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1. 发明公开

EP2123554A1 AIRCRAFT WINDOW MEMBER, ITS MANUFACTURING METHOD, AND AIRCRAFT WINDOW ASSEMBLY 失效转让
标题翻译： FLUGZEUGFENSTERELEMENT，VERFAHREN ZU SEINER HERSTELLUNG UND FLUGZEUGFENSTERBAUGRUPPE
公开(公告)号：EP2123554A1
公开(公告)日：2009-11-25
申请号：EP08711500.2
申请日：2008-02-18
申请人： Mitsubishi Heavy Industries, Ltd. , Fujiwara Co., Ltd.
发明人： OGURI, Kazuyuki , OKADA, Katsuto
IPC分类号： B64C1/14 , H05K9/00
CPC分类号： B64C1/1484 , B64D2045/006 , H05K9/0086 , H05K9/0094 , Y10T156/10 , Y10T442/10
摘要： An aircraft window member excellent in durability, a method of manufacturing the same, and an aircraft window assembly are provided. The aircraft window member includes: a film 5 made of acrylic resin; a conductive mesh 7 which is formed on the film 5 and in which a conductive material is formed in a mesh shape so as to have optical transparency for ensuring visibility and to have electromagnetic-wave shielding properties; and a window main body 3 which is made of acrylic resin and to which the film 5 on which the conductive mesh 7 is formed is attached.
摘要翻译：提供了耐久性优异的飞机窗构件，其制造方法以及飞机窗组件。飞机窗构件包括：由丙烯酸树脂制成的薄膜5; 导电网7，其形成在膜5上，其中导电材料形成为网状，以具有用于确保可视性和具有电磁波屏蔽性的光学透明性; 以及由丙烯酸树脂制成并且形成有导电网7的薄膜5的窗主体3。

3. 发明公开

EP2612891A1 ANTISTATIC COATING, AND STRUCTURE MADE OF COMPOSITE MATERIAL USING SAME AND PRODUCTION METHOD THEREFOR 审中-公开
标题翻译：防静电涂层和结构由复合材料使用制造方法及过程
公开(公告)号：EP2612891A1
公开(公告)日：2013-07-10
申请号：EP11821418.8
申请日：2011-06-30
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： KAMINO, Yuichiro , OGURI, Kazuyuki , YAMAGUCHI, Hiroaki
IPC分类号： C09D201/00 , C09D5/00 , C09D5/24 , C09D7/12
CPC分类号： C09D5/08 , C08J7/047 , C08K3/08 , C08K7/04 , C08K2003/0806 , C09D5/24 , C09D7/70
摘要： The purpose of the present invention is to provide a coating capable of preventing electrolytic corrosion, and which is resistant to electrostatic build-up. An antistatic coating comprising an inorganic fiber containing Si, Ti or Zr, C, and O, or an Ag filler, is provided to the primer. Further, a structure made of composite material which is not susceptible to electrolytic corrosion and electrostatic build-up, is obtained as a result of the formation of a layer by coating the antistatic coating comprising an inorganic fiber that contains Si, Ti or Zr, C, and O, or comprising an Ag filler, on the surface of the structure made of composite material.
摘要翻译：本发明的目的是提供一种能够防止电解腐蚀的涂层，并且所有这些都对静电积聚有抗性。抗静电涂层包含含有的Si，Ti或Zr，C和O，或Ag填料无机纤维的，被提供给引物。此外，结构由复合材料制成，所有这些是不容易受到电解腐蚀和静电积聚，通过涂布所述抗静电涂层包含无机纤维的获得作为层的形成的结果做了含有Si，Ti或Zr，C 和O，或Ag的含有填料，由复合材料制成的结构的表面上。

4. 发明公开

EP1995032A1 METHOD OF MOLDING PRETREATMENT, BONDED ARTICLE AND PROCESS FOR PRODUCING THE SAME, AND COATED ARTICLE AND PROCESS FOR PRODUCING THE SAME 有权
标题翻译：制备成型，粘合制品及其生产方法和涂覆制品及其制造方法过程的
公开(公告)号：EP1995032A1
公开(公告)日：2008-11-26
申请号：EP07708296.4
申请日：2007-02-09
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： OGURI, Kazuyuki
IPC分类号： B29C37/00 , B05D3/12 , B05D7/02 , B24C1/06
CPC分类号： B29C59/022 , B05D3/12 , B24C1/06 , B24C11/00 , B29C65/48 , B29C65/4815 , B29C65/484 , B29C65/8207 , B29C65/8253 , B29C66/02245 , B29C66/026 , B29C66/41 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/72143 , B29C66/73161 , B29C66/7392 , B29C66/73921 , B29C66/7394 , B29C66/73941 , B29C2059/027 , B29K2027/06 , B29K2055/02 , B29K2063/00 , B29K2067/00 , B29K2069/00 , B29K2077/00 , B29K2101/10 , B29K2101/12 , B29K2105/06 , B29K2277/00 , B29K2277/10 , B29K2307/00 , B29K2307/02 , B29K2309/02 , B29K2309/04 , B29K2309/08 , B29C65/00 , B29K2307/04 , B29K2067/06 , B29K2033/12
摘要： The surface of a formed article that comprises a resin is finely roughened without damaging the surface. Particles with an average particle size of not more than 200 µm are projected onto at least a portion of the surface of the formed article that comprises a resin.
摘要翻译：的成形品的表面做了包括树脂被精细而不会损坏表面粗糙化。与上不超过200微米的平均颗粒尺寸的颗粒被投射到至少所述制品的表面的一部分也FORMED包括树脂。

5. 发明公开

EP2354003A1 FUEL TANK OF AIRCRAFT 失效
标题翻译： TREIBSTOFFTANKFÜREIN LUFTFAHRZEUG
公开(公告)号：EP2354003A1
公开(公告)日：2011-08-10
申请号：EP09830233.4
申请日：2009-06-24
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： YAMAGUCHI, Hiroaki , KAMINO, Yuichiro , HASHIGAMI, Tooru , OGURI, Kazuyuki
IPC分类号： B64D37/32 , B64D45/02
CPC分类号： B64D37/32 , B64C3/34 , B64D45/02
摘要： An aircraft fuel tank that is capable of suppressing the occurrence of sparks on a pipe caused by a lightning current through the pipe during a lightning strike, and also suppressing static electricity charging of a pipe caused by flow electrification generated by the fuel. An aircraft fuel tank (1) in which a storage section is formed using a conductive upper skin (5), a conductive lower skin (7) and conductive spars (9), the tank comprising: pipes inside the tank, such as a refuel pipe (17), an engine feed pipe (19) and an inert gas pipe (21), which are disposed inside the storage section and are earthed (27) at a plurality of locations, and pipe outer surface layers (31) having semiconductor properties that are formed in an integrated manner on the outer surfaces of the pipes inside the tank such as the replenishing pipe (17), the supply pipe (19) and the gas pipe (21).
摘要翻译：一种飞机燃料箱，其能够抑制由于在雷击期间通过管道的雷电流引起的管道上的火花的发生，并且还抑制由燃料产生的流动电气引起的管道的静电充电。一种飞机燃料箱（1），其中使用导电上皮（5），导电下皮（7）和导电柱（9）形成存储部分，所述罐包括：罐内的管，例如加油管道（17），发动机供给管（19）和惰性气体管道（21），其设置在存储部分的内部并在多个位置处接地（27），以及具有半导体的管外表面层在补充管（17），供给管（19）和气管（21）内的槽内的管的外表面上一体形成的特性。

6. 发明公开

EP2028100A1 FASTENER 有权
标题翻译：紧固件
公开(公告)号：EP2028100A1
公开(公告)日：2009-02-25
申请号：EP07745044.3
申请日：2007-06-11
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： OGURI, Kazuyuki , KAMINO, Yuichiro
IPC分类号： B64C1/00 , B29C65/48 , B64D45/02 , F16B33/06 , F16B35/00
CPC分类号： F16B33/004 , B29C65/562 , B29C65/564 , B29C66/1122 , B29C66/45 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/723 , B29C66/742 , B29K2305/00 , B29K2305/02 , B29K2307/00 , B29K2309/08 , B29K2995/0005 , B29K2995/0007 , B29L2009/00 , B29L2031/3076 , B29L2031/3082 , B29L2031/3085 , F16B35/06 , B29K2307/04 , B29K2081/04 , B29K2079/08 , B29K2067/003 , B29K2067/00 , B29K2023/12
摘要： A fastener, of which severe strength is demanded and which can also be applied to a location, in which a flush surface equipment is taken into consideration, and which can be manufactured readily and quickly and reduced in manufacturing cost, is provided. A fastener (1) joins a skin of an airplane and a structural material positioned inside the skin and one end surface of a flush head (3) is covered by an insulator layer (5).
摘要翻译：本发明提供一种紧固件，其要求有较高的强度，并且还可应用于其中考虑到齐平表面设备的位置，并且该紧固件能够容易且快速地制造并且降低制造成本。紧固件（1）连接飞机的皮肤和定位在皮肤内的结构材料，并且齐平头（3）的一个端面被绝缘层（5）覆盖。

7. 发明授权

EP2028100B1 FASTENER 有权
公开(公告)号：EP2028100B1
公开(公告)日：2013-05-15
申请号：EP07745044.3
申请日：2007-06-11
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： OGURI, Kazuyuki , KAMINO, Yuichiro
IPC分类号： B64C1/00 , B29C65/48 , B64D45/02 , F16B33/06 , F16B35/00
CPC分类号： F16B33/004 , B29C65/562 , B29C65/564 , B29C66/1122 , B29C66/45 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/723 , B29C66/742 , B29K2305/00 , B29K2305/02 , B29K2307/00 , B29K2309/08 , B29K2995/0005 , B29K2995/0007 , B29L2009/00 , B29L2031/3076 , B29L2031/3082 , B29L2031/3085 , F16B35/06 , B29K2307/04 , B29K2081/04 , B29K2079/08 , B29K2067/003 , B29K2067/00 , B29K2023/12

8. 发明公开

EP2415666A1 FUEL TANK FOR AIRCRAFT 有权
标题翻译： KRAFTSTOFFTANKFÜRFLUGZEUGE
公开(公告)号：EP2415666A1
公开(公告)日：2012-02-08
申请号：EP10758565.5
申请日：2010-03-26
申请人： Mitsubishi Heavy Industries, Ltd. , THE SOCIETY OF JAPANESE AEROSPACE COMPANIES
发明人： YAMAGUCHI, Hiroaki , KAMINO, Yuichiro , HASHIGAMI, Tooru , OGURI, Kazuyuki , NAKAMURA, Koichi
IPC分类号： B64C3/34 , B64D37/02
CPC分类号： B64C3/34 , B64D37/32 , B64D45/02
摘要： An aircraft fuel tank capable of suppressing electrostatic charging caused, for example, by flow electrification with the fuel. The aircraft fuel tank comprises an upper skin (5) and a lower skin (7) that exhibit conductivity and form a portion of a container for storing fuel, an internal structure (19) formed from a metal, and an inner surface layer (15) which has semiconductor properties or insulating properties and is formed in an integral manner on the inner surfaces of the upper skin (5) and the lower skin (7) in a location where the internal structure (19) contacts the upper skin (5) and the lower skin (7), and in the surrounding portion thereof, wherein the inner surface layer (15) is formed, at least in the surrounding portion, from a material having semiconductor properties.
摘要翻译：能够抑制静电充电的飞机燃料箱，例如通过与燃料的流动通电。飞机燃料箱包括显示导电性并形成用于储存燃料的容器的一部分的上皮（5）和下皮（7），由金属形成的内部结构（19）和内表面层（15）），其具有半导体性质或绝缘性能，并且在内部结构（19）接触上皮肤（5）的位置中以整体形式形成在上皮肤（5）和下皮肤（7）的内表面上，和下表皮（7），并且在其周围部分中，至少在周围部分中，由具有半导体特性的材料形成内表面层（15）。

9. 发明公开

EP2399739A1 METHOD FOR PRODUCING RESIN-BASED COMPOSITE 审中-公开
标题翻译：方法用于生产树脂基的复合物质
公开(公告)号：EP2399739A1
公开(公告)日：2011-12-28
申请号：EP10743663.6
申请日：2010-02-08
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： KISHIDA, Tomone , OGURI, Kazuyuki
IPC分类号： B32B27/18 , B32B5/28
CPC分类号： B32B27/04 , B32B7/12 , B32B27/08 , B32B27/12 , B32B27/20 , B32B27/308 , B32B27/38 , B32B27/40 , B32B27/42 , B32B2255/10 , B32B2255/205 , B32B2262/101 , B32B2262/106 , B32B2264/105 , B32B2307/202 , B32B2307/546 , B32B2307/5825 , B32B2307/71 , B32B2307/732 , B64D45/02
摘要： Provided is a method for producing, with good work performance, a composite comprising a lightning-resistant layer having excellent adhesion with a resin-based composite and good fatigue properties. The method for producing a resin-based composite comprises a step for forming a laminate by the successive lamination, on a first resin sheet (11) formed primarily from a fiber-reinforced resin, of a conductive layer (12) formed from a resin containing metal powder and a second resin sheet (13) formed primarily from a fiber-reinforced resin; and a step for baking the laminate and bonding the first resin sheet (11), conductive layer (12), and second resin sheet (13) to form a resin-based composite (10),

10. 发明授权

EP2354003B1 FUEL TANK OF AIRCRAFT 失效
标题翻译：燃油箱飞机
公开(公告)号：EP2354003B1
公开(公告)日：2014-10-15
申请号：EP09830233.4
申请日：2009-06-24
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： YAMAGUCHI, Hiroaki , KAMINO, Yuichiro , HASHIGAMI, Tooru , OGURI, Kazuyuki
IPC分类号： B64D37/32 , B64D45/02
CPC分类号： B64D37/32 , B64C3/34 , B64D45/02

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