere inside the autoclave 26, and the thermal inertia of the mandrel 10, the layer 18, and the mold 20, cause the temperature of these components to rise slower than the temperature of the atmosphere. Thus, the curing of the layer 18 in the fourth step is smoothly followed by the melting of the mandrel 10 in the fifth step, and the removal of the melted mandrel 10 in the sixth step. The temperature is maintained at 170° C. for a sufficiently long time for the layer 18 or the structure 24 to achieve vitrification or full cure of the resin in the seventh step.
[0081] After the mold 20 has been placed in the autoclave, as described above, the pressure source 28 increases the pressure of the atmosphere to an elevated pressure in the range 7-8 bar. The pressure is maintained until the seventh step is complete. When the temperature of the mandrel approaches the melting temperature of polyethylene, the mandrel 10 becomes soft and pliable. When this happens, the elevated pressure inside the autoclave 26 forces the mandrel 10 to press the layer 18 against the mold and form the structure 24, thus enabling the fourth step of the method.
[0082] In the second step above described in relation to
[0083] After the seventh step, the layer 18 or structure 24 is removed from the mold in an eighth step, which is illustrated in
[0084] As described above, the embodiment involves a mandrel 10 configured to be placed in the mold cavity 22 of the mold 20. The mold has an opening 32 to allow access to the mold cavity 22 from outside the mold 20. The mandrel 10 has a hollow interior 14 and an aperture 16, and the mandrel 10 is configured to allow the aperture 16 to be accessed via the opening when it is placed in the mold cavity 22. Further, the mandrel 10 is manufactured of a material that is rigid at room temperature and becomes soft and pliable when the temperature approaches its melting temperature. The mandrel of the second aspect allows for the method of first aspect to be performed.
[0085] A molding system is also described above in relation to
[0086] In the above embodiment, the mandrel 10 is shaped to conform with and follow the shape of the mold cavity 22. This is achieved by having a mandrel with a square cross-section, as is illustrated in
[0087] A second embodiment of a method for manufacturing a fiber-reinforced structure is illustrated in
[0088] In the first step illustrated in
[0089] In the third step illustrated in
[0090] In the fourth step, which is illustrated in
[0091] In the fifth step, the mandrel 10 is heated so that the mandrel 10, including its protruding portion 38, melts, which is illustrated in
[0092] A third embodiment of a method for manufacturing a fiber-reinforced structure is illustrated in
[0093] In the first step illustrated in
[0094] In the third step illustrated in
[0095] In the fourth step, which is illustrated in
[0096] In the fifth step, the heater 50 provides more heat to the flow of pressurized fluid, which causes the melting of the mandrel 10, which is illustrated in
[0097] A fourth embodiment of a method for manufacturing a fiber-reinforced structure is illustrated in
[0098] In the first step illustrated in
[0099] The protruding portion 38 on which the aperture 16 is located is joined to the annular center. The protruding portion 38 is of the same material as the rest of the mandrel 10.
[0100] In the second step, which is illustrated in
[0101] In the third step illustrated in
[0102] The mold 20 has additional outside surface 70 and an additional layer 78 of the second material is applied to the additional outside surface 70 of the mold and joined to the layer 18 provided on the outside surface 12 of the mandrel 10 via all the gaps 66. The additional layer 78 is applied in sheets in the same manner as the layer 18, which is described in relation to
[0103] The mold 20 has an opening 32 with a circular cross-section through which the protruding portion 38 extends and positions the aperture 16 on the outside of the mold 20. The protruding portion 38 engages the inside of the opening 32 provide a sealing between protruding portion 38 and the mold 20.
[0104] The fourth step is illustrated in
[0105] As in the first embodiment, the autoclave 26 has a pressure source 28 in the form of an air compressor that can generate a pressurized atmosphere inside the pressure chamber 32 of the closed autoclave 26. The autoclave further has a heating element 30 that can heat the pressurized atmosphere. The fourth step is performed in the autoclave 26, where the heated atmosphere heats the whole contents inside the bag 74, which includes the mandrel 10 and the layer 18. The pressurized atmosphere enters the interior 14 of the mandrel 10 via the aperture 16 and forces the mandrel 10 to expand outward and press the layer against the mold 20, after which the layer 18 cures in this position, as is illustrated in
[0106] Simultaneously, the heated pressurized atmosphere also forces the additional layer 78 against the additional outside surface 70 and heats the additional layer 78 to a temperature above the curing temperature of the second material, which is also illustrated in
[0107] The fourth step is concluded by removing the mold from the bag 74. This is followed by the fifth step in which the mandrel 10 is heated to a temperature above the melting point of the first material so that the mandrel 10 melts. This is followed by the sixth step, in which the melted mandrel 10 flows out through the opening 32 of the mold 20 on its own accord. The fifth and sixth steps are illustrated in
[0108] In the seventh step, which is illustrated in
[0109] In an alternative embodiment to the fourth embodiment, the protruding portion 38 is located on the mandrel 10 at the tip 68 of one of the protrusions 58 so that it extends through one of the gaps 66. Thus, the gap 66 has the function of the opening, but with the difference that there is no sealing between the protruding portion and the opening. This alternative embodiment is illustrated in
[0110] The protruding portion 38 leaves an access hole 94 in the final rim through which the hollow inside of the spoke can be reached. After the mold has been removed from the bag 74, corresponding holes are drilled in each of the other spokes. This is followed by the sixth step, in which the wheel is rotated around the rotational axis 58 so that the melted mandrel 10 is forced out through the holes and is thereby removed from the structure. This is followed by the eighth step, in which the final structure 24 or wheel 82 is removed from the mold 20.
ITEMLIST
[0111] 10 mandrel
[0112] 12 outside surface
[0113] 14 hollow interior
[0114] 16 aperture
[0115] 18 layer
[0116] 20 mold
[0117] 22 mold cavity
[0118] 24 structure
[0119] 26 autoclave
[0120] 28 pressure source
[0121] 30 heating element
[0122] 32 opening of mold
[0123] 34 rectangular wall sections
[0124] 36 screws
[0125] 37 holes
[0126] 38 protruding portion
[0127] 40 pressure conduit
[0128] 42 oven
[0129] 44 pump
[0130] 50 heater
[0131] 52 additional opening of mold
[0132] 54 annular center
[0133] 56 protrusion
[0134] 58 rotational axis
[0135] 60 first part
[0136] 62 second part
[0137] 64 bolt
[0138] 66 gap
[0139] 68 tip of protrusion
[0140] 70 additional outside surface
[0141] 72 fleece
[0142] 74 bag
[0143] 76 lead-throughs
[0144] 78 additional layer
[0145] 80 outlet
[0146] 82 wheel
[0147] 84 rim
[0148] 86 cylindrical sleeve
[0149] 88 free edges
[0150] 90 hub
[0151] 92 spokes
[0152] 94 access hole