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公开(公告)号：US10059279B2
公开(公告)日：2018-08-28
申请号：US15101790
申请日：2014-10-27
CPC分类号： B60R11/0241 , B60R1/04 , B60R11/0258 , B60R2011/0033 , B60R2011/0059 , B60R2011/0071 , B60R2011/0089 , B60R2011/0294 , H02J7/025 , H02J7/355 , H02J50/10
摘要： A support is provided for attachment to an internal rear-view mirror made from plastic material or lightweight metal for a portable device having a telephone or GPS display screen or for generally electronic, electrical or other devices. The support includes a hooking member shaped to engage with another part of the rear-view mirror, the upper edge thereof, via two hooks, located to either side of a ball pin attaching the rear-view mirror to the windscreen. The hooking member is formed in part from a plurality of links articulated by hinges, in the manner of a metal watch strap. The hooking member is started by a hook-shaped link that secures to the upper edge of the rear-view mirror, followed by a series of links, varying in number, so as to match and constrain the shape of the rear-view mirror, and is finished by two leg feet that form a slide.
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公开(公告)号：US10052976B2
公开(公告)日：2018-08-21
申请号：US14856532
申请日：2015-09-16
申请人： STELIA AEROSPACE
发明人： Bastien Atger , Laurent Cecinas
CPC分类号： B60N2/22 , B60N2/62 , B60N2/686 , B64D11/064
摘要： A driving seat comprises a base and a back rest forming a support structure. The back rest is articulated onto the base about an axis of inclination of the back rest to provide an adjustable back rest inclination angle. The base comprises a rear base panel of fixed inclination and a front base panel with an adjustable base inclination angle relative to the rear base panel. The back rest comprises a lower back rest panel and an upper back rest panel with an adjustable raising angle relative to the lower back rest panel. In operation, the back rest inclination angle, the base inclination angle and the raising angle are adjustable to adapt the configuration of the seat to a working configuration, a standby configuration, a rest configuration or a crash configuration.
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公开(公告)号：US10052803B2
公开(公告)日：2018-08-21
申请号：US14976203
申请日：2015-12-21
申请人： ROCTOOL
CPC分类号： B29C45/7312 , B22C9/065 , B29C33/06 , B29C33/38 , B29C45/27 , B29C45/38 , B29C45/73 , B29C45/7331 , B29C2045/7368 , B29K2827/18 , B29K2905/08 , B29K2905/10 , B29K2907/04 , B29K2909/00 , H05B6/42
摘要： A mold having a first part with a carcass with a molding zone added thereto to provide a mechanical interface between the molding zone and the carcass. Inductors of the mold extend along a longitudinal direction in cavities between the mechanical interface and the molding zone. A cooling device of the mold extends at the mechanical interface between the molding zone and the carcass.
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公开(公告)号：US10029441B2
公开(公告)日：2018-07-24
申请号：US14655303
申请日：2013-12-16
发明人： Caroline Petiot , Michel Bermudez , Didier Mesnage
摘要： A device for absorbing kinetic energy for an aircraft structural element undergoing a dynamic impact. The device includes an outer enclosure made from a braided composite material configured to preserve its integrity after an impact, and a foam core contained in the outer enclosure and to at least partially fill the outer enclosure. The foam core configured to at least partially absorb the kinetic energy generated by the impact. Reinforcing elements include at least one dry composite fiber preform integrated into the foam core to dissipate, in combination with the foam core, the kinetic energy generated by the impact. A method for integrating the device for absorbing kinetic energy.
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公开(公告)号：US10016028B2
公开(公告)日：2018-07-10
申请号：US15120601
申请日：2014-08-27
申请人： KASHIKEY CO., LTD.
发明人： Keiko Shirasaka
摘要： A substantially annular-shaped accessory includes multiple arc-shaped structural elements that form a C-shaped annulus (major arc-shaped annulus) and a core. The core has a structure formed into a C-shaped annular-shaped accessory having an end gap of expandable/contractible width. One end of the core having a C-shaped member and an elastic body are fasten to a locking projection inside the arc-shaped structural element constituting one end section. Another end of the core is fasten to the locking projection inside the arc-shaped structural element constituting another end section.
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公开(公告)号：US09995579B2
公开(公告)日：2018-06-12
申请号：US14647791
申请日：2013-12-02
发明人： Frederick Boudin
CPC分类号： G01C9/06 , G01B11/26 , G01C5/04 , G01C9/22 , G01C2009/066
摘要： A tiltmeter to measure a variation in inclination of a structure from a given starting position. The tiltmeter has two pots, each pot contains an identical volume and identical height of an identical liquid. A communication device connects the two pots and allows the liquid to flow between the two pots by the principle of communicating vessels. Two optical measuring devices are provided, one optical measuring device per pot. Each optical measuring device measures a variation in height of the level of liquid in the associated pot. The optical measuring devices are fiber optic devices coupled to a common light source.
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公开(公告)号：US09988162B2
公开(公告)日：2018-06-05
申请号：US15039018
申请日：2014-11-24
摘要： A method to control a sunlight acquisition phase of a spacecraft with a nonzero angular momentum of an axis DH. The spacecraft includes a solar generator configured to rotate about an axis Y. The spacecraft actuators are controlled to place the spacecraft in an intermediate orientation in which the axis Y is substantially orthogonal to the axis DH. The solar generator is controlled to orientate the solar generator towards the sun. The spacecraft actuators are controlled to reduce the angular momentum of the spacecraft. The actuators of the spacecraft engine are controlled to place the spacecraft in an acquisition orientation in which the axis Y is substantially orthogonal to the direction of the sun with respect to the spacecraft.
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公开(公告)号：US09926087B2
公开(公告)日：2018-03-27
申请号：US15549165
申请日：2016-02-09
发明人： Patrick Doubrere
摘要： A satellite, intended to be placed in a station in orbit about a celestial body, including a first electrical thruster of orientatable thrust direction, a second electrical thruster of orientatable thrust direction, and an electrical thruster of fixed orientation that is fixed with respect to the satellite and of line of thrust passing through the center of gravity of the satellite. The satellite includes two electrical-thruster power units and an electrically interconnecting network connecting a first power unit to the first thruster of orientatable thrust direction and to the thruster of fixed orientation, and connecting a second power unit to the second thruster of orientatable thrust direction and to the thruster of fixed orientation. Each of the power units is configured to power either the associated thruster of orientatable thrust direction or the thruster of fixed orientation.
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39.发明授权公开(公告)号：US09892561B2
公开(公告)日：2018-02-13
申请号：US15285554
申请日：2016-10-05
申请人： FITTINGBOX
发明人： Ariel Choukroun , Jerome Guenard
IPC分类号： G06T19/00 , G06T5/00 , G06T5/50 , G06T7/00 , G06T17/00 , G06T15/10 , G06K9/00 , G06F3/00 , G06Q30/06 , G06T7/40
CPC分类号： G06T19/006 , G06F3/005 , G06K9/00255 , G06K9/00281 , G06K9/0061 , G06K9/00671 , G06K9/00711 , G06K2209/40 , G06Q30/0623 , G06Q30/0643 , G06T5/005 , G06T5/50 , G06T7/004 , G06T7/408 , G06T7/70 , G06T7/75 , G06T7/90 , G06T11/00 , G06T15/10 , G06T17/00 , G06T19/20 , G06T2207/20221 , G06T2207/30201 , G06T2219/2012 , G06T2219/2021
摘要： A method for generating a final image from an initial image including an object suitable to be worn by an individual. The presence of the object in the initial image is detected. A first layer is superposed on the initial image. The first layer includes a mask at least partially covering the object in the initial image. The appearance of at least one part of the mask is modified. The suppression of all or part of an object in an image or a video is enabled. Also, a process of augmented reality intended to be used by an individual wearing a vision device on the face, and a try-on device for a virtual object.
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公开(公告)号：US09879287B2
公开(公告)日：2018-01-30
申请号：US15106988
申请日：2014-12-24
申请人： INSTITUT NATIONAL DE LA RECHERCHE AGRONOMIQUE , CIRAD (CENTRE DE COOPÉRATION INTERNATIONALE EN RECHERCHE AGRONOMIQUE POUR LE DÉVELOPPEMENT
IPC分类号： C12P7/10 , B02C23/08 , B03C7/00 , C01B3/02 , C10L1/02 , C10L3/08 , C10L5/36 , C10L5/44 , C12P3/00 , C12P5/02 , C12P19/02 , C12P19/14
CPC分类号： C12P7/10 , B02C23/08 , B03C7/006 , C01B3/02 , C10L1/02 , C10L3/08 , C10L5/366 , C10L5/44 , C10L2200/0469 , C10L2290/26 , C10L2290/28 , C10L2290/54 , C12P3/00 , C12P5/023 , C12P19/02 , C12P19/14 , C12P2201/00 , Y02E50/10 , Y02E50/16 , Y02E50/30 , Y02E50/343 , Y02P20/582 , Y02P30/20
摘要： The process for the dry fractionation of lignocellulosic biomass of at least 50% by weight of lignins, cellulose and hemicelluloses. The biomass is fragmented to obtain an ultrafine powder. The process includes at least one step of separating a fraction enriched with cellulose and a fraction enriched with lignin, hemicelluloses and minerals by electrostatic sorting of the ultrafine particles. Preferably, the fraction separation step includes a step of triboelectrostatic charging of ultrafine particles and at least one step of deviating a path in the electric field of the charged particles to sort the particles.
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