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    DUCT ARRANGEMENT
    2.
    发明申请
    DUCT ARRANGEMENT 有权
    道路安排

    公开(公告)号：US20140150919A1

    公开(公告)日：2014-06-05

    申请号：US14087623

    申请日：2013-11-22

    Applicant: ROLLS-ROYCE PLC

    Inventor： John Richard WEBSTER ,  Paul John NEWTON ,  Paul FLETCHER

    IPC: F16L9/00

    CPC classification number: F16L9/00 ,  B63H11/00 ,  B63H11/04 ,  B63H11/103 ,  B63H2011/004 ,  B63H2011/043

    Abstract: A duct arrangement 18 for a waterjet propulsor 10. The duct arrangement 18 comprises a main duct 30 having an inlet 20. The inlet 20 has an elongate main portion 32 extending along a principal axis 34, and at least one lateral portion 36 in fluid communication with the main portion 34. The at least one lateral portion 36 extends part way only along the length of the main portion 34.

    Abstract translation: 用于水射流推进器10的管道装置18.管道装置18包括具有入口20的主管道30.入口20具有沿主轴线34延伸的细长主体部分32和与流体连通的至少一个横向部分36 主体部分34.至少一个横向部分36仅沿主体部分34的长度部分地延伸。

    BEARING ARRANGEMENT
    4.
    发明申请
    BEARING ARRANGEMENT 有权
    轴承安排

    公开(公告)号：US20140369830A1

    公开(公告)日：2014-12-18

    申请号：US14290512

    申请日：2014-05-29

    Applicant: ROLLS-ROYCE PLC

    Inventor： Paul FLETCHER ,  John Richard WEBSTER ,  Alan Robert MAGUIRE

    IPC: F01D25/16 ,  F16C41/00 ,  F16C37/00

    CPC classification number: F01D25/16 ,  F01D25/162 ,  F02C7/28 ,  F05D2300/174 ,  F05D2300/501 ,  F16C19/10 ,  F16C19/54 ,  F16C25/083 ,  F16C27/08 ,  F16C35/077 ,  F16C37/007 ,  F16C41/004 ,  F16C41/02 ,  F16C2202/08 ,  F16C2204/42 ,  F16C2360/23

    Abstract: A bearing arrangement is disclosed. The bearing arrangement includes first and second bearings, with each bearing including a respective support element and a respective set of rolling elements and defining a respective load path extending through the respective support element and rolling elements. The support elements are coupled such that a load applied to either support element is transmitted through both the first and second load paths. The arrangement further includes a pair of superelastic titanium alloy elements located in the respective load paths to provide resilient movement between the bearings when a load is applied to the bearing arrangement.

    Abstract translation: 公开了一种轴承装置。 轴承装置包括第一和第二轴承，每个轴承包括相应的支撑元件和相应的一组滚动元件，并且限定延伸通过相应支撑元件和滚动元件的相应负载路径。 支撑元件被耦合，使得施加到任一支撑元件的负载通过第一和第二负载路径传输。 该装置还包括位于相应负载路径中的一对超弹性钛合金元件，以在负载施加到轴承装置时在轴承之间提供弹性运动。

    GAS TURBINE ENGINE EXHAUST NOZZLE
    5.
    发明申请
    GAS TURBINE ENGINE EXHAUST NOZZLE 审中-公开
    气体涡轮发动机排气喷嘴

    公开(公告)号：US20140145008A1

    公开(公告)日：2014-05-29

    申请号：US14079966

    申请日：2013-11-14

    Applicant: Rolls-Royce PLC

    Inventor： John Richard WEBSTER

    IPC: F02K1/12

    CPC classification number: F02K1/1207 ,  F02K1/085 ,  F02K1/50

    Abstract: An exhaust nozzle 234 comprising inner and outer walls defined by a turbine casing 233 and a nacelle 230 respectively. A duct in the form of a bypass duct 232 is defined therebetween through which a bypass flow B flows in use. The nacelle 230 comprises a fixed upstream wall section 240 and at least one radially movable downstream wall section 242. At least one closure element in the form of a first slat 248 is provided, which is locatable across the second outlet 246 extending in a generally axial direction. A downstream end 250 of the first slat 248 is radially moveable between an open position in which the second outlet 246 is open, and a closed position in which the second outlet 246 is closed.

    Abstract translation: 排气喷嘴234包括由涡轮壳体233和机舱230分别限定的内壁和外壁。 旁通管232形式的管道被限定在旁路流B在其中流动使用。 机舱230包括固定的上游壁部分240和至少一个径向可移动的下游壁部分242.提供呈第一板条248形式的至少一个闭合元件，其可跨越第二出口246定位，该第二出口246以大致轴向延伸 方向。 第一条板248的下游端250可在第二出口246打开的打开位置和第二出口246关闭的关闭位置之间径向移动。

    GEAR TRAINS
    6.
    发明申请
    GEAR TRAINS 审中-公开
    齿轮火车

    公开(公告)号：US20170074356A1

    公开(公告)日：2017-03-16

    申请号：US15235832

    申请日：2016-08-12

    Applicant: ROLLS-ROYCE plc

    Inventor： John Richard WEBSTER

    IPC: F16H1/46 ,  F02C7/36 ,  F16H1/28

    CPC classification number: F16H1/46 ,  F02C7/36 ,  F02K3/04 ,  F05D2240/35 ,  F05D2260/40311 ,  F16H1/2809 ,  F16H57/082

    Abstract: A gear train comprising: an input shaft; a first sun gear coupled to the input shaft; a plurality of first planet gears engaging the first sun gear; a first ring gear engaging the plurality of first planet gears; and a first planet carrier coupled to the plurality of first planet gears; a second sun gear coupled to the input shaft; a plurality of second planet gears engaging the second sun gear; a second ring gear engaging the plurality of second planet gears; and a second planet carrier coupled to the plurality of second planet gears; and an output member coupled to the first planet carrier at a first torque transfer location and coupled to the second planet carrier at a second torque transfer location, different to the first torque transfer location.

    Abstract translation: 一种齿轮系，包括：输入轴; 耦合到输入轴的第一太阳齿轮; 与第一太阳齿轮接合的多个第一行星齿轮; 与所述多个第一行星齿轮接合的第一齿圈; 以及耦合到所述多个第一行星齿轮的第一行星架; 耦合到所述输入轴的第二太阳齿轮; 与所述第二太阳齿轮接合的多个第二行星齿轮; 接合所述多个第二行星齿轮的第二齿圈; 以及联接到所述多个第二行星齿轮的第二行星架; 以及输出构件，其在第一扭矩传递位置处联接到所述第一行星架，并且在与所述第一扭矩传递位置不同的第二扭矩传递位置处联接到所述第二行星架。

    BEARING ARRANGEMENT AND METHOD
    7.
    发明申请
    BEARING ARRANGEMENT AND METHOD 审中-公开
    轴承安装和方法

    公开(公告)号：US20170003196A1

    公开(公告)日：2017-01-05

    申请号：US15264187

    申请日：2016-09-13

    Applicant: ROLLS-ROYCE plc

    Inventor： Stephen GALLIMORE ,  Paul FLETCHER ,  John Richard WEBSTER ,  Alan Robert MAGUIRE

    IPC: G01M13/04 ,  F16C41/02 ,  F16C27/08 ,  F16C19/54 ,  F16C19/52

    CPC classification number: G01M13/04 ,  F01D25/162 ,  F05D2240/52 ,  F05D2260/83 ,  F05D2300/501 ,  F16C19/16 ,  F16C19/522 ,  F16C19/54 ,  F16C19/542 ,  F16C25/083 ,  F16C27/08 ,  F16C33/586 ,  F16C41/02 ,  F16C2233/00 ,  F16C2237/00 ,  F16C2360/23 ,  Y02T50/671

    Abstract: A method of determining the axial load on load-sharing thrust bearings including: providing first and second thrust bearings, each including an inner race and an outer race supported by at least one resilient element; applying a test axial load to each of the first and second thrust bearings to elastically deform the at least one resilient element so as to axially displace the outer race; determining the test axial displacement of each outer race to obtain calibration data comprising values of axial load versus axial displacement; applying an in-service axial load to the first and second thrust bearings to elastically deform the resilient elements so as to axially displace the respective outer races; measuring the in-service axial displacement of each outer race; and based on the measured in-service axial displacements, inferring from the calibration data the values of the in-service axial loads on the first and second thrust bearings.

    Abstract translation: 一种确定负载共享止推轴承上的轴向载荷的方法，包括：提供第一和第二推力轴承，每个包括内座圈和由至少一个弹性元件支承的外座圈; 对所述第一推力轴承和所述第二推力轴承中的每一个施加测试轴向载荷，以使所述至少一个弹性元件弹性变形，从而轴向地移动所述外圈; 确定每个外圈的测试轴向位移以获得包括轴向载荷与轴向位移的值的校准数据; 对第一和​​第二止推轴承施加在役轴向载荷以使弹性元件弹性变形，从而轴向移动相应的外圈; 测量每个外圈的在役轴向位移; 并且基于测量的在役轴向位移，从校准数据推断第一和第二止推轴承上的在用轴向载荷的值。

    BEARING ARRANGEMENT
    8.
    发明申请
    BEARING ARRANGEMENT 有权
    轴承安排

    公开(公告)号：US20150267745A1

    公开(公告)日：2015-09-24

    申请号：US14631180

    申请日：2015-02-25

    Applicant: ROLLS-ROYCE PLC

    Inventor： Stephen GALLIMORE ,  John Richard WEBSTER

    IPC: F16C32/06 ,  F16C25/08 ,  F16C19/54

    CPC classification number: F16C39/04 ,  F16C19/16 ,  F16C19/54 ,  F16C19/547 ,  F16C25/08 ,  F16C33/586 ,  F16C41/02 ,  F16C2360/23

    Abstract: A bearing arrangement includes: first and second thrust bearings, arranged on a shaft and including respective first and second pressure faces; and a hydraulic connection, connecting the first and second thrust bearings and having a non-compressible fluid. Applying a shaft thrust load axially moves the first thrust bearing so that the first pressure face displaces the non-compressible fluid from the first thrust bearing to the second thrust bearing so as to apply a reaction force to the second pressure face, in order that the thrust load is shared between the first and second thrust bearings.

    Abstract translation: 轴承装置包括：第一和第二推力轴承，布置在轴上并包括相应的第一和第二压力面; 以及连接第一和第二推力轴承并具有不可压缩流体的液压连接。 施加轴推力负载使第一止推轴承轴向移动，使得第一压力面将不可压缩流体从第一推力轴承移位到第二推力轴承，以便向第二压力面施加反作用力，以便 推力载荷在第一和第二推力轴承之间共享。

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