公开(公告)号：EP2994311B1

公开(公告)日：2018-06-20

申请号：EP14723058.5

申请日：2014-05-07

申请人： Saint-Gobain Isover

发明人： THIERY, Julien ,  PASSON, Ulrich ,  GERHARDS, Wolf

IPC分类号： B32B37/18 ,  E04B1/80 ,  F16L59/065 ,  B32B5/02

CPC分类号： F16L59/02 ,  B32B3/04 ,  B32B5/02 ,  B32B15/14 ,  B32B27/12 ,  B32B27/302 ,  B32B27/32 ,  B32B27/34 ,  B32B37/0007 ,  B32B37/142 ,  B32B37/18 ,  B32B2305/22 ,  B32B2307/304 ,  B32B2307/31 ,  B32B2307/718 ,  B32B2607/00 ,  E04B1/803 ,  F16L59/065 ,  Y02A30/242 ,  Y02B80/12

摘要： The invention relates to a method for manufacturing vacuum insulation panels with a fiber core, comprising the steps of: providing a core blank of fibers, compressing the core blank to a predetermined final thickness for forming the core, evacuating a foil sleeve enclosing the core up to a pressure of ≦1 mbar, and sealing the foil sleeve. The method according to the invention is characterized by the fact that, in the compression step, the core blank is arranged between two cover elements and is mechanically compressed therebetween, that the core is kept under compression pressure until the foil sleeve is sealed, and that the compression step is performed at the place of manufacture at room temperature without thermal impact. Thus, a method for manufacturing vacuum insulation panels with a fiber core can be improved such that it can be performed with reduced energy requirement and yet the insulating effect of the vacuum insulation panels does not suffer therefrom.

公开(公告)号：EP3330055A1

公开(公告)日：2018-06-06

申请号：EP16201748.7

申请日：2016-12-01

申请人： Tarkett GDL S.A.

发明人： SKALSKI, Marek

IPC分类号： B29C43/48 ,  E04F15/10 ,  B29C43/34 ,  B29C70/50 ,  B29C43/30 ,  B32B37/10 ,  B32B37/24 ,  B32B38/00 ,  B32B37/02 ,  B32B5/26 ,  B29C43/26 ,  B32B37/00 ,  B29L31/00 ,  B29K101/12 ,  B29K105/08 ,  B29C43/40 ,  B29K309/08

CPC分类号： B29C43/48 ,  B29C43/265 ,  B29C70/506 ,  B29C2043/3416 ,  B29C2043/483 ,  B29C2793/009 ,  B29K2101/12 ,  B29K2105/0818 ,  B29K2105/0845 ,  B29K2309/08 ,  B29K2995/0087 ,  B29L2031/732 ,  B32B5/022 ,  B32B5/26 ,  B32B37/0007 ,  B32B37/02 ,  B32B37/1027 ,  B32B37/1036 ,  B32B37/24 ,  B32B38/145 ,  B32B2260/021 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2307/412 ,  B32B2315/085 ,  B32B2327/06 ,  B32B2419/04 ,  B32B2471/00 ,  E04F15/105 ,  E04F15/107

摘要： A process for manufacturing floor tiles comprising the following steps:
- scattering granules (62) of a thermoplastic material on a conveying member (52) in order to obtain a first layer of granules (64),
- superimposing several sheets (5B, 5C) in order to obtain a plurality of adjacent sheets on the first layer of granules (64), each of the sheets containing at least 50 wt% of glass fibers,
- scattering granules (70) of a thermoplastic material on the uppermost sheet (5B) in order to obtain a second layer of granules (72),
- pressing and heating the first layer of granules, the plurality of adjacent sheets and the second layer of granules,
- melting or at least softening the first layer of granules and the second layer of granules, the plurality of sheets being at least partly impregnated by the thermoplastic material of the first layer of granules and of the second layer of granules in order to obtain a core layer after cooling, and
- using the core layer to produce at least a slab, and using the slab to obtain the floor tiles.

公开(公告)号：EP3310575A1

公开(公告)日：2018-04-25

申请号：EP16741132.1

申请日：2016-05-25

申请人： Incussus, LLC

发明人： CERIZZA, Giuseppe ,  CONDE BALZA, Hugo Enrique

IPC分类号： B32B21/02 ,  B32B21/08 ,  B32B27/08 ,  B32B27/30 ,  B32B27/32 ,  B32B27/36

CPC分类号： B32B21/08 ,  B32B3/30 ,  B32B7/04 ,  B32B7/12 ,  B32B21/02 ,  B32B27/08 ,  B32B27/22 ,  B32B27/304 ,  B32B27/32 ,  B32B27/36 ,  B32B37/0007 ,  B32B37/0053 ,  B32B37/06 ,  B32B37/10 ,  B32B37/12 ,  B32B37/153 ,  B32B37/203 ,  B32B38/0004 ,  B32B38/06 ,  B32B2037/0092 ,  B32B2250/24 ,  B32B2307/402 ,  B32B2307/412 ,  B32B2307/50 ,  B32B2307/546 ,  B32B2307/558 ,  B32B2307/732 ,  B32B2307/734 ,  B32B2309/02 ,  B32B2309/105 ,  B32B2309/14 ,  B32B2419/04 ,  B32B2451/00 ,  B32B2479/00

摘要： A method for manufacturing a flat laminate sheet comprises coupling first and second thermoplastic layers to one another without glue by superficially heating coupling surfaces of the two layers and pressing the heated layers onto one another without glue to form a first combined thermoplastic multilayer free from glue, the layers each being a film free of plasticizers and comprising PVC, PET, PETG, PP, and/or PE, and coupling a third thermoplastic layer of a film comprising PVC, PET, PETG, PP, and/or PE to the first combined thermoplastic multilayer by superficially heating coupling surfaces of the third layer and the first combined thermoplastic multilayer and pressing the heated third layer and the first combined thermoplastic multilayer onto one another without glue to form a multilayer laminate sheet free from glue, being planar, flat, and rigid, and having a thickness between approximately 0.75 to 4 mm.

公开(公告)号：EP2774758A4

公开(公告)日：2015-11-11

申请号：EP12846142

申请日：2012-10-30

申请人： HYUNDAI DYMOS INC

发明人： JOUNG HA GYUN ,  CHO JIN BAE ,  LEE MAN HO

IPC分类号： B32B38/18 ,  B32B5/18 ,  B32B9/02 ,  B65H29/24

CPC分类号： B29C65/7894 ,  B32B9/025 ,  B32B37/0007 ,  B32B37/06 ,  B32B37/1284 ,  B32B37/22 ,  B32B38/1858 ,  B32B2305/022 ,  B32B2317/08 ,  B32B2601/00 ,  B65H29/006 ,  B65H29/242 ,  B65H39/14 ,  B65H2220/02 ,  B65H2301/4191 ,  B65H2301/41912 ,  B65H2301/44734 ,  B65H2701/178 ,  B65H2701/194 ,  B65H2220/01

摘要： The present invention relates to an apparatus for adhering a soft slab and a covering material together. The apparatus for adhering the soft slab and the covering material together includes: a moving unit consisting of a plurality of rollers for moving the soft slab; a conveyor unit including a belt configured such that air passes through the top and bottom surface thereof, and a driving unit for driving the belt, the conveyor unit being intended for transferring a covering material seated on the top surface of the belt toward an adhesive surface of the soft slab; and an air suction unit provided at the bottom surface of the belt so as to suction air such that the covering material is tightly attached onto the top surface of the belt, thereby attaching the covering material onto the adhesive surface of the soft slab without generating pleats.

公开(公告)号：EP2296873B1

公开(公告)日：2015-08-12

申请号：EP09731704.4

申请日：2009-02-20

申请人： Airbus Operations GmbH

发明人： KOLAX, Michael ,  DOLZINSKI, Wolf-Dietrich

IPC分类号： B32B3/12 ,  B32B3/28 ,  B32B38/10

CPC分类号： B29C70/086 ,  B29D99/0021 ,  B29K2063/00 ,  B29K2105/246 ,  B29K2707/04 ,  B29L2031/608 ,  B32B3/12 ,  B32B5/024 ,  B32B5/026 ,  B32B5/26 ,  B32B7/045 ,  B32B7/14 ,  B32B15/14 ,  B32B29/02 ,  B32B37/0007 ,  B32B37/146 ,  B32B38/10 ,  B32B2260/021 ,  B32B2260/028 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/50 ,  B32B2307/718 ,  B32B2605/18 ,  Y10T156/1025 ,  Y10T156/103 ,  Y10T156/1033 ,  Y10T156/1051 ,  Y10T428/24149 ,  Y10T428/24157

公开(公告)号：EP2035230B1

公开(公告)日：2013-12-11

申请号：EP07764778.2

申请日：2007-06-22

申请人： OVD Kinegram AG

发明人： MINNETIAN, Ohannes

IPC分类号： B32B38/00 ,  B42D15/10

CPC分类号： B42D25/455 ,  B32B27/304 ,  B32B37/0007 ,  B32B38/0036 ,  B32B2038/0048 ,  B32B2038/006 ,  B32B2425/00 ,  B42D25/00 ,  B42D25/23 ,  B42D25/29 ,  B42D25/318 ,  B42D25/378 ,  B42D2033/30 ,  Y10T428/31855

公开(公告)号：EP2637849A2

公开(公告)日：2013-09-18

申请号：EP11779591.4

申请日：2011-11-07

申请人： Airbus Operations GmbH

发明人： NAUMANN, Niko ,  WILLAMOWSKI, Michaela

IPC分类号： B29K105/10 ,  B29C51/14 ,  B29C51/08 ,  B29C70/46 ,  B29C70/54

CPC分类号： B29C33/12 ,  B29C43/203 ,  B29C43/58 ,  B29C70/46 ,  B29C70/543 ,  B32B37/0007 ,  B32B37/08 ,  B32B37/10 ,  B32B37/203 ,  B32B2305/07 ,  B32B2309/02 ,  B32B2309/10 ,  B32B2309/72 ,  B32B2605/18 ,  B64F5/10 ,  Y02T50/43

摘要： A method for producing an aircraft structural component includes the steps of introducing a plurality of semi-finished product layers for producing a component from a fibre-reinforced, thermoplastic plastic material into a compression mould, applying pressure to the stacked semi-finished product layers, the stacked semi-finished product layers being fixed, before pressure is applied, at particular points in their position in the compression mould and/or relative to one another in such a way that, while pressure is being applied to the semi-finished product layers stacked in the compression mould, a sliding movement of the semi-finished product layers relative to one another and/or relative to the compression mould, preventing wrinkling in the semi-finished product layers, takes place, and removing the aircraft structural component from the compression mould.

摘要翻译： 一种飞机结构部件的制造方法，其特征在于，将从所述纤维强化热塑性塑料材料制成的多个半成品层引入到压缩模具中，对叠层的半成品层施加压力， 堆叠的半成品层在压力施加之前被固定在它们在压缩模具中的位置的特定点处和/或相对于彼此的位置，使得当压力施加到半成品层时 堆叠在压缩模具中，半成品层相对于彼此和/或相对于压缩模具的滑动运动，防止半成品层中的起皱，并且将飞机结构部件从 压模。

公开(公告)号：EP2516147A4

公开(公告)日：2013-07-31

申请号：EP10845381

申请日：2010-02-05

申请人： BELL HELICOPTER TEXTRON INC

发明人： HETHCOCK JAMES D JR ,  NUNN KENNETH E JR ,  MAY CARL A

IPC分类号： B32B3/12 ,  B29C70/08 ,  B29C70/34 ,  B29C70/86 ,  B32B37/10 ,  B32B37/14

CPC分类号： B32B37/146 ,  B29C70/086 ,  B29C70/342 ,  B29C70/86 ,  B29D24/007 ,  B29K2105/0097 ,  B32B3/12 ,  B32B7/06 ,  B32B7/12 ,  B32B15/08 ,  B32B27/06 ,  B32B37/0007 ,  B32B37/12 ,  B32B2262/00 ,  B32B2307/546 ,  B32B2307/732 ,  Y10T428/236 ,  Y10T428/24149 ,  Y10T428/24157

摘要： A method of making a core-stiffened structure includes the steps of providing a honeycomb core having an adhesive disposed on first and second surfaces thereof, providing a first skin and a second skin, and assembling the first skin, the second skin, and the honeycomb core to form the core-stiffened structure. The method further includes the steps of curing the core-stiffened structure and inhibiting at least one of the first skin and the second skin from protruding into at least one cell of the honeycomb core during the step of curing the core-stiffened structure.

公开(公告)号：EP2584614A1

公开(公告)日：2013-04-24

申请号：EP12807423.4

申请日：2012-07-03

申请人： Nisshinbo Holdings Inc.

发明人： NAKAHAMA, Hidenari ,  IIDA, Hirotaka ,  NAKANO, Hiroshi

IPC分类号： H01L31/042 ,  B29C65/02

CPC分类号： H01L31/0481 ,  B29C65/18 ,  B29C65/787 ,  B29C66/0044 ,  B29C66/342 ,  B29C66/433 ,  B29C66/71 ,  B29C66/7465 ,  B29C66/81261 ,  B29C66/81264 ,  B29C66/81455 ,  B29C66/8322 ,  B29C66/91421 ,  B29C66/919 ,  B29K2995/0083 ,  B32B37/0007 ,  B32B37/003 ,  B32B37/1009 ,  B32B37/1018 ,  B32B2457/12 ,  C08F210/18 ,  C08L2203/206 ,  H01L31/048 ,  H01L31/18 ,  Y02E10/50 ,  B29K2023/083 ,  B29K2009/00 ,  B29K2023/16

摘要： The performances and durability of a diaphragm sheet of a solar cell laminator are enhanced, and a favorable lamination work is stably performed over a long period of time. In addition, by stably performing sufficient and uniform lamination over a long period of time, a high-quality module is stably manufactured over a long period of time.
A solar cell module is manufactured by using a diaphragm sheet formed of a composition containing an ethylene-propylene-diene rubber (EPDM), which is low in creep deformation and high in durability against an organic peroxide and a silane coupling agent.

摘要翻译： 性能和太阳能电池层压机的隔膜片的耐久性得到增强，和有利的层压工作稳定地进行在一段长的时间。 此外，通过在相当长的时间周期进行稳定的充分和均匀的层压，高品质的模块稳定地在一段长时间制造。 一种太阳能电池组件，通过使用形成了含有乙烯 - 丙烯 - 二烯橡胶（EPDM）的组合物的隔膜片，所有这些是在蠕变变形低和高的耐久性，以抵抗有机过氧化物和硅烷偶联剂制造。

公开(公告)号：EP2332725A3

公开(公告)日：2012-01-11

申请号：EP10014959.0

申请日：2007-12-14

申请人： United Technologies Corporation

发明人： Vontell, John H. ,  Salisbury, George A.

IPC分类号： B32B37/10 ,  B29C33/20

CPC分类号： B32B37/10 ,  B29C33/20 ,  B32B37/0007 ,  B32B37/0015 ,  B32B37/0046 ,  B32B37/26 ,  B32B2309/02 ,  B32B2309/12 ,  B32B2309/66 ,  B32B2309/68 ,  B32B2311/00 ,  B32B2603/00

摘要： A tool (10) for laminating a metal foil (23) and polymer film (25) to form a laminate structure (20) is disclosed. A method of using the tool (10) to form a laminate structure (20) is also disclosed. The tool (10) comprises movable platens (11) having sealing surfaces (12) which form a cavity (19). The cavity (19) is pressurized and heated to form the laminated structure (20) and evacuated to remove volatiles from the structure (20).