Integrated cartridge double-row ball bearing for a nuclear reactor control rod drive mechanism
    141.
    发明授权
    Integrated cartridge double-row ball bearing for a nuclear reactor control rod drive mechanism 有权
    用于核反应堆控制棒驱动机构的集成筒式双列球轴承

    公开(公告)号:US09109623B2

    公开(公告)日:2015-08-18

    申请号:US13872320

    申请日:2013-04-29

    Abstract: A duplex bearing is configured for use with a nuclear reactor control rod drive mechanism. The duplex includes an outer member and an inner member wherein each defines an interior surface and an exterior surface. The outer member interior surface defines a first and second outer raceway; and the inner member defines a first and second inner raceway. A first plurality of load-carrying rolling elements and a first plurality of spacer rolling elements are disposed in a first annular cavity defined between the first inner raceway and first outer raceway. A second plurality of load-carrying rolling elements and a second plurality of spacer rolling elements are disposed in a second annular cavity defined between the second inner raceway and the second outer raceway. The duplex bearing is configured to operate with sealed de-ionized water exhibiting a temperature in the range of up to about 1200° F. as a sole lubricant.

    Abstract translation: 双轴承座被配置为与核反应堆控制杆驱动机构一起使用。 双面包括外部构件和内部构件,其中每个限定内部表面和外部表面。 外部构件内表面限定第一和第二外部滚道; 并且所述内部构件限定第一和第二内部滚道。 第一多个承载滚动元件和第一多个间隔件滚动元件设置在限定在第一内滚道和第一外滚道之间的第一环形空腔中。 第二多个承载滚动元件和第二多个间隔件滚动元件设置在限定在第二内滚道和第二外滚道之间的第二环形空腔中。 双轴承轴承被配置为以显示温度在高达约1200°F范围内的密封去离子水作为唯一润滑剂来操作。

    Self-aligning track roller bearing
    143.
    发明授权
    Self-aligning track roller bearing 有权
    自调心滚子轴承

    公开(公告)号:US08851755B2

    公开(公告)日:2014-10-07

    申请号:US14084999

    申请日:2013-11-20

    CPC classification number: F16C23/045 F16C27/063 F16C33/201

    Abstract: A self-aligning track roller bearing includes an inner member having a central axis and a convex surface and an outer member has a concave surface and is angularly displaceable relative to the central axis. A lubricious liner is positioned between the convex surface and the concave surface. The lubricious liner creates a force resisting movement of the inner member relative to the outer member. The bearing includes a snubber engaging an axially facing surface of the outer member and another snubber engaging another axially facing surface of the outer member. Outer rings are coupled to opposing axially facing surfaces of the inner member to retain the snubbers in engagement therewith. One or more of the snubbers are elastically deformable in response to angular displacement of the outer member and have a resilience set to overcome the force and urge the outer member to be concentric with the central axis.

    Abstract translation: 自调心滚子轴承包括具有中心轴线和凸形表面的内部构件,外部构件具有凹形表面并且相对于中心轴线可角度地移位。 光滑的衬垫位于凸面和凹面之间。 光滑衬套产生抵抗内部构件相对于外部构件的力的作用力。 轴承包括接合外部构件的轴向面向表面的缓冲器和接合外部构件的另一轴向面向表面的另一个缓冲器。 外环耦合到内部构件的相对的轴向面对的表面以保持缓冲器与其接合。 缓冲器中的一个或多个可以响应于外部构件的角位移而弹性变形,并且具有弹性设定以克服力并促使外部构件与中心轴线同心。

    NEEDLE ROLLER CAM FOLLOWER FOR HIGHER MILEAGE APPLICATIONS OF LIGHT, MEDIUM AND HEAVY DUTY VEHICLES
    144.
    发明申请
    NEEDLE ROLLER CAM FOLLOWER FOR HIGHER MILEAGE APPLICATIONS OF LIGHT, MEDIUM AND HEAVY DUTY VEHICLES 有权
    轻型,中型和重型车辆的较高应用的针式滚轮凸轮

    公开(公告)号:US20140261269A1

    公开(公告)日:2014-09-18

    申请号:US14211916

    申请日:2014-03-14

    Abstract: A roller assembly for a diesel engine used in a high mileage vehicle includes a roller having an exterior roller surface and an interior surface that defines a bore extending therethrough. A pin is positioned in the bore and defines an exterior pin surface. A plurality of rolling elements is positioned between the exterior pin surface and the roller interior surface. Each of the rolling elements rollingly engages the exterior pin surface and the roller interior surface. The roller assembly defines a clearance of between about 0.01 mm to about 0.03 mm between the rolling elements, the exterior pin surface and the interior surface. The roller assembly is configured to achieve extended life criteria wherein the clearance does not increase to more than 0.02 mm to 0.06 mm after 500,000 miles of travel of a vehicle powered by a diesel engine having the roller assembly installed therein.

    Abstract translation: 用于在高里程车辆中使用的柴油发动机的辊组件包括具有外辊表面和限定延伸穿过其中的孔的内表面的辊。 销定位在孔中并限定外部销表面。 多个滚动元件位于外销表面和滚子内表面之间。 每个滚动元件滚动地接合外销表面和滚子内表面。 辊组件在滚动元件,外部销表面和内表面之间限定了约0.01mm至约0.03mm之间的间隙。 辊组件被配置成实现延长的寿命标准,其中在由其中安装有辊组件的柴油发动机驱动的车辆的行驶500,000英里之后,间隙不会增加到大于0.02mm至0.06mm。

    SELF LUBRICATED SPHERICAL TRANSOM BEARING
    145.
    发明申请
    SELF LUBRICATED SPHERICAL TRANSOM BEARING 有权
    自润滑球轴承

    公开(公告)号:US20140158016A1

    公开(公告)日:2014-06-12

    申请号:US13939736

    申请日:2013-07-11

    Inventor: James Voisine

    CPC classification number: B61F99/00 B61F5/52 F16C23/045 F16C2326/10

    Abstract: A suspension system for a rail car has at least two undercarriage members and at least one equalizer bar removably and pivotally secured to and between the two undercarriage members. A spherical bearing has an outer member that surrounds an inner member. The outer member is removably secured to one of the undercarriage members. The inner member is removably secured to the equalizer bar. The outer member defines at least one outer member section having an arcuate interior surface and the inner member defines at least one inner member section having an arcuate exterior surface. A low friction liner is disposed on at least one of the arcuate interior surface or the arcuate exterior surface.

    Abstract translation: 用于轨道车辆的悬挂系统具有至少两个底架构件和至少一个均衡杆,可移除地和枢转地固定到两个起落架构件之间和之间。 球面轴承具有围绕内部构件的外部构件。 外部构件可移除地固定到一个起落架构件。 内部构件可移除地固定到均衡器杆。 外部构件限定具有弧形内表面的至少一个外部构件部分,并且内部构件限定具有弧形外表面的至少一个内部构件部分。 低摩擦衬套设置在弧形内表面或弧形外表面中的至少一个上。

    TWO STAGE SEAL FOR A BEARING ASSEMBLY
    146.
    发明申请
    TWO STAGE SEAL FOR A BEARING ASSEMBLY 有权
    两段密封用于轴承组件

    公开(公告)号:US20140093198A1

    公开(公告)日:2014-04-03

    申请号:US14099121

    申请日:2013-12-06

    Inventor: James Voisine

    Abstract: A bearing assembly includes an inner member having an outer engagement surface and an outer race. The outer race has an inner surface defining a first end and a second end and an inner engagement surface therebetween, the inner engagement surface is positioned on the outer engagement surface of the inner member. A first annular groove is formed in the inner surface, proximate one of the first end and the second end. A second annular groove is formed in the inner surface and is positioned axially inward from the first annular groove. An external seal is positioned in first annular groove and slidably engages the inner member. An internal seal is positioned in the second annular groove and slidingly engages the inner member.

    Abstract translation: 轴承组件包括具有外接合表面和外座圈的内部构件。 外圈具有限定第一端和内部接合表面的内表面,内部接合表面位于内部构件的外部接合表面上。 第一环形槽形成在内表面中,靠近第一端和第二端中的一个。 第二环形槽形成在内表面中并且从第一环形槽轴向向内定位。 外部密封件定位在第一环形槽中并可滑动地接合内部构件。 内部密封件定位在第二环形槽中并滑动地接合内部构件。

    ACTUATION SYSTEM FOR A LIFT ASSISTING DEVICE AND LINED TRACK ROLLERS USED THEREIN
    147.
    发明申请
    ACTUATION SYSTEM FOR A LIFT ASSISTING DEVICE AND LINED TRACK ROLLERS USED THEREIN 有权
    用于升降机辅助装置的启动系统和用于其的内置轨道滚子

    公开(公告)号:US20140061381A1

    公开(公告)日:2014-03-06

    申请号:US13719541

    申请日:2012-12-19

    Abstract: An actuation system for deploying and retracting a lift assisting device of a leading edge of a wing of an aircraft including a track pivotally coupled to the lift assisting device. The track has first and second outer surfaces and side surfaces. The actuation system includes a shaft rotationally coupled within the wing of the aircraft and operable, in response to flight control signals, to deploy or retract the lift assisting device. The actuation system includes an actuator for actuating the lift assisting device, coupled to the shaft, between a retracted position to a deployed position along an arcuate path. The actuation system includes a plurality of track roller bearings rotatably contacting the first and second outer surfaces of the track to guide the track along the arcuate path. The plurality of track roller bearings includes one or more lined track roller assembly.

    Abstract translation: 一种用于展开和缩回飞行器机翼的前缘的升降机辅助装置的致动系统,包括枢转地联接到升降机辅助装置的轨道。 轨道具有第一和第二外表面和侧表面。 致动系统包括旋转地联接在飞行器的翼内的轴,并且响应于飞行控制信号而可操作以展开或缩回提升辅助装置。 所述致动系统包括致动器,所述致动器用于致动所述提升辅助装置,所述升降机构联接到所述轴,在沿着弓形路径的缩回位置到展开位置之间。 致动系统包括多个滚动滚子轴承,其可旋转地接触轨道的第一和第二外表面以沿着弧形路径引导轨道。 多个滚轮轴承包括一个或多个衬里的滚轮组件。

    STEERING AXLE ASSEMBLY WITH SELF-LUBRICATED BEARINGS
    148.
    发明申请
    STEERING AXLE ASSEMBLY WITH SELF-LUBRICATED BEARINGS 有权
    带自润滑轴承的转向轴组件

    公开(公告)号:US20140035247A1

    公开(公告)日:2014-02-06

    申请号:US13945575

    申请日:2013-07-18

    Abstract: A steering axle assembly includes a wheel end having a knuckle section comprising a first arm and a second arm each extending therefrom. The steering axle assembly includes an axle beam having a connecting end. A pin is disposed in respective bores of the first and second arms and of the connecting end. The steering axle assembly includes a self-lubricated bearing system that including a first tubular bushing, a second tubular busing and an annular thrust bearing. The self-lubricated bearing system has an adequate amount of lubricant therein at a beginning of life state and the amount of the lubricant being sufficient for an end of life state defined by at least one million miles of operation of the heavy duty truck, without replenishment of the lubricant.

    Abstract translation: 转向轴组件包括具有转向节部分的车轮端部,转向节部分包括从其延伸的第一臂和第二臂。 转向轴组件包括具有连接端的轴梁。 销设置在第一和第二臂和连接端的相应孔中。 转向轴组件包括自润滑的轴承系统,其包括第一管状衬套,第二管状衬套和环形推力轴承。 自润滑轴承系统在生命状态开始时具有足够的润滑剂,并且润滑剂的量足以使重型卡车运行至少一百万英里所限定的寿命状态,而不需要补充 的润滑剂。

    Flexible alignment sealing coupling
    149.
    发明授权

    公开(公告)号:US12158226B2

    公开(公告)日:2024-12-03

    申请号:US17319721

    申请日:2021-05-13

    Inventor: Smail Vila

    Abstract: A seal for a flexible alignment sealing coupling. The seal includes an annular member being symmetric about a longitudinal axis. The annular member has a radially inward facing surface extending an axial width between a first axial end and a second axial end. In a relaxed state of the seal, the radially inward facing surface has an asymmetric generally concave V-shaped cross section and is defined by a first section and a second section. The first section has a first seal taper angle measured relative to a line parallel to the longitudinal axis. The second section has a second seal taper angle measured relative to another line parallel to the longitudinal axis. The first seal taper angle is less than the second seal taper angle. Each of the first seal taper angle and the second seal taper angle is greater than zero degrees and less than 90 degrees.

    Spherical plain bearing with lubrication features

    公开(公告)号:US11982313B2

    公开(公告)日:2024-05-14

    申请号:US17850433

    申请日:2022-06-27

    Inventor: James Voisine

    Abstract: A spherical plain bearing includes an outer ring and an inner ring that are each coaxial with a longitudinal axis of the bearing. The outer ring has a first axial outer ring end, a second axial outer ring end, and an interior spherical concave bearing surface extending therebetween. The inner ring has a first axial inner ring end, a second axial inner ring end, and an interior cylindrical bearing surface defining a bore and an exterior spherical convex bearing surface extending therebetween. The exterior spherical convex bearing surface is in interfacial sliding engagement with the interior spherical concave bearing surface. A plurality of circumferential lubrication grooves and one or more curved lubrication channels are in the exterior spherical convex bearing surface. The curved lubrication channels are positioned to intersect each of the circumferential lubrication grooves. A plurality of profiled annular lubrication grooves circumferentially extend into the interior cylindrical bearing surface.

Patent Agency Ranking