公开(公告)号：WO2013074776A1

公开(公告)日：2013-05-23

申请号：PCT/US2012/065260

申请日：2012-11-15

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  PALLINI, Robert A.

Inventor： PALLINI, Robert A.

IPC: F16C13/00 ,  F16H53/06 ,  B21D51/26

CPC classification number: B21D51/2669 ,  B29C45/14 ,  F16C13/006 ,  F16C19/06 ,  F16C19/54 ,  F16C33/586 ,  F16C35/067 ,  F16C2360/18 ,  F16H53/06 ,  Y10T74/2107

Abstract: A cam follower (10) for a ram of a metal can necker machine and a method of making the same. An outer ring (40, 70) has an outer ring bearing surface (42, 72) and an exterior surface (44, 74) defining a groove (46, 76) extending along at least a portion thereof. An inner ring (50, 80) is coaxially in the outer ring (40, 70) and has an inner ring bearing surface (52, 82). A plurality of rolling elements (54, 84) is disposed in an annular cavity (59, 89) between the outer ring bearing surface (42, 72) and the inner ring bearing surface (52, 82). The plurality of rolling elements (54, 84) are in rolling engagement with the outer ring bearing surface (42, 72) and the inner ring bearing surface (52, 82) so that the outer ring (40, 70) is rotatable relative to the inner ring (50, 80) about an axis of rotation (A). The outer ring (40, 70) is received in a tire (100). A least a portion of the tire (100) is disposed in the groove (46, 76) to inhibit axial movement of the tire (100) relative to the outer ring (40, 70).

Abstract translation: 一种用于金属罐颈机的冲头的凸轮从动件（10）及其制造方法。 外环（40,70）具有外环支承表面（42,72）和限定沿其至少一部分延伸的凹槽（46,76）的外表面（44,47）。 内环（50,80）同轴地位于外圈（40,70）中并具有内环支承表面（52,82）。 多个滚动元件（54,84）设置在外圈支承表面（42,72）和内圈支承表面（52,82）之间的环形空腔（59,89）中。 多个滚动元件（54,84）与外圈支承表面（42,42）和内圈支承表面（52,82）滚动接合，使得外圈（40,70）相对于 所述内环（50,80）围绕旋转轴线（A）。 外圈（40,70）被容纳在轮胎（100）中。 轮胎（100）的至少一部分设置在凹槽（46,76）中以阻止轮胎（100）相对于外圈（40,70）的轴向移动。

公开(公告)号：WO2013013005A1

公开(公告)日：2013-01-24

申请号：PCT/US2012/047331

申请日：2012-07-19

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  VOISINE, James ,  SMITH, Bradley

Inventor： VOISINE, James ,  SMITH, Bradley

IPC: F16C11/06 ,  F16C33/74 ,  F16J15/32

CPC classification number: F16C11/0676 ,  F16C33/74 ,  F16J15/3284 ,  F16J15/52 ,  Y10T29/49636

Abstract: A sealing system for a spherical plain bearing assembly is provided and includes a flexible seal defining a base and a head. At least one low-friction liner is disposed on the flexible seal.

Abstract translation: 提供了一种用于球面滑动轴承组件的密封系统，并且包括限定底座和头部的柔性密封件。 至少一个低摩擦衬垫设置在柔性密封件上。

公开(公告)号：WO2012129223A1

公开(公告)日：2012-09-27

申请号：PCT/US2012/029797

申请日：2012-03-20

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  GYURICSKO, Frederick S. ,  SIMPSON, Maura

Inventor： GYURICSKO, Frederick S. ,  SIMPSON, Maura

IPC: B64C9/22 ,  F16C29/04 ,  F16C23/04

CPC classification number: B64C9/22 ,  F16C17/02 ,  F16C23/043 ,  F16C33/201 ,  F16C33/203 ,  F16C2326/43

Abstract: An aircraft wing (12) includes a wing structure (12a), a slat panel (16) mounted on a track (18), and an actuator mechanism (26) on the wing structure coupled to the track for moving the slat panel between a deployed position and a retracted position. Track roller bearings (38) on the wing structure rotatably contact the track, and side roller bearings on the wing structure rotatably contact at least one side of the track. In another configuration, the actuator mechanism includes a shaft rotatably mounted on the wing structure, an actuator arm coupled to the track by a bearing linkage, and an actuator lever coupled to the shaft by a bearing linkage and to the actuator arm by a bearing linkage. At least one bearing linkage includes a spherical plain bearing.

Abstract translation: 飞机机翼（12）包括机翼结构（12a），安装在轨道（18）上的板条板（16）以及耦合到轨道的机翼结构上的致动器机构（26），用于将板条板移动到 展开位置和缩回位置。 机翼结构上的履带滚子轴承（38）可旋转地接触轨道，机翼结构上的侧滚子轴承可旋转地接触轨道的至少一侧。 在另一种构造中，致动器机构包括可旋转地安装在机翼结构上的轴，通过轴承联动装置联接到轨道的致动器臂，以及通过轴承联接件联接到轴的致动器杆，以及通过轴承连杆 。 至少一个轴承连接件包括球面滑动轴承。

公开(公告)号：WO2009009645A2

公开(公告)日：2009-01-15

申请号：PCT/US2008/069608

申请日：2008-07-10

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  HABIBVAND, Alex

Inventor： HABIBVAND, Alex

IPC: F16C19/49 ,  F16C33/32 ,  F16C33/62

CPC classification number: F16C19/49 ,  F16C19/505 ,  F16C19/54 ,  F16C33/303 ,  F16C33/32 ,  F16C33/62 ,  F16C2361/91

Abstract: A ground-based power generator that produces hot gas and that has a hot gas valving system includes a butterfly valve in a gas flow conduit. The generator is improved in that the butterfly valve is mounted in the conduit by a ball-roller bearing.

Abstract translation: 产生热气体并具有热气阀系统的地面发电机包括气流导管中的蝶阀。 发电机的改进在于，蝶阀通过滚珠轴承安装在导管中。

公开(公告)号：WO2008011171A1

公开(公告)日：2008-01-24

申请号：PCT/US2007/016502

申请日：2007-07-19

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  GAUMER, Brian

Inventor： GAUMER, Brian

IPC: F16C33/10 ,  F16C23/02 ,  F16C23/04

CPC classification number: F16C33/74 ,  F16C23/045 ,  F16C33/103 ,  F16C33/1065 ,  F16C2240/42 ,  F16C2240/70 ,  Y10T29/49702

Abstract: A spherical plain bearing has outer and inner rings each having a bearing surface, one bearing surface being in sliding disposition to the other. The inner ring has a third bearing surface for engaging a member to be mounted to the bearing. There is a lubrication groove in one or more of the first, second or third bearing surfaces, the lubrication groove comprising a contoured side. In an alternative a spherical plain bearing, there is a segmented lubrication groove in the third bearing surface that might have a sharp edge or a contoured side. A contoured lubrication groove can be formed by forming a lubrication groove that has a sharp edge; and machining the sharp edge to a contoured side having a reduced tendency to wipe lubricant from a second surface facing the lubrication groove.

Abstract translation: 球面滑动轴承具有外圈和内圈，每个圈具有支承面，一个支承面相对于另一个滑动布置。 内圈具有用于接合待安装到轴承的构件的第三轴承表面。 在第一，第二或第三轴承表面中的一个或多个中存在润滑槽，润滑槽包括成型侧。 在另一种球面滑动轴承中，在第三轴承表面有一个分段的润滑槽，其可能具有尖锐的边缘或轮廓的侧面。 轮廓润滑槽可以通过形成具有尖锐边缘的润滑槽来形成; 以及将锋利边缘加工成具有降低的倾向的轮廓面，以从面向润滑槽的第二表面擦拭润滑剂。

公开(公告)号：WO2014134492A1

公开(公告)日：2014-09-04

申请号：PCT/US2014/019522

申请日：2014-02-28

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  HABIBVAND, Alex

Inventor： HABIBVAND, Alex

IPC: F16C33/78 ,  F16C33/36 ,  F16C23/08

CPC classification number: F16C33/7889 ,  F16C19/38 ,  F16C23/086 ,  F16C33/7806 ,  F16C33/7816 ,  F16C33/783 ,  F16C33/7856 ,  F16C2300/02

Abstract: A seal for a bearing includes a first annular retaining ring (72) defining a first radially outermost portion (72X) and a second annular retaining ring (74) defining a second radially outermost portion (74X). The seal includes a resilient ring (76) defining a third radially outermost portion (76X). 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（72X）的第一环形保持环（72）和限定第二径向最外部分（74X）的第二环形保持环（74）。 密封件包括限定第三径向最外部分（76X）的弹性环（76）。 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。

公开(公告)号：WO2014100411A1

公开(公告)日：2014-06-26

申请号：PCT/US2013/076557

申请日：2013-12-19

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  GYURICSKO, Frederick S. ,  PHOENIX, Jay ,  FREDERICKSEN, Arnold ,  COWLES, JR., John H.

Inventor： GYURICSKO, Frederick S. ,  PHOENIX, Jay ,  FREDERICKSEN, Arnold ,  COWLES, JR., John H.

IPC: B64C9/22 ,  F16C11/02 ,  F16C23/04 ,  F16C29/04

CPC classification number: B64C9/22 ,  F16C11/02 ,  F16C17/24 ,  F16C23/041 ,  F16C29/045 ,  F16C2326/43 ,  Y02T50/44

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，所述升降辅助装置联接到所述轴，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。

公开(公告)号：WO2014081568A2

公开(公告)日：2014-05-30

申请号：PCT/US2013/068626

申请日：2013-11-06

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  GAUMER, Brian ,  LUGOSI, Robert ,  VOISINE, James

Inventor： GAUMER, Brian ,  LUGOSI, Robert ,  VOISINE, James

IPC: F16C33/10 ,  F16C23/02

CPC classification number: F16C33/74 ,  F16C23/045 ,  F16C33/10 ,  F16C33/743 ,  F16C2240/42 ,  F16C2240/70

Abstract: A spherical bearing has an outer ring with a concave bearing surface and an inner ring having a convex bearing surface, which is in sliding engagement with the concave bearing surface. A lubrication groove is formed in the convex bearing surface and/or the concave bearing surface. The lubrication groove is defined by a concave central portion and by convex side portions. The concave central portion has a first radius of curvature and the convex side portions have a second radius of curvature. The second radius of curvature is at least 0.7 times the first radius of curvature.

Abstract translation: 球面轴承具有带有凹形轴承表面的外圈和具有凸形轴承表面的内圈，该内圈与凹形轴承表面滑动接合。 润滑槽形成在凸形轴承表面和/或凹形轴承表面中。 润滑槽由凹入的中心部分和凸出的侧面部分限定。 凹入的中央部分具有第一曲率半径，并且凸出的侧部分具有第二曲率半径。 第二曲率半径至少是第一曲率半径的0.7倍。

公开(公告)号：WO2013180858A1

公开(公告)日：2013-12-05

申请号：PCT/US2013/038112

申请日：2013-04-25

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC.

Inventor： PORTER, Matthew ,  JAMES, JR., Robert Allan ,  GOSTOMSKI, Michael S.

IPC: F16C11/06 ,  F16C33/16

CPC classification number: F16C33/24 ,  F16C11/068 ,  F16C23/046 ,  F16C33/1095 ,  F16C33/16 ,  F16C2204/10

Abstract: A spherical plain bearing (10) includes an inner ring (12) defining a convex outer surface (14) and an outer ring (16) defining a concave inner surface (18). The outer ring encircles the inner ring and one or more of the outer surface and the inner surface have a plurality of pockets (20) formed therein. A solid graphite plug (22) is disposed in one or more of the plurality of pockets and slidingly engages the outer surface and/or the inner surface.

Abstract translation: 球面滑动轴承（10）包括限定凸形外表面（14）的内圈（12）和限定凹形内表面（18）的外圈（16）。 外环围绕内圈，外表面和内表面中的一个或多个具有形成在其中的多个凹穴（20）。 固体石墨塞（22）设置在所述多个凹穴中的一个或多个中并滑动地接合外表面和/或内表面。

公开(公告)号：WO2013082026A1

公开(公告)日：2013-06-06

申请号：PCT/US2012/066649

申请日：2012-11-27

Applicant: ROLLER BEARING COMPANY OF AMERICA, INC. ,  GUILFORD, Werner B.

Inventor： GUILFORD, Werner B.

IPC: F16C33/72

CPC classification number: F16C33/723 ,  F16C13/006 ,  F16C33/76

Abstract: An end cap (12) for a bearing assembly includes a first body portion (40) having a substantially annular sealing surface (42) positioned radially away from a central axis of the first body portion (40). The end cap includes a second body portion (46) extending from the first body portion, the second body portion (46) having at least one protrusion (51) extending radially therefrom.

Abstract translation: 用于轴承组件的端盖（12）包括具有径向远离第一主体部分（40）的中心轴线定位的基本上环形的密封表面（42）的第一主体部分（40）。 端盖包括从第一主体部分延伸的第二主体部分（46），第二主体部分（46）具有至少一个从其径向延伸的突出部（51）。