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1. 发明授权

US09090355B2 Composite tank, wing, and method for manufacturing composite tank 有权
标题翻译：复合罐，翼，及复合罐制造方法
公开(公告)号：US09090355B2
公开(公告)日：2015-07-28
申请号：US13258179
申请日：2010-03-17
申请人： Hiroaki Yamaguchi , Yuichiro Kamino , Koichi Nakamura , Tooru Hashigami
发明人： Hiroaki Yamaguchi , Yuichiro Kamino , Koichi Nakamura , Tooru Hashigami
IPC分类号： B64D15/04 , B64D37/06 , B64C3/34 , B64D37/32
CPC分类号： B64D37/06 , B64C3/34 , B64D37/32 , Y02T50/44
摘要： A composite tank that can suppress electrification, corrosion and strength degradation, a wing comprising the composite tank, and a method for manufacturing the composite tank. The composite tank comprises: a tank body inside which a combustible material is stored, having a first resin portion (11, 12) formed from a fiber reinforced resin and a metal portion formed from a metal material, a second resin portion (22) formed from a fiber reinforced resin, which covers at least those regions on the inner surface of the tank body where the first resin portion (11, 12) adjoins the metal portion, and a plurality of conductive portions (23) that enable charge transfer through the second resin portion (22), from the surface that contacts the combustible material to the first resin portion (11, 12), wherein the fiber in the second resin portion (22) has a higher electrical resistivity than fiber in the first resin portion (11, 12), and the second resin portion (22) forms a layer that isolates the first resin portion (11, 12) from the metal portion.
摘要翻译：可抑制带电，腐蚀和强度降低的复合罐，包括复合罐的翼，以及制造复合罐的方法。复合罐包括：储存有可燃材料的罐体，具有由纤维增强树脂形成的第一树脂部分（11,12）和由金属材料形成的金属部分，形成第二树脂部分（22）至少覆盖在第一树脂部分（11,12）与金属部分相邻的罐体内表面上的那些区域的多个导电部分（23），所述多个导电部分（23）能够通过第二树脂部分（22）从与可燃材料接触的表面到第一树脂部分（11,12），其中第二树脂部分（22）中的纤维具有比第一树脂部分中的纤维更高的电阻率 11,12），第二树脂部（22）形成使第一树脂部（11,12）与金属部分隔离的层。

2. 发明申请

US20120012710A1 COMPOSITE TANK, WING, AND METHOD FOR MANUFACTURING COMPOSITE TANK 有权
标题翻译：复合罐，WING和制造复合油罐的方法
公开(公告)号：US20120012710A1
公开(公告)日：2012-01-19
申请号：US13258179
申请日：2010-03-17
申请人： Hiroaki Yamaguchi , Yuichiro Kamino , Koichi Nakamura , Tooru Hashigami
发明人： Hiroaki Yamaguchi , Yuichiro Kamino , Koichi Nakamura , Tooru Hashigami
IPC分类号： B64C3/34 , B65D90/02 , B32B38/00 , B32B38/10 , B32B38/08
CPC分类号： B64D37/06 , B64C3/34 , B64D37/32 , Y02T50/44
摘要： A composite tank that can suppress electrification, corrosion and strength degradation, a wing comprising the composite tank, and a method for manufacturing the composite tank. The composite tank comprises: a tank body inside which a combustible material is stored, having a first resin portion (11, 12) formed from a fiber reinforced resin and a metal portion formed from a metal material, a second resin portion (22) formed from a fiber reinforced resin, which covers at least those regions on the inner surface of the tank body where the first resin portion (11, 12) adjoins the metal portion, and a plurality of conductive portions (23) that enable charge transfer through the second resin portion (22), from the surface that contacts the combustible material to the first resin portion (11, 12), wherein the fiber in the second resin portion (22) has a higher electrical resistivity than fiber in the first resin portion (11, 12), and the second resin portion (22) forms a layer that isolates the first resin portion (11, 12) from the metal portion.
摘要翻译：可抑制带电，腐蚀和强度降低的复合罐，包括复合罐的翼，以及制造复合罐的方法。复合罐包括：储存有可燃材料的罐体，具有由纤维增强树脂形成的第一树脂部分（11,12）和由金属材料形成的金属部分，形成第二树脂部分（22）至少覆盖在第一树脂部分（11,12）与金属部分相邻的罐体内表面上的那些区域的多个导电部分（23），所述多个导电部分（23）能够通过第二树脂部分（22）从与可燃材料接触的表面到第一树脂部分（11,12），其中第二树脂部分（22）中的纤维具有比第一树脂部分中的纤维更高的电阻率 11,12），第二树脂部（22）形成将第一树脂部（11,12）与金属部分隔离的层。

3. 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）。

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。

6. 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。

7. 发明授权

US09071050B2 Current generating device 有权
标题翻译：电流发生装置
公开(公告)号：US09071050B2
公开(公告)日：2015-06-30
申请号：US13698151
申请日：2011-05-19
申请人： Nobuyuki Kamihara , Yuichiro Kamino , Tooru Hashigami , Hiroki Makimura , Koki Higashide , Masaki Kitaoka , Naotatsu Ishimaru
发明人： Nobuyuki Kamihara , Yuichiro Kamino , Tooru Hashigami , Hiroki Makimura , Koki Higashide , Masaki Kitaoka , Naotatsu Ishimaru
IPC分类号： H02H3/08 , H02H9/02 , H02H7/06 , H02H3/087 , H03K3/53 , H02H3/05
CPC分类号： H02H7/06 , H02H3/05 , H02H3/087 , H03K3/53
摘要： Even when a large-current, high-voltage load is applied, damage is prevented. A current generating device (1) supplies a current simulating a current flowing when lightning occurs to a test piece (9) subjected to a lightning resistance test using power supplied from a power supply device (2). The current generating device (1) includes electric double-layer capacitors that store and discharge power supplied from the power supply device (2), a semiconductor switch (3) that switches between supplying and not supplying the power stored in the electric double-layer capacitors to the test piece (9), and a protection unit (4) that is connected between the semiconductor switch (3) and the test piece (9) and that cuts the connection between the semiconductor switch (3) and the test piece (9) when a current larger than a predetermined value flows through the semiconductor switch (3).
摘要翻译：即使施加大电流高压负载，也可以防止损坏。电流产生装置（1）向使用从电源装置（2）提供的电力进行耐雷电试验的试验片（9）提供模拟雷电发生的电流的电流。电流产生装置（1）包括存储和放电从电源装置（2）提供的电力的双电层电容器;半导体开关（3），其在供应和不提供存储在电双层中的功率连接在半导体开关（3）和测试片（9）之间并且切断半导体开关（3）和测试片（3）之间的连接的保护单元（4）如图9所示，当大于预定值的电流流过半导体开关（3）时。

8. 发明申请

US20130057996A1 CURRENT GENERATING DEVICE 有权
标题翻译：当前生成装置
公开(公告)号：US20130057996A1
公开(公告)日：2013-03-07
申请号：US13698151
申请日：2011-05-19
申请人： Nobuyuki Kamihara , Yuichiro Kamino , Tooru Hashigami , Hiroki Makimura , Koki Higashide , Masaki Kitaoka , Naotatsu Ishimaru
发明人： Nobuyuki Kamihara , Yuichiro Kamino , Tooru Hashigami , Hiroki Makimura , Koki Higashide , Masaki Kitaoka , Naotatsu Ishimaru
IPC分类号： H02H3/08
CPC分类号： H02H7/06 , H02H3/05 , H02H3/087 , H03K3/53
摘要： Even when a large-current, high-voltage load is applied, damage is prevented. A current generating device (1) supplies a current simulating a current flowing when lightning occurs to a test piece (9) subjected to a lightning resistance test using power supplied from a power supply device (2). The current generating device (1) includes electric double-layer capacitors that store and discharge power supplied from the power supply device (2), a semiconductor switch (3) that switches between supplying and not supplying the power stored in the electric double-layer capacitors to the test piece (9), and a protection unit (4) that is connected between the semiconductor switch (3) and the test piece (9) and that cuts the connection between the semiconductor switch (3) and the test piece (9) when a current larger than a predetermined value flows through the semiconductor switch (3).
摘要翻译：即使施加大电流高压负载，也可以防止损坏。电流产生装置（1）向使用从电源装置（2）提供的电力进行耐雷电试验的试验片（9）提供模拟雷电发生的电流的电流。电流产生装置（1）包括存储和放电从电源装置（2）提供的电力的双电层电容器;半导体开关（3），其在供应和不提供存储在电双层中的功率连接在半导体开关（3）和测试片（9）之间并且切断半导体开关（3）和测试片（3）之间的连接的保护单元（4）如图9所示，当大于预定值的电流流过半导体开关（3）时。

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