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    High load capacity bi-directional tapered roller bearing
    3.
    发明授权
    High load capacity bi-directional tapered roller bearing 有权
    高负载能力双向圆锥滚子轴承

    公开(公告)号：US06464401B1

    公开(公告)日：2002-10-15

    申请号：US09771194

    申请日：2001-01-26

    申请人： Kenneth L. Allard

    发明人： Kenneth L. Allard

    IPC分类号： F16C3358

    CPC分类号： F16C19/364 ,  F16C19/225 ,  F16C23/08 ,  F16C33/605 ,  F16C35/063 ,  F16C2360/23

    摘要： The present invention is a bi-directional tapered roller bearing having a first cone rib ring thrust face “C” adjacent and facing the small diameter end faces of the roller elements, a second cone rib ring thrust face “B” adjacent and facing the large diameter end faces of the roller elements, and a cup rib ring thrust face “A” adjacent and facing the large diameter end faces of the roller elements. The bearing components are arranged such that, during primary thrust load operation, there is a gap between thrust face C and the small diameter end faces of the roller elements, a gap between thrust face A and the large diameter end faces of the roller elements, and contact between thrust face B and the large diameter end faces of the roller elements. With this arrangement, bearing roller element centrifugal loads act to reduce the contact forces between the roller elements and the bearing races.

    摘要翻译： 本发明是一种双向圆锥滚子轴承，其具有与滚子元件的小直径端面相邻并面对的第一锥形肋环推力面“C”，与第二锥形肋环推力面相邻并面对大的 滚子元件的直径端面，以及与罗拉元件的大直径端面相邻并面对的杯肋环推力面“A”。 轴承部件布置成使得在主推力加载操作期间，推力面C和滚子元件的小直径端面之间存在间隙，止推面A和滚子元件的大直径端面之间的间隙， 并且推力面B与滚子元件的大直径端面之间的接触。 通过这种布置，轴承滚子元件的离心载荷用于减小滚子元件和轴承座圈之间的接触力。

    Active clearance control
    4.
    发明授权
    Active clearance control 失效
    主动间隙控制

    公开(公告)号：US4576547A

    公开(公告)日：1986-03-18

    申请号：US548466

    申请日：1983-11-03

    申请人： Harvey I. Weiner ,  Kenneth L. Allard

    发明人： Harvey I. Weiner ,  Kenneth L. Allard

    IPC分类号： F01D11/08 ,  F01D11/24 ,  F02C7/18 ,  F02C7/28 ,  F04D29/52 ,  F02C7/16

    CPC分类号： F01D11/24

    摘要： The bore of the compressor for a gas turbine engine is heated by selectively bleeding compressor air from downstream stages so that heating only occurs at discreet times during the engine operating envelope. The bled air is admitted into the bore at the mid-stage station of the compressor wherein the compressor disks are scrubbed so as to expand and close the gap between the outer air seal and tips of the compressor blades during cruise of the aircraft and prevented from heating the disks during the high powered operations of the engine.

    摘要翻译： 用于燃气涡轮发动机的压缩机的孔通过从下游级选择性地排出压缩机空气来加热，使得加热仅在发动机操作范围内的谨慎时间发生。 流出的空气进入压缩机中段的孔中，其中压缩机盘被擦洗，以在飞行器巡航期间扩展和关闭外部空气密封件与压缩机叶片的尖端之间的间隙，并且防止 在发动机高功率操作期间加热盘。

    Bifurcated oil scavenge system for a gas turbine engine
    5.
    发明授权
    Bifurcated oil scavenge system for a gas turbine engine 有权
    用于燃气涡轮发动机的分叉除油系统

    公开(公告)号：US06996968B2

    公开(公告)日：2006-02-14

    申请号：US10738354

    申请日：2003-12-17

    申请人： Robert E. Peters ,  Dwayne Messerschmidt ,  J. Axel Glahn ,  Kenneth L. Allard ,  Hsianmin F. Jen ,  Larry W. Spires ,  Roger M. Barnsby

    发明人： Robert E. Peters ,  Dwayne Messerschmidt ,  J. Axel Glahn ,  Kenneth L. Allard ,  Hsianmin F. Jen ,  Larry W. Spires ,  Roger M. Barnsby

    IPC分类号： F02C7/06

    CPC分类号： F01D25/18 ,  F05D2260/60 ,  F05D2260/602 ,  F16C33/6685 ,  F16C2360/23

    摘要： An oil scavenge system includes a tangential scavenge scoop and a settling area adjacent thereto which separately communicate with a duct which feeds oil into an oil flow path and back to an oil sump. A shield is mounted over the settling area to at least partially shield the collecting liquid oil from interfacial shear. A multiple of apertures are located through the shield to permit oil flow through the shield and into the duct. The scavenge scoop forms a partition which separates the duct into a first portion and a second portion. The first portion processes upstream air/oil mixture that is captured by the tangential scoop while the second portion receives the oil collected in the settling area.

    摘要翻译： 油清除系统包括切向扫气勺和与其相邻的沉降区域，其与将油输送到油流路并返回到油底壳的管道分开连通。 屏蔽件安装在沉降区域上，以至少部分地屏蔽收集液体油不受界面剪切。 通过屏蔽件定位了多个孔，以允许油流过屏蔽并流入管道。 扫气勺形成将管道分成第一部分和第二部分的隔板。 第一部分处理由切向勺捕获的上游空气/油混合物，而第二部分接收在沉降区域中收集的油。

    Method of scavenging oil within a gas turbine engine
    6.
    发明授权
    Method of scavenging oil within a gas turbine engine 有权
    在燃气涡轮发动机内清除油的方法

    公开(公告)号：US07373780B2

    公开(公告)日：2008-05-20

    申请号：US11257689

    申请日：2005-10-25

    申请人： Robert E. Peters ,  Dwayne Messerschmidt ,  J. Axel Glahn ,  Kenneth L. Allard ,  Hsianmin F. Jen ,  Larry W. Spires ,  Roger M. Barnsby

    发明人： Robert E. Peters ,  Dwayne Messerschmidt ,  J. Axel Glahn ,  Kenneth L. Allard ,  Hsianmin F. Jen ,  Larry W. Spires ,  Roger M. Barnsby

    IPC分类号： F02C7/00

    CPC分类号： F01D25/18 ,  F05D2260/60 ,  F05D2260/602 ,  F16C33/6685 ,  F16C2360/23

    摘要： An oil scavenge system includes a tangential scavenge scoop and a settling area adjacent thereto which separately communicate with a duct which feeds oil into an oil flow path and back to an oil sump. A shield is mounted over the settling area to at least partially shield the collecting liquid oil from interfacial shear. A multiple of apertures are located through the shield to permit oil flow through the shield and into the duct. The scavenge scoop forms a partition which separates the duct into a first portion and a second portion. The first portion processes upstream air/oil mixture that is captured by the tangential scoop while the second portion receives the oil collected in the settling area.

    摘要翻译： 油清除系统包括切向扫气勺和与其相邻的沉降区域，其与将油输送到油流路并返回到油底壳的管道分开连通。 屏蔽件安装在沉降区域上以至少部分地屏蔽收集液体油不受界面剪切。 通过屏蔽件定位了多个孔，以允许油流过屏蔽并流入管道。 扫气勺形成将管道分成第一部分和第二部分的隔板。 第一部分处理由切向勺捕获的上游空气/油混合物，而第二部分接收在沉降区域中收集的油。