公开(公告)号：EP1292437A1

公开(公告)日：2003-03-19

申请号：EP01934661.8

申请日：2001-05-04

申请人： Bale Fusion Limited

发明人： Lewis, Peter Joseph Lelievre

IPC分类号： B29C43/02 ,  B29C43/18 ,  B29C43/52 ,  B29C70/34 ,  B29C70/42

CPC分类号： B29B17/0026 ,  B29C35/0238 ,  B29C43/00 ,  B29K2105/16 ,  B29K2105/26 ,  B29K2995/0001 ,  Y02W30/62 ,  Y10S264/911 ,  Y10S264/914 ,  Y10T428/24174

摘要： A method for forming an article in which thermoplastics materials are used as the binding agent. Materials (21) are shredded in a shredder (1), compressed in a compressing chamber (15) and moulded in a moulding chamber (16, 17, 19, 20, 26, 27). The thermoplastics material is heated whilst the material is held under compression and then cooled to bind the material together. In one embodiment superheated steam is supplied via tubes (31) having apertures there along. In another embodiment superheated steam is supplied via apertures in side walls of the mould (58, 59). Blocks (62, 72) formed by the method and apparatus of the invention may find application as construction materials etc. and have good structural, thermal and acoustic properties.

公开(公告)号：EP3263308A1

公开(公告)日：2018-01-03

申请号：EP16803113.6

申请日：2016-05-23

申请人： Mitsubishi Heavy Industries, Ltd.

发明人： KAMIHARA, Nobuyuki ,  ABE, Toshio

IPC分类号： B29C35/08 ,  B29C70/06 ,  B82Y5/00

CPC分类号： B29C35/0238 ,  B29C35/002 ,  B29C35/0272 ,  B29C35/0805 ,  B29C37/0064 ,  B29C70/025 ,  B29C70/46 ,  B29C2035/0855 ,  B29C2035/0861 ,  B29K2105/162 ,  B82Y5/00 ,  C08J3/247 ,  C08J5/042 ,  C08J5/043 ,  C08J5/24 ,  C08J2300/22 ,  C08J2300/24 ,  C08K3/08 ,  C08K2003/0831 ,  C08K2003/085 ,  C08K2003/0862

摘要： In order to save labor when molding a resin composite material, to simplify the curing equipment and save energy, and to decrease manufacturing costs of a molded resin article, this curing device (1) of a resin composite material is provided with: an environment setting unit (an electromagnetic wave irradiation unit (5)) which applies a prescribed physical environment that increases the amount of momentum of the molecules in an object (for example, irradiation by electromagnetic waves (EW)) to an uncured resin composite material (2) which contains a metal nanomaterial (2a) that self-heats when placed in the aforementioned specific physical environment (the electromagnetic waves (EW)); a pressing body (6) which is provided so as to be capable of pressing against the surface of the resin composite material (2); and a pressing driving unit (7) which presses the pressing body (6) against the surface of the resin composite material (2) in a state in which the environment setting unit (the electromagnetic wave irradiation unit (5)) is applying the aforementioned specific physical environment (for example, irradiation by electromagnetic waves (EW)) to the resin composite material (2).

摘要翻译： 为了节省树脂复合材料成型时的劳力，简化固化设备并节约能源，并降低成型树脂制品的制造成本，该树脂复合材料固化装置（1）具有：环境设定 在未固化的树脂复合材料（2）上施加使物体内的分子的动量增加的规定的物理环境（例如电磁波（EW）的照射）的单元（电磁波照射单元（5） 其包含当置于上述特定物理环境（电磁波（EW））中时自加热的金属纳米材料（2a）; 按压体（6），其设置成能够按压树脂复合材料（2）的表面; 和在环境设定单元（电磁波照射单元（5））正在施加前述的状态下将按压体（6）按压在树脂复合材料（2）的表面上的按压驱动单元（7） （2）的特定的物理环境（例如电磁波（EW）的照射）。

公开(公告)号：EP1292437A4

公开(公告)日：2004-07-21

申请号：EP01934661

申请日：2001-05-04

申请人： BALE FUSION LTD

发明人： LEWIS PETER JOSEPH LELIEVRE

IPC分类号： B29B17/00 ,  B29C35/02 ,  B29C43/00 ,  B29C43/02 ,  B29C43/18 ,  B29C43/52 ,  B29C70/34 ,  B29C70/42

CPC分类号： B29B17/0026 ,  B29C35/0238 ,  B29C43/00 ,  B29K2105/16 ,  B29K2105/26 ,  B29K2995/0001 ,  Y02W30/62 ,  Y10S264/911 ,  Y10S264/914 ,  Y10T428/24174

摘要： A method for forming an article in which thermoplastics materials are used as the binding agent. Materials (21) are shredded in a shredder (1), compressed in a compressing chamber (15) and moulded in a moulding chamber (16, 17, 19, 20, 26, 27). The thermoplastics material is heated whilst the material is held under compression and then cooled to bind the material together. In one embodiment superheated steam is supplied via tubes (31) having apertures there along. In another embodiment superheated steam is supplied via apertures in side walls of the mould (58, 59). Blocks (62, 72) formed by the method and apparatus of the invention may find application as construction materials etc. and have good structural, thermal and acoustic properties.

公开(公告)号：EP3263308A4

公开(公告)日：2018-04-04

申请号：EP16803113

申请日：2016-05-23

申请人： MITSUBISHI HEAVY IND LTD

发明人： KAMIHARA NOBUYUKI ,  ABE TOSHIO

IPC分类号： B29C35/08 ,  B29C35/02 ,  B29C37/00 ,  B29C70/02 ,  B29C70/06 ,  B82Y5/00

CPC分类号： B29C35/0238 ,  B29C35/002 ,  B29C35/0272 ,  B29C35/0805 ,  B29C37/0064 ,  B29C70/025 ,  B29C70/46 ,  B29C2035/0855 ,  B29C2035/0861 ,  B29K2105/162 ,  B82Y5/00 ,  C08J3/247 ,  C08J5/042 ,  C08J5/043 ,  C08J5/24 ,  C08J2300/22 ,  C08J2300/24 ,  C08K3/08 ,  C08K2003/0831 ,  C08K2003/085 ,  C08K2003/0862

摘要： In order to save labor when molding a resin composite material, to simplify the curing equipment and save energy, and to decrease manufacturing costs of a molded resin article, this curing device (1) of a resin composite material is provided with: an environment setting unit (an electromagnetic wave irradiation unit (5)) which applies a prescribed physical environment that increases the amount of momentum of the molecules in an object (for example, irradiation by electromagnetic waves (EW)) to an uncured resin composite material (2) which contains a metal nanomaterial (2a) that self-heats when placed in the aforementioned specific physical environment (the electromagnetic waves (EW)); a pressing body (6) which is provided so as to be capable of pressing against the surface of the resin composite material (2); and a pressing driving unit (7) which presses the pressing body (6) against the surface of the resin composite material (2) in a state in which the environment setting unit (the electromagnetic wave irradiation unit (5)) is applying the aforementioned specific physical environment (for example, irradiation by electromagnetic waves (EW)) to the resin composite material (2).

公开(公告)号：EP2735504B1

公开(公告)日：2017-01-18

申请号：EP12382459.1

申请日：2012-11-22

申请人： Airbus Operations S.L.

发明人： Guinaldo Fernàndez, Enrique ,  Garcia Nieto, Carlos ,  Honorato Ruiz, Francisco Javier ,  Cruz Dominguez, Francisco José ,  Vélez De Mendizàbal Alonso, Iker ,  Màs Màs, Paula

IPC分类号： B64C3/20 ,  B64C5/02 ,  B29C70/30 ,  B64C3/18 ,  B29D99/00 ,  B29L31/30 ,  B29C35/02

CPC分类号： B64C3/182 ,  B29C35/0238 ,  B29C70/30 ,  B29D99/0014 ,  B29L2031/3085 ,  B64C3/185 ,  B64C3/187 ,  B64C3/20 ,  B64C5/02 ,  Y02T50/43

摘要： The invention provides an aircraft lifting surface with a monolithic main supporting structure (14) of a composite material comprising an upper skin (21) including at least a part of the upper aerodynamic profile of the leading edge (11) and/or of the trailing edge (15), a lower skin, a front spar (18), a rear spar (20), a plurality of leading edge ribs and/or a plurality of trailing edge ribs. This main supporting structure allows a weight and cost reduction of aircraft lifting surfaces. The invention also provides a manufacturing method of said monolithic main supporting structure (14).

公开(公告)号：EP2986451A2

公开(公告)日：2016-02-24

申请号：EP14728716.3

申请日：2014-04-14

申请人： Corning Incorporated

发明人： JOUANNO, Jean-Marc Martin Gerard ,  KANG, Kiat Chyai ,  LEWIS, Sue Camille ,  NATARAJAN, Govindarajan ,  XIAO, Yu

IPC分类号： B32B17/06 ,  B32B17/10

CPC分类号： C03B27/012 ,  B29C35/0238 ,  B29C35/0277 ,  B29C43/30 ,  B29C43/52 ,  B29C44/06 ,  B29C44/24 ,  B32B17/061 ,  B32B17/064 ,  B32B17/10036 ,  B32B37/06 ,  B32B37/08 ,  B32B37/10 ,  B32B2457/20

摘要： A method of forming a laminated glass structure includes introducing a continuous ribbon of flexible glass substrate having a thickness of no greater than about 0.3 mm to a substrate material. The substrate material has a coefficient of thermal expansion (CTE) that is greater than that of the flexible glass substrate. The flexible glass substrate is laminated to the substrate material at an elevated temperature. The substrate material is cooled to introduce a compressive stress across a thickness of the flexible glass substrate.

公开(公告)号：EP2735504A1

公开(公告)日：2014-05-28

申请号：EP12382459.1

申请日：2012-11-22

申请人： Airbus Operations S.L.

发明人： Guinaldo Fernàndez, Enrique ,  Garcia Nieto, Carlos ,  Honorato Ruiz, Francisco Javier ,  Cruz Dominguez, Francisco José ,  Vélez De Mendizàbal Alonso, Iker ,  Màs Màs, Paula

IPC分类号： B64C3/20 ,  B64C5/02 ,  B29C70/30

CPC分类号： B64C3/182 ,  B29C35/0238 ,  B29C70/30 ,  B29D99/0014 ,  B29L2031/3085 ,  B64C3/185 ,  B64C3/187 ,  B64C3/20 ,  B64C5/02 ,  Y02T50/43

摘要： The invention provides an aircraft lifting surface with a monolithic main supporting structure (14) of a composite material comprising an upper skin (21) including at least a part of the upper aerodynamic profile of the leading edge (11) and/or of the trailing edge (15), a lower skin, a front spar (18), a rear spar (20), a plurality of leading edge ribs and/or a plurality of trailing edge ribs. This main supporting structure allows a weight and cost reduction of aircraft lifting surfaces. The invention also provides a manufacturing method of said monolithic main supporting structure (14).

摘要翻译： 对本发明的飞机升力面提供与包含上蒙皮（21）的复合材料制成的整体式主支撑结构（14）至少包括前缘的上空气动力学轮廓的一部分（11）和/或尾部的 边缘（15），下皮，前节省（18），一个后保存（20），前缘肋和/或后缘肋的多个复数。 该主支撑结构允许一个重量和成本的降低的飞机升力面。 因此，该发明是提供上述的单片主支撑结构（14）的制造方法。