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

US09239112B2 Metal gasket 有权
标题翻译：金属垫片
公开(公告)号：US09239112B2
公开(公告)日：2016-01-19
申请号：US12311713
申请日：2007-12-27
申请人： Kenji Uchida , Toru Takasu , Kazuya Yoshijima
发明人： Kenji Uchida , Toru Takasu , Kazuya Yoshijima
IPC分类号： F16J15/08
CPC分类号： F16J15/0825 , F16J2015/085 , F16J2015/0862 , F16J2015/0868 , F16J2015/0875
摘要： A metal gasket 10 includes a pair of bead plates 14 and 14 having a cylinder hole 12 corresponding to a cylinder bore, a full bead 22 surrounding the cylinder hole, a first intermediate plate 18 interposed between the pair of bead plates, and a shim plate 16 interposed between the first intermediate plate and one bead plate in an area around the cylinder hole. The shim plate 16 is disposed to overlap with the full bead 22, and the thickness of a contact portion 19 to contact with the shim plate 16 of the first intermediate plate changes in the peripheral direction of the cylinder hole.
摘要翻译：金属垫圈10包括一对胎圈板14和14，其具有对应于缸孔的缸孔12，围绕缸孔的整个胎圈22，插入在一对胎圈板之间的第一中间板18和垫板 16插入在第一中间板和一个胎圈板之间的区域中。垫板16设置成与整个胎圈22重叠，并且与第一中间板的垫板16接触的接触部分19的厚度在缸孔的周向方向上变化。

2. 发明申请

US20100025940A1 Metal gasket 有权
标题翻译：金属垫片
公开(公告)号：US20100025940A1
公开(公告)日：2010-02-04
申请号：US12311713
申请日：2007-12-27
申请人： Kenji Uchida , Toru Takasu , Kazuya Yoshijima
发明人： Kenji Uchida , Toru Takasu , Kazuya Yoshijima
IPC分类号： F02F11/00
CPC分类号： F16J15/0825 , F16J2015/085 , F16J2015/0862 , F16J2015/0868 , F16J2015/0875
摘要： The effective utilization of the elasticity of a full bead is prevented from being interfered by a thickness portion of the shim plate by providing a shim plate inside a full bead, thereby a lowering of the follow-up performance to head amplitude at the time of combustion is prevented, and the improvement of the sealability is achieved.A metal gasket 10 includes a pair of bead plates 14 and 14 having a cylinder hole 12 corresponding to a cylinder bore and a full bead 22 surrounding the cylinder hole, a first intermediate plate 18 interposed between the pair of bead plates, and a shim plate 16 interposed between the first intermediate plate and one bead plate in an area around the cylinder hole. The shim plate 16 is disposed to overlap with the full bead 22, and the thickness of a contact portion 19 to contact the shim plate 16 of the first intermediate plate changes in the peripheral direction of the cylinder hole.
摘要翻译：通过在整个焊道内部设置垫板，防止整个焊道的弹性的有效利用被垫片的厚度部分所干扰，从而降低燃烧时的磁头振幅的跟踪性能并且可以实现密封性的提高。金属垫圈10包括一对胎圈板14和14，其具有对应于缸孔的缸孔12和围绕缸孔的全胎22，夹在一对胎圈板之间的第一中间板18和垫板 16插入在第一中间板和一个胎圈板之间的区域中。垫板16设置成与整个胎圈22重叠，并且接触第一中间板的垫板16的接触部分19的厚度在缸孔的周向方向上变化。

3. 发明授权

US08960681B2 Cylinder head gasket 有权
标题翻译：气缸盖垫片
公开(公告)号：US08960681B2
公开(公告)日：2015-02-24
申请号：US12737268
申请日：2009-07-06
申请人： Yasumaro Takeda , Toru Takasu , Ryosuke Fujiki , Kazuya Yoshijima , Yoshihiko Masuda
发明人： Yasumaro Takeda , Toru Takasu , Ryosuke Fujiki , Kazuya Yoshijima , Yoshihiko Masuda
IPC分类号： F02F11/00 , F16J15/08
CPC分类号： F16J15/0831 , F16J15/0825 , F16J2015/085 , F16J2015/0856 , F16J2015/0862 , F16J2015/0868
摘要： A cylinder head gasket 1 is sandwiched between a cylinder head 2 and a cylinder block 3 with a cylinder bore 4 and includes a substrate 10 with a combustion chamber hole 14 drilled at a position of the cylinder bore 4, and seal plates 11 to 13, the substrate 10 and the seal plates are stacked on one another. Fixation members 21 and 22 are secured to the substrate around a periphery of the combustion chamber hole. The seal plates include an engagement hole 23 formed therein and with which the fixation members are engaged. The engagement hole is engaged with the fixation members. The fixation members are sandwiched between the cylinder head and the cylinder block. The cylinder head and the cylinder block can be firmly coupled together via the fixation members.
摘要翻译：气缸盖垫片1夹在气缸盖2和具有气缸孔4的气缸体3之间，并且包括在气缸孔4的位置处钻有燃烧室孔14的基板10和密封板11至13，基板10和密封板彼此堆叠。固定构件21和22在燃烧室孔的周围固定到基板。密封板包括形成在其中的接合孔23，固定构件与其接合。接合孔与固定构件接合。固定构件夹在气缸盖和气缸体之间。气缸盖和气缸体可以通过固定构件牢固地连接在一起。

4. 发明申请

US20110095492A1 CYLINDER HEAD GASKET 有权
标题翻译：气缸头垫
公开(公告)号：US20110095492A1
公开(公告)日：2011-04-28
申请号：US12737268
申请日：2009-07-06
申请人： Yasumaro Takeda , Toru Takasu , Ryosuke Fujiki , Kazuya Yoshijima , Yoshihiko Masuda
发明人： Yasumaro Takeda , Toru Takasu , Ryosuke Fujiki , Kazuya Yoshijima , Yoshihiko Masuda
IPC分类号： F02F11/00
CPC分类号： F16J15/0831 , F16J15/0825 , F16J2015/085 , F16J2015/0856 , F16J2015/0862 , F16J2015/0868
摘要： A cylinder head gasket 1 is sandwiched between a cylinder head 2 and a cylinder block 3 with a cylinder bore 4 and includes a substrate 10 with a combustion chamber hole 14 drilled at a position of the cylinder bore 4, and seal plates 11 to 13, the substrate 10 and the seal plates are stacked on one another. Fixation members 21 and 22 are secured to the substrate around a periphery of the combustion chamber hole. The seal plate includes an engagement hole 23 formed therein and with which the fixation members are engaged. The engagement hole is engaged with the fixation members. The fixation members are sandwiched between the cylinder head and the cylinder block. The cylinder head and the cylinder block can be firmly coupled together via the fixation members. This allows deformation of the cylinder block caused by explosion pressure in an engine to be suppressed. As a result, possible degradation of sealability can be prevented.
摘要翻译：气缸盖垫片1夹在气缸盖2和具有气缸孔4的气缸体3之间，并且包括在气缸孔4的位置处钻有燃烧室孔14的基板10和密封板11至13，基板10和密封板彼此堆叠。固定构件21和22在燃烧室孔的周围固定到基板。密封板包括形成在其中并与固定构件接合的接合孔23。接合孔与固定构件接合。固定构件夹在气缸盖和气缸体之间。气缸盖和气缸体可以通过固定构件牢固地连接在一起。由此，能够抑制发动机的爆炸压力引起的缸体的变形。结果，可以防止密封性的降低。

5. 发明授权

US08967543B2 Aircraft ice protection system and aircraft provided with the same 有权
标题翻译：飞机防冰系统和飞机提供的相同
公开(公告)号：US08967543B2
公开(公告)日：2015-03-03
申请号：US13816562
申请日：2011-08-30
申请人： Isao Saito , Tatsuo Ishiguro , Shigeki Abe , Hideaki Tanaka , Toru Takasu , Motohiro Atsumi , Masakazu Nakanishi , Minoru Kamogari
发明人： Isao Saito , Tatsuo Ishiguro , Shigeki Abe , Hideaki Tanaka , Toru Takasu , Motohiro Atsumi , Masakazu Nakanishi , Minoru Kamogari
IPC分类号： B64D15/02 , F01D25/02 , B64D15/04
CPC分类号： F01D25/02 , B64D15/04
摘要： An aircraft ice protection system is provided for preventing ice accretion on a wing of an aircraft or removing the accreted ice. Bleed air extracted from a main engine of the aircraft and air introduced from an air intake installed on an airframe and heated by a heat source of the airframe of the aircraft are selectively supplied to a hot air chamber formed inside the wing, thereby carrying out ice protection.
摘要翻译：提供了一种飞机防冰系统，用于防止飞机机翼上的积冰或排除积冰。从飞机的主发动机抽出的排出的空气和从安装在机身上的进气引入并由飞机的机体的热源加热的空气被选择性地供应到形成在机翼内部的热空气室，从而进行冰保护。

6. 发明授权

US06659704B2 Loading bridge for air cargo loading 失效
公开(公告)号：US06659704B2
公开(公告)日：2003-12-09
申请号：US10132728
申请日：2002-04-26
申请人： Yugo Fukuhara , Toru Takasu
发明人： Yugo Fukuhara , Toru Takasu
IPC分类号： B64F1305
CPC分类号： B64F1/3055
摘要： In the conventional air cargo transportation system, the transportation of the cargo that is stored inside of the airport terminal building, to the area of the loading/unloading door is normally performed using the package/cargo carts. However, numerous workers were needed to load the cargo and drive the carts, which is very labor intensive and entails high manpower costs. The conventional system is also dangerous as they move along the complex tarmac markings. To solve these problems, this invention discloses a loading bridge which employs a cargo conveyor line comprising a transport means such as a conveyer, which can be extended or retracted, that connects with a rotunda extending from the airport terminal building; a cargo conveyor junction having a means to change the direction of the cargo conveyance by rotating the conveyor surface or changing its angle to alter the direction of the cargo conveyance to match the next conveyor line; and another cargo conveyor line to reach the cargo loading/unloading door of the aircraft, to thereby enable the automated conveyance of cargo for the aircraft from the airport terminal cargo holding area to the cargo door of the aircraft to eliminate the possibility of equipment collisions, to reduce manpower costs, and to shorten the time required for loading the aircraft.

7. 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。

8. 发明申请

US20130195658A1 AIRCRAFT ICE PROTECTION SYSTEM AND AIRCRAFT PROVIDED WITH THE SAME 有权
标题翻译：飞机冰保护系统和飞机提供
公开(公告)号：US20130195658A1
公开(公告)日：2013-08-01
申请号：US13816562
申请日：2011-08-30
申请人： Isao Saito , Tatsuo Ishiguro , Shigeki Abe , Hideaki Tanaka , Toru Takasu , Motohiro Atsumi , Masakazu Nakanishi , Minoru Kamogari
发明人： Isao Saito , Tatsuo Ishiguro , Shigeki Abe , Hideaki Tanaka , Toru Takasu , Motohiro Atsumi , Masakazu Nakanishi , Minoru Kamogari
IPC分类号： F01D25/02
CPC分类号： F01D25/02 , B64D15/04
摘要： An aircraft ice protection system is provided for preventing ice accretion on a wing of an aircraft or removing the accreted ice. Bleed air extracted from a main engine of the aircraft and air introduced from an air intake installed on an airframe and heated by a heat source of the airframe of the aircraft are selectively supplied to a hot air chamber formed inside the wing, thereby carrying out ice protection.
摘要翻译：提供了一种飞机防冰系统，用于防止飞机机翼上的积冰或排除积冰。从飞机的主发动机抽出的排出的空气和从安装在机身上的进气引入并由飞机的机体的热源加热的空气被选择性地供应到形成在机翼内部的热空气室，从而进行冰保护。

9. 发明授权

US07343995B2 Air cargo transport system 失效
标题翻译：空运货物运输系统
公开(公告)号：US07343995B2
公开(公告)日：2008-03-18
申请号：US10132741
申请日：2002-04-26
申请人： Yugo Fukuhara , Toru Takasu
发明人： Yugo Fukuhara , Toru Takasu
IPC分类号： B62D1/24
CPC分类号： B64F1/368 , B64F1/00 , B64F1/3055 , B64F1/32
摘要： The cargo transport system according to this invention employs a tow vehicle that can automatically follow and run upon guide lines. The tow vehicle can tow cargo laden equipment such as container dollies to thereby automatically transport the air cargo. The air cargo is conveyed by an underground air cargo conveyor mechanism which has the conveyor line including the guide line installed underground to link the air cargo holding area in the airport terminal building and the aircraft parking area. Further, the system connects the loading/unloading cargo door of the aircraft and the underground loading/unloading position for the underground air cargo conveyor mechanism by an air cargo elevator.
摘要翻译：根据本发明的货物运输系统采用能够自动跟随并在导向线上运行的牵引车辆。牵引车辆可以拖曳货物装载如货柜车从而自动运送空运货物。空运货物由地下空运货物输送机构输送，该机械具有输送线，该输送线包括地下安装的引导线，以连接机场候机楼大楼的空运货舱区和飞机停放区。此外，系统通过空运货梯将地下空运货物输送机构的装卸货物门与地下装卸位置连接起来。

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