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公开(公告)号：US09822817B2
公开(公告)日：2017-11-21
申请号：US15076119
申请日：2016-03-21
Inventor： Craig M. Price , Andrew D. Copeland
CPC classification number: F16C33/6681 , F16C19/06 , F16C33/3843 , F16C33/3887 , F16C33/4623 , F16C33/467 , F16C33/6677 , F16C37/007 , F16C2360/23
Abstract: A bearing assembly includes an outer race, a cage, a plurality of internal rotating members, and an inner race. Lubricant flows through the bearing assembly to withdraw heat generated during operation of the bearing assembly.
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公开(公告)号：US20160377121A1
公开(公告)日：2016-12-29
申请号：US15158076
申请日：2016-05-18
Inventor： Andrew D. Copeland , Craig M. Price
CPC classification number: F16C33/6696 , F16C19/06 , F16C19/08 , F16C33/30 , F16C33/303 , F16C33/44 , F16C33/445 , F16C33/62 , F16C2240/40 , F16C2360/00
Abstract: An expendable bearing and a method for making the same including an inner race defining an inner bearing diameter, an outer race defining an outer bearing diameter, a seal attached to the outer race and positioned adjacent and in contact with the inner race, where the inner race, the outer race, and the seal define a bearing cavity, a plurality of rolling elements positioned adjacent to the inner and outer races in the bearing cavity, a dry film lubricant on a surface of at least one of the inner race, the outer race, or the plurality of rolling elements, and a powder lubricant comprising carbon nanotubes disposed in the bearing cavity.
Abstract translation: 一种可消耗的轴承及其制造方法，其包括限定内轴承直径的内圈，限定外轴承直径的外座圈，附接到外座圈的密封件，并且定位成与内座圈相邻并与其接触， 所述外圈和所述密封件限定轴承腔，与所述轴承腔中的所述内圈和外圈相邻定位的多个滚动元件，所述内圈，所述外圈中的至少一个的外表面上的干膜润滑剂 种族或多种滚动元件，以及包含设置在轴承腔中的碳纳米管的粉末润滑剂。
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公开(公告)号：US20160319872A1
公开(公告)日：2016-11-03
申请号：US15076119
申请日：2016-03-21
Inventor： Craig M. Price , Andrew D. Copeland
CPC classification number: F16C33/6681 , F16C19/06 , F16C33/3843 , F16C33/3887 , F16C33/4623 , F16C33/467 , F16C33/6677 , F16C37/007 , F16C2360/23
Abstract: According to the present disclosure, a bearing assembly includes an outer race, a cage, a plurality of internal rotating members, and an inner race. Lubricant flows through the bearing assembly to withdraw heat generated during operation of the bearing assembly.
Abstract translation: 根据本公开，轴承组件包括外圈，保持架，多个内部旋转构件和内圈。 润滑剂流过轴承组件以退回轴承组件运行期间产生的热量。
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公开(公告)号：US09051882B2
公开(公告)日：2015-06-09
申请号：US14137147
申请日：2013-12-20
Applicant: Rolls-Royce Corporation
Inventor： Andrew D. Copeland , John H. Munson
CPC classification number: F02C7/28 , F01D11/003 , F01D25/183 , F05D2260/95 , F05D2300/611 , F16J15/3496 , F16J15/441 , F16J15/443
Abstract: A seal assembly for use in a gas turbine engine includes a first component, a second component, and a sealing unit. The first component is spaced apart from the second component to form a gap therebetween. The sealing unit is positioned in the gap between the first and second components to block liquids and/or gasses from traveling through the gap.
Abstract translation: 用于燃气涡轮发动机的密封组件包括第一部件，第二部件和密封单元。 第一部件与第二部件间隔开，以在它们之间形成间隙。 密封单元位于第一和第二部件之间的间隙中，以阻止液体和/或气体穿过间隙。
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公开(公告)号：US20200284201A1
公开(公告)日：2020-09-10
申请号：US16293030
申请日：2019-03-05
Applicant: Rolls-Royce Corporation
Inventor： John R. Gebhard , Adam L. Kempers , Andrew D. Copeland
Abstract: A gas turbine engine includes a first spool and a second spool. The first spool includes a compressor stage, a first turbine stage, and a first shaft configured to transmit rotational energy between the first turbine stage and the compressor stage. The second spool includes a fan, a second turbine stage, and a second shaft configured to transmit rotational energy between the second turbine stage and the fan.
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Patent Agency Ranking
公开(公告)号：US20150046061A1
公开(公告)日：2015-02-12
申请号：US14095478
申请日：2013-12-03
Applicant: Rolls-Royce Corporation
Inventor： Andrew D. Copeland , Alan B. Cookerly
IPC: F02C9/48
CPC classification number: F02C9/48 , F01D11/20 , F01D25/164 , F02C7/06 , F05D2240/53 , F16C27/02 , F16C27/045 , F16C33/106 , F16F15/0237
Abstract: An aircraft powerplant having a shaft is disclosed in one embodiment in which a squeeze-film damper is used. The squeeze-film damper includes a plurality of sectors having a working fluid. A pressure can be controlled in the working fluid to the sectors to discourage changes in the sectors as a result of vehicle maneuvering. A controller is used to operate upon sensed aircraft motion and regulate pressure in the sectors.
Abstract translation: 在其中使用挤压薄膜阻尼器的一个实施例中公开了具有轴的飞行器动力装置。 挤膜膜阻尼器包括具有工作流体的多个扇区。 可以将工作流体中的压力控制到扇区，以阻止车辆操纵导致的扇区变化。 控制器用于对感测到的飞机运动进行操作并调节扇区中的压力。
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公开(公告)号：US20150014937A1
公开(公告)日：2015-01-15
申请号：US14145301
申请日：2013-12-31
Applicant: Rolls-Royce Corporation
Inventor： Chad A. Behrman , Andrew D. Copeland
CPC classification number: F16J15/164 , F16J15/3204 , F16J15/3244 , F16J15/40
Abstract: A fluid sealing assembly includes a shaft and a seal. The shaft includes a surface portion having a microstructural geometry. The seal has a radially flexible portion disposed in proximity to the surface portion having the microstructural geometry such that when the shaft is rotated a pressure differential is generated at the interface of the seal and the surface portion having the microstructural geometry that pushes or pulls fluid relative to the interface.
Abstract translation: 流体密封组件包括轴和密封件。 轴包括具有微结构几何形状的表面部分。 密封件具有设置在具有微结构几何形状的表面部分附近的径向柔性部分，使得当轴旋转时，在密封件的界面处产生压差，并且具有推动或拉动流体的微结构几何形状的表面部分 到界面
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公开(公告)号：US11067006B2
公开(公告)日：2021-07-20
申请号：US16293030
申请日：2019-03-05
Applicant: Rolls-Royce Corporation
Inventor： John R. Gebhard , Adam L. Kempers , Andrew D. Copeland
Abstract: A gas turbine engine includes a first spool and a second spool. The first spool includes a compressor stage, a first turbine stage, and a first shaft configured to transmit rotational energy between the first turbine stage and the compressor stage. The second spool includes a fan, a second turbine stage, and a second shaft configured to transmit rotational energy between the second turbine stage and the fan.
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公开(公告)号：US12000299B1
公开(公告)日：2024-06-04
申请号：US18238267
申请日：2023-08-25
Applicant: Rolls-Royce Corporation
Inventor： Andrew D. Copeland
CPC classification number: F01D25/183 , F01D25/16 , F05D2240/50 , F05D2260/98
Abstract: A rotor assembly includes an oil jet assembly, an inner shaft assembly, an outer shaft assembly, and an oil mist shield. The oil jet assembly selectively ejects oil for lubrication. The inner shaft assembly is configured to rotate about a central axis. The outer shaft assembly is configured to rotate selectively about the central axis independent of the inner shaft assembly. The oil mist shield is coupled with the outer shaft and is configured to selectively block and allow the oil from the oil jet assembly from passing into a cavity.
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公开(公告)号：US09964152B2
公开(公告)日：2018-05-08
申请号：US15158076
申请日：2016-05-18
Inventor： Andrew D. Copeland , Craig M. Price
CPC classification number: F16C33/6696 , F16C19/06 , F16C19/08 , F16C33/30 , F16C33/303 , F16C33/44 , F16C33/445 , F16C33/62 , F16C2240/40 , F16C2360/00
Abstract: An expendable bearing and a method for making the same including an inner race defining an inner bearing diameter, an outer race defining an outer bearing diameter, a seal attached to the outer race and positioned adjacent and in contact with the inner race, where the inner race, the outer race, and the seal define a bearing cavity, a plurality of rolling elements positioned adjacent to the inner and outer races in the bearing cavity, a dry film lubricant on a surface of at least one of the inner race, the outer race, or the plurality of rolling elements, and a powder lubricant comprising carbon nanotubes disposed in the bearing cavity.
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