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1. 发明授权

EP2415693B1 COMPOSITE TANK, MANUFACTURING METHOD THEREFOR, AND WING 有权
公开(公告)号：EP2415693B1
公开(公告)日：2020-11-11
申请号：EP10758416.1
申请日：2010-03-17
申请人： Mitsubishi Heavy Industries, Ltd. , THE SOCIETY OF JAPANESE AEROSPACE COMPANIES
发明人： YAMAGUCHI, Hiroaki , KAMINO, Yuichiro , NAKAMURA, Koichi , HASHIGAMI, Tooru
IPC分类号： B65D90/46 , B64D37/06

2. 发明公开

EP3680614A1 GYROSCOPE BASED ON MACH-ZEHNDER-TYPE ATOMIC INTERFERENCE 审中-公开
公开(公告)号：EP3680614A1
公开(公告)日：2020-07-15
申请号：EP18866418.9
申请日：2018-07-25
申请人： Tokyo Institute of Technology , Osaka University , Japan Aviation Electronics Industry, Limited , Mitsubishi Heavy Industries, Ltd.
发明人： KOZUMA, Mikio , INOUE, Ryotaro , MUKAIYAMA, Takashi , MORIMOTO, Seiichi , YOSHIOKA, Kazunori , TANAKA, Atsushi , KAMINO, Yuichiro
IPC分类号： G01C19/58
摘要： A gyroscope of the present invention includes a moving standing light wave generator 301 to generate three moving standing light waves 201a, 201b and 201c, an atomic beam source 101 to continuously generate an atomic beam 101a in which individual atoms are in the same state, an interference device 201 that exerts a Sagnac effect through interaction between the atomic beam 101a and the three moving standing light waves 201a, 201b and 201c, and a monitor 400 to detect angular velocity or acceleration by monitoring an atomic beam 101b from the interference device 201. Each moving standing light wave satisfies an n-th order Bragg condition, where n is a positive integer of 2 or more.

3. 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

4. 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）。

5. 发明授权

EP2979976B1 FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY 有权
公开(公告)号：EP2979976B1
公开(公告)日：2019-04-10
申请号：EP14774804.0
申请日：2014-02-18
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： KAMIHARA, Nobuyuki , KISHIMOTO, Kazuaki , ABE, Toshio , KAMINO, Yuichiro
IPC分类号： B64D45/02 , B64C3/34 , B32B5/00 , B32B7/02 , B60K15/03 , H01M8/04 , B64D37/06

6. 发明公开

EP2979977A1 FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY 有权
标题翻译：燃料箱，主翼，飞机机身，飞机和移动车身
公开(公告)号：EP2979977A1
公开(公告)日：2016-02-03
申请号：EP14776202.5
申请日：2014-01-28
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： KAMIHARA, Nobuyuki , KISHIMOTO, Kazuaki , ABE, Toshio , KAMINO, Yuichiro
IPC分类号： B64C3/34 , B32B5/00 , B32B7/02 , B60K15/03 , B64D45/02 , H01M8/00 , H01M8/04
CPC分类号： B64D37/32 , B32B1/02 , B32B7/08 , B32B15/08 , B32B27/12 , B32B27/20 , B32B2262/106 , B32B2307/20 , B32B2605/00 , B32B2605/18 , B64C3/34 , B64D37/005 , B64D37/04 , B64D37/06 , B64D45/02 , Y02T50/44
摘要： The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in quality management to be reduced, and weight increases to be prevented. The fuel tank comprises a structural member that uses a carbon fiber reinforced plastic (CFRP) (15) including a reinforcing material containing carbon fiber and a matrix containing plastic. The structural member is formed by laminating conductive sheets (17) between prepregs of the carbon fiber reinforced plastic (CFRP) (15), and being formed with a fastening hole (22) in which a bolt is fastened.
摘要翻译：本发明的目的是提供一种燃料箱，主翼，飞机机身，飞机和移动体，其能够减少质量管理中涉及的工作时间和成本，并且防止重量增加。燃料箱包括使用碳纤维增强塑料（CFRP）（15）的结构构件，该碳纤维增强塑料（CFRP）（15）包括含碳纤维的增强材料和含塑料的基体。结构部件通过在碳纤维增强塑料（CFRP）（15）的预浸料坯之间层压导电片（17）形成，并形成有紧固螺栓的紧固孔（22）。

7. 发明公开

EP2979976A1 FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY 有权
标题翻译： KRAFTSTOFFTANK，HAUPTTRAGFLÄCHEN，FLUGZEUGRUMPF，FLUGZEUG UND BEWEGLICHERKÖRPER
公开(公告)号：EP2979976A1
公开(公告)日：2016-02-03
申请号：EP14774804.0
申请日：2014-02-18
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： KAMIHARA, Nobuyuki , KISHIMOTO, Kazuaki , ABE, Toshio , KAMINO, Yuichiro
IPC分类号： B64C3/34 , B32B5/00 , B32B7/02 , B60K15/03 , B64D45/02 , H01M8/04
CPC分类号： B64C3/34 , B32B5/00 , B32B7/02 , B32B2439/00 , B64D37/06 , B64D45/02 , H01M8/04208 , Y02P70/56 , Y02T50/44
摘要： The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in a manufacturing process to be reduced, and weight increases to be prevented. The fuel tank comprises a structural member in which carbon fiber reinforced plastic (CFRP) (15) is used, the carbon fiber reinforced plastic (CFRP) (15) comprising a reinforcing material that includes carbon fibers and a matrix that includes plastic. The structural member is formed by laminating a conductive sheet (17) between prepregs of the carbon fiber reinforced plastic (CFRP) (15). In this case, a cut surface (11a) of the structural member formed by cutting the structural member may be exposed on the inside in which fuel is stored.
摘要翻译：本发明的目的是提供一种燃料箱，主机翼，飞机机身，飞机和移动体，其能够减少制造过程中涉及的工作时间和成本，并且可以防止重量增加。燃料箱包括其中使用碳纤维增强塑料（CFRP）（15）的结构构件，碳纤维增强塑料（CFRP）（15）包括包含碳纤维的增强材料和包括塑料的基质。通过在碳纤维增强塑料（CFRP）（15）的预浸料之间层压导电片17而形成结构件。在这种情况下，通过切割结构构件形成的结构构件的切割面（11a）可以暴露在储存燃料的内部。

8. 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

9. 发明公开

EP2613130A1 CAPACITANCE METER 有权
标题翻译： KAPAZITÄTSMESSGERÄT
公开(公告)号：EP2613130A1
公开(公告)日：2013-07-10
申请号：EP11821384.2
申请日：2011-05-24
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： YAMAGUCHI, Hiroaki , KAMINO, Yuichiro
IPC分类号： G01F23/26
CPC分类号： G01F23/263 , G01F23/266 , G01F23/268
摘要： Provided is a fuel oil gauge (15), comprising: a columnar interior structural body (27) formed from an insulator; a hollow cylindrical exterior structural body (23) formed from an insulator, which is positioned on the exterior circumference side of the interior structural body (27) around the total perimeter thereof with a gap therebetween; an interior electrode (29) which is affixed to the exterior circumference face of the interior structural body (27); and an exterior electrode (25) which is affixed to the interior circumference face of the exterior structural body (23). The fuel oil gauge (15) measures capacitance between the interior electrode (29) and the exterior electrode (25), and detects the level of fuel present between the interior electrode (29) and the exterior electrode (25). The exterior structural body (23) further comprises a plurality of exterior side through holes (31) that allow electrical charge to move from the exterior circumference face thereof to the exterior electrode (25).
摘要翻译：提供一种燃油表（15），包括：由绝缘体形成的柱状内部结构体（27）; 由绝缘体形成的中空圆柱形外部结构体（23），所述中空圆柱形外部结构体（23）由绝缘体形成，所述绝缘体围绕所述内部结构体的整个周边定位在所述内部结构体（27）的外周侧上，其间具有间隙; 内部电极（29），其固定在所述内部结构体（27）的外周面上; 和固定在外部结构体（23）的内周面上的外部电极（25）。燃油表（15）测量内部电极（29）和外部电极（25）之间的电容，并且检测存在于内部电极（29）和外部电极（25）之间的燃料的水平。外部结构体（23）还包括允许电荷从其外周面移动到外部电极（25）的多个外部侧通孔（31）。

10. 发明授权

EP2184227B1 LIGHTING-RESISTING FASTENER 有权
标题翻译：防雷紧固件
公开(公告)号：EP2184227B1
公开(公告)日：2013-01-09
申请号：EP08833183.0
申请日：2008-09-25
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： KASHIWAGI, Masahiro , KAMINO, Yuichiro , OGURI, Kazuyuki , TARUMI, Takeyasu , BESSHO, Masahiro , YAMAKOSHI, Hideo , ISHIKAWA, Naomoto
IPC分类号： F16B33/00 , F16B35/06 , B64D45/02 , F16B33/06 , F16B37/14
CPC分类号： B64D45/02 , F16B33/004 , F16B33/06 , F16B35/06 , F16B37/14

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