专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08634177B2 Coupling structure for airframe components 有权
标题翻译：机身部件联轴器结构
公开(公告)号：US08634177B2
公开(公告)日：2014-01-21
申请号：US13418865
申请日：2012-03-13
申请人： Koji Kawahara , Hideo Yamakoshi , Yuichiro Kamino , Atsuhiro Iyomasa , Toru Hashigami
发明人： Koji Kawahara , Hideo Yamakoshi , Yuichiro Kamino , Atsuhiro Iyomasa , Toru Hashigami
IPC分类号： H02H1/04 , H02H3/22
CPC分类号： H01R4/06 , B64C3/34 , B64D45/02 , F16B5/02 , F16B15/02 , F16B37/14 , F16B2001/0064 , H05H3/02
摘要： Provided is a coupling structure for airframe components that is capable of ensuring sufficient lightning protection capability. A conductive pattern part 40 made of a conductive material is formed around each fastener member 24 between wing surface panels 21A and 21B. The conductive pattern part 40 is formed, for example, around each of holes 21c and 21d on the plane on which the wing surface panel 21A and the wing surface panel 21B abut against each other. Then, the conductive pattern part 40 is pushed against both the wing surface panel 21A and the wing surface panel 21B by the fastening power of the fastener members 24, whereby electrical conduction between the wing surface panel 21A and the wing surface panel 21B can be achieved.
摘要翻译：提供了能够确保足够的防雷能力的机身部件的联接结构。在机翼表面面板21A和21B之间的每个紧固件24周围形成由导电材料制成的导电图案部分40。导电图案部40例如形成在机翼面板21A和翼面板21B彼此抵接的平面上的各孔21c，21d的周围。然后，通过紧固件24的紧固力将导电图案部40推压到翼面21A和翼面板21B上，由此能够实现翼面21A和翼面面板21B之间的导电。

2. 发明授权

US08587916B2 Lightning protection fastener, aircraft assembly, and method of manufacturing aircraft assembly component 有权
标题翻译：防雷紧固件，飞机组件和制造飞机组件的方法
公开(公告)号：US08587916B2
公开(公告)日：2013-11-19
申请号：US13420008
申请日：2012-03-14
申请人： Hideo Yamakoshi , Yuichiro Kamino , Yuji Asahara , Yasunori Watanabe , Atsuhiro Iyomasa , Toru Hashigami , Kohei Murakami , Tomonori Okumura
发明人： Hideo Yamakoshi , Yuichiro Kamino , Yuji Asahara , Yasunori Watanabe , Atsuhiro Iyomasa , Toru Hashigami , Kohei Murakami , Tomonori Okumura
IPC分类号： H05F3/00
CPC分类号： B64D45/02 , F16B5/0258 , F16B43/001
摘要： A long-life lightning protection fastener or the like to prevent explosion for aircrafts at low cost is provided, the fastener having a light weight, ensuring sufficient lightning protection, and having extremely less failures and high reliability. A ring-shaped ring member 40A made of resin is mounted on a collar 26. This ring member 40A is interposed between a member 22 and the collar 26 and is in intimate contact with both of the member 22 and the collar 26, thereby sealing an interface with the member 22 for sealing and preventing the occurrence of an arc at an outer perimeter edge of the collar 26.
摘要翻译：提供了一种长寿命防雷紧固件等，以便以低成本防止飞机爆炸，该紧固件具有重量轻，确保足够的防雷保护，并具有极少的故障和高的可靠性。由树脂制成的环形环构件40A安装在套环26上。该环件40A插入在构件22和套环26之间，并且与构件22和套环26两者紧密接触，从而密封与构件22接合，用于密封并防止在套环26的外周边缘处发生电弧。

3. 发明授权

US08711541B2 Lightning-protective explosion-preventive fastener 有权
标题翻译：防雷防爆紧固件
公开(公告)号：US08711541B2
公开(公告)日：2014-04-29
申请号：US13432649
申请日：2012-03-28
申请人： Soichiro Umemoto , Hideo Yamakoshi , Atsuhiro Iyomasa , Toru Hashigami
发明人： Soichiro Umemoto , Hideo Yamakoshi , Atsuhiro Iyomasa , Toru Hashigami
IPC分类号： H05F3/00
CPC分类号： B64D45/02
摘要： In an insulating cover 50A according to the present invention, a dimension of each of an outer-circumferential-side cylindrical part 50c and an inner-circumferential-side cylindrical part 50b fitting in step parts 40 and 41 in an axial direction of a fastener body 25 is set large with respect to a tip covering part 50a covering a tip surface 26a of a fastening member 26. As a result, on an outer circumferential side and an inner circumferential side of the fastening member 26, a distance from a member 22 is sufficiently ensured by the cylindrical part 50b and 50c. The tip covering part 50a is thinner than the cylindrical part 50B and 50c. Therefore, when the fastener body 25 and the fastening member 26 are fastened together, the amount of deformation of the tip covering part 50a in a thickness direction can be made small.
摘要翻译：在根据本发明的绝缘盖50A中，沿着紧固件主体的轴向安装在台阶部40和41中的外周侧圆筒部50c和内周侧圆筒部50b的尺寸 25相对于覆盖紧固部件26的前端面26a的顶部覆盖部50a设定得较大。结果，在紧固部件26的外周侧和内周侧，与部件22的距离为由圆柱形部分50b和50c充分确保。尖端覆盖部50a比圆筒部50B，50c薄。因此，当紧固件主体25和紧固构件26紧固在一起时，能够使顶部覆盖部50a在厚度方向上的变形量变小。

4. 发明申请

US20090288602A1 Electrode and Vacuum Processing Apparatus 审中-公开
标题翻译：电极和真空处理设备
公开(公告)号：US20090288602A1
公开(公告)日：2009-11-26
申请号：US12087071
申请日：2007-03-20
申请人： Kouji Satake , Satoshi Sakai , Atsuhiro Iyomasa , Toshiya Watanabe , Hideo Yamakoshi , Toshiaki Monaka
发明人： Kouji Satake , Satoshi Sakai , Atsuhiro Iyomasa , Toshiya Watanabe , Hideo Yamakoshi , Toshiaki Monaka
IPC分类号： C23C16/54
CPC分类号： H01J37/32541 , C23C16/4412 , C23C16/45578 , C23C16/509 , H01J37/3244 , H05H1/46 , H05H2001/466
摘要： An electrode and a vacuum processing apparatus are provided that are capable of improving the film deposition rate and the uniformity of the distribution of the deposited film. The electrode includes a plurality of electrodes (17A, 17B) extending from positions arranged at a predetermined interval along a surface of a substrate to be processed (3). Buffer chambers (25) each extend along and between two of the plurality of electrodes (17A, 17B). A plurality of first gas injection holes (27) are arranged in the direction in which the electrodes (17A, 17B) extend and which supply a reactant gas into the buffer chamber (25). A second gas injection hole (23) has a slit form extending in the direction in which the electrodes (17A, 17B) extend, and which supplies the reactant gas from the buffer chamber (25) toward the substrate to be processed (3).
摘要翻译：提供了能够提高成膜速度和沉积膜的分布均匀性的电极和真空处理装置。电极包括沿着待处理基板（3）的表面以预定间隔布置的位置延伸的多个电极（17A，17B）。缓冲室（25）各自沿着多个电极（17A，17B）中的两个延伸。多个第一气体喷射孔（27）沿电极（17A，17B）延伸的方向排列，并将反应气体供应到缓冲室（25）中。第二气体注入孔（23）具有沿电极（17A，17B）延伸的方向延伸的狭缝形状，并且将缓冲室（25）的反应气体朝向待处理基板（3）供给。

5. 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）。

6. 发明申请

US20130223951A1 CAP AND FIXING STRUCTURE USING THE SAME 审中-公开
标题翻译：盖和固定结构使用它
公开(公告)号：US20130223951A1
公开(公告)日：2013-08-29
申请号：US13880272
申请日：2012-04-20
申请人： Masahiro Bessho , Takamitsu Himeno , Yasunori Watanabe , Hideo Yamakoshi , Soichiro Umemoto , Wataru Nishimura , Yuichiro Kamino , Naomoto Ishikawa , Nobuyuki Kamihara , Fumitoshi Moriya , Yoshiro Aoshima , Toru Takasu
发明人： Masahiro Bessho , Takamitsu Himeno , Yasunori Watanabe , Hideo Yamakoshi , Soichiro Umemoto , Wataru Nishimura , Yuichiro Kamino , Naomoto Ishikawa , Nobuyuki Kamihara , Fumitoshi Moriya , Yoshiro Aoshima , Toru Takasu
IPC分类号： F16B37/14
CPC分类号： F16B37/14 , B64D45/02
摘要： A cap (9) that is used in a fixing structure (1) for fixing a plurality of overlaid structural members (3) by means of a fastener (5) inserted into through-holes (3a) formed in the overlaid structural members and a collar (7) fastened onto a distal end (5a) of the fastener protruding from a surface of the structural members and that is disposed so as to surround the distal end of the fastener and the collar. The cap is attached, in a non-engaged state, to the distal end of the fastener and the collar, and a concave groove (9d) that accommodates a sealant (11) to be filled in a space formed between an inner peripheral surface (9e) and the surface of the structural members is formed in the inner peripheral surface.
摘要翻译：一种用于固定结构（1）的盖（9），用于通过插入到形成在重叠的结构构件中的通孔（3a）中的紧固件（5）固定多个重叠的结构构件（3），以及紧固在从结构件的表面突出的紧固件的远端（5a）上的环（7）并且被设置成围绕紧固件和套环的远端。盖以非接合状态附接到紧固件和套环的远端，以及容纳密封剂（11）的凹槽（9d），填充在形成在内周面 9e），并且结构构件的表面形成在内周面中。

7. 发明授权

US08651413B2 Lightning-protection fastener 有权
标题翻译：防雷紧固件
公开(公告)号：US08651413B2
公开(公告)日：2014-02-18
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 , B64C1/12
CPC分类号： B64D45/02 , F16B33/004 , F16B33/06 , F16B35/06 , F16B37/14
摘要： A lightning-protection fastener is provided that is capable of reliably preventing peeling off of an insulation layer during the operation of an aircraft and 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：提供一种防雷紧固件，其能够可靠地防止在飞行器的操作期间剥离绝缘层并提高防雷击能力和可靠性。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）。

8. 发明授权

US08034177B2 Inner electrode for barrier film formation and apparatus for film formation 有权
标题翻译：用于阻挡膜形成的内部电极和用于成膜的装置
公开(公告)号：US08034177B2
公开(公告)日：2011-10-11
申请号：US11660201
申请日：2005-10-17
申请人： Seiji Goto , Hideo Yamakoshi , Atsushi Ueda , Kenichi Okamoto , Yuji Asahara , Minoru Danno
发明人： Seiji Goto , Hideo Yamakoshi , Atsushi Ueda , Kenichi Okamoto , Yuji Asahara , Minoru Danno
IPC分类号： C23C16/00 , C23C16/50 , C23F1/00 , H01L21/306
CPC分类号： C23C16/26 , C23C16/045 , C23C16/505
摘要： An inner electrode for barrier film formation is an inner electrode for barrier film formation that is inserted inside a plastic container having an opening, supplies a medium gas to the inside of the plastic container, and supplies high frequency power to an outer electrode arranged outside the plastic container, thereby generating discharge plasma on the inner surface of the plastic container to form a barrier film on the inner surface of the plastic container, and that is provided with a gas supply pipe (101) having a gas flow path (101a) to supply a medium gas (G) and an insulating member (103) screwed into an end portion of the gas supply pipe (101) to be flush therewith and having a gas outlet (102) communicated with the gas flow path (101a).
摘要翻译：用于形成阻挡膜的内部电极是插入到具有开口的塑料容器内的用于阻挡膜形成的内部电极，将中等气体供应到塑料容器的内部，并将高频电力提供给布置在外部的外部电极塑料容器，从而在塑料容器的内表面上产生放电等离子体，以在塑料容器的内表面上形成阻挡膜，并且设置有气体供给管（101），该气体供给管具有气体流路（101a）供给与气体供给管（101）的端部螺纹连接的中间气体（G）和绝缘构件（103），与该气体供给管（101）齐平并具有与气体流路（101a）连通的气体出口（102）。

9. 发明授权

US07733563B2 Optical properties restoration apparatus, the restoration method, and an optical system used in the apparatus 失效
标题翻译：光学性能恢复装置，恢复方法以及该装置中使用的光学系统
公开(公告)号：US07733563B2
公开(公告)日：2010-06-08
申请号：US11682794
申请日：2007-03-06
申请人： Satoshi Sakai , Shigenori Tsuruga , Hideo Yamakoshi , Shizuma Kuribayashi , Minoru Danno , Hiroshi Futami , Noriko Yamazaki
发明人： Satoshi Sakai , Shigenori Tsuruga , Hideo Yamakoshi , Shizuma Kuribayashi , Minoru Danno , Hiroshi Futami , Noriko Yamazaki
IPC分类号： G02B5/20
CPC分类号： G02B27/0006 , B08B7/0035 , B08B17/00 , G02B1/14
摘要： An optical system has fluoride compounds provided in an environment exposed by vacuum ultraviolet light or plasma light, which has higher photon energy than an absorption wavelength of a base stock of the optical system. 1-layer of a protective film of SiO2 or metal oxides having a film thickness of 2-20 nm is formed at least on the light irradiation side (inner side) of the optical system to prevent the stripping of the fluorine atoms from the surface of the optical system. In addition, the protective film is a 1-layer film selected from one of SiO2, MgO, TiO2, or ZrO2.
摘要翻译：光学系统具有在由真空紫外线或等离子体光暴露的环境中提供的氟化合物，其具有比光学系统的基础材料的吸收波长更高的光子能量。至少在光学系统的光照射侧（内侧）形成有SiO 2的保护膜或膜厚度为2-20nm的金属氧化物的1层，以防止氟原子从表面剥离光学系统。此外，保护膜是选自SiO 2，MgO，TiO 2或ZrO 2中的一层膜。

10. 发明申请

US20080017113A1 Inner Electrode for Barrier Film Formation and Apparatus for Film Formation 有权
标题翻译：用于阻挡膜形成的内部电极和用于成膜的装置
公开(公告)号：US20080017113A1
公开(公告)日：2008-01-24
申请号：US11660201
申请日：2005-10-17
申请人： Seiji Goto , Hideo Yamakoshi , Atsushi Ueda , Kenichi Okamoto , Yuji Asahara , Minoru Danno
发明人： Seiji Goto , Hideo Yamakoshi , Atsushi Ueda , Kenichi Okamoto , Yuji Asahara , Minoru Danno
IPC分类号： C23C16/513
CPC分类号： C23C16/26 , C23C16/045 , C23C16/505
摘要： An inner electrode for barrier film formation is an inner electrode for barrier film formation that is inserted inside a plastic container having an opening, supplies a medium gas to the inside of the plastic container, and supplies high frequency power to an outer electrode arranged outside the plastic container, thereby generating discharge plasma on the inner surface of the plastic container to form a barrier film on the inner surface of the plastic container, and that is provided with a gas supply pipe (101) having a gas flow path (101a) to supply a medium gas (G) and an insulating member (103) screwed into an end portion of the gas supply pipe (101) to be flush therewith and having a gas outlet (102) communicated with the gas flow path (101a).
摘要翻译：用于形成阻挡膜的内部电极是插入到具有开口的塑料容器内的用于阻挡膜形成的内部电极，将中等气体供应到塑料容器的内部，并将高频电力提供给布置在外部的外部电极塑料容器，从而在塑料容器的内表面上产生放电等离子体，在塑料容器的内表面上形成阻挡膜，并且设置有具有气体流路（101a）的气体供给管（101）供给与气体供给管（101）的端部螺纹连接的中间气体（G）和绝缘部件（103），与该气体流通通路（101a）连通的气体出口（102）。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式