Laminated structure and method for manufacturing the same
10603869 ยท 2020-03-31
Assignee
Inventors
- Ryo Morihashi (Kobe, JP)
- Takeshi Hasegawa (Aioi, JP)
- Yosuke Tsumura (Kobe, JP)
- Takeshi Takagi (Kakogawa, JP)
Cpc classification
B32B27/304
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
B29C65/4895
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/003
PERFORMING OPERATIONS; TRANSPORTING
B29C65/06
PERFORMING OPERATIONS; TRANSPORTING
B32B27/28
PERFORMING OPERATIONS; TRANSPORTING
B32B5/18
PERFORMING OPERATIONS; TRANSPORTING
B32B37/04
PERFORMING OPERATIONS; TRANSPORTING
B29C66/71
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/54
PERFORMING OPERATIONS; TRANSPORTING
B32B37/144
PERFORMING OPERATIONS; TRANSPORTING
B29D99/0021
PERFORMING OPERATIONS; TRANSPORTING
B29K2079/085
PERFORMING OPERATIONS; TRANSPORTING
B32B5/32
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/106
PERFORMING OPERATIONS; TRANSPORTING
B29K2081/06
PERFORMING OPERATIONS; TRANSPORTING
B29C66/45
PERFORMING OPERATIONS; TRANSPORTING
B29K2079/085
PERFORMING OPERATIONS; TRANSPORTING
B29K2679/085
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2681/06
PERFORMING OPERATIONS; TRANSPORTING
B32B2266/0214
PERFORMING OPERATIONS; TRANSPORTING
B29C66/712
PERFORMING OPERATIONS; TRANSPORTING
B60R13/00
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7394
PERFORMING OPERATIONS; TRANSPORTING
B32B37/12
PERFORMING OPERATIONS; TRANSPORTING
B29K2067/003
PERFORMING OPERATIONS; TRANSPORTING
B29K2081/06
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/3065
PERFORMING OPERATIONS; TRANSPORTING
B29C66/1122
PERFORMING OPERATIONS; TRANSPORTING
B32B5/245
PERFORMING OPERATIONS; TRANSPORTING
B29C66/71
PERFORMING OPERATIONS; TRANSPORTING
B29C65/48
PERFORMING OPERATIONS; TRANSPORTING
B32B2266/0235
PERFORMING OPERATIONS; TRANSPORTING
B29K2667/003
PERFORMING OPERATIONS; TRANSPORTING
B29K2995/0016
PERFORMING OPERATIONS; TRANSPORTING
B29K2079/08
PERFORMING OPERATIONS; TRANSPORTING
B32B2266/0285
PERFORMING OPERATIONS; TRANSPORTING
B32B2260/021
PERFORMING OPERATIONS; TRANSPORTING
B32B27/20
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B5/24
PERFORMING OPERATIONS; TRANSPORTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
B32B37/04
PERFORMING OPERATIONS; TRANSPORTING
B32B37/12
PERFORMING OPERATIONS; TRANSPORTING
B29C65/48
PERFORMING OPERATIONS; TRANSPORTING
B32B7/02
PERFORMING OPERATIONS; TRANSPORTING
B32B27/06
PERFORMING OPERATIONS; TRANSPORTING
B32B27/20
PERFORMING OPERATIONS; TRANSPORTING
B60R13/00
PERFORMING OPERATIONS; TRANSPORTING
B32B5/18
PERFORMING OPERATIONS; TRANSPORTING
B29D99/00
PERFORMING OPERATIONS; TRANSPORTING
B32B5/32
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B32B27/28
PERFORMING OPERATIONS; TRANSPORTING
B32B27/30
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A laminated structure has a first layer formed from a fiber reinforced plastic, a second layer formed from a fiber reinforced plastic and arranged opposed to the first layer, a first core layer formed from a first resin foam and arranged between the first layer and the second layer, and a second core layer formed from a second resin foam and arranged between the first core later and the second layer. The first resin foam has a higher flame resistance than the second resin foam. A laminated structure having flame resistance and high strength enough to endure a bird strike or the like at the same time can be manufactured at relatively low manufacturing cost.
Claims
1. A laminated structure comprising: a first layer formed from a fiber reinforced plastic; a second layer formed from a fiber reinforced plastic and arranged opposed to the first layer; a first core layer formed from a first resin foam and arranged between the first layer and the second layer; and a second core layer formed from a second resin foam and arranged between the first core layer and the second layer, wherein a thickness of the second core layer is thicker than a thickness of the first core layer, wherein the first resin foam has a higher flame resistance than the second resin foam, wherein the second resin foam has a higher strength than the first resin foam, and wherein a neutral plane of shear stress is located within the second core layer.
2. The laminated structure according to claim 1, wherein the first core layer and the second core layer are joined.
3. The laminated structure according to claim 2, wherein the first core layer and the second core layer are joined by any one of bonding, welding, fusing, or any combination thereof.
4. The laminated structure according to claim 1, wherein the first layer and the first core layer are joined by a part of resin forming the first layer.
5. The laminated structure according to claim 1, wherein the second layer and the second core layer are joined by a part of resin forming the second layer.
6. The laminated structure according to claim 1, wherein a third core layer formed from a resin foam which has a higher flame resistance than the second resin foam is arranged between the second core layer and the second layer.
7. The laminated structure according to claim 6, wherein the second core layer and the third core layer are joined.
8. The laminated structure according to claim 7, wherein the second core layer and the third core layer are joined by any one of bonding, welding, fusing, or any combination thereof.
9. The laminated structure according to claim 6, wherein the second layer and the third core layer are joined by a part of resin forming the second layer.
10. The laminated structure according to claim 1, wherein the first resin foam is formed from any one of polyethylene terephthalate, phenol resin, or polyether sulfone.
11. The laminated structure according to claim 1, wherein the second resin foam is formed from any one of polyvinyl chloride, polymethacrylimide, polyimide, or polyetherimide.
12. The laminated structure according to claim 1, wherein the laminated structure is used as a structural member forming at least a part of a front bodyshell of a front car of a railway vehicle.
13. The laminated structure according to claim 1, wherein the fiber reinforced plastic is formed using a thermosetting resin.
14. A manufacturing method of a laminated structure, comprising: forming a first core member from a first resin foam; forming a second core member from a second resin foam; forming a core member assembly by laminating the first core member and the second core member, wherein a thickness of the second core member is thicker than a thickness of the first core member; laminating a reinforcing fiber for forming a first fiber reinforced plastic layer on a mold; making the first core member side of the core member assembly opposite to a surface of the reinforcing fiber for forming the first fiber reinforced plastic layer so as to be laminated on the same surface; and laminating a reinforcing fiber for forming a second fiber reinforced plastic layer on the second core member side of the core member assembly, wherein the first resin foam has a higher flame resistance than the second resin foam and wherein the second resin foam has a higher strength than the first resin foam, and wherein a neutral plane of shear stress is located within the second core member.
15. The manufacturing method of a laminated structure according to claim 14, further comprising a step of forming a third core member between the second core member and the second layer.
16. The manufacturing method of a laminated structure according to claim 14, wherein the first layer and the second layer, and a core member adjacent to the layers are joined by a part of resin forming each of the first layer and the second layer.
17. The manufacturing method of a laminated structure according to claim 14, wherein the fiber reinforced plastic is formed using a thermosetting resin.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
(7)
DESCRIPTION OF EMBODIMENTS
(8) Hereunder, a laminated structure according to an embodiment of the present invention will be described referring to the figures.
(9) The laminated structure according to the embodiment is particularly suitable for a structural member of a front bodyshell of a front car of a high-speed railcar. However, the present invention is not only applicable to the front bodyshell of the front car of the high-speed railcar, but also applicable to structural members of a side bodyshell, roof bodyshell, and an end body shell of the high-speed railcar and a general railcar.
(10) As illustrated in
(11) Note that, when using the laminated structure 1 for the front bodyshell of the front car of the high-speed railcar, the first FRP layer 10 is positioned to an external surface side of the front bodyshell of the front car and the second FRP layer 11 is positioned to an inner surface side of the front bodyshell of the front car when flame resistance is to be given to the external surface side of the front bodyshell, for example.
(12) A flame resistant core layer (first core layer) 12 formed from a first resin foam is arranged between the first FRP layer 10 and the second FRP layer 11. A high-strength core layer (second core layer) 13 formed from a second resin foam is arranged between the flame resistant core layer 12 and the second FRP layer 11.
(13) The first FRP layer 10 and the second FRP layer 11 may be formed using the same kind of fiber reinforced plastic or may be formed using different kinds of fiber reinforced plastics. It is preferable that they are formed using a thermosetting resin.
(14) As materials of the fiber reinforced plastic, any kind of fibers can be used, such as carbon fibers, glass fibers, and aramid fibers. Also, any kind of method can be employed for weaving fibers, such as plain weave, twill weave, satin weave, unidirectional weave, nonwoven fabric, or the like.
(15) Also, any kind of resin can be used for the fiber reinforced plastic, but it is preferable that the thermosetting resin with good fluidity is used therefor. Specifically, epoxy resin, unsaturated polyester resin, vinyl ester resin, phenol resin, bismaleimide resin, or the like is used.
(16) Also, autoclave/prepreg molding which is a method of bagging or pressurizing and heating, oven curing prepreg molding, VaRTM, RTM, or the like can be employed as a method for molding the fiber reinforced plastic regardless of their kinds.
(17) The first FRP layer 10 and the flame resistant core layer 12 are joined by a part of resin forming the first FRP layer 10. The second FRP layer 11 and the high-strength core layer 13 are joined by a part of resin forming the second FRP layer 11.
(18) The flame resistant core layer 12 and the high-strength core layer 13 are joined by an adhesive, welding, fusing, or the like. Any kind of adhesive can join the both core layers 12, 13. Also, there is a method of joining the both core layers 12, 13 by making them in a dissolved state (state that the both core layer 12, 13 are dissolved into a solvent as a solute) to be joined as an example of welding, and there is a method of joining the both core layers 12, 13 by making then in a locally fused state with friction heat generated by vibrating the both core layers 12, 13 as an example of fusing. However, welding method and fusing method are not limited to them.
(19) In the laminated structure 1 according to the embodiment, the first resin foam for forming the flame resistant core layer 12 has a higher flame resistance than the second resin foam for forming the high-strength core layer 13. For example, polyethylene terephthalate (PET) can be used for the first resin foam, and polyvinyl chloride (PVC) can be used for the second resin foam. Polymethacrylimide (PMI) can also be used as the first resin foam. However, PET is more advantageous than PMI in regards to cost.
(20) It is preferable that the second resin foam for forming the high-strength core layer 13 has higher strength than the first resin foam for forming the flame resistant core layer 12. PVC and PMI of the above-mentioned materials have higher strength than PET.
(21) As illustrated in
(22) Namely, by the laminated structure 1 according to the embodiment, a core material configuring the laminated structure 1 has a two-layered structure composed of the flame resistant core layer 12 and the high-strength core layer 13, and therefore the flame resistant core layer 12 can take the flame resistant capacity and the high-strength core layer 13 can take the shear resistant strength, respectively.
(23) Therefore, the laminated structure 1 having the flame resistance and the high-strength at the same time can be manufactured at a respectively low manufacturing cost.
(24) Also, the thickness of the whole core layer can be thinner compared to a case that a core material excellent in flame resistance but inferior in strength is used to ensure a desired strength by increasing its thickness. Accordingly, manufacture becomes easy (it becomes easy to correspond to the form of a mold) and weight and cost can be reduced.
(25) Also, in the laminated structure 1 according to the embodiment, a neutral plane 14 of shear stress is positioned in the impact resistant core layer 13, and therefore the maximum shear stress generated when an object (a bird, for example) collides with the laminated structure 1 can be taken by the high-strength core layer 13. Thereby, it can be surely prevented that a damage such as a crack is generated in the laminated structure 1 by an impact.
(26) Note that, when using the laminated structure 1 for the front bodyshell of the front car of the high-speed railcar, the first FRP layer 10 is positioned to an external surface side of the front bodyshell of the front car and the second FRP layer 11 is positioned to an inner surface side of the front bodyshell of the front car when the flame resistance is to be given to the external surface side of the front bodyshell, for example.
(27) In contrast, when the flame resistance is to be given to the internal surface side of the front bodyshell of the front car, arrangements of the first FRP layer 10 and the second FRP layer 11 are reversed.
(28) Also, when the flame resistance is to be applied to the both external surface side and internal surface side of the front bodyshell of the front car, a laminated structure according to another embodiment of the present invention, which will be described below, can be used.
(29) Hereunder, a laminated structure according to another embodiment of the present invention will be described referring to
(30) In a laminated structure 1A according to the embodiment, an additional flame resistant core layer (third core layer) 15 is arranged between the high-strength core layer 13 and the second FRP layer 11. Hereunder, the flame resistant core layer 12 on the first FRP layer 10 side is referred to as the first flame resistant core layer 12 and the flame resistant core layer 15 on the second FRP layer 11 side is referred to as the second flame resistant core layer 15.
(31) The second flame resistant core layer 15 is formed from a resin foam having higher flame resistance than the second resin foam forming the high-strength core layer 13. The second flame resistant core layer 15 may be formed from the same kind of resin foam as the first flame resistant core layer 12 or may be formed from different kinds of resin foam.
(32) In the laminated structure 1A according to the embodiment, the thickness T1 of the first flame resistant core layer 12 and a thickness T3 of the second flame resistant core layer 15 are the same. Components can be shared by forming the first flame resistant core layer 12 and the second flame resistant core layer 15 of the same material.
(33) Also, the thickness T1 of the first flame resistant core layer 12 and the thickness T3 of the second flame resistant core layer 15 can be different. However, note that it is preferable that each layer thickness T1, T2, T3 is set so that the neutral plane 14 of shear stress is positioned in the high-strength core layer 13 in order to sufficiently secure the strength of the laminated structure 1A.
(34) The second FRP layer 11 and the second flame resistant core layer 15 are joined by a part of resin forming the second FRP layer 11. The flame resistant core layer 13 and the second high-strength core layer 15 are joined by an adhesive, welding, fusing, or the like.
(35) A kind of material which can be used as the first resin foam and the second resin foam is the same as that which is described on the laminated structure 1 in
(36) Also in the laminated structure 1A according to the embodiment, the same function and effect as the laminated structure 1 in
(37) Also, as the thickness T1 of the first flame resistant core layer 12 and the thickness T3 of the second flame resistant core layer 15 are the same, the laminated structure 1A can be used without distinguishing the outside and inside of the same, provided the both core layers 12 and 15 are formed from the same material.
(38) Next, a laminated structure according to a variation of the embodiment in
(39) In the laminated structure 1B, the thickness T1 of the first flame resistant core layer 12, the thickness T2 of the high strength core layer 13, and the thickness T3 of the second flame resistant core layer 15 are set to the same thickness.
(40) A kind of material which can be used as the first resin foam and the second resin foam is the same as that which is described on the laminated structure 1 in
(41) Also in a laminated structure 1B according to the embodiment, the neutral plane 14 of shear stress is positioned in the high-strength core layer 13, and therefore the strength of the laminated structure 1B can be secured.
(42) Also, as the thickness T1 of the first flame resistant core layer 12 and the thickness T3 of the second flame resistant core layer 15 are the same, the laminated structure 1B can be used without distinguishing the outside and inside of the same, provided the both core layers 12 and 15 are formed from the same material.
(43) Next, a method of manufacturing a laminated structure according to an embodiment of the present invention will be described referring to
(44) As illustrated in
(45) Next, the flame resistant core member and the high strength core member are laminated and they are joined to each other so as to form a core member assembly (step S2). The both core members are joined by an adhesive, welding, fusing, or the like.
(46) Next, reinforcing fibers for forming the first FRP layer are laminated on a mold (step S3). Also, the flame resistant core member of the core member assembly is opposed to and laminated on the surface of the reinforcing fibers for forming the first FRP layer (step S4). Further, reinforcing fibers for forming the second FRP layer are laminated on the surface of the high strength core member of the core member assembly (step S5). Finally, the laminated structure 1 of FRP is formed using various FRP manufacturing methods such as autoclave molding, RTM, VaRTM, or the like (step S6).
(47) Kinds of materials which can be used as the first resin foam and the second resin foam are the same as that which are already described on the laminated structure 1 in
(48) Next, a method of manufacturing a laminated structure according to another embodiment of the present invention will be described referring to
(49) As illustrated in
(50) Next, the pair of flame resistant core members are laminated on the both sides of the high strength core member and joined to each other so as to form a core member assembly (step S2A). The core members are joined by an adhesive, welding, fusing, or the like.
(51) Next, reinforcing fibers for forming the first FRP layer are laminated on a mold (step S3A). Also, one of the flame resistant core members of the core member assembly is opposed to and laminated on the surface of the reinforcing fibers for forming the first FRP layer (step S4A). Also, reinforcing fibers for forming the second FRP layer are laminated on the surface of the other of the flame resistant core members of the core member assembly (step S5A). Finally, the laminated structures 1A, 1B of FRP are formed using various FRP manufacturing methods such as autoclave molding, RTM, VaRTM, or the like (step S6A).
(52) Kinds of materials which can be used as the first resin foam and the second resin foam are the same as that which are already described on the laminated structures 1A, 1B in
REFERENCE SIGNS LIST
(53) 1, 1A, 1B . . . laminated structure 10 . . . first FRP layer 11 . . . second FRP layer 12 . . . flame resistant core layer (first flame resistant core layer) 13 . . . high strength core layer 14 . . . neutral surface of shear stress 15 . . . flame resistant core layer (second flame resistant core layer)