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1. 发明公开

US20230257865A1 Method for reinforcing a steel component by carbonitriding 审中-公开
公开(公告)号：US20230257865A1
公开(公告)日：2023-08-17
申请号：US18106960
申请日：2023-02-07
申请人： SKF Aerospace France S.A.S
发明人： Jean-Baptiste Coudert , Alexandre Mondelin
IPC分类号： C23C8/32 , C21D9/40 , C21D1/74 , C22C38/00 , F16C13/02 , F16C19/06
CPC分类号： C23C8/32 , C21D9/40 , C21D1/74 , C22C38/00 , F16C13/02 , F16C19/06 , C21D2211/001
摘要： A method for reinforcing a steel component, having a carbonitriding step providing a first substep of case-hardening, and a second substep of nitriding, the first and second substeps of case-hardening and of nitriding of the step of carbonitriding the component are performed in one and the same heat treatment cycle.

2. 发明申请

US20230021400A1 SPHERICAL BEARING HAVING A SWAGED OUTER RING 有权
公开(公告)号：US20230021400A1
公开(公告)日：2023-01-26
申请号：US17860558
申请日：2022-07-08
申请人： SKF Aerospace France S.A.S
发明人： Florent RIVIERE , Justin ESTEVE
IPC分类号： F16C23/04
摘要： A spherical bearing having an outer ring and an inner ring respectively including an inner surface and an outer surface that are in contact with one another. Moreover, the material of the outer ring provides an alloy having the formula NiCr19Fe18Nb or an alloy having the formula X6NiCrTiMoVB25-15-2.

3. 发明申请

US20210269090A1 LIGHTWEIGHT SUSPENSION UPRIGHT OR KNUCKLE 有权
公开(公告)号：US20210269090A1
公开(公告)日：2021-09-02
申请号：US17324218
申请日：2021-05-19
申请人： Aktiebolaget SKF , SKF Aerospace France S.A.S.
发明人： Valentin Fleury , Marco Falossi , Remi Sarlin
IPC分类号： B62D7/18 , B29C43/00 , B29C45/00 , B29C65/00 , B60G99/00
摘要： A lightweight suspension upright or knuckle for a vehicle including a bearing connection interface arranged coaxial with the rolling bearing and including a first sleeve element and a second sleeve element arranged radially outside the first sleeve element and including a BMC/LFT/DLFT annular body that is sandwiched between a first and second shell elements, which are coupled together in a radially superimposed manner and which are preferably obtained in a semi-cured state as self-supporting elements, to be chemically and mechanically bonded together and with the BMC/LFT/DLFT annular body in a later stage during a step of forming a core (11) to fill either completely or partially an empty space (12) delimited between the first and second shell elements (8,9).

4. 发明申请

US20180017206A1 CONNECTOR ASSEMBLY FITTING WITH ANTI-PUNCTURING FEATURE 审中-公开
公开(公告)号：US20180017206A1
公开(公告)日：2018-01-18
申请号：US15208836
申请日：2016-07-13
申请人： Florent Fauchery , Anthony Jerome , Nicolas Marotel
发明人： Florent Fauchery , Anthony Jerome , Nicolas Marotel
IPC分类号： F16M13/02 , F16B43/00
CPC分类号： F16M13/025 , F16B5/02 , F16B43/00
摘要： A connector assembly includes a fitting having first and second mounting portions having integrally connected inner ends and opposing outer ends. The first mounting portion is connectable to the first member and the second mounting portion is inclined with respect to the first portion and connectable to the second member. The first mounting portion has inner and outer surfaces, one or more mounting holes extending between the surfaces and a load surface section extending about each mounting hole. The first mounting portion also has a recessed section located between each mounting hole and the second mounting portion and adjacent to the washer load surface section. A washer is disposeable upon the first portion load surface section and sized such that an outer portion of the washer extends over the recessed section so that a clearance gap is defined between a washer inner surface and the first mounting portion.

5. 发明授权

US09702406B2 Plain bearing 有权
公开(公告)号：US09702406B2
公开(公告)日：2017-07-11
申请号：US14737582
申请日：2015-06-12
申请人： Andrew Bell , Michael Colton , Camille Dayot , Noemie PEron
发明人： Andrew Bell , Michael Colton , Camille Dayot , Noemie PEron
IPC分类号： F16C33/18 , F16C33/20 , F16C33/10
CPC分类号： F16C33/201 , F16C33/1095 , F16C33/205 , F16C33/208 , F16C2208/02 , F16C2208/86 , F16C2240/06 , Y10T29/49679
摘要： A bearing comprising: (a) an inner ring, (b) an outer ring, and (c) a bearing liner disposed therebetween, wherein the bearing liner comprises a resin having a glass transition temperature of less than 150° C.

6. 发明授权

US09695873B2 Plain bearing 有权
公开(公告)号：US09695873B2
公开(公告)日：2017-07-04
申请号：US14737555
申请日：2015-06-12
申请人： Andrew Bell , Michael Colton , Camille Dayot , Noemie Peron
发明人： Andrew Bell , Michael Colton , Camille Dayot , Noemie Peron
IPC分类号： F16C33/18 , F16C33/20 , F16C23/04
CPC分类号： F16C33/201 , F16C23/045 , F16C33/205 , F16C33/208 , F16C2208/02 , F16C2208/86 , F16C2240/12 , F16C2326/43 , Y10T29/49679
摘要： A bearing comprising (a) an inner ring, (b) an outer ring, and (c) a bearing liner disposed therebetween, wherein the bearing liner comprises a resin and the bearing liner has at least one of: (a) a flexural modulus of from 20 to 35 GPa and (b) a flexural strength of from 500 to 700 MPa.

7. 发明申请

US20170102036A1 BEARING CAGE WITH ANTENNA AND METHOD FOR DETECTING FAILURE OF A BEARING CAGE 有权
公开(公告)号：US20170102036A1
公开(公告)日：2017-04-13
申请号：US15278082
申请日：2016-09-28
申请人： Yoann Hebrard , Defeng Lang , Andreas Karlsson , Victor Martinez , Frank de Wit
发明人： Yoann Hebrard , Defeng Lang , Andreas Karlsson , Victor Martinez , Frank de Wit
IPC分类号： F16C41/00 , F16C33/46 , H01Q7/00 , F16C33/56 , G01M13/04 , F16C33/38 , F16C33/44
CPC分类号： F16C41/008 , F16C19/386 , F16C19/52 , F16C33/3831 , F16C33/44 , F16C33/4611 , F16C33/4635 , F16C33/56 , F16C41/002 , F16C2202/40 , F16C2233/00 , F16C2300/02 , G01M13/04 , H01Q1/27 , H01Q7/00
摘要： The invention relates to a bearing cage including a bearing cage main body made of a polymer material and having pockets for receiving at least one row of rolling elements of a bearing. The cage is provided with a passive resonant circuit including an antenna coil attached to the cage main body. It is proposed that the antenna coil is formed as a conductive layer directly attached to the cage material of the bearing cage main body and is designed so as to have a breaking point less than or equal to a breaking point of the cage material. Thus, a rupture in the cage main body ruptures the antenna coil, changing the resonance behaviour of the passive resonant circuit.

8. 发明申请

US20150176638A1 DEVICE FOR MEASURING THE WEAR OF A BALL-AND-SOCKET JOINT, BALL-AND-SOCKET JOINT INCORPORATING SAID DEVICE AND METHOD FOR MEASURING THE WEAR OF SUCH A BALL-AND-SOCKET JOINT 审中-公开
标题翻译：用于测量球窝接头，球窝接头的装置和装置的测量装置和测量这种球窝接头的方法的装置
公开(公告)号：US20150176638A1
公开(公告)日：2015-06-25
申请号：US14572842
申请日：2014-12-17
申请人： Yoann HEBRARD
发明人： Yoann HEBRARD
IPC分类号： F16C11/06 , G01N27/24
CPC分类号： F16C11/0647 , F16C17/246 , G01B7/144 , G01D5/24 , G01N27/24 , Y10T403/32631
摘要： A device adapted to measure the wear of a ball-and-socket joint. The ball-and-socket joint comprising a first ring, which delimits a spherical housing, a second spherical ring, which is positioned concentrically in the housing of the first ring, and a lining, which is made from an elastically insulating material and is inserted between the second ring and the spherical housing of the first ring. A wear measuring feature includes at least two electrodes provided to be connected to the first ring and the second ring, respectively, or to the lining, so as to form a capacitor structure and a capacitance measuring device for measuring the capacity of the capacitor thus formed. The device further comprises an electronic circuit, which is a resonant circuit including the capacitor, an inductance and a resistance positioned in series.
摘要翻译：适用于测量球窝接头磨损的装置。球窝接头包括限定球形壳体的第一环，同心地位于第一环的壳体中的第二球形环，以及由弹性绝缘材料制成并被插入的衬里在第二环和第一环的球形壳体之间。磨损测量特征包括至少两个电极，分别连接到第一环和第二环或衬里，以形成电容器结构和电容测量装置，用于测量如此形成的电容器的容量。该装置还包括电子电路，其是包括电容器，电感和串联定位的电阻的谐振电路。

9. 发明授权

US08820172B2 Flight unit control system, flight control device including such a system, and use of such a system 有权
标题翻译：飞行单位控制系统，包括这种系统的飞行控制装置，以及这种系统的使用
公开(公告)号：US08820172B2
公开(公告)日：2014-09-02
申请号：US13101369
申请日：2011-05-05
申请人： Franck Bouillot , Cédric Milord
发明人： Franck Bouillot , Cédric Milord
IPC分类号： F16B31/02 , B64C13/28 , B64C9/02
CPC分类号： B64C13/28 , B64C9/02 , Y10T29/4973
摘要： A flight unit control system having at least one instrumented fastening bolt connecting an aircraft carrier structure and a load path, the instrumented bolt having at least one measurement area for detecting that the load path is under load and including a fastener for locking the instrumented bolt in a position relative to the aircraft carrier structure and load path and wherein the measurement area has two cavities and at least one strain gauge and wherein the fastener includes a plate which is positioned at a threaded end of the instrumented bolt which bears against one of the aircraft carrier structure and the load path and which extends perpendicularly to an axis of the bolt and a nut which is placed at the threaded end of the instrumented bolt to immobilize the instrumented bolt relative to the aircraft structure or the load path.
摘要翻译：一种飞行单元控制系统，其具有连接航空母舰结构和负载路径的至少一个仪表式紧固螺栓，所述仪表螺栓具有至少一个测量区域，用于检测所述负载路径处于负载状态，并且包括用于将所述装置螺栓锁定的紧固件相对于航空母舰结构和载荷路径的位置，并且其中所述测量区域具有两个空腔和至少一个应变计，并且其中所述紧固件包括板，所述板位于所述仪表螺栓的螺纹端部，载体结构和载荷路径，并且其垂直于螺栓的轴线延伸，并且螺母被放置在仪表螺栓的螺纹端，以固定相对于飞机结构或载荷路径的仪表螺栓。

10. 发明申请

US20130283942A1 CONNECTING ROD FOR AERONAUTICAL MECHANISM AND AERONAUTICAL MECHANISM COMPRISING SUCH A CONNECTING ROD 有权
标题翻译：用于气动机构的连接杆和包括连接杆的气动机构
公开(公告)号：US20130283942A1
公开(公告)日：2013-10-31
申请号：US13819834
申请日：2011-08-30
申请人： Franck Bouillot , Cedric Milord
发明人： Franck Bouillot , Cedric Milord
IPC分类号： F16C7/04
CPC分类号： F16C7/04 , B64D45/0005 , B64D2045/001 , F16C2326/43 , G01L5/101 , Y10T74/18568 , Y10T74/2144
摘要： A connecting rod for an aeronautical actuator system, having one shaft transmitting forces applied in tension and/or compression along a longitudinal axis of the rod. When the connecting rod is in service, an elastically deformable element connected to the shaft is configured to react to the forces applied to the shaft, and displays elastic deformation when effected by these forces. The deformable element has a peripheral part rigidly connected to a member of the rod in which the shaft is slidably mounted. Measurement means associated with the deformable element determine the forces. The measurement means is partially housed in the deformable element. The deformable element includes a central part elongated along the longitudinal axis, which is rigidly connected to the shaft and in which the measurement means are at least partially housed. An intermediate part runs transversally to the central part and connects the central part and the peripheral part.
摘要翻译：一种用于航空执行器系统的连杆，具有沿杆的纵向轴线施加张力和/或压缩力的一个轴传递力。当连杆正在使用时，连接到轴的可弹性变形的元件构造成对施加到轴的力作出反应，并且当这些力受到影响时显示出弹性变形。可变形元件具有刚性地连接到杆的构件的周边部分，其中轴可滑动地安装在该构件中。与可变形元件相关联的测量装置确定力。测量装置部分地容纳在可变形元件中。可变形元件包括沿着纵向轴线伸长的中心部分，该中心部分刚性地连接到轴上，并且测量装置至少部分地被容纳在该中心部分中。中间部分横向延伸到中心部分并连接中心部分和周边部分。

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