CN101500771A - 制造复合材料的方法及装置 - Google Patents
制造复合材料的方法及装置 Download PDFInfo
- Publication number
- CN101500771A CN101500771A CNA2007800293797A CN200780029379A CN101500771A CN 101500771 A CN101500771 A CN 101500771A CN A2007800293797 A CNA2007800293797 A CN A2007800293797A CN 200780029379 A CN200780029379 A CN 200780029379A CN 101500771 A CN101500771 A CN 101500771A
- Authority
- CN
- China
- Prior art keywords
- matrix
- sheet material
- described method
- irradiation
- fibre sheet
- 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.)
- Pending
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 15
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 12
- 239000011159 matrix material Substances 0.000 claims abstract description 54
- 238000000034 method Methods 0.000 claims abstract description 36
- 239000000835 fiber Substances 0.000 claims description 45
- 239000000463 material Substances 0.000 claims description 42
- 239000000945 filler Substances 0.000 claims description 10
- 238000005470 impregnation Methods 0.000 claims description 7
- 230000005855 radiation Effects 0.000 claims description 7
- 238000009434 installation Methods 0.000 claims description 3
- 241000094396 Bolitoglossa carri Species 0.000 claims 4
- 230000001678 irradiating effect Effects 0.000 abstract 1
- 239000012528 membrane Substances 0.000 description 12
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 230000004888 barrier function Effects 0.000 description 5
- 229920001169 thermoplastic Polymers 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000009832 plasma treatment Methods 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 150000003254 radicals Chemical class 0.000 description 4
- 239000004416 thermosoftening plastic Substances 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 238000007598 dipping method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000004744 fabric Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- 239000004696 Poly ether ether ketone Substances 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 150000001336 alkenes Chemical class 0.000 description 2
- 150000001345 alkine derivatives Chemical class 0.000 description 2
- 238000010923 batch production Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 229940110728 nitrogen / oxygen Drugs 0.000 description 2
- 229920002530 polyetherether ketone Polymers 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 230000009183 running Effects 0.000 description 2
- 241000894007 species Species 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 241000446313 Lamella Species 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 239000011147 inorganic material Substances 0.000 description 1
- 239000013067 intermediate product Substances 0.000 description 1
- JRZJOMJEPLMPRA-UHFFFAOYSA-N olefin Natural products CCCCCCCC=C JRZJOMJEPLMPRA-UHFFFAOYSA-N 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C59/00—Surface shaping of articles, e.g. embossing; Apparatus therefor
- B29C59/14—Surface shaping of articles, e.g. embossing; Apparatus therefor by plasma treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
- B29B15/12—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
- B29B15/12—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length
- B29B15/122—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length with a matrix in liquid form, e.g. as melt, solution or latex
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
- B29C70/506—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands and impregnating by melting a solid material, e.g. sheet, powder, fibres
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249924—Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Reinforced Plastic Materials (AREA)
- Chemical Or Physical Treatment Of Fibers (AREA)
- Treatments Of Macromolecular Shaped Articles (AREA)
Abstract
本发明涉及制造复合片材的装置和方法,所述方法包括:a.在基本上为大气压的压力下以等离子体在辐照区(33)辐照纤维片材(20)和/或基质(11、13),和b.在粘接区(32)以所述基质浸渍所述纤维片材;其中,工序a.和工序b.同时进行。
Description
技术领域
本发明涉及制造复合材料的方法和装置。
背景技术
在US5108780中,强化丝的单根纤维在以热塑性涂料涂覆之前在真空室中用等离子体辐照。以热塑性涂料立即涂覆经等离子体处理的纤维产生了比当纤维在被涂覆前即暴露于空气或其它自由基淬灭物种时更强的界面抗剪强度。
JP2005171432的摘要描述了用于聚合物复合物强化的纤维的制造方法。该纤维在常压下经受第一等离子体处理,随后于常压下在含有气态烯烃或炔烃的介质中经受第二等离子体处理。在等离子体处理之后施以粘合剂。
发明内容
本发明的第一方案提供了制造复合片材的方法,该方法包括:
a.在基本上为大气压的压力下以等离子体在辐照区辐照纤维片材和/
或基质,和
b.在粘接区以所述基质浸渍所述纤维片材;
其中,工序a.和b.同时进行。
本发明的第一方案辐照纤维片材(而不是单根纤维)并且同时进行浸渍工序从而产生以基质浸渍过的纤维片材(通常在本领域中称为“预浸料”)。这与只生产纤维的单丝的上述在先技术形成了对比。本方法使得不必以中间产品(例如US5108780中的热塑性涂料或者JP2005171432中的烯烃/炔烃)处理纤维就能形成片材。
所述纤维片材可以完全浸渍,也可以只有部分浸渍从而形成所谓的“部分预浸料”。
在基本上为大气压的压力下辐照是指辐照区不需要特殊的封闭体系。
通常来说工序b也在基本上为大气压的压力下进行,通常是在空气中进行。这与需要在受控环境中(即,在真空中或者惰性气体中)涂覆纤维的US5108780的教导相反。
可以通过施用流体基质熔融物来浸渍所述纤维片材,所述基质也可以在工序b期间处于片状。直接施用流体基质熔融物提供了可省去加工步骤(形成基质片材)的优势。然而,优选的是使用基质片材,这是因为这对常规制造方法需要的修改较少,使得基质更容易被辐照,并且如果需要,可制备部分预浸料。
优选所述纤维片材和/或所述基质在步骤a期间保持移动,并且优选所述纤维片材在步骤b期间保持移动。这提高了该方法的速度,并且确保均匀的辐照。
优选该方法进一步包括用少于30秒将所述纤维片材和/或所述基质从所述辐照区移动到所述粘接区。
本发明的第二方案提供了复合预浸料的制造装置,该装置包括:
等离子体源,所述等离子体源用于在基本上为大气压的压力下以等离子体辐照纤维片材和/或基质,和
用于以所述基质浸渍所述纤维片材的单元。
本发明的第三方案提供了复合材料的制造方法,该方法包括:
以等离子体辐照基质,和
以经辐照的所述基质被覆填料。
本发明的第三方案认识到辐照所述基质可以(必要时与辐照所述填料相结合)用于增强所述填料和所述基质之间的粘接。所述填料可以是纤维片材(与本发明的第一方案相符),也可以是非纤维材料或单根纤维。
本发明的第四方案提供了用于制造复合材料的装置,该装置包括:
用于以等离子体辐照基质的等离子体源,和
用于以经辐照的所述基质被覆填料的单元。
附图说明
现在将通过参照以下附图描述本发明的实施方式:
图1显示了复合预浸料的制造方法的第一步骤;和
图2显示了该方法的第二步骤。
具体实施方式
参见图1,所示的是用于制造基质膜的装置1。涂覆头2包括装有液态基质材料4(“熔融物”或者分散液)的漏斗3。漏斗3的开口位于一对辊筒5之间。液态基质材料4通过辊筒5而被施用于从隔离纸卷7连续送出的隔离纸6的片材的上表面。基质膜8和隔离纸6的片材被卷绕在辊筒10上。当已经形成所需尺寸的卷时,停止从涂覆头流出基质4,并倒转辊筒10。基质膜8经由导辊12被卷绕在辊筒上从而形成基质膜卷11。与此同时将隔离纸6回卷到隔离纸卷7上。随后移去卷11并且重复该工序以形成图2所示的基质膜的另一卷13。
基质材料4通常是聚合物,并且可以是热固性的(例如环氧树脂)或热塑性的(例如聚醚醚酮——PEEK)。
参见图2,将纤维片材20从辊筒(未显示)经由一对导辊21、22送出。构成片材20的纤维可以由诸如碳、玻璃、天然纤维或热塑性塑料等任何有机材料或无机材料制成。片材20可以是单向带的形式或机织织物的形式。将一对基质膜从基质膜卷11、13经由辊筒22、23退卷。随后将该三层组装体以加热器24加热并在三对压固辊25之间压缩。这使片材浸渍有基质材料从而形成预浸料26的片材。预浸料26在图2中显示为两层,但其实际上有效地变为单层的经基质浸渍的纤维。随后将预浸料26与一层隔离纸28共同卷在辊筒27上,所述隔离纸28从隔离纸卷29退卷并通过一对辊筒30、31而被施用于预浸料。
在进入粘接区(概括地在32标出,由辊筒22、33、加热器24和压固辊25界定)之前,纤维片层20和/或来自卷11、13的基质膜在辐照区(概括性地标为33)受到等离子体的辐照。图2中显示了三个等离子体源:
●第一源40,其指向辊筒22的辊隙从而辐照纤维片材与下部基质膜的相对的那些面;
●第二源41,其指向辊筒23的辊隙从而辐照纤维片材与上部基质膜的相对的那些面;和
●第三源42,其只指向上部基质膜。
虽然图2中显示了三个源,但可以按照需要使用更多或更少的等离子体源。因此一般来说,可以使用等离子体源只辐照纤维片材;只辐照一层或两层基质膜;或者辐照纤维片材和一层或两层基质膜(如图2所示)。
每一等离子体源可以是例如:
●由加拿大蒙特利尔的Plasmatec Inc.提供的“Plasmatec”等离子体单元;
●由英国塔姆沃思的Dyne Technology Ltd.提供的“Tantec”等离子体单元;或者
●由英国豪斯罗工商区(Hounslow Business Park)的Adtec EuropeLtd(UK)提供的“AX系列”等离子体单元。
等离子体源在基本上为大气压的压力下产生等离子体。这意味着不需要将等离子体源像在US5108780中那样安放在真空室中,而是可以与装置的其余部分一起在正常条件(即在大气压力下的空气中)下安放。
辐照工序和浸渍工序同时进行,而不是像分批法(batch process)那样依次进行。这使得纤维片材在辐照之后当活性自由基依然存在时即被迅速浸渍。
辊筒持续运转,从而使纤维片材和基质膜在辐照和浸渍期间保持移动。
等离子体可以在环境温度或更高温度中产生,并且可以是诸如氧、氩和氮等气体以任意比例混合从而形成处理材料所需的离子物种的任意混合物。例如,等离子体可以是:
●氮/氩
●氮/氧
●氮/氧/氩
●空气
虽然图2中只显示了三个等离子体源,但取决于片材20的幅宽,可以以阵列(即,在图2的平面之外)布置更多的等离子体源以辐照纤维片材和/或基质膜的全部幅宽。所述幅宽可以为3毫米~20米。
对纤维和/或基质的辐照在它们的表面上产生自由基并且增强预浸料中这些成分之间的粘接。这些自由基具有有限的停留时间(dwell time),因此将等离子体源40~42放置得足够接近辊筒22、23,并且辊筒以足够的速度运转,从而确保在辐照之后尽快(通常在辐照之后不到30秒,优选在辐照之后不到1秒)通过辊筒22、23将这些片层聚集在一起。虽然这一工序的速度可以高达400米/分钟,但通常以2米/分钟~10米/分钟进行。
在纤维片材与基质结合之前不对纤维片材施用单独的粘合剂。
预浸料可以用于形成诸如机翼蒙皮(wing skin)、长桁(stringer)、翼梁(spar)、机翼通路板(wing access panel)或扰流器等飞行器部件;或诸如自行车架、工业制品、体育用品、汽车产品、风能产品或航海产品(如船壳)等非飞行器部件。
虽然以上通过参照一个或多个优选的实施方式对本发明进行了描述,但应该认识到的是可以做出各种变化或修改,而不背离如所附权利要求书中所限定的本发明的范围。
Claims (20)
1.一种制造复合片材的方法,所述方法包括:
a.在基本上为大气压的压力下以等离子体在辐照区辐照纤维片材和/或基质,和
b.在粘接区以所述基质浸渍所述纤维片材;
其中,工序a.和b.同时进行。
2.如权利要求1所述的方法,其中,工序b.在基本上为大气压的压力下进行。
3.如前述权利要求中任一项所述的方法,其中,所述基质在工序b.期间为片状。
4.如前述权利要求中任一项所述的方法,其中,所述纤维片材和/或所述基质在工序a.期间保持移动。
5.如前述权利要求中任一项所述的方法,其中,所述纤维片材在工序b.期间保持移动。
6.如前述权利要求中任一项所述的方法,其中,工序b.在空气中进行。
7.如前述权利要求中任一项所述的方法,所述方法进一步包括用少于30秒将所述纤维片材和/或所述基质从所述辐照区移动至所述粘接区。
8.通过前述权利要求中任一项所述的方法制造的复合片材。
9.一种复合片材的制造装置,所述装置包括:
a.用于在基本上为大气压的压力下以等离子体辐照纤维片材和/或基质的等离子体源,和
b.用于以所述基质浸渍所述纤维片材的单元。
10.一种制造复合材料的方法,所述方法包括:
a.以等离子体辐照基质,和
b.以经辐照的所述基质被覆填料。
11.如权利要求10所述的方法,其中,工序a.在基本上为大气压的压力下进行。
12.如权利要求10或11所述的方法,其中,工序b.在基本上为大气压的压力下进行。
13.如权利要求10~12中任一项所述的方法,其中,所述填料包括片材。
14.如权利要求10~13中任一项所述的方法,其中,所述基质包括片材。
15.如权利要求10~14中任一项所述的方法,其中,所述基质在工序a.中随着其移动穿过辐照区而被辐照;并且在工序b.中随着其移动穿过粘接区而被覆所述填料。
16.如权利要求10~15中任一项所述的方法,其中,工序a.和工序b.同时进行。
17.如权利要求10~16中任一项所述的方法,其中,工序b.在空气中进行。
18.如权利要求10~17中任一项所述的方法,其中,所述基质在工序a.中在辐照区被辐照,并在工序b.中在粘接区被覆所述填料,并且其中,所述方法进一步包括用少于30秒将所述基质从所述辐照区移动至所述粘接区。
19.通过权利要求10~18中任一项所述的方法制造的复合材料。
20.一种复合材料的制造装置,所述装置包括:
a.用于以等离子体辐照基质的等离子体源,和
b.用于以经辐照的所述基质被覆填料的单元。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0615644A GB0615644D0 (en) | 2006-08-07 | 2006-08-07 | Method of manufacturing composite material |
GB0615644.2 | 2006-08-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN101500771A true CN101500771A (zh) | 2009-08-05 |
Family
ID=37027350
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNA2007800293797A Pending CN101500771A (zh) | 2006-08-07 | 2007-08-01 | 制造复合材料的方法及装置 |
Country Status (9)
Country | Link |
---|---|
US (2) | US8241711B2 (zh) |
EP (1) | EP2049312B1 (zh) |
JP (1) | JP2010500441A (zh) |
CN (1) | CN101500771A (zh) |
BR (1) | BRPI0714911A2 (zh) |
CA (1) | CA2660256A1 (zh) |
GB (1) | GB0615644D0 (zh) |
RU (1) | RU2009106583A (zh) |
WO (1) | WO2008017882A1 (zh) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104723582A (zh) * | 2015-03-27 | 2015-06-24 | 解廷秀 | 一种连续纤维增强热塑性复合材料的制造设备及其应用 |
CN106715548A (zh) * | 2014-09-29 | 2017-05-24 | 可隆工业株式会社 | 用于燃料电池分离板的热塑性预浸料中间材料及使用其制造用于燃料电池分离板的热塑性预浸料的方法 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201222934D0 (en) * | 2012-12-19 | 2013-01-30 | Cytec Ind Inc | Particle toughening for improving fracture toughness |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5774115A (en) | 1980-10-27 | 1982-05-10 | Res Dev Corp Of Japan | Manufacture of prepreg sheet |
DE3277873D1 (en) | 1981-04-04 | 1988-02-04 | Nat Res Dev | Polymers in matrix reinforcement |
US4496415A (en) * | 1982-04-08 | 1985-01-29 | Westinghouse Electric Corp. | Method for impregnating resin powder directly into a laminate lay up |
US4606930A (en) * | 1984-03-02 | 1986-08-19 | Sumitomo Chemical Company, Limited | Method for treating fibers |
US4664936A (en) | 1985-01-30 | 1987-05-12 | Shin-Etsu Chemical Co., Ltd. | Aromatic polyamide fiber-based composite prepreg |
JPH01272731A (ja) | 1988-04-22 | 1989-10-31 | Ube Ind Ltd | 繊維強化金属複合材料の製造方法 |
US5180780A (en) * | 1989-01-12 | 1993-01-19 | Idemitsu Petrochemical Company Limited | Rubber-modified styrene-based copolymer |
US5549780A (en) | 1990-10-23 | 1996-08-27 | Semiconductor Energy Laboratory Co., Ltd. | Method for plasma processing and apparatus for plasma processing |
US5108780A (en) | 1991-01-28 | 1992-04-28 | Brigham Young University | Enhanced thermoplastic adhesion to fibers by using plasma discharge |
US5391855A (en) | 1991-08-01 | 1995-02-21 | Komoto Tech, Inc. | Apparatus for atmospheric plasma treatment of a sheet-like structure |
GB9216186D0 (en) | 1992-07-30 | 1992-09-09 | Ciba Geigy Ag | Product and production method |
US5266139A (en) * | 1992-10-02 | 1993-11-30 | General Dynamics Corporation, Space Systems Division | Continuous processing/in-situ curing of incrementally applied resin matrix composite materials |
KR960702844A (ko) | 1993-05-28 | 1996-05-23 | 앤 제이. 로버슨 | 중합체 물질을 대기압하에서 글로우 방전 플라즈마로 처리하는 방법 및 장치(nethod and apparatus for glow discharge plasma treatment of polymer materials at atmospheric pressure) |
DE19610113C2 (de) * | 1996-03-14 | 1998-01-22 | Reinhausen Maschf Scheubeck | Verfahren zur Herstellung eines faserverstärkten Isolierkörpers |
US5895622A (en) * | 1997-04-07 | 1999-04-20 | Purdue Research Foundation | Method and apparatus for composite manufacture |
JP3430897B2 (ja) * | 1998-01-27 | 2003-07-28 | 松下電工株式会社 | プリプレグ及び積層板 |
US6066826A (en) | 1998-03-16 | 2000-05-23 | Yializis; Angelo | Apparatus for plasma treatment of moving webs |
US6828578B2 (en) | 1998-12-07 | 2004-12-07 | Meridian Research And Development | Lightweight radiation protective articles and methods for making them |
US6709718B2 (en) | 2001-04-10 | 2004-03-23 | Exxonmobil Oil Corporation | Porous plasma treated sheet material |
US6555778B1 (en) * | 2001-11-19 | 2003-04-29 | Geomat Insights, Llc | Plasma enhanced sheet bonding method and device |
JP2005171432A (ja) | 2003-12-12 | 2005-06-30 | Teijin Techno Products Ltd | 高分子複合体補強用繊維の製造方法 |
GB0410749D0 (en) * | 2004-05-14 | 2004-06-16 | Dow Corning Ireland Ltd | Coating apparatus |
-
2006
- 2006-08-07 GB GB0615644A patent/GB0615644D0/en not_active Ceased
-
2007
- 2007-08-01 WO PCT/GB2007/050462 patent/WO2008017882A1/en active Application Filing
- 2007-08-01 RU RU2009106583/05A patent/RU2009106583A/ru not_active Application Discontinuation
- 2007-08-01 EP EP07766474.6A patent/EP2049312B1/en not_active Not-in-force
- 2007-08-01 CN CNA2007800293797A patent/CN101500771A/zh active Pending
- 2007-08-01 BR BRPI0714911-5A patent/BRPI0714911A2/pt not_active IP Right Cessation
- 2007-08-01 JP JP2009523353A patent/JP2010500441A/ja active Pending
- 2007-08-01 CA CA 2660256 patent/CA2660256A1/en not_active Abandoned
- 2007-08-01 US US12/375,108 patent/US8241711B2/en not_active Expired - Fee Related
-
2012
- 2012-08-01 US US13/564,289 patent/US8420183B2/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106715548A (zh) * | 2014-09-29 | 2017-05-24 | 可隆工业株式会社 | 用于燃料电池分离板的热塑性预浸料中间材料及使用其制造用于燃料电池分离板的热塑性预浸料的方法 |
CN104723582A (zh) * | 2015-03-27 | 2015-06-24 | 解廷秀 | 一种连续纤维增强热塑性复合材料的制造设备及其应用 |
Also Published As
Publication number | Publication date |
---|---|
JP2010500441A (ja) | 2010-01-07 |
BRPI0714911A2 (pt) | 2013-05-28 |
WO2008017882A1 (en) | 2008-02-14 |
RU2009106583A (ru) | 2010-09-20 |
CA2660256A1 (en) | 2008-02-14 |
US20090297726A1 (en) | 2009-12-03 |
US20120292828A1 (en) | 2012-11-22 |
EP2049312A1 (en) | 2009-04-22 |
US8241711B2 (en) | 2012-08-14 |
GB0615644D0 (en) | 2006-09-13 |
US8420183B2 (en) | 2013-04-16 |
EP2049312B1 (en) | 2016-12-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4844764A (en) | Process of in-line coating and decorative-layer lamination with panel board material employing electron beam irradiation | |
JP2016501971A (ja) | 表面開口部のある硬化性プリプレグ | |
US10207287B2 (en) | Machine and treatment process via chromatogenous grafting of a hydroxylated substrate | |
CN1039212C (zh) | 复合薄膜 | |
CN101500771A (zh) | 制造复合材料的方法及装置 | |
CN102765271B (zh) | 一种油墨热压转移载体膜及其制作方法 | |
EP0103344A2 (en) | Process of in-line coating and decorative layer lamination with panel board material and the like employing electron-beam irradiation, and decorated panel produced thereby | |
KR20180080849A (ko) | 스마트 윈도우 필름의 제조 장치 | |
EP0041849B1 (en) | Pvc fabric | |
JPS6251670B2 (zh) | ||
JP2001002794A (ja) | 一方向炭素繊維テープ及びその製造方法 | |
CN103407203B (zh) | 一种在线加纤维覆膜的防伪标签制作装置及方法 | |
CN111890595A (zh) | 一种复合熔渗热塑性碳纤维预浸织物的系统及制备方法 | |
CN1493453A (zh) | 制备聚乙烯层压复合材料的方法 | |
CA1206403A (en) | Method and apparatus for the manufacture of a sandwich web | |
US3849226A (en) | Producing fiber reinforced resin panels with gelcoat fiber layer and lacquer protective | |
CN109762479A (zh) | 多层复合型屏下指纹解锁保护膜和成型方法 | |
CN212266355U (zh) | 一种复合熔渗热塑性碳纤维预浸织物的系统 | |
JPH02182450A (ja) | 吸音断熱板 | |
CN217444176U (zh) | Eb辐照制备云母带的系统 | |
JPH0220345A (ja) | 膜構造材料およびその製造方 | |
US20200131696A1 (en) | Method for continuously producing a pattern at the surface of a flexible substrate and related apparatus | |
JP6480883B2 (ja) | 溶液製膜方法 | |
US20110091699A1 (en) | Method for manufacturing a laminate and product obtained | |
CN114843051A (zh) | 一种eb辐照制备云母带的系统 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20090805 |