JPWO2016198884A5 - - Google Patents
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- JPWO2016198884A5 JPWO2016198884A5 JP2018516642A JP2018516642A JPWO2016198884A5 JP WO2016198884 A5 JPWO2016198884 A5 JP WO2016198884A5 JP 2018516642 A JP2018516642 A JP 2018516642A JP 2018516642 A JP2018516642 A JP 2018516642A JP WO2016198884 A5 JPWO2016198884 A5 JP WO2016198884A5
- Authority
- JP
- Japan
- Prior art keywords
- core portion
- central core
- microspheres
- unit load
- load device
- 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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- 239000004005 microsphere Substances 0.000 claims description 15
- 239000000835 fiber Substances 0.000 claims description 11
- 230000002787 reinforcement Effects 0.000 claims description 9
- 239000011159 matrix material Substances 0.000 claims description 8
- 239000002131 composite material Substances 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 5
- 230000002093 peripheral Effects 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 3
- 210000000088 Lip Anatomy 0.000 claims 1
- 210000003850 cellular structures Anatomy 0.000 claims 1
- 239000011162 core material Substances 0.000 description 16
- 239000006260 foam Substances 0.000 description 6
- 239000002245 particle Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 210000003660 Reticulum Anatomy 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000001413 cellular Effects 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Description
好適には、粒子そのものは、コアの30容量%~74容量%を構成してよく、より好適には、コアの50容量%~70容量%を構成してもよい。コアの強度と重量とのバランスをとるためには、コアの大部分が、マトリックス材料内に保持された粒子から成ることが好適である。 Suitably, the particles themselves may constitute 30% to 74% by volume of the core , more suitably 50% to 70% by volume of the core . In order to balance the strength and weight of the core, it is preferred that the majority of the core consist of particles held within a matrix material.
好適には、パネルの縁部において、粒子が短繊維補強材など他の材料にほぼ置換されるように、コアの構造体を変更することができる。短繊維補強材は、短繊維補強材そのものがコアの0容量%~40容量%を構成し得るように、そのコア中の少なくとも一部、又は全部の粒子を置換することができる。 Advantageously, the structure of the core can be modified so that at the edges of the panel the particles are largely replaced by other materials such as short fiber reinforcement. The short fiber reinforcement can replace at least some or all of the particles in the core such that the short fiber reinforcement itself can constitute 0% to 40% by volume of the core.
複合フォームコア3は、軽量な中空ガラスミクロスフェアを含有するマトリックス材料から製造される。このミクロスフェアの大部分は、40μm以下、好適には9~25μmの範囲の直径及び/又は40MPa超の圧潰強度を有する。複合フォームコア3は、50~70容量%のミクロスフェアを含み、そのミクロスフェアはエポキシ樹脂マトリックス材料によって囲まれている。 The composite foam core 3 is manufactured from a matrix material containing lightweight hollow glass microspheres. The majority of the microspheres have a diameter of 40 μm or less, preferably in the range of 9-25 μm and/or a crush strength of greater than 40 MPa. The composite foam core 3 contains 50-70% by volume microspheres surrounded by an epoxy resin matrix material.
図4に示すように、一実施形態において、パネルの周縁部における複合フォームの組成は、ミクロスフェアが減少して0%となり、次いで、その複合フォームの最大40容量%を構成する短繊維補強材7によって置換されるものである。このような実施形態は、平均100μmの繊維長を有するミルド炭素繊維補強材を使用するが、短繊維は、炭素繊維、アラミド繊維、玄武岩繊維、及び/又はファイバガラス繊維であってよい。中央パネルコアから周縁部への組成における変更を容易にするために、周縁領域はセル状ハニカムを含有し得る。これは、中央複合フォームコアの残りから、局所的に変更されたコア材料を仕切る。これに代えて、短繊維補強材は中央コア内にのみ配置されることができるか、又はコアと周縁の縁部領域との両方において使用されることができる。 As shown in FIG. 4, in one embodiment, the composition of the composite foam at the perimeter of the panel is reduced to 0% microspheres, followed by short fiber reinforcement comprising up to 40% by volume of the composite foam. It is replaced by material 7. Such embodiments use milled carbon fiber reinforcement with an average fiber length of 100 μm, but the staple fibers may be carbon, aramid, basalt, and/or fiberglass fibers. The peripheral region may contain cellular honeycomb to facilitate changes in composition from the central panel core to the peripheral edge. This partitions the locally modified core material from the rest of the central composite foam core. Alternatively, short fiber reinforcements can be placed only in the central core, or can be used in both the core and the peripheral edge regions.
本発明の他の実施形態では、中央コア構造体の50%超を構成する複合フォームは、少なくてコアの30容量%であり最大で74容量%の、マイクロメートルスケールのミクロスフェアを含む。このミクロスフェアは、中実又は中空であってよく、ガラス材料、炭素材料、金属材料、ポリマー材料、又はセラミック材料から製造され得る。 In another embodiment of the invention, the composite foam comprising more than 50% of the central core structure comprises at least 30% and at most 74% by volume of the core micrometer-scale microspheres. The microspheres can be solid or hollow and can be made from glass, carbon, metal, polymer, or ceramic materials.
Claims (11)
繊維補強材料を含む上面層と、
繊維補強材料を含む下面層と、
中央コア部分であって、前記中央コア部分は、マトリックス材料中において固着された複数のミクロスフェアを含み、そのミクロスフェアは前記中央コア部分の30容量%~74容量%を構成する、中央コア部分と、を含んで成り、
前記上面層と前記下面層とには、前記上面層と前記下面層とを前記中央コア部分に対して固着させる前記マトリックス材料が設けられ、
前記30容量%~74容量%のミクロスフェアは40μm未満の直径を有し、
前記下面層は前記ユニットロードデバイスの底面側に設けられ、
前記中央コア部分は、少なくとも部分的に前記30容量%~74容量%のミクロスフェアで充填されているセル状構造体を含んで成る、ユニットロードデバイス。 A unit load device having a base panel, the base panel comprising:
a top layer comprising a fiber reinforcement material;
a bottom layer comprising a fiber reinforcement material;
A central core portion, said central core portion comprising a plurality of microspheres anchored in a matrix material, said microspheres comprising 30% to 74% by volume of said central core portion. comprising a part and
the top layer and the bottom layer are provided with the matrix material for securing the top layer and the bottom layer to the central core portion;
30% to 74% by volume of the microspheres have a diameter of less than 40 μm;
the bottom layer is provided on the bottom side of the unit load device;
A unit load device, wherein said central core portion comprises a cellular structure at least partially filled with said 30% to 74% by volume microspheres.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1510082.9 | 2015-06-10 | ||
GB1510082.9A GB2539392B (en) | 2015-06-10 | 2015-06-10 | A composite sandwich structure |
PCT/GB2016/051718 WO2016198884A2 (en) | 2015-06-10 | 2016-06-10 | A composite sandwich structure |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2018527265A JP2018527265A (en) | 2018-09-20 |
JPWO2016198884A5 true JPWO2016198884A5 (en) | 2022-08-01 |
JP7148132B2 JP7148132B2 (en) | 2022-10-05 |
Family
ID=53785249
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2018516642A Active JP7148132B2 (en) | 2015-06-10 | 2016-06-10 | Composite sandwich structure |
Country Status (10)
Country | Link |
---|---|
US (1) | US10780678B2 (en) |
EP (1) | EP3307607A2 (en) |
JP (1) | JP7148132B2 (en) |
CN (1) | CN107921725B (en) |
AU (1) | AU2016275292B2 (en) |
CA (1) | CA3026980C (en) |
GB (1) | GB2539392B (en) |
SG (1) | SG11201811818QA (en) |
TW (1) | TWI730964B (en) |
WO (1) | WO2016198884A2 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA3148693C (en) | 2014-06-04 | 2023-08-15 | Sti Holdings, Inc. | Composite panel edge treatments and joints and cargo body having same |
US9896137B2 (en) * | 2016-02-25 | 2018-02-20 | Nexgen Composites Llc | Unitary floor |
US10315799B2 (en) * | 2017-08-31 | 2019-06-11 | Aemerge, LLC | Palletized integrated box |
US10814581B2 (en) | 2018-07-03 | 2020-10-27 | STI Holdings, Iinc. | Composite sidewall and cargo body having same |
US11136072B2 (en) | 2018-08-07 | 2021-10-05 | Sti Holdings, Inc. | Cargo body with recessed logistics track |
US10889336B2 (en) * | 2018-12-17 | 2021-01-12 | Ford Global Technologies, Llc | Polymeric vehicle floor |
CN112223874A (en) * | 2019-08-22 | 2021-01-15 | 尹君 | Method for producing a continuous three-dimensional reinforcing structure from a microporous material |
CN111516761B (en) * | 2020-04-20 | 2022-10-11 | 重庆长安汽车股份有限公司 | Carbon fiber composite material automobile front floor, manufacturing method and automobile |
IT202000013177A1 (en) * | 2020-06-04 | 2021-12-04 | Andrea Nespoli | SANDWICH PANEL USABLE IN THE FURNISHING SECTOR AND METHOD FOR THE PRODUCTION OF SAID PANEL |
CN113601693B (en) * | 2021-10-11 | 2021-12-28 | 佛山市东鹏陶瓷有限公司 | Process technology for preparing strengthened and toughened rock plate by layering distribution |
JP2023145101A (en) * | 2022-03-28 | 2023-10-11 | 盟和産業株式会社 | Laminated plate |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2153309A1 (en) * | 1970-10-30 | 1972-05-04 | Kureha Kagaku Kogyo K.K., Tokio- | Sandwich panel and process for its manufacture |
US4013810A (en) * | 1975-08-22 | 1977-03-22 | The Babcock & Wilcox Company | Sandwich panel construction |
US4250136A (en) * | 1979-10-22 | 1981-02-10 | Composite Technology Corporation | Method of forming a composite structure |
DE3126242A1 (en) * | 1981-07-03 | 1983-01-20 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Moulding of sandwich construction and semi-finished product for the production thereof |
LU87866A1 (en) * | 1990-01-04 | 1991-05-07 | Piero Dr Ing Cresti | FLOOR FOR VEHICLES AND INDUSTRIAL TRANSPORT CONTAINERS, THERMALLY INSULATED, WITH LAMINATE POLYESTER-FIBER RESIN COATING AND STRUCTURE, AND WITH THE REMOVAL OF NON-HOMOGENEOUS MATERIALS WITH RESINS |
US5773121A (en) * | 1994-07-29 | 1998-06-30 | Isorca Inc. | Syntactic foam core incorporating honeycomb structure for composites |
JP2003226268A (en) | 2002-02-07 | 2003-08-12 | Toray Ind Inc | Truck parts, and manufacturing method thereof |
TW200635830A (en) * | 2004-12-29 | 2006-10-16 | Hunter Paine Entpr Llc | Composite structural material and method of making the same |
US20070101679A1 (en) | 2005-10-25 | 2007-05-10 | L&L Products, Inc. | Panel structure |
DE102006056167B4 (en) * | 2006-11-28 | 2011-04-14 | Fachhochschule Landshut | Lightweight molded part with support core and corresponding manufacturing process |
JP2008290441A (en) | 2007-04-25 | 2008-12-04 | Sekisui Chem Co Ltd | Manufacturing method of sandwich material made of reinforced plastic |
WO2009015228A1 (en) | 2007-07-23 | 2009-01-29 | Sunrez Corporation | Sandwich panel end effectors |
US9248958B2 (en) | 2011-12-27 | 2016-02-02 | Advanced Composite Structures, Llc | Air cargo container |
US8776698B2 (en) * | 2012-10-08 | 2014-07-15 | Advanced Composite Structures, Llc | Composite air cargo pallet |
-
2015
- 2015-06-10 GB GB1510082.9A patent/GB2539392B/en active Active
-
2016
- 2016-06-10 WO PCT/GB2016/051718 patent/WO2016198884A2/en active Application Filing
- 2016-06-10 CN CN201680033846.2A patent/CN107921725B/en active Active
- 2016-06-10 SG SG11201811818QA patent/SG11201811818QA/en unknown
- 2016-06-10 JP JP2018516642A patent/JP7148132B2/en active Active
- 2016-06-10 EP EP16738493.2A patent/EP3307607A2/en active Pending
- 2016-06-10 AU AU2016275292A patent/AU2016275292B2/en active Active
- 2016-06-10 US US15/580,758 patent/US10780678B2/en active Active
- 2016-06-10 CA CA3026980A patent/CA3026980C/en active Active
- 2016-06-13 TW TW105118386A patent/TWI730964B/en active
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