WO2017191668A1 - 繊維強化樹脂成形体およびその製造方法 - Google Patents

繊維強化樹脂成形体およびその製造方法 Download PDF

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Publication number
WO2017191668A1
WO2017191668A1 PCT/JP2016/063531 JP2016063531W WO2017191668A1 WO 2017191668 A1 WO2017191668 A1 WO 2017191668A1 JP 2016063531 W JP2016063531 W JP 2016063531W WO 2017191668 A1 WO2017191668 A1 WO 2017191668A1
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Prior art keywords
fiber
core layer
resin
impregnated
skin
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PCT/JP2016/063531
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English (en)
French (fr)
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吉田 武
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日産自動車株式会社
ルノー エス.ア.エス.
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Application filed by 日産自動車株式会社, ルノー エス.ア.エス. filed Critical 日産自動車株式会社
Priority to CN201680085306.9A priority Critical patent/CN109071836B/zh
Priority to US16/089,424 priority patent/US10723100B2/en
Priority to PCT/JP2016/063531 priority patent/WO2017191668A1/ja
Priority to EP16901055.0A priority patent/EP3453738A4/en
Priority to JP2018515369A priority patent/JP6564530B2/ja
Publication of WO2017191668A1 publication Critical patent/WO2017191668A1/ja

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/28Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/28Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer comprising a deformed thin sheet, i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/30Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer formed with recesses or projections, e.g. hollows, grooves, protuberances, ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/022Non-woven fabric
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/22Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • B32B5/26Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04Reinforcing macromolecular compounds with loose or coherent fibrous material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04Impregnation, embedding, or binder material
    • B32B2260/046Synthetic resin
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/10Fibres of continuous length
    • B32B2305/18Fabrics, textiles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/10Fibres of continuous length
    • B32B2305/20Fibres of continuous length in the form of a non-woven mat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2313/00Elements other than metals
    • B32B2313/04Carbon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00Vehicles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24521Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness with component conforming to contour of nonplanar surface
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628Nonplanar uniform thickness material

Definitions

  • the present invention relates to a fiber-reinforced resin molded product and a method for producing the same.
  • Patent Document 1 a core layer made of non-woven fabric is sandwiched between two carbon fiber layers forming a skin layer to form a laminate, and the laminate is impregnated with a resin for impregnation and cured. Material compacts are described.
  • Patent No. 4615398 gazette
  • the skin layer and the core layer are only bonded by the resin, the bonding force between the skin layer and the core layer is small, and the load is input to the carbon fiber composite body molded body. At the same time, the skin layer and the core layer may be separated between layers.
  • an object of this invention is to suppress that a skin layer and a core layer peel from each other by raising the bond strength of a skin layer and a core layer.
  • a first aspect of the present invention is a fiber-reinforced resin molded article comprising: a non-woven fabric and a core layer comprising an impregnated resin impregnated in the non-woven fabric; and a pair of skin layers comprising fibers and a matrix resin for covering the fibers.
  • the skin layer is formed on the surface on the core layer side, has a recess in which a part of the fiber is exposed from the matrix resin, and a part of the non-woven fabric and the impregnated resin is in the recess.
  • a second aspect of the present invention is a method of producing a fiber-reinforced resin molded article.
  • This manufacturing method comprises the steps of forming a recess in which a part of the fibers is exposed from the matrix resin on the surface on the core layer side of the skin layer, disposing the non-woven fabric between the pair of skin layers, And allowing the skin layer and the core layer to be joined together.
  • separation between the skin layer and the core layer can be suppressed by enhancing the bonding strength between the skin layer and the core layer.
  • FIG. 1 is an exploded perspective view of a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 2 is a cross-sectional view of a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 3A is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 3B is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 3C is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 3A is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 3B is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to
  • FIG. 3D is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 3E is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to an embodiment of the present invention.
  • FIG. 4A is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to another embodiment of the present invention.
  • FIG. 4: B is explanatory drawing of the manufacturing method of the fiber reinforced resin molded object which concerns on other embodiment of this invention.
  • FIG. 4C is an explanatory diagram of a method of manufacturing a fiber-reinforced resin molded product according to another embodiment of the present invention.
  • FIG. 4D is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to another embodiment of the present invention.
  • FIG. 4E is an explanatory view of a method of manufacturing a fiber-reinforced resin molded product according to another embodiment of the present invention.
  • a fiber-reinforced resin molded product 10 according to an embodiment of the present invention will be described based on FIGS. 1 to 3.
  • the fiber-reinforced resin molded body 10 can be applied to, for example, vehicle components such as a hood (bonnet), a door panel, a bumper, a trunk lid, a rear gate, a fender panel, a side body panel, and a roof panel.
  • vehicle components such as a hood (bonnet), a door panel, a bumper, a trunk lid, a rear gate, a fender panel, a side body panel, and a roof panel.
  • the fiber reinforced resin molded object 10 is not limited to the structural member for vehicles, It is possible to apply to various structural members.
  • the fiber reinforced resin molded object 10 is provided with the core layer 11 and a pair of outer skin layer 12 couple
  • the core layer 11 is a non-woven fabric layer including a non-woven fabric 13 and an impregnated resin 14 impregnated in the non-woven fabric 13.
  • the thickness of the core layer 11 is, for example, about 0.2 mm to 10.0 mm.
  • the non-woven fabric 13 is made of, for example, known fibers such as cotton, rayon, nylon, polyester, polypropylene, and aramid fibers.
  • the impregnated resin 14 is formed of, for example, a thermosetting resin such as an epoxy resin, an unsaturated polyester resin, a vinyl ester resin, or a phenol resin.
  • the impregnated resin 14 may be formed of, for example, a thermoplastic resin such as a polyamide resin, a polyolefin resin, a dicyclopentadiene resin, or a polyurethane resin.
  • the skin layer 12 is a fiber layer including fibers 15 and a matrix resin 16 covering the fibers 15. That is, the skin layer 12 is what is called a so-called FRP (fiber reinforced resin).
  • the thickness of the skin layer 12 is, for example, about 0.4 mm to 5.0 mm.
  • the fibers 15 are formed of various fibers such as, for example, carbon fibers, glass fibers, aramid fibers (Kevlar fibers).
  • the matrix resin 16 is formed of, for example, a thermosetting resin such as an epoxy resin, an unsaturated polyester resin, a vinyl ester resin, or a phenol resin.
  • the matrix resin 16 may be formed of, for example, a thermoplastic resin such as a polyamide resin, a polyolefin resin, a dicyclopentadiene resin, or a polyurethane resin.
  • the impregnated resin 14 of the core layer 11 and the matrix resin 16 of the skin layer 12 may be of the same type or different types. From the viewpoint of enhancing the bonding strength between the core layer 11 and the skin layer 12, it is preferable that the impregnated resin 14 of the core layer 11 and the matrix resin 16 of the skin layer 12 be a resin having high affinity.
  • the skin layer 12 is formed on the surface 17 on the core layer 11 side, and has a plurality of recesses 18 in which a part of the fibers 15 are exposed from the matrix resin 16. Then, the matrix resin 16 of the skin layer 12 and the impregnated resin 14 of the core layer 11 are bonded (adhered) in a state where the nonwoven fabric 13 and a part of the impregnated resin 14 enter each of the concave portions 18. For this reason, the fiber reinforced resin molded body 10 is formed in the joint part 19 of the core layer 11 and the skin layer 12, and is provided with a plurality of mixed regions 20 in which the non-woven fabric 13 and the fibers 15 are mixed.
  • the recesses 18 and the mixed regions 20 are spaced in the longitudinal and lateral directions in the plane of the skin layer 12 as can be seen from FIG. Although the recessed part 18 and the mixed area
  • the positions of the recess 18 and the mixed region 20 in the in-plane direction (the direction parallel to the surface) of the skin layer 12 are the core layer 11 in one and the other of the pair of skin layers 12 and 12. It is asymmetric with respect to That is, the concave portion 18 and the mixed region 20 are disposed at different positions in one and the other of the pair of skin layers 12 and 12.
  • the present invention is not limited to this, and the positions of the recess 18 and the mixed region 20 in the in-plane direction of the skin layer 12 are symmetrical with respect to the core layer 11 in one and the other of the pair of skin layers 12 and 12 It is also good.
  • the sheet or bundle of fibers 15 is coated with the wax 21 so as to be scattered, and the applied wax 21 is cured and solidified.
  • thermoplastic resins such as polyvinyl alcohol (PVA), polyethylene (PE), polypropylene (PP), for example. Since polyethylene and polypropylene have relatively low melting points, when these polyethylene and polypropylene are used as wax 21, the injection temperature of matrix resin 16 needs to be equal to or lower than the melting points of polyethylene and polypropylene.
  • the fibers 15 are placed in a mold, and the matrix resin 16 is injected into the mold to impregnate the fibers 15 with the matrix resin 16. Then, the impregnated matrix resin 16 is cured and hardened to produce the skin layer 12.
  • the recess 21 is formed in the skin layer 12 by melting the wax 21 with warm water or a solvent.
  • the lost wax manufacturing method is used as a method of forming the recess 18 in the skin layer 12.
  • the non-woven fabric 13 is laminated between the pair of skin layers 12, 12 to produce a laminate 22.
  • the laminate 22 is placed in a mold, and the impregnating resin 14 is injected into the mold to impregnate the nonwoven fabric 13 with the impregnating resin 14.
  • the nonwoven fabric 13 and a part of the impregnating resin 14 are inserted into each recess 18, and the nonwoven fabric 13 is entangled with the fibers 15 exposed by the removal of the wax 21.
  • the impregnated resin 14 is cured and solidified to produce the fiber-reinforced resin molded body 10.
  • an RTM molding method (Resin Transfer Molding) is used as a method of molding the laminate 22.
  • the fiber-reinforced resin molded product 10 includes the non-woven fabric 13 and the core layer 11 including the impregnated resin 14 impregnated in the non-woven fabric 13 and the matrix resin 16 covering the fibers 15 and 15 And a pair of skin layers 12, 12 bonded to both sides of the layer 11.
  • the skin layer 12 is formed on the surface 17 on the core layer 11 side, has a recess 18 in which a part of the fiber 15 is exposed from the matrix resin 16, and a part of the non-woven fabric 13 and the impregnated resin 14 enter the recess 18.
  • the matrix resin 16 of the skin layer 12 and the impregnated resin 14 of the core layer 11 are in a state in which the nonwoven fabric 13 and a part of the impregnated resin 14 enter each recess 18. It is combined. That is, the mixed region 20 in which the non-woven fabric 13 and the fibers 15 are mixed is formed at the bonding portion 19 between the core layer 11 and the skin layer 12. For this reason, the bond strength between the skin layer 12 and the core layer 11 can be enhanced, and there is a possibility that the skin layer 12 and the core layer 11 may be separated between layers even if a load is input to the fiber reinforced resin molded body 10 It can be reduced.
  • the fiber-reinforced resin molded product 10 it is possible to suppress the peeling of the skin layer 12 and the core layer 11 by enhancing the bonding force between the skin layer 12 and the core layer 11 It is possible.
  • the position in the in-plane direction of the skin layer 12 of the mixed region 20 in which the non-woven fabric 13 and the fibers 15 are mixed can be shifted between one and the other of the pair of skin layers 12 and 12, and the density of the non-woven fabric 13 is low. It is possible to suppress the occurrence of locations in the core layer 11.
  • the step of forming the recess 18 where a part of the fiber 15 is exposed from the matrix resin 16 is formed on the surface 17 of the skin layer 12 on the core layer 11 side.
  • the nonwoven fabric 13 is disposed between the pair of skin layers 12 and 12 and at the same time, the nonwoven fabric 13 and a part of the impregnated resin 14 are made to enter the recess 18 and the skin layer 12 and the core layer 11 in that state.
  • a step of combining step 2.
  • the matrix resin 16 of the skin layer 12 and the impregnating resin 14 of the core layer 11 are bonded in a state where the nonwoven fabric 13 and a part of the impregnating resin 14 are intruding into the respective concave portions 18. That is, a mixed region 20 in which the non-woven fabric 13 and the fibers 15 are mixed is formed at the bonding portion 19 between the core layer 11 and the skin layer 12. For this reason, the bond strength between the skin layer 12 and the core layer 11 can be enhanced, and there is a possibility that the skin layer 12 and the core layer 11 may be separated between layers even if a load is input to the fiber reinforced resin molded body 10 It can be reduced.
  • the separation between the skin layer 12 and the core layer 11 is suppressed by enhancing the bonding force between the skin layer 12 and the core layer 11 It is possible.
  • the recess 18 is formed by the lost wax manufacturing method.
  • wax 21 is applied so as to be scattered on a sheet or bundle of fibers 15, and the applied wax 21 is cured and solidified.
  • the fibers 15 are placed in a mold, and the matrix resin 16 is injected into the mold to impregnate the fibers 15 with the matrix resin 16. Then, the impregnated matrix resin 16 is cured and hardened to produce the skin layer 12.
  • the recess 21 is formed in the skin layer 12 by melting the wax 21 with warm water or a solvent.
  • a non-woven fabric-containing adhesive (non-woven fabric 13 impregnated with the impregnating resin 14 in advance) is laminated between the pair of skin layers 12, 12 to produce a laminate 23.
  • the laminate 23 is placed in a mold, and the fiber-reinforced resin molding 10 is molded in the mold.
  • the nonwoven fabric 13 and a part of the impregnated resin 14 are introduced into the respective recesses 18 and the nonwoven fabric 13 is entangled with the exposed fibers 15 by the removal of the wax 21.
  • the impregnated resin 14 is cured and solidified to produce the fiber-reinforced resin molded body 10.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Materials Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

繊維強化樹脂成形体(10)は、不織布(13)および不織布(13)に含浸された含浸樹脂(14)を含むコア層(11)と、繊維(15)および繊維(15)を被覆するマトリックス樹脂(16)を含み、コア層(11)の両面に結合された一対の表皮層(12,12)と、備える。表皮層(12)は、コア層(11)側の面(17)に形成され、繊維(15)の一部がマトリックス樹脂(16)から露出する凹部(18)を有し、凹部(18)に、不織布(13)および含浸樹脂(14)の一部が入り込んでいる。

Description

繊維強化樹脂成形体およびその製造方法
 本発明は、繊維強化樹脂成形体およびその製造方法に関する。
 従来から、複合材料の一種であるFRP(Fiber Reinforced Plastics)を含んで構成される繊維強化樹脂成形体が公知である(例えば、特許文献1参照)。
 特許文献1には、表皮層を形成する2層の炭素繊維層の間に不織布からなるコア層が挟持されて積層体をなし、この積層体に含浸用樹脂を含浸して硬化した炭素繊維複合材料成形体が記載されている。
特許第4615398号公報
 前述の炭素繊維複合材料成形体では、表皮層とコア層とは樹脂によって結合されるだけであるので、表皮層とコア層との結合力が小さく、荷重が炭素繊維複合材料成形体に入力された際に、表皮層とコア層とが層間で剥離する可能性がある。
 そこで、本発明は、表皮層とコア層との結合力を高めることにより、表皮層とコア層とが剥離することを抑制することを目的とする。
 本発明の第1の態様は、不織布および不織布に含浸された含浸樹脂を含むコア層と、繊維および繊維を被覆するマトリックス樹脂を含む一対の表皮層と、備える繊維強化樹脂成形体である。表皮層は、コア層側の面に形成され、繊維の一部がマトリックス樹脂から露出する凹部を有し、凹部に、不織布および含浸樹脂の一部が入り込んでいる。
 本発明の第2の態様は、繊維強化樹脂成形体の製造方法である。この製造方法は、表皮層のコア層側の面に、繊維の一部がマトリックス樹脂から露出する凹部を形成する工程と、一対の表皮層の間に不織布を配置するとともに、不織布および含浸樹脂の一部を凹部に入り込ませ、その状態で表皮層とコア層とを結合する工程と、を備える。
 本発明によれば、表皮層とコア層との結合力を高めることにより、表皮層とコア層とが剥離することを抑制することができる。
図1は、本発明の実施形態に係る繊維強化樹脂成形体の分解斜視図である。 図2は、本発明の実施形態に係る繊維強化樹脂成形体の断面図である。 図3Aは、本発明の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図3Bは、本発明の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図3Cは、本発明の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図3Dは、本発明の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図3Eは、本発明の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図4Aは、本発明の他の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図4Bは、本発明の他の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図4Cは、本発明の他の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図4Dは、本発明の他の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。 図4Eは、本発明の他の実施形態に係る繊維強化樹脂成形体の製造方法の説明図である。
 以下、本発明の実施形態を図面とともに詳述する。
 本発明の実施形態に係る繊維強化樹脂成形体10を、図1から図3に基づいて説明する。
 繊維強化樹脂成形体10は、例えば、フード(ボンネット)、ドアパネル、バンパー、トランクリッド、リアゲート、フェンダパネル、サイドボディパネル、ルーフパネルなどの車両用構成部材に適用することができる。また、繊維強化樹脂成形体10は、車両用構成部材に限定されず、各種構成部材に適用することが可能である。
 図1および図2に示すように、繊維強化樹脂成形体10は、コア層11と、コア層11の両面に結合された一対の表皮層12,12と、備える。
 コア層11は、不織布13と、不織布13に含浸された含浸樹脂14とを含んで構成される不織布層である。コア層11の厚さは、例えば、0.2mm~10.0mm程度の厚さとされる。不織布13は、例えば、綿、レーヨン、ナイロン、ポリエステル、ポリプロピレン、アラミド繊維など、公知の繊維により形成される。含浸樹脂14は、例えば、エポキシ樹脂、不飽和ポリエステル樹脂、ビニルエステル樹脂、フェノール樹脂などの熱硬化性樹脂により形成される。また、含浸樹脂14は、例えば、ポリアミド樹脂、ポリオレフィン樹脂、ジシクロペンタジエン樹脂、ポリウレタン樹脂などの熱可塑性樹脂により形成されてもよい。
 表皮層12は、繊維15と、繊維15を被覆するマトリックス樹脂16とを含んで構成される繊維層である。すなわち、表皮層12は、いわゆるFRP(繊維強化樹脂)と称されるものである。表皮層12の厚さは、例えば、0.4mm~5.0mm程度の厚さとされる。繊維15は、例えば、炭素繊維、ガラス繊維、アラミド繊維(ケブラー繊維)など、種々の繊維により形成される。マトリックス樹脂16は、例えば、エポキシ樹脂、不飽和ポリエステル樹脂、ビニルエステル樹脂、フェノール樹脂などの熱硬化性樹脂により形成される。また、マトリックス樹脂16は、例えば、ポリアミド樹脂、ポリオレフィン樹脂、ジシクロペンタジエン樹脂、ポリウレタン樹脂などの熱可塑性樹脂により形成されてもよい。
 コア層11の含浸樹脂14と表皮層12のマトリックス樹脂16とは、同じ種類のものであってもよく、異なる種類のものであってもよい。コア層11と表皮層12との結合力を高めるという観点からは、コア層11の含浸樹脂14と表皮層12のマトリックス樹脂16とは親和性の高い樹脂であることが好ましい。
 表皮層12は、コア層11側の面17に形成され、繊維15の一部がマトリックス樹脂16から露出する複数の凹部18を有する。そして、各凹部18に不織布13および含浸樹脂14の一部が入り込んでいる状態で、表皮層12のマトリックス樹脂16とコア層11の含浸樹脂14とが結合(接着)されている。このため、繊維強化樹脂成形体10は、コア層11と表皮層12との結合部19に形成され、不織布13と繊維15とが混在する複数の混在領域20を備えている。
 凹部18および混在領域20は、図1から分かるように、表皮層12の面内の縦方向および横方向に間隔をおいて配設されている。凹部18および混在領域20は、図示例では等間隔で配設されているが、これに限定はされず、等間隔で配設されていなくてもよい。
 また、表皮層12の面内方向(面と平行な方向)における凹部18および混在領域20の位置は、図2から分かるように、一対の表皮層12,12の一方と他方とでコア層11に対して非対称である。すなわち、凹部18および混在領域20は、一対の表皮層12,12の一方と他方とで異なる箇所に配設されている。しかしながら、これに限定はされず、表皮層12の面内方向における凹部18および混在領域20の位置は、一対の表皮層12,12の一方と他方とでコア層11に対して対称であってもよい。
 次に、本実施形態に係る繊維強化樹脂成形体10の製造方法を説明する。
 1.ワックスの塗布
 まず、図3Aに示すように、繊維15のシートまたは束にワックス21を点在するように塗布し、塗布したワックス21を硬化させて固める。
 ワックス21としては、例えば、ポリビニルアルコール(PVA)、ポリエチレン(PE)、ポリプロピレン(PP)などの熱可塑性樹脂を使用することが可能である。ポリエチレンおよびポリプロピレンは比較的融点が低いので、これらポリエチレンおよびポリプロピレンをワックス21として使用する場合、マトリックス樹脂16の注入温度はポリエチレンおよびポリプロピレンの融点以下にする必要がある。
 2.マトリックス樹脂の型内への注入
 次に、図3Bに示すように、繊維15を型内に配置し、当該型内にマトリックス樹脂16を注入して、繊維15にマトリックス樹脂16を含浸させる。そして、含浸させたマトリックス樹脂16を硬化させて固めて、表皮層12を作製する。
 3.ワックスの除去
 次に、図3Cに示すように、ワックス21を温水または溶剤によって溶かすことにより、表皮層12に凹部18を形成する。
 すなわち、本実施形態では、凹部18を表皮層12に形成する方法には、ロストワックス製法を用いている。
 4.積層
 次に、図3Dに示すように、一対の表皮層12,12の間に不織布13を積層して、積層体22を作製する。
 5.含浸樹脂の型内への注入
 次に、図3Eに示すように、積層体22を型内に配置し、当該型内に含浸樹脂14を注入して、不織布13に含浸樹脂14を含浸させる。この含浸樹脂14を型内に注入する工程において、各凹部18に不織布13および含浸樹脂14の一部を入り込ませ、ワックス21の除去により露出した繊維15に不織布13を絡ませる。そして、含浸樹脂14を硬化させて固めて、繊維強化樹脂成形体10を作製する。
 すなわち、本実施形態では、積層体22を成形する方法には、RTM成形法(Resin Transfer Molding)を用いている。
 以下に、本実施形態による作用効果を説明する。
 (1)本実施形態に係る繊維強化樹脂成形体10は、不織布13および不織布13に含浸された含浸樹脂14を含むコア層11と、繊維15および繊維15を被覆するマトリックス樹脂16を含み、コア層11の両面に結合された一対の表皮層12,12と、備える。表皮層12は、コア層11側の面17に形成され、繊維15の一部がマトリックス樹脂16から露出する凹部18を有し、凹部18に、不織布13および含浸樹脂14の一部が入り込んでいる。
 本実施形態に係る繊維強化樹脂成形体10では、各凹部18に不織布13および含浸樹脂14の一部が入り込んでいる状態で、表皮層12のマトリックス樹脂16とコア層11の含浸樹脂14とが結合されている。すなわち、コア層11と表皮層12との結合部19に、不織布13と繊維15とが混在する混在領域20が形成されている。このため、表皮層12とコア層11との結合力を高めることができ、荷重が繊維強化樹脂成形体10に入力されても、表皮層12とコア層11とが層間で剥離する可能性を低減することができる。
 したがって、本実施形態に係る繊維強化樹脂成形体10によれば、表皮層12とコア層11との結合力を高めることにより、表皮層12とコア層11とが剥離することを抑制することが可能である。
 (2)表皮層12の面内方向における凹部18の位置は、一対の表皮層12,12の一方と他方とでコア層11に対して非対称である。
 これにより、不織布13と繊維15とが混在する混在領域20の表皮層12の面内方向における位置を一対の表皮層12,12の一方と他方とでずらすことができ、不織布13の密度の低い箇所がコア層11に生じることを抑制することが可能である。
 (3)本実施形態に係る繊維強化樹脂成形体10の製造方法は、表皮層12のコア層11側の面17に、繊維15の一部がマトリックス樹脂16から露出する凹部18を形成する工程(第1工程)と、一対の表皮層12,12の間に不織布13を配置するとともに、不織布13および含浸樹脂14の一部を凹部18に入り込ませ、その状態で表皮層12とコア層11とを結合する工程(第2工程)と、を備える。
 これにより、各凹部18に不織布13および含浸樹脂14の一部が入り込んでいる状態で、表皮層12のマトリックス樹脂16とコア層11の含浸樹脂14とが結合される。すなわち、コア層11と表皮層12との結合部19に、不織布13と繊維15とが混在する混在領域20が形成される。このため、表皮層12とコア層11との結合力を高めることができ、荷重が繊維強化樹脂成形体10に入力されても、表皮層12とコア層11とが層間で剥離する可能性を低減することができる。
 したがって、本実施形態に係る繊維強化樹脂成形体10の製造方法によれば、表皮層12とコア層11との結合力を高めることにより、表皮層12とコア層11とが剥離することを抑制することが可能である。
 (4)凹部18をロストワックス製法により形成する。
 これにより、凹部18を表皮層12に精度よく形成することが可能である。
 [他の実施形態]
 次に、他の実施形態に係る繊維強化樹脂成形体10の製造方法を図4に基づいて説明する。
 1.ワックスの塗布
 まず、図4Aに示すように、繊維15のシートまたは束にワックス21を点在するように塗布し、塗布したワックス21を硬化させて固める。
 2.マトリックス樹脂の型内への注入
 次に、図4Bに示すように、繊維15を型内に配置し、当該型内にマトリックス樹脂16を注入して、繊維15にマトリックス樹脂16を含浸させる。そして、含浸させたマトリックス樹脂16を硬化させて固めて、表皮層12を作製する。
 3.ワックスの除去
 次に、図4Cに示すように、ワックス21を温水または溶剤によって溶かすことにより、表皮層12に凹部18を形成する。
 4.積層
 次に、図4Dに示すように、一対の表皮層12,12の間に、不織布入り接着剤(含浸樹脂14が予め含浸された不織布13)を積層して、積層体23を作製する。
 5.繊維強化樹脂成形体の成形
 次に、図4Eに示すように、積層体23を型内に配置し、当該型内で繊維強化樹脂成形体10を成形する。この繊維強化樹脂成形体10を型内で成形する工程において、各凹部18に不織布13および含浸樹脂14の一部を入り込ませ、ワックス21の除去により露出した繊維15に不織布13を絡ませる。そして、含浸樹脂14を硬化させて固めて、繊維強化樹脂成形体10を作製する。
 この実施形態では、繊維強化樹脂成形体10を成形する方法には、ホットプレス成形法やオートクレーブ成形法を用いることが可能である。
 このような繊維強化樹脂成形体10の製造方法によっても、表皮層12とコア層11との結合力を高めることにより、表皮層12とコア層11とが剥離することを抑制することが可能である。
 以上、実施例に沿って本発明の内容を説明したが、本発明はこれらの記載に限定されるものではなく、種々の変形及び改良が可能であることは、当業者には自明である。
10 繊維強化樹脂成形体
11 コア層
12 表皮層
13 不織布
14 含浸樹脂
15 繊維
16 マトリックス樹脂
17 コア層側の面
18 凹部
19 結合部
20 混在領域

Claims (5)

  1.  不織布および前記不織布に含浸された含浸樹脂を含むコア層と、
     繊維および前記繊維を被覆するマトリックス樹脂を含み、前記コア層の両面に結合された一対の表皮層と、備え、
     前記表皮層は、前記コア層側の面に形成され、前記繊維の一部が前記マトリックス樹脂から露出する凹部を有し、
     前記凹部に、前記不織布および前記含浸樹脂の一部が入り込んでいる
     ことを特徴とする繊維強化樹脂成形体。
  2.  前記表皮層の面内方向における前記凹部の位置は、前記一対の表皮層の一方と他方とで前記コア層に対して非対称である
     ことを特徴とする請求項1に記載の繊維強化樹脂成形体。
  3.  不織布および前記不織布に含浸された含浸樹脂を含むコア層と、
     繊維および前記繊維を被覆するマトリックス樹脂を含み、前記コア層を間に挟んで結合された一対の表皮層と、
     前記コア層と前記表皮層との結合部に形成され、前記不織布と前記繊維とが混在する混在領域と、を備える
     ことを特徴とする繊維強化樹脂成形体。
  4.  不織布および前記不織布に含浸された含浸樹脂を含むコア層と、繊維および前記繊維を被覆するマトリックス樹脂を含み、前記コア層の両面に結合された一対の表皮層と、備える繊維強化樹脂成形体を製造する方法であって、
     前記表皮層の前記コア層側の面に、前記繊維の一部が前記マトリックス樹脂から露出する凹部を形成する工程と、
     前記一対の表皮層の間に前記不織布を配置するとともに、前記不織布および前記含浸樹脂の一部を前記凹部に入り込ませ、その状態で前記表皮層と前記コア層とを結合する工程と、を備える
     ことを特徴とする繊維強化樹脂成形体の製造方法。
  5.  前記凹部をロストワックス製法により形成する
     ことを特徴とする請求項4に記載の繊維強化樹脂成形体の製造方法。
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EP3453738A4 (en) 2019-05-08
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