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1. 发明申请

US20170368764A1 POLYUREA PERIMETER SEAL FOR AN AIRCRAFT ANTENNA OR OTHER AIRCRAFT PART 审中-公开
公开(公告)号：US20170368764A1
公开(公告)日：2017-12-28
申请号：US15683219
申请日：2017-08-22
申请人： THE PATENT WELL LLC
发明人： Jeff Busby , Chad Knight , Kent Boomer , Mike Dry , Matt Boyd
IPC分类号： B29C65/48 , B64C1/36 , F16J15/10 , H01Q1/28 , B29K105/00
CPC分类号： B29C65/4805 , B29K2105/0026 , B64C1/36 , C08G2190/00 , F16J15/065 , F16J15/102 , F16J15/108 , F16J15/14 , H01Q1/28
摘要： A sealant is provided for use on an aircraft or other vehicle. The sealant may be used with a gasket. The sealant is a perimeter seal that comprises a polyurea member. The polyurea member is a self-curing, two-component mix. It may cure to a hardness in the range of about 40 to 100 (Shore A). It may maintain an adequate peel strength to withstand multiple thermal and pressure cycling, and may have a working life, wherein it may be shaped, of less than about eleven minutes.

2. 发明申请

US20170157840A1 METHOD FOR SEALING A JOINT 有权
公开(公告)号：US20170157840A1
公开(公告)日：2017-06-08
申请号：US15297184
申请日：2016-10-19
申请人： TOLI Corporation
发明人： Atsushi Kodera , Shinichi Kotani , Hidenori Wada , Kazuki Yoshikawa , Masaaki Inuma
IPC分类号： B29C65/50 , B29C35/08 , B29C65/54 , B29C65/00 , F16J15/02 , B29C65/48
CPC分类号： B29C65/5042 , B29C35/0805 , B29C37/04 , B29C65/48 , B29C65/4815 , B29C65/4845 , B29C65/4895 , B29C65/5028 , B29C65/524 , B29C65/542 , B29C66/1142 , B29C66/14 , B29C66/32 , B29C66/43 , B29C66/435 , B29C66/71 , B29C66/73921 , B29C2035/0827 , B29K2027/06 , B29L2031/732 , E04F15/02016 , E04F21/1652 , F16J15/14 , B29K2023/00
摘要： Provided is a joint treatment method that enables smooth joint treatment without damaging the ultraviolet radiation curable resin formed on the interior sheet surface. The joint treatment method is for joining a butt joint portion of interior sheets, the protective layer being formed as a surface layer of each of the interior sheets. The method includes: (1) a step of injecting a joint treatment agent, which has no dissolving ability with respect to at least the protective layer, into the butt joint portion; and (2) a step of attaching, before the injected joint treatment agent is cured, an adhesive tape so as to straddle the butt joint portion such that the tape is in contact with the protective layer and the joint treatment agent present in the butt joint portion.

3. 发明授权

US09671023B2 Spacer and gasket assembly for use on an aircraft 有权
公开(公告)号：US09671023B2
公开(公告)日：2017-06-06
申请号：US14698416
申请日：2015-04-28
申请人： AVIATION DEVICES & ELECTRONIC COMPONENTS, LLC
发明人： Matt Boyd , David Schmidt , Jeff Busby
IPC分类号： B29C65/00 , F16J15/06 , B64C1/18 , F16J15/10 , F16J15/12 , F16J15/14 , H01Q1/28
CPC分类号： F16J15/061 , B64C1/18 , F16J15/104 , F16J15/122 , F16J15/127 , F16J15/14 , H01Q1/283 , Y10T29/49622
摘要： A spacer and gasket assembly is shown for receipt between a static structure having a surface and fastener holes therethrough and a removable structure having a surface and fastener holes. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing surfaces. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a sticky, deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness. The spacer and the gasket are adapted to be placed substantially between the facing walls of the static structure and the removable structure and the removable structure will compress and deform the gasket when the fasteners are torqued down.

4. 发明授权

US09568035B2 Fastener joint with sealing gasket 有权
标题翻译：带密封垫片的紧固件接头
公开(公告)号：US09568035B2
公开(公告)日：2017-02-14
申请号：US13744054
申请日：2013-01-17
申请人： Airbus Operations Limited
发明人： Colin John West , David Alistair Sutton
IPC分类号： F16J15/14 , F16B19/00 , F16B33/00 , F16B43/00
CPC分类号： F16B19/008 , F16B33/004 , F16B43/001 , F16J15/14 , Y10T29/49947 , Y10T403/52
摘要： A joint comprising: a first component having a face and a bore defined by a bore wall; a second component; a fastener joining the first component to the second component, the fastener comprising a head and a shaft protruding from the head; and a polysulphide gasket comprising a ring which is compressed between the head of the fastener and the face of the first component; and a collar between the shaft of the fastener and the bore wall. The gasket comprises a ring of sealing material surrounding a hole for receiving a fastener, the sealing material comprising an at least partially cured polysulphide sealant. The gasket has a region of increased thickness positioned towards the inner periphery of the ring which flows to form the collar.
摘要翻译：一种接头，包括：具有由孔壁限定的面和孔的第一部件; 第二个组成部分将所述第一部件连接到所述第二部件的紧固件，所述紧固件包括头部和从所述头部突出的轴; 以及多硫化物垫圈，其包括在紧固件的头部和第一部件的表面之间被压缩的环; 以及紧固件的轴和孔壁之间的套环。垫圈包括围绕用于接收紧固件的孔的密封材料环，密封材料包括至少部分固化的聚硫化物密封剂。垫圈具有朝向环的内周边定位的厚度增加的区域，该区域流动以形成套环。

5. 发明申请

US20170021559A1 AUTOMATED TREATMENT PROCESS AND APPARATUS 审中-公开
标题翻译：自动处理工艺及设备
公开(公告)号：US20170021559A1
公开(公告)日：2017-01-26
申请号：US15215850
申请日：2016-07-21
申请人： FORD GLOBAL TECHNOLOGIES, LLC
发明人： Tsunou Chang , Jonathan Richard Bishop
IPC分类号： B29C65/48 , F02F7/00 , F01M11/00 , F02F11/00
CPC分类号： B29C65/48 , B05C5/0212 , B05C5/0216 , B29L2031/26 , F01M11/0004 , F01M2011/0062 , F02F7/0095 , F02F11/002 , F16J15/14
摘要： An automated sealing process (100) for sealing a casing, the casing comprising a first casing portion (107) having a first sealing surface (115), and a second casing portion having a second sealing surface configured to engage the first sealing surface (115), the first casing portion (107) being assembled from at least two components such that the first sealing surface (115) comprises a joint (100) between the components, the process (100) comprising: applying a surface treatment to the joint (117) of the first sealing surface (115) using an automated treatment apparatus (101); and applying a sealant to at least one of the first sealing surface (115) and the second sealing surface prior to bringing the first and second sealing surfaces into engagement.
摘要翻译：一种用于密封壳体的自动密封过程（100），所述壳体包括具有第一密封表面（115）的第一壳体部分（107）和具有构造成接合所述第一密封表面（115）的第二密封表面的第二壳体部分），所述第一壳体部分（107）由至少两个部件组装，使得所述第一密封表面（115）包括所述部件之间的接头（100），所述方法（100）包括：对所述接头施加表面处理（ 117）使用自动化处理装置（101）; 以及在使所述第一和第二密封表面接合之前，将密封剂施加到所述第一密封表面（115）和所述第二密封表面中的至少一个。

6. 发明授权

US09394436B2 Form in-place gasket with tack free surface 有权
标题翻译：形成就地垫圈，具有无粘性表面
公开(公告)号：US09394436B2
公开(公告)日：2016-07-19
申请号：US14010228
申请日：2013-08-26
申请人： Aysegul Kascatan Nebioglu , Marufur Rahim
发明人： Aysegul Kascatan Nebioglu , Marufur Rahim
IPC分类号： C08L33/14 , B32B27/40 , F16J15/14 , C08G18/48 , C08G18/67 , C09D175/16
CPC分类号： C08L33/14 , B32B27/40 , C08G18/4854 , C08G18/672 , C09D175/16 , F16J15/14 , Y10T428/31551 , C08G18/48
摘要： A method of preparing a flexible, substantially tack free gasket by forming a liquid composition which is a radiation polymerizable admixture of a free radical polymerizable urethane(meth)acrylate monomer, free radical polymerizable urethane(meth)acrylate oligomer, or combinations thereof; a free radical polymerizable diluent; a free radical polymerization photoinitiator; a wax; a thixotropic agent; and optionally an adhesion promoter and a colorant. The composition is distributed onto a substrate and then exposed to actinic radiation to cure the liquid composition into a flexible, substantially tack free gasket having a Shore A hardness of from about A20 to about A80.
摘要翻译：通过形成可自由基聚合的氨基甲酸酯（甲基）丙烯酸酯单体，可自由基聚合的氨基甲酸酯（甲基）丙烯酸酯低聚物或其组合的可辐射聚合的混合物的液体组合物来制备柔性的，基本上无粘性的垫片的方法; 可自由基聚合的稀释剂; 自由基聚合光引发剂; 蜡触变剂; 和任选的粘合促进剂和着色剂。将组合物分布在基底上，然后暴露于光化辐射，以将液体组合物固化成具有约A20至约A80的肖氏A硬度的柔性基本上无粘性垫片。

7. 发明授权

US09347563B2 Gas lock, and coating apparatus comprising a gas lock 有权
标题翻译：气锁和包括气锁的涂覆装置
公开(公告)号：US09347563B2
公开(公告)日：2016-05-24
申请号：US13881068
申请日：2011-10-20
申请人： David Pocza , Stefan Reber , Martin Arnold , Norbert Schillinger
发明人： David Pocza , Stefan Reber , Martin Arnold , Norbert Schillinger
IPC分类号： F16K11/20 , F16J15/14 , C23C14/56 , C23C16/455 , C23C16/52 , C23C16/54
CPC分类号： F16J15/14 , C23C14/56 , C23C16/45506 , C23C16/45589 , C23C16/45591 , C23C16/52 , C23C16/54 , Y10T137/0318 , Y10T137/2224
摘要： The present invention relates to a gas lock for separating two gas chambers, which while taking up minimal space makes it possible to achieve the separation of gases without contact with the product/educt/transporting system. The gas lock according to the invention is distinguished in that at least one means for manipulation of the flow is present in a flow passage of the gas lock. Also, the present invention relates to a coating device which comprises a gas lock according to the invention. Also provided are possibilities for using the gas lock according to the invention.
摘要翻译：本发明涉及一种用于分离两个气室的气锁，其在占用最小空间的同时，可以实现气体的分离，而不与产品/喷射/输送系统接触。根据本发明的气锁的特征在于，在气锁的流动通道中存在至少一个用于操纵流动的装置。此外，本发明涉及一种包括根据本发明的气锁的涂覆装置。还提供了使用根据本发明的气锁的可能性。

8. 发明申请

US20160116064A1 SEALING ASSEMBLY BETWEEN COMPONENTS 审中-公开
标题翻译：密封组件之间的密封
公开(公告)号：US20160116064A1
公开(公告)日：2016-04-28
申请号：US14990829
申请日：2016-01-08
申请人： Caterpillar Inc.
发明人： Scott D. Larson , Richard A. Matzelle , Cole C. Deichert
IPC分类号： F16J15/14 , G02F1/01 , F16J15/10
CPC分类号： F16J15/14 , F16J15/10 , G02F1/133308
摘要： A sealing assembly between a first component and a second component is provided. The sealing assembly includes a first flange extending from the first component. The first flange includes a first mating surface. The sealing assembly further includes a second flange extending from the second component. The second flange includes a second mating surface adapted to abut the first mating surface of the first flange. The second flange further includes a slanted surface extending from the second mating surface at an angle with respect to the second mating surface of the second flange. The slanted surface is being disposed at an angle with respect to the second mating surface of the second flange. The sealing assembly further includes a sealant disposed between the first mating surface of the first flange and the second mating surface of the second flange.
摘要翻译：提供了第一部件和第二部件之间的密封组件。密封组件包括从第一部件延伸的第一凸缘。第一凸缘包括第一配合表面。密封组件还包括从第二部件延伸的第二凸缘。第二凸缘包括适于邻接第一凸缘的第一配合表面的第二配合表面。第二凸缘还包括从第二配合表面相对于第二凸缘的第二配合表面成角度延伸的倾斜表面。倾斜表面相对于第二凸缘的第二配合表面成一定角度设置。密封组件还包括设置在第一凸缘的第一配合表面和第二凸缘的第二配合表面之间的密封剂。

9. 发明授权

US09296457B2 Outboard motor 有权
标题翻译：舷外马达
公开(公告)号：US09296457B2
公开(公告)日：2016-03-29
申请号：US14730376
申请日：2015-06-04
申请人： YAMAHA HATSUDOKI KABUSHIKI KAISHA
发明人： Kimitaka Saruwatari , Kouichi Isozaki
IPC分类号： B63H20/32 , B63H21/36 , B63H20/14 , F01M1/02 , B63H20/06 , F16J15/08 , F16J15/14 , F02B61/04
CPC分类号： B63H20/14 , B63H20/06 , B63H20/20 , F01M1/02 , F01M11/0004 , F01M2001/0292 , F01M2011/0062 , F02B61/045 , F16J15/0818 , F16J15/14
摘要： An outboard motor includes an engine including a cylinder body and a crank case, an engine holder configured to come into contact with both the cylinder body and the crank case along a second bonding surface, a power transmission shaft passing through a hole between the engine holder and both the cylinder body and the crank case, and a first sealing member between a portion of the power transmission shaft above the second bonding surface and above both the cylinder body and the crank case to separate an oil region above the first sealing member from an external water entering region below the first sealing member.
摘要翻译：舷外马达包括：发动机，其包括缸体和曲轴箱;发动机保持器，其构造成沿着第二接合面与所述缸体和所述曲轴箱接触;动力传递轴，其穿过所述发动机保持架以及缸体和曲轴箱之间的第二密封构件，以及位于第二接合面上方的动力传递轴的一部分之间的第一密封构件，并且在缸主体和曲轴箱之间，将第一密封构件上方的油区域从第一密封构件外部水进入第一密封构件下方的区域。

10. 发明申请

US20150148434A1 SYSTEM AND METHOD FOR SEALING A SYNGAS COOLER 有权
标题翻译：用于密封SYGAS COOLER的系统和方法
公开(公告)号：US20150148434A1
公开(公告)日：2015-05-28
申请号：US14091791
申请日：2013-11-27
申请人： General Electric Company
发明人： Anindra Mazumdar , Jay Christopher Schleicher , Atul Kumar Vij , Uma Chinnadurai , Paromita Bhattacharya , Rajeshwar Sripada
IPC分类号： C07C1/04 , G05D7/06 , G05B15/02 , F16J15/14
CPC分类号： G05B15/02 , C01B3/00 , C01B31/18 , C01B31/20 , C01B32/40 , C01B32/50 , C01B2203/0283 , C01B2203/0415 , C01B2203/0485 , C01B2203/0883 , C10J3/485 , C10J3/74 , C10J3/82 , C10J2300/092 , C10J2300/0936 , F16J15/14 , Y02E20/16 , Y02P20/13
摘要： A system includes a syngas cooler and a compatible seal gas system. The syngas cooler may be configured to cool a syngas. The compatible seal gas system may be configured to supply a compatible seal gas to a seal of the syngas cooler. The seal may be configured to block the syngas from a passage between an outer wall of the syngas cooler and a tube cage of the syngas cooler.
摘要翻译：系统包括合成气冷却器和兼容的密封气体系统。合成气冷却器可以被配置为冷却合成气。可兼容的密封气体系统可被配置为将合适的密封气体提供给合成气冷却器的密封件。密封件可以被构造成从合成气冷却器的外壁和合成气冷却器的管笼之间的通道阻挡合成气。

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