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1. 发明授权

US08678320B2 Aircraft fuel tank 有权
标题翻译：飞机油箱
公开(公告)号：US08678320B2
公开(公告)日：2014-03-25
申请号：US13131063
申请日：2009-06-24
申请人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri
发明人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri
IPC分类号： B64D37/02
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且在多个位置处接地（27），以及具有半导体的管外表面层一体地形成在罐内的管子的外表面上的诸如补充管（17），供应管（19）和气管（21）的特性。

2. 发明申请

US20110297790A1 AIRCRAFT FUEL TANK 有权
标题翻译：飞机燃油箱
公开(公告)号：US20110297790A1
公开(公告)日：2011-12-08
申请号：US13201916
申请日：2010-03-26
申请人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri , Koichi Nakamura
发明人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri , Koichi Nakamura
IPC分类号： B64D37/06
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。飞机燃料箱包括表现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）的位置中一体地形成在上皮肤（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）。

3. 发明申请

US20130152821A1 ANTISTATIC COATING, STRUCTURE MADE OF COMPOSITE MATERIAL USING SAME, AND PRODUCTION METHOD THEREFOR 审中-公开
标题翻译：抗静电涂料，使用其的复合材料的结构及其生产方法
公开(公告)号：US20130152821A1
公开(公告)日：2013-06-20
申请号：US13818881
申请日：2011-06-30
申请人： Yuichiro Kamino , Kazuyuki Oguri , Hiroaki Yamaguchi
发明人： Yuichiro Kamino , Kazuyuki Oguri , Hiroaki Yamaguchi
IPC分类号： C09D5/08
CPC分类号： C09D5/08 , C08J7/047 , C08K3/08 , C08K7/04 , C08K2003/0806 , C09D5/24 , C09D7/70
摘要： Provided is a coating material that can prevent galvanic corrosion and is resistant to electrostatic charging. An antistatic coating comprising a primer containing either an inorganic fiber comprising Si, Ti or Zr, C, and O, or an Ag filler. Further, a structure made of a composite material which is resistant to galvanic corrosion and electrostatic charging is obtained by applying the antistatic coating containing either an inorganic fiber comprising Si, Ti or Zr, C, and O, or an Ag filler to the surface of the structure made of a composite material to form a layers.
摘要翻译：提供能够防止电偶腐蚀并且耐静电的涂料。一种抗静电涂层，其包含含有包含Si，Ti或Zr，C和O的无机纤维或Ag填料的底漆。此外，通过将包含Si，Ti或Zr，C和O的无机纤维或Ag填料的抗静电涂层施加到表面，获得由耐电镀腐蚀和静电充电的复合材料制成的结构由复合材料制成的结构形成层。

4. 发明授权

US08550403B2 Aircraft fuel tank 有权
标题翻译：飞机油箱
公开(公告)号：US08550403B2
公开(公告)日：2013-10-08
申请号：US13201916
申请日：2010-03-26
申请人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri , Koichi Nakamura
发明人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri , Koichi Nakamura
IPC分类号： B64D37/04
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。飞机燃料箱包括表现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）的位置中一体地形成在上皮肤（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. 发明申请

US20110284694A1 AIRCRAFT FUEL TANK 有权
标题翻译：飞机燃油箱
公开(公告)号：US20110284694A1
公开(公告)日：2011-11-24
申请号：US13131063
申请日：2009-06-24
申请人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri
发明人： Hiroaki Yamaguchi , Yuichiro Kamino , Tooru Hashigami , Kazuyuki Oguri
IPC分类号： B64D37/02 , B64D45/02 , B64D37/32
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且在多个位置处接地（27），以及具有半导体的管外表面层一体地形成在罐内的管子的外表面上的诸如补充管（17），供应管（19）和气管（21）的特性。

6. 发明申请

US20100320315A1 LIGHTNING-PROTECTION FASTENER 有权
标题翻译：防雷保护紧固件
公开(公告)号：US20100320315A1
公开(公告)日：2010-12-23
申请号：US12677380
申请日：2008-09-25
申请人： Masahiro Kashiwagi , Yuichiro Kamino , Kazuyuki Oguri , Takeyasu Tarumi , Masahiro Bessho , Hideo Yamakoshi , Naomoto Ishikawa
发明人： Masahiro Kashiwagi , Yuichiro Kamino , Kazuyuki Oguri , Takeyasu Tarumi , Masahiro Bessho , Hideo Yamakoshi , Naomoto Ishikawa
IPC分类号： B64D45/02
CPC分类号： B64D45/02 , F16B33/004 , F16B33/06 , F16B35/06 , F16B37/14
摘要： Provided is a lightning-protection fastener that is capable of reliably preventing peeling off of an insulation layer during the operation of an aircraft and of improving the anti-lightning-strike capability and reliability. There is a lightning-protection fastener that fastens a skin of an aircraft and a structural member positioned inside the skin, in which an insulation layer is melt adhered so as to cover one end surface of a head portion and also to mechanically engage with a fastener-side engagement portion (engagement portion) formed on the end surface.
摘要翻译：本发明提供一种能够可靠地防止飞机运转时的绝缘层的剥离以及提高防雷击能力和可靠性的防雷紧固件。存在一个防雷紧固件，其紧固飞机的外观和定位在皮肤内部的结构构件，其中绝缘层被熔化粘附以覆盖头部的一个端面并且还与紧固件机械接合形成在端面上的侧面接合部（接合部）。

7. 发明授权

US08413929B2 Aircraft assembly 有权
标题翻译：飞机组装
公开(公告)号：US08413929B2
公开(公告)日：2013-04-09
申请号：US12739060
申请日：2009-03-23
申请人： Yuichiro Kamino , Kazuyuki Oguri , Koichi Nakamura
发明人： Yuichiro Kamino , Kazuyuki Oguri , Koichi Nakamura
IPC分类号： B64C1/12 , B64D45/02
CPC分类号： B64C3/26 , B29C65/562 , B29C65/564 , B29C66/1122 , B29C66/43441 , B29C66/474 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72321 , B29C66/742 , B29C70/088 , B29C70/885 , B29D99/001 , B29K2105/06 , B29K2305/02 , B29K2305/10 , B29K2307/00 , B29K2309/08 , B29K2705/10 , B29K2995/0005 , B29L2009/003 , B29L2031/3082 , B29L2031/3085 , B64D45/02 , F16B33/004 , F16B35/06 , F16B37/14 , B29K2307/04 , B29K2079/08 , B29K2071/00
摘要： An aircraft assembly is equipped with a lightning protection structure that is not easily destroyed by lightning current and that is highly reliable. The aircraft assembly includes a skin in which a CFRP layer serves as a main structure, a shear-tie that supports the skin from the inside, and a fastener that couples the skin and the shear-tie. A copper foil and an outside GRFP layer are provided on an outer surface side of the skin, in this order towards the outside, and a copper paint layer, which contains copper powder, is provided on the outside GFRP layer.
摘要翻译：飞机组件配有防雷结构，不易受雷击电流的破坏，高可靠性。飞行器组件包括其中CFRP层用作主要结构的皮肤，从内部支撑皮肤的剪切带以及连接皮肤和剪切带的紧固件。在外表面侧设置铜箔和外部GRFP层，朝向外侧依次设置有铜箔和外部GRFP层，在外部GFRP层上设置有含有铜粉末的铜涂层。

8. 发明申请

US20090173828A1 Fastener 有权
标题翻译：紧固件
公开(公告)号：US20090173828A1
公开(公告)日：2009-07-09
申请号：US12227642
申请日：2007-06-11
申请人： Kazuyuki Oguri , Yuichiro Kamino
发明人： Kazuyuki Oguri , Yuichiro Kamino
IPC分类号： B64C1/12 , F16B1/00
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：提供了一种紧固件，其具有强大的强度，并且还可以应用于其中考虑到冲洗表面设备并且可以容易且快速地制造并且制造成本降低的位置。紧固件（1）连接飞机的皮肤和位于皮肤内部的结构材料，并且冲洗头（3）的一个端面被绝缘体层（5）覆盖。

9. 发明申请

US20070081874A1 Fastener 有权
标题翻译：紧固件
公开(公告)号：US20070081874A1
公开(公告)日：2007-04-12
申请号：US11529244
申请日：2006-09-29
申请人： Yuichiro Kamino , Kazuyuki Oguri , Makoto Senda , Takahiro Sekigawa , Akiko Inoue
发明人： Yuichiro Kamino , Kazuyuki Oguri , Makoto Senda , Takahiro Sekigawa , Akiko Inoue
IPC分类号： F16B37/14
CPC分类号： B64D45/02 , F16B11/00 , F16B35/06 , F16B37/14 , F16B2001/0064
摘要： There is provided a fastener able to prevent damage due to environmental factors such as ultraviolet rays, and impact from sanddust, lumps of ice, and raindrops without obstructing a flow of electric shock current that flows along a top surface of an outer skin. The fastener connects an outer skin of an aircraft to a structural member positioned inside this outer skin, and is provided with a dielectric layer arranged to cover one end surface of a head section, and a conductive layer arranged to cover one end surface of this dielectric layer.
摘要翻译：提供了一种紧固件，其能够防止由于诸如紫外线的环境因素以及来自沙尘，冰块和雨滴的冲击而造成的损坏，而不会阻碍沿着外皮的顶表面流动的电击电流。紧固件将飞行器的外皮连接到位于该外皮内部的结构构件，并且设置有布置成覆盖头部的一个端面的介电层和布置成覆盖该电介质的一个端面的导电层层。

10. 发明申请

US20100224724A1 AIRCRAFT ASSEMBLY 有权
标题翻译：飞机装配
公开(公告)号：US20100224724A1
公开(公告)日：2010-09-09
申请号：US12739060
申请日：2009-03-23
申请人： Yuichiro Kamino , Kazuyuki Oguri , Koichi Nakamura
发明人： Yuichiro Kamino , Kazuyuki Oguri , Koichi Nakamura
IPC分类号： B64D45/02
CPC分类号： B64C3/26 , B29C65/562 , B29C65/564 , B29C66/1122 , B29C66/43441 , B29C66/474 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72321 , B29C66/742 , B29C70/088 , B29C70/885 , B29D99/001 , B29K2105/06 , B29K2305/02 , B29K2305/10 , B29K2307/00 , B29K2309/08 , B29K2705/10 , B29K2995/0005 , B29L2009/003 , B29L2031/3082 , B29L2031/3085 , B64D45/02 , F16B33/004 , F16B35/06 , F16B37/14 , B29K2307/04 , B29K2079/08 , B29K2071/00
摘要： Provided is an aircraft assembly equipped with a lightning protection structure that is not easily destroyed by lightning current and that is highly reliable. In an aircraft assembly including a skin (10) in which a CFRP layer (12) serves as a main structure; a shear-tie (11) that support the skin (10) from the inside; and a fastener (1) that couples the skin (10) and the shear-tie (11), a copper foil (13) and an outside GRFP layer (14) are provided on an outer surface side of the skin (10), in this order towards the outside, and a copper paint layer (19), which contains copper powder, is provided on the outside GFRP layer (14).
摘要翻译：提供了一种装备有雷电保护结构的飞机组件，其不易被雷电流破坏并且是高度可靠的。在包括其中CFRP层（12）用作主结构的皮肤（10）的飞行器组件中; 从内部支撑皮肤（10）的剪切带（11）; 在所述皮肤（10）的外表面侧设置有连接所述皮肤（10）和所述剪切带（11）的铜箔（13）和外部GRFP层（14）的紧固件（1）并且在外部GFRP层（14）上设置含有铜粉末的铜漆层（19）。

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