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公开(公告)号：US20170299827A1
公开(公告)日：2017-10-19
申请号：US15489991
申请日：2017-04-18
发明人： YANNICK PELLETIER
CPC分类号： G02B6/4251 , G02B6/3816 , G02B6/387 , G02B6/3885 , G02B6/3894 , G02B6/3897
摘要： A connector joins the core of at least one optical fiber to the core of another fiber in a manner that is functional and leaktight against the external media, including: a cylindrical body, whose inner portion includes an insert provided with longitudinal through-holes or through-conduits; at least one optical linkage device including a cylindrical ferrule, generally made of ceramic, pierced for the passage of the core of the fiber, and a ferrule holder joined to the end of the associated fibre and providing the mechanical linkage between the ferrule and the insert; and an O-ring seal provided between the ferrule holder and the receiving conduit of the insert. The body of the connector and the insert form a monobloc assembly, either realized as a single piece or realized with the aid of two complementary pieces, fixed to each other in a totally leaktight or hermetic fashion.
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公开(公告)号：US09617665B2
公开(公告)日：2017-04-11
申请号：US13930054
申请日：2013-06-28
发明人： Briand Valérie
CPC分类号： D03D1/04 , B60K15/03177 , B60K2015/03375 , B60K2015/03407 , B60K2015/03493 , B60Y2200/24 , B60Y2200/51 , B60Y2200/52 , D02G3/442 , D03D1/0041 , D03D11/00 , D03D13/008 , D03D15/00 , D03D15/0011 , D03D15/0027 , D03D2700/0137 , D03D2700/0148 , D03D2700/03 , D10B2331/021 , Y10T428/1314 , Y10T428/1362 , Y10T428/249921
摘要： Embodiments of the present invention relate generally to reinforcement materials for use in reinforcing flexible tank walls, and particularly to hybrid textiles and weaving patterns that have been found particularly useful with such hybrid textiles.
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公开(公告)号：US11142324B2
公开(公告)日：2021-10-12
申请号：US15841871
申请日：2017-12-14
发明人： Valerie Briand
摘要： A pneumatic deicing device (1) for breaking and removing an ice deposit accumulated on the outer surface (2) of an aircraft, in particular on an airplane wing. The device (1) includes an outer layer (10) intended to withstand the outside environment, an inner interface layer (50) intended to be bonded to the outer surface of the aircraft, and at least two outer (30) and inner (40) intermediate layers connected to one another by a network of stitches (36) spaced apart to define deicing chambers (35) that can be inflated using injected pressurized air so as to create an expansion of the device causing a mechanical action to break the ice. The inner interface layer (50) with the outer surface (2) of the aircraft includes at least one textile layer (54) having an inner surface (55) intended to be in direct contact with an outer surface (2) of the aircraft.
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公开(公告)号：US20160312938A1
公开(公告)日：2016-10-27
申请号：US15202596
申请日：2016-07-06
发明人： Amine Sannadi , Nicolas Picco
CPC分类号： F16L37/12 , B64D37/005 , F16L37/18
摘要： Embodiments of the present invention provide a lever quick connect and disconnect fitting that provides a secure fit for tank-to-tank connections and prevents any leakage from occurring. The fitting provide two separate, independent locking features that can secure tank sleeves to one another. There is provided male and female components that are coupled together by a lever connect and by a safety ring.
摘要翻译： 本发明的实施例提供了一种杠杆快速连接和断开配件，其提供了罐到罐连接的牢固配合，并防止发生任何泄漏。 配件提供两个独立的独立锁定功能，可以将油箱套筒彼此固定。 提供通过杠杆连接和安全环联接在一起的阳和阴部件。
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5.发明申请公开(公告)号：US20180178918A1
公开(公告)日：2018-06-28
申请号：US15841871
申请日：2017-12-14
发明人： Valerie Briand
CPC分类号： B64D15/166 , B29C66/433 , B29C66/729
摘要： A pneumatic deicing device (1) for breaking and removing an ice deposit accumulated on the outer surface (2) of an aircraft, in particular on an airplane wing. The device (1) includes an outer layer (10) intended to withstand the outside environment, an inner interface layer (50) intended to be bonded to the outer surface of the aircraft, and at least two outer (30) and inner (40) intermediate layers connected to one another by a network of stitches (36) spaced apart to define deicing chambers (35) that can be inflated using injected pressurized air so as to create an expansion of the device causing a mechanical action to break the ice. The inner interface layer (50) with the outer surface (2) of the aircraft includes at least one textile layer (54) having an inner surface (55) intended to be in direct contact with an outer surface (2) of the aircraft.
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公开(公告)号：US09784394B2
公开(公告)日：2017-10-10
申请号：US15202596
申请日：2016-07-06
发明人： Amine Sannadi , Nicolas Picco
CPC分类号： F16L37/12 , B64D37/005 , F16L37/18
摘要： Embodiments of the present invention provide a lever quick connect and disconnect fitting that provides a secure fit for tank-to-tank connections and prevents any leakage from occurring. The fitting provide two separate, independent locking features that can secure tank sleeves to one another. There is provided male and female components that are coupled together by a lever connect and by a safety ring.
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公开(公告)号：US09321539B2
公开(公告)日：2016-04-26
申请号：US14668701
申请日：2015-03-25
发明人： Valérie Briand
CPC分类号： B64D37/32 , B32B1/02 , B32B5/024 , B32B27/065 , B32B27/12 , B32B2250/40 , B32B2262/0269 , B32B2262/0276 , B32B2262/101 , B32B2262/106 , B32B2307/558 , B32B2307/702 , B32B2605/00 , B64D37/06 , D03D15/00 , Y02T50/44
摘要： Embodiments of the present invention relate generally to fuel tanks for aviation, and particularly to construction of rigid tank walls that have been found useful in absorbing energy of a magnitude expected during a crash. In some aspects, the rigid tank wall construction includes particular materials, such as a thermoplastic resin matrix. In some aspects, the rigid tank wall construction includes a particular arrangement of reinforcing fibers, such as a twill weave pattern.
摘要翻译： 本发明的实施例一般涉及用于航空的燃料箱，特别涉及用于吸收在碰撞期间预期的大小的能量的刚性罐壁的结构。 在一些方面，刚性罐壁结构包括特定材料，例如热塑性树脂基体。 在一些方面，刚性罐壁结构包括加强纤维的特定布置，例如斜纹组织图案。
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公开(公告)号：US10399691B2
公开(公告)日：2019-09-03
申请号：US15585447
申请日：2017-05-03
IPC分类号： B64D37/06 , B32B7/12 , B32B25/10 , B32B25/16 , B32B25/20 , B32B27/12 , B32B27/18 , B32B27/20 , B32B27/28 , B32B27/30 , B32B27/34 , B32B27/40 , B32B1/02 , B29C49/04 , B29C65/02 , B29C65/48 , B64D37/32 , B29L31/00
摘要： A flexible fuel tank (10) has, from the inside to the outside of the tank: a single-layer or multilayer liner (2) having properties of sealing with respect to the liquid, impermeability to the vapor of said fuel, and dissipation of electrostatic charges. The liner (2) includes an inner face (2a) intended to be in contact with the fuel and an outer face (2b). An intermediate layer (3) is in contact with the outer face (2b) of the liner (2), for example a coating layer; and a textile reinforcing layer (4) is in contact with the intermediate layer (3).
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9.发明申请公开(公告)号：US20180178919A1
公开(公告)日：2018-06-28
申请号：US15842023
申请日：2017-12-14
发明人： Valerie Briand
CPC分类号： B64D15/166 , B29C66/433 , B29C66/729
摘要： A pneumatic deicing device (1) is provided for breaking and removing an ice deposit accumulated on the outer surface (2) of an aircraft, in particular on an airplane wing. The device (1) includes an outer layer (15) intended to withstand the outside environment, an inner interface layer (50) intended to be connected to the outer surface (2) of the aircraft, and at least two outer (30) and inner (40) intermediate layers connected to one another by an array of stitches (36) so as to define deicing chambers (35) that can be inflated quickly to cause a mechanical action to break the ice. The outer intermediate layer (30) includes a knit textile layer (34). At least one interlayer (20; 32) made from polar elastomer material is arranged above the knit textile layer (34) and immediately in contact with the outer layer (15) and the knit textile layer (34).
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公开(公告)号：US20170320588A1
公开(公告)日：2017-11-09
申请号：US15585447
申请日：2017-05-03
CPC分类号： B64D37/06 , B29C49/04 , B29C65/02 , B29C65/48 , B29L2031/7172 , B32B1/02 , B32B7/12 , B32B25/10 , B32B25/16 , B32B25/20 , B32B27/12 , B32B27/18 , B32B27/20 , B32B27/281 , B32B27/285 , B32B27/286 , B32B27/288 , B32B27/304 , B32B27/306 , B32B27/34 , B32B27/40 , B32B2264/105 , B32B2264/108 , B32B2307/302 , B32B2307/7242 , B32B2307/7265 , B32B2605/12 , B32B2605/18 , B64D37/32 , Y02T90/44
摘要： A flexible fuel tank (10) has, from the inside to the outside of the tank: a single-layer or multilayer liner (2) having properties of sealing with respect to the liquid, impermeability to the vapor of said fuel, and dissipation of electrostatic charges. The liner (2) includes an inner face (2a) intended to be in contact with the fuel and an outer face (2b). An intermediate layer (3) is in contact with the outer face (2b) of the liner (2), for example a coating layer; and a textile reinforcing layer (4) is in contact with the intermediate layer (3).
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