COMPOSITE ANNULAR SEAL ASSEMBLY FOR BEARINGS IN AIRCRAFT
    101.
    发明申请
    COMPOSITE ANNULAR SEAL ASSEMBLY FOR BEARINGS IN AIRCRAFT 有权
    用于飞机轴承的复合环形密封组件

    公开(公告)号:US20140339369A1

    公开(公告)日:2014-11-20

    申请号:US14294947

    申请日:2014-06-03

    Inventor: Alex Habibvand

    Abstract: An edge flap arrangement is provided for an aircraft wing and includes a main flap element and an actuator for moving the main flap element relative to the wing. A linkage arrangement supports the main flap element from the aircraft wing for movement relative to the wing, and includes including a drop hinge link arrangement having a fixed strut secured to the aircraft wing and a drop link secured to the main flap element. The fixed strut and drop link are pivotally connected by a hinge point having a bearing installed therein. The bearing includes an outer race, an inner race and an annular seal assembly snap-fit into the outer race. The annular seal assembly includes first and second annular retaining rings and a resilient ring disposed between the first and second annular retaining rings.

    Abstract translation: 为飞行器机翼提供边缘翼片装置,并且包括主翼片元件和用于使主翼片元件相对于机翼移动的致动器。 连接装置支撑来自飞机机翼的主翼片元件相对于机翼移动,并且包括包括固定在飞行器机翼上的固定支柱的下降铰链连接装置和固定到主翼片元件的下降连杆。 固定的支柱和下降连杆通过其中安装有轴承的铰链点枢转地连接。 轴承包括外圈,内圈和与外圈卡扣配合的环形密封组件。 环形密封组件包括第一和第二环形保持环和设置在第一和第二环形保持环之间的弹性环。

    COMPOSITE ANNULAR SEAL ASSEMBLY FOR BEARINGS
    102.
    发明申请
    COMPOSITE ANNULAR SEAL ASSEMBLY FOR BEARINGS 审中-公开
    用于轴承的复合环形密封组件

    公开(公告)号:US20140248016A1

    公开(公告)日:2014-09-04

    申请号:US14194016

    申请日:2014-02-28

    Inventor: Alex Habibvand

    Abstract: A seal for a bearing includes a first annular retaining ring defining a first radially outermost portion and a second annular retaining ring defining a second radially outermost portion. The seal includes a resilient ring defining a third radially outermost portion. The resilient ring is disposed between the first annular retaining ring and the second annular retaining ring. The first radially outermost portion, the second radially outermost portion and the third radially outermost portion are aligned with one another. The resilient ring projects radially inward from the first annular retaining ring and the second annular retaining ring. The resilient ring is more compressible and flexible than the first annular retaining ring and the second annular retaining ring.

    Abstract translation: 用于轴承的密封件包括限定第一径向最外部分的第一环形保持环和限定第二径向最外部分的第二环形保持环。 密封件包括限定第三径向最外侧部分的弹性环。 弹性环设置在第一环形保持环和第二环形保持环之间。 第一径向最外部分,第二径向最外部分和第三径向最外部分彼此对准。 弹性环从第一环形保持环和第二环形保持环径向向内突出。 弹性环比第一环形保持环和第二环形保持环更可压缩和柔性。

    SLOTTED BEARINGS WITH WEAR-RESISTANT TREATMENTS FOR GEARBOX MOUNTING IN A GEARED TURBOFAN ENGINE
    103.
    发明申请
    SLOTTED BEARINGS WITH WEAR-RESISTANT TREATMENTS FOR GEARBOX MOUNTING IN A GEARED TURBOFAN ENGINE 有权
    带有耐磨材料的齿轮轴承,用于齿轮箱安装在齿轮涡轮发动机

    公开(公告)号:US20130160604A1

    公开(公告)日:2013-06-27

    申请号:US13715315

    申请日:2012-12-14

    Inventor: Scott McNeil

    Abstract: A load slot bearing system for a mounting system for a gearbox on a geared turbofan engine includes a load slot bearing assembly having a cobalt alloy inner member and a precipitation-hardenable alloy outer member. The inner member defines an outer engagement surface and the outer member defines an inner engagement surface slidably and rotatably engaged with the inner engagement surface. One of the outer engagement surface or the inner engagement surface has boron diffused therein. The load slot bearing system includes first and second slots extending inward from a face defined by the outer member, the second slot being positioned generally diametrically opposite the first slot. A first element is located in the bore of the inner member of the load slot bearing assembly and is connected to the inner member. A second element is connected to the outer member of the load slot bearing assembly.

    Abstract translation: 用于齿轮箱的齿轮箱的安装系统的负载槽轴承系统包括具有钴合金内部构件和可沉淀硬化的合金外部构件的装载槽轴承组件。 内部构件限定外部接合表面,并且外部构件限定与内部接合表面可滑动地和可旋转地接合的内部接合表面。 外部接合表面或内部接合表面中的一个具有在其中扩散的硼。 所述载荷槽轴承系统包括从由所述外部构件限定的面向内延伸的第一和第二槽,所述第二槽大致沿径向相对于所述第一槽定位。 第一元件位于负载槽轴承组件的内部构件的孔中并连接到内部构件。 第二元件连接到负载槽轴承组件的外部构件。

    SINGLE SLOT LOADER SLOT BEARING
    106.
    发明公开

    公开(公告)号:US20240218903A1

    公开(公告)日:2024-07-04

    申请号:US18608590

    申请日:2024-03-18

    Abstract: A loader slot bearing includes a housing and a truncated ball. The housing has an interior area that is defined by an inner bearing surface which has a concave contour defining a circumference. A single slot extends axially partway into the inner bearing surface and has a slot arc section area extending axially inward. The slot arc section area has a first circumferential slot-end, a second circumferential slot-end, and a slot arc length measured between the first circumferential slot-end and the second circumferential slot-end. A ratio of the slot arc length to the circumference of the interior area is about 0.20 to 0.35. The truncated ball has a convex exterior surface. The truncated ball is positioned in the slot and rotated so that the truncated ball is rotatably retained by the inner bearing surface. The truncated ball is angularly misalignable relative to the annular housing.

    Single slot loader slot bearing
    107.
    发明授权

    公开(公告)号:US11933354B2

    公开(公告)日:2024-03-19

    申请号:US17676984

    申请日:2022-02-22

    Abstract: A loader slot bearing includes a housing and a truncated ball. The housing has an interior area that is defined by an inner bearing surface which has a concave contour defining a circumference. A single slot extends axially partway into the inner bearing surface and has a slot arc section area extending axially inward. The slot arc section area has a first circumferential slot-end, a second circumferential slot-end, and a slot arc length measured between the first circumferential slot-end and the second circumferential slot-end. A ratio of the slot arc length to the circumference of the interior area is about 0.20 to 0.35. The truncated ball has a convex exterior surface. The truncated ball is positioned in the slot and rotated so that the truncated ball is rotatably retained by the inner bearing surface. The truncated ball is angularly misalignable relative to the annular housing.

    WEAR RESISTANT BEARING SYSTEM
    108.
    发明公开

    公开(公告)号:US20230383789A1

    公开(公告)日:2023-11-30

    申请号:US18201349

    申请日:2023-05-24

    Abstract: A wear resistant bearing system includes an inner member that has an internal core and a bearing surface which has a 50 Rockwell C scale hardness or greater. The inner member has a chemical composition that is uniform throughout the internal core and the bearings surface. The wear resistant bearing system includes an outer member that partially surrounds the inner member and includes a receiving surface that has liner system adhered thereto. The liner system includes a wear resistant matrix that has one or more reinforcing fiber systems and has one or more lubricative fibers system dispersed in the wear resistant matrix. The liner system has a wear surface that has portions of both the reinforcing fiber system and the lubricative fiber system. The wear surface is continuous.

    Rotor blade lead-lag hydraulic damper with centrifugal force compensating damping characteristics

    公开(公告)号:US11697492B2

    公开(公告)日:2023-07-11

    申请号:US17225763

    申请日:2021-04-08

    CPC classification number: B64C27/51

    Abstract: A piston assembly for a lead-lag damper for a blade mounted on a rotor of a helicopter includes a piston-rod that has an inside surface and a piston-head that extends radially outward therefrom. The piston-rod has two ports extending therethrough on opposing sides of the piston-head. A sleeve is positioned in the piston-rod and has two annular passages that communicate with the respective ports. A valve spool is disposed in and slidingly engages the sleeve. The valve spool has a channel which is in variable fluid communication with two passages. The piston assembly includes a biasing member that biases the valve spool axially away from it. The channel has an axial width configured to variably regulate fluid flow between the two ports to control dampening of the piston-rod in response to centrifugal forces applied to the valve spool.

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