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1.发明申请ACTUATION SYSTEM FOR A LIFT ASSISTING DEVICE AND LINED TRACK ROLLERS USED THEREIN 审中-公开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：US20160046363A1
公开(公告)日：2016-02-18
申请号：US14928171
申请日：2015-10-30
Applicant: Roller Bearing Company of America, Inc.
Inventor： Frederick S. Gyuricsko , Jay Phoenix , Arnold E. Fredericksen , John H. Cowles, JR.
CPC classification number: B64C9/02 , B64C9/22 , F16C11/02 , 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。
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公开(公告)号：US20150260225A1
公开(公告)日：2015-09-17
申请号：US14728402
申请日：2015-06-02
Applicant: Roller Bearing Company of America, Inc.
Inventor： Alex Habibvand , Frederick S. Gyuricsko , Jay Phoenix , Arnold E. Fredericksen , John H. Cowles, Jr.
CPC classification number: F16C33/36 , B64C9/02 , B64C9/16 , F16C11/0614 , F16C19/38 , F16C23/041 , F16C23/086 , F16C33/62 , F16C2240/70 , F16C2326/43
Abstract: In one aspect, the present invention resides in an edge flap arrangement for an aircraft wing that has a main flap element and an actuator for moving the main flap element relative to the wing, a linkage arrangement that supports the main flap element from the aircraft wing for movement relative to the wing, the linkage arrangement including a drop link and a hinge point. The fixed strut and the drop link are pivotally connected by the hinge point. The hinge point includes a bearing. The bearing is an hourglass bearing assembly that has an inner raceway outer raceway. The outer raceway is positioned around the inner raceway. A plurality of rollers is disposed between the inner raceway and the outer raceway. The plurality of rollers, the outer raceway and/or the inner raceway are manufactured from CREN and/or CRES.
Abstract translation: 在一个方面，本发明涉及一种用于飞行器机翼的边缘翼片装置，其具有主翼片元件和用于相对于翼片移动主翼片元件的致动器，连接装置，其从飞机机翼支撑主翼片元件 用于相对于机翼的运动，所述连接装置包括下降连杆和铰链点。 固定支柱和下降连杆通过铰链点枢转连接。 铰链点包括一个轴承。 轴承是具有内滚道外滚道的沙漏轴承组件。 外滚道位于内滚道周围。 多个辊子设置在内滚道和外滚道之间。 多个辊，外滚道和/或内滚道由CREN和/或CRES制成。
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3.发明申请ELECTRICAL CONDUCTOR FOR LINED TRACK ROLLERS USED ON ACTUATION SYSTEM FOR AIRCRAFT LIFT ASSISTING DEVICES 审中-公开用于航空升降机辅助装置的执行系统的用于线性轨道滚子的电导体公开(公告)号：US20140339358A1
公开(公告)日：2014-11-20
申请号：US14287572
申请日：2014-05-27
Applicant: Roller Bearing Company of America, Inc.
Inventor： Curtis M. Swartley , Arnold E. Fredericksen , Frederick S. Gyuricsko , Jesse D. Marek , Michael J. Cunningham
CPC classification number: H01R41/00 , B64C9/02 , B64C9/22 , B64D45/02 , F16C11/02 , F16C17/10 , F16C23/041 , F16C29/045 , F16C33/74 , F16C33/7886 , F16C2326/43 , Y02T50/44
Abstract: An electrical conductor for a bearing includes an electrically conductive spring ring having a split therein. The spring ring has a plurality of first electrical contact surfaces in electrical communication with a plurality of second electrical contact surfaces. The plurality of second electrical contact surfaces are positioned radially outward from the plurality of first electrical contact surfaces. The plurality of first electrical contact surfaces and the plurality of second electrical contact surfaces are movable relative to one another.
Abstract translation: 用于轴承的电导体包括其中分开的导电弹簧环。 弹簧环具有与多个第二电接触表面电连通的多个第一电接触表面。 多个第二电接触表面从多个第一电接触表面径向向外定位。 多个第一电接触表面和多个第二电接触表面可相对于彼此移动。
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Patent Agency Ranking
4.发明申请SEAL AND ELECTRICAL CONDUCTOR FOR LINED TRACK ROLLERS USED ON ACTUATION SYSTEM FOR AIRCRAFT LIFT ASSISTING DEVICES 审中-公开用于航空器助力装置的执行系统的线性履带式滚子的密封和电导体公开(公告)号：US20140131512A1
公开(公告)日：2014-05-15
申请号：US13940305
申请日：2013-07-12
Applicant: Roller Bearing Company of America, Inc.
Inventor： Frederick S. Gyuricsko
CPC classification number: B64C9/02 , B64C9/22 , B64D45/02 , F16C11/02 , F16C13/006 , F16C17/107 , F16C23/041 , F16C29/045 , F16C33/74 , F16C33/7886 , F16C41/002 , F16C2326/43 , H01R41/00 , Y02T50/44
Abstract: An electrical conductor for a bearing defines an annular base and is manufactured from an electrically conductive material. The electrical conductor includes a first electrical connector positioned proximate a radially outer peripheral area of the annular base. The electrical conductor includes a second electrical connector positioned proximate a radially inner peripheral area of the annular base. The second electrical connector defines one or more contact edges extending away from the annular base. The contact edge is configured for sliding electrical contact with the bearing.
Abstract translation: 用于轴承的电导体限定了环形基座并且由导电材料制造。 电导体包括靠近环形基座的径向外周区域定位的第一电连接器。 电导体包括靠近环形基座的径向内周区域定位的第二电连接器。 第二电连接器限定远离环形基部延伸的一个或多个接触边缘。 接触边缘被配置为与轴承滑动电接触。
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公开(公告)号：US10023302B2
公开(公告)日：2018-07-17
申请号：US13719541
申请日：2012-12-19
Applicant: Roller Bearing Company of America, Inc.
Inventor： Frederick S. Gyuricsko , Jay Phoenix , Arnold E. Fredericksen , John H. Cowles, Jr.
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.
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公开(公告)号：US10012265B2
公开(公告)日：2018-07-03
申请号：US14728402
申请日：2015-06-02
Applicant: Roller Bearing Company of America, Inc.
Inventor： Alex Habibvand , Frederick S. Gyuricsko , Jay Phoenix , Arnold E. Fredericksen , John H. Cowles, Jr.
CPC classification number: F16C33/36 , B64C9/02 , B64C9/16 , F16C11/0614 , F16C19/38 , F16C23/041 , F16C23/086 , F16C33/62 , F16C2240/70 , F16C2326/43
Abstract: In one aspect, the present invention resides in an edge flap arrangement for an aircraft wing that has a main flap element and an actuator for moving the main flap element relative to the wing, a linkage arrangement that supports the main flap element from the aircraft wing for movement relative to the wing, the linkage arrangement including a drop link and a hinge point. The fixed strut and the drop link are pivotally connected by the hinge point. The hinge point includes a bearing. The bearing is an hourglass bearing assembly that has an inner raceway outer raceway. The outer raceway is positioned around the inner raceway. A plurality of rollers is disposed between the inner raceway and the outer raceway. The plurality of rollers, the outer raceway and/or the inner raceway are manufactured from CREN and/or CRES.
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公开(公告)号：US20180290732A1
公开(公告)日：2018-10-11
申请号：US16008225
申请日：2018-06-14
Applicant: Roller Bearing Company of America, Inc.
Inventor： Frederick S. Gyuricsko , Jay Phoenix , Arnold E. Fredericksen , John H. Cowles, JR.
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.
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8.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
Applicant: ROLLER BEARING COMPANY OF AMERICA, INC
Inventor： Frederick S. Gyuricsko , Jay Phoenix , Arthur Gay , Nirad Patel , Arnold Fredericksen
IPC: B64C13/28
CPC classification number: B64C13/28 , B64C9/02 , B64C9/22 , F16C11/02 , 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。
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