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1.发明申请公开(公告)号：US20200240470A1
公开(公告)日：2020-07-30
申请号：US16845568
申请日：2020-04-10
摘要： A maintenance-free bearing system having self-lubricating features, seals, grooves and slots for use in a cushion hitch assembly for a hitch pull scraper vehicle. An interconnected bearing linkage system having two or more horizontal two-axis combined journal and thrust bearings with self-lubricating liners therein, two or more vertical single-axis sleeve bearings with self-lubricating liners therein and one or more vertical thrust bearing with self-lubricating liners therein, that cooperate with one another to accommodate vertical and horizontal angular movement relative to one another. The vertical thrust bearings incorporate an outer seal assembly and/or an inner seal assembly with a tapered configuration that improves retention of the seal assembly during rotation.
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公开(公告)号：US20160327091A1
公开(公告)日：2016-11-10
申请号：US14572260
申请日：2014-12-16
CPC分类号： F16C33/36 , B64C9/16 , B64C9/18 , B64C13/28 , F16C11/06 , F16C19/38 , F16C23/086 , F16C23/088 , F16C2240/70 , F16C2326/43
摘要： An edge flap arrangement for an aircraft wing includes a main flap element and an actuator for moving the main flap element relative to the aircraft wing. A linkage arrangement supports the main flap element and includes 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 the drop link are connected by a hinge point having an hourglass bearing assembly having hourglass shaped rollers with a circular cross section symmetrical about a longitudinal axis, first and second axial ends, and an exterior surface. The exterior surface defines a concave engagement surface having a first radius of curvature R1 and a second radius of curvature which is greater than the first radius of curvature R1. The first radius of curvature is between 50 and 95 percent of the second radius of curvature.
摘要翻译： 用于飞机机翼的边缘翼片装置包括主翼片元件和用于相对于飞机机翼移动主翼片元件的致动器。 连接装置支撑主翼片元件并且包括具有固定到飞机机翼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。 固定支柱和下降连杆通过铰链点连接，铰链点具有沙漏轴承组件，该沙漏轴承组件具有沙漏形滚子，其具有围绕纵向轴线，第一和第二轴向端部以及外部表面对称的圆形横截面。 外表面限定具有第一曲率半径R1和大于第一曲率半径R1的第二曲率半径的凹形接合表面。 第一曲率半径在第二曲率半径的50％至95％之间。
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3.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
CPC分类号： B64C9/02 , B64C9/22 , F16C11/02 , F16C23/041 , F16C29/045 , F16C2326/43 , Y02T50/44
摘要： 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.
摘要翻译： 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：US20150292549A1
公开(公告)日：2015-10-15
申请号：US14686413
申请日：2015-04-14
发明人： John H. Cowles, JR. , James Beavers
IPC分类号： F16C7/02
CPC分类号： F16C7/02 , B64C13/30 , F16C2326/43
摘要： A compression rod has a buckling initiating feature. The compression rod includes an elongate body. The elongate body has a first cross sectional area along a first a length of the elongate body and a second cross sectional area along a second length of the elongate body. The second cross sectional area defines the buckling initiating feature. The second cross sectional area is configured to cause buckling along the elongate body upon application of a predetermined axially oriented compressive force.
摘要翻译： 压缩杆具有弯曲起始特征。 压缩杆包括细长体。 细长主体具有沿着细长主体的第一长度的第一横截面面积和沿着细长主体的第二长度的第二横截面积。 第二横截面区域限定起皱特征。 第二横截面积被构造成在施加预定的轴向定向的压缩力时沿着细长主体产生弯曲。
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公开(公告)号：US20160083081A1
公开(公告)日：2016-03-24
申请号：US14959589
申请日：2015-12-04
CPC分类号： F16C19/48 , B64C9/02 , B64C9/22 , B64D45/02 , F16C11/02 , F16C17/10 , F16C23/041 , F16C29/045 , F16C33/60 , F16C33/74 , F16C33/7886 , F16C2326/43 , Y02T50/44
摘要： A track roller assembly includes a split inner ring, a split outer ring, a one piece inner ring and/or a one piece outer ring and a liner or plurality of rolling elements engaging therewith, the track roller assembly being disposed in a structure of an Airbus A-350 aircraft, an Airbus A-320 aircraft, an Airbus A320Neo aircraft, an Airbus A330 aircraft, an Airbus A330Neo aircraft, an Airbus A321 aircraft, an Airbus A340 aircraft, and an Airbus A380 aircraft.
摘要翻译： 轨道滚子组件包括分割内圈，分裂外圈，单件内圈和/或单件外圈以及与其接合的衬套或多个滚动元件，所述履带滚子组件设置在 空客A-350飞机，空中客车A-320飞机，空中客车A320Neo飞机，空中客车A330飞机，空中客车A330Neo飞机，空中客车A321飞机，空中客车A340飞机和空中客车A380飞机。
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公开(公告)号：US20150336658A1
公开(公告)日：2015-11-26
申请号：US14728452
申请日：2015-06-02
IPC分类号： B64C9/16
CPC分类号： B64C9/16 , B64C9/02 , B64C9/22 , F16C11/0614 , F16C19/38 , F16C23/086 , F16C33/36 , F16C33/48 , F16C33/495 , F16C33/7806 , F16C33/784 , F16C2240/76 , F16C2326/43
摘要： An edge flap arrangement for an aircraft wing includes a main flap element and an actuator. A linkage arrangement supports the main flap. The linkage arrangement includes a drop hinge link arrangement. The drop hinge link arrangement includes a fixed strut and a drop link. The fixed strut and the drop link are pivotally connected by a hinge point. The hinge point includes an hourglass bearing. The hourglass bearing includes an inner member, an outer member, and a plurality of hourglass rollers. Any combination of the inner member, the outer member, and the hourglass rollers are fabricated from CREN, Cronidur 30, XD15NW, 422 Stainless Steel, CRES, and/or 440C Stainless Steel. A cage is disposed between the inner member and the outer member. The cage includes a plurality of first rails and a plurality of second rails. Opposing pairs of first rails and second rails define a plurality of pockets.
摘要翻译： 用于飞机机翼的边缘翼片装置包括主翼片元件和致动器。 连接装置支撑主瓣。 连接装置包括一个液滴铰链连接装置。 液滴铰链连接装置包括固定支柱和下降连杆。 固定支柱和下降连杆通过铰链点枢转连接。 铰链点包括沙漏轴承。 沙漏轴承包括内部构件，外部构件和多个沙漏辊。 内部构件，外部构件和沙漏滚子的任何组合由CREN，Cronidur 30，XD15NW，422不锈钢，CRES和/或440C不锈钢制成。 保持架设置在内部构件和外部构件之间。 笼包括多个第一轨道和多个第二轨道。 相对的第一轨道和第二轨道对限定了多个口袋。
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7.发明申请公开(公告)号：US20200291979A1
公开(公告)日：2020-09-17
申请号：US16457301
申请日：2019-06-28
摘要： A bolt for an interference fastener and a fastener system is provided. The bolt has a body extending axially between a first end and a second end. The body has a threaded area extending axially inward from the second end and a head configured on the first end. A cylindrical expansion area extends axially between the head and the transition area. The transition area is disposed axially between the cylindrical expansion area and the threaded area.
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8.发明申请公开(公告)号：US20200248746A1
公开(公告)日：2020-08-06
申请号：US16775533
申请日：2020-01-29
摘要： A ball bearing assembly includes a one piece outer ring having a first and second outer race and an exterior surface; and a one piece inner ring having a first and second inner race, the inner ring is integrally formed on a shaft. A first plurality of balls is disposed between the first outer race and the first inner race; and a second plurality of balls is disposed between the second outer race and the second inner race. The first plurality of balls has a first contact and the second plurality of balls has a second contact angle.
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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
摘要： 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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