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23 条记录 (耗时 0.021 秒)

    Shroud for an air turbine starter
    1.
    发明申请
    Shroud for an air turbine starter 有权
    用于空气涡轮起动器的护罩

    公开(公告)号：US20060257253A1

    公开(公告)日：2006-11-16

    申请号：US11128644

    申请日：2005-05-12

    申请人： Paulynn Dong ,  Kellan Geck ,  David Mathis ,  James Hall ,  David Gentile ,  Jennifer Zonneveld

    发明人： Paulynn Dong ,  Kellan Geck ,  David Mathis ,  James Hall ,  David Gentile ,  Jennifer Zonneveld

    IPC分类号： F04D29/44

    CPC分类号： F02C7/277 ,  F01D21/04 ,  F01D21/045

    摘要： A shroud is provided for separating an air turbine starter housing from a turbine wheel. The shroud comprises a ring and a bumper. The ring is configured to be disposed between the turbine wheel and the housing and has an outer peripheral surface and an inner peripheral surface that defines a flow channel. The bumper is coupled to and extends radially inwardly from the ring inner peripheral surface and defines a bumper section of the ring flow channel. At least a portion of the bumper section has a cross-sectional flow area that is less than another cross sectional flow area of the ring flow channel.

    摘要翻译： 提供了用于将空气涡轮起动器壳体与涡轮机叶轮分离的护罩。 护罩包括环和保险杠。 环被配置为设置在涡轮机叶轮和壳体之间，并且具有限定流动通道的外周表面和内周表面。 保险杠从环内周表面连接并径向向内延伸并且限定了环流通道的缓冲部分。 保险杠部分的至少一部分具有小于环形流动通道的另一横截面流动面积的横截面流动面积。

    Accessory lubrication system for a turbine plant
    2.
    发明申请
    Accessory lubrication system for a turbine plant 有权
    涡轮机配件润滑系统

    公开(公告)号：US20060056958A1

    公开(公告)日：2006-03-16

    申请号：US10880827

    申请日：2004-06-29

    申请人： Louie Gaines ,  Kellan Geck ,  Todd Langston ,  David Mathis ,  Jennifer Zonneveld

    发明人： Louie Gaines ,  Kellan Geck ,  Todd Langston ,  David Mathis ,  Jennifer Zonneveld

    IPC分类号： F03B11/00

    CPC分类号： F01D25/18 ,  F02C7/32

    摘要： A lubrication system for supplying lubricants between two environments is provided. The first environment is disposed within a first housing and the second environment is disposed within a second housing having a supply opening and an exhaust opening. The system includes a lubricant supply tube disposed within the supply opening and configured to supply lubricant from the first environment to the second environment. The system also includes a receptacle disposed within the second housing and configured to receive lubricant supplied from the supply tube and to hold a predetermined volume of the lubricant. A check valve is disposed within the second housing and is in fluid communication with the exhaust opening. The check valve is configured to receive overflow lubricant from the receptacle, if the lubricant exceeds the predetermined volume and to provide a seal between the first and second environments in response to a pressure differential therebetween.

    摘要翻译： 提供了一种用于在两种环境之间提供润滑剂的润滑系统。 第一环境设置在第一壳体内，第二环境设置在具有供给开口和排气口的第二壳体内。 该系统包括设置在供应开口内的润滑剂供应管，并且构造成将润滑剂从第一环境供应到第二环境。 该系统还包括设置在第二壳体内并且构造成容纳从供给管提供的润滑剂并保持预定体积的润滑剂的容器。 止回阀设置在第二壳体内并与排气口流体连通。 止回阀配置成从容器接收溢流润滑剂，如果润滑剂超过预定体积，并且响应于它们之间的压差，在第一和第二环境之间提供密封。

    ACTUATION ASSEMBLY
    3.
    发明申请
    ACTUATION ASSEMBLY 失效
    执行装配

    公开(公告)号：US20120181372A1

    公开(公告)日：2012-07-19

    申请号：US12252175

    申请日：2008-10-15

    申请人： Casey Hanlon ,  Kellan Geck ,  Andrew T. Johnson

    发明人： Casey Hanlon ,  Kellan Geck ,  Andrew T. Johnson

    IPC分类号： F42B15/01 ,  F15B15/18 ,  F15B15/02

    CPC分类号： F42B10/663 ,  F42B10/665 ,  Y10T74/18568

    摘要： An actuation assembly is provided. The actuation assembly includes a casing, a plurality of linear actuators coupled to the casing, each of the linear actuators having first and second components and being configured to move the second component thereof relative to the first component thereof along a respective first axis, and a plurality of translational member sets, each being coupled to the second component of a respective one of the linear actuators and the casing and being configured such that when the second component of the respective linear actuator moves along the respective first axis, a selected portion of the translational member set moves substantially along a respective second axis.

    摘要翻译： 提供致动组件。 致动组件包括壳体，联接到壳体的多个线性致动器，每个线性致动器具有第一和第二部件，并且构造成沿相应的第一轴线相对于其第一部件移动其第二部件，并且 多个平移构件组，每个平行构件组联接到线性致动器和壳体中的相应一个的第二部件，并且构造成使得当相应的线性致动器的第二部件沿着相应的第一轴线移动时，所选择的部分 平移构件组基本上沿相应的第二轴线移动。

    AIRCRAFT ELECTRIC BRAKE ACTUATOR ASSEMBLY WITH LINE REPLACEABLE ACTUATOR BRAKE
    4.
    发明申请
    AIRCRAFT ELECTRIC BRAKE ACTUATOR ASSEMBLY WITH LINE REPLACEABLE ACTUATOR BRAKE 有权
    航空电动制动器组件与线路可更换执行器制动器

    公开(公告)号：US20110198163A1

    公开(公告)日：2011-08-18

    申请号：US12704971

    申请日：2010-02-12

    申请人： Casey Hanlon ,  Kellan Geck ,  James Neil Quitmeyer

    发明人： Casey Hanlon ,  Kellan Geck ,  James Neil Quitmeyer

    IPC分类号： F16D55/02

    CPC分类号： B60T7/042 ,  B60T8/00 ,  B60T13/746 ,  F16D65/18 ,  F16D2125/40 ,  F16D2125/48 ,  F16D2127/06

    摘要： An aircraft electric brake actuator assembly includes an actuator housing, a motor housing, an actuator, an electric motor, and an actuator brake. The actuator housing is configured to be mounted on an aircraft landing gear. The motor housing is coupled to the actuator housing and is removable therefrom. The motor housing is also accessible when the actuator housing is mounted on an aircraft. The electric motor is disposed within the motor housing and is coupled to the actuator. The actuator brake is disposed within the motor housing and is removably coupled to the motor.

    摘要翻译： 飞行器电动制动器致动器组件包括致动器壳体，马达壳体，致动器，电动马达和致动器制动器。 致动器壳体构造成安装在飞机起落架上。 马达壳体联接到致动器壳体并且可从其移除。 当执行器外壳安装在飞机上时，马达外壳也可以接近。 电动机设置在电动机壳体内并联接到致动器。 致动器制动器设置在马达壳体内并且可拆卸地联接到马达。

    AIRCRAFT BRAKE ACTUATOR THERMAL INSULATOR AND TANGENTIAL MOVEMENT COMPENSATOR
    5.
    发明申请
    AIRCRAFT BRAKE ACTUATOR THERMAL INSULATOR AND TANGENTIAL MOVEMENT COMPENSATOR 有权
    飞机制动器执行器热绝缘器和电机运动补偿器

    公开(公告)号：US20060086576A1

    公开(公告)日：2006-04-27

    申请号：US10973572

    申请日：2004-10-25

    申请人： James Quitmeyer ,  Donald Christensen ,  Kellan Geck

    发明人： James Quitmeyer ,  Donald Christensen ,  Kellan Geck

    IPC分类号： F16D55/08

    CPC分类号： F16D65/18 ,  F16D65/0971 ,  F16D65/847 ,  F16D2125/06

    摘要： An aircraft brake actuation system includes an actuator for selectively moving to a position that corresponds to a commanded brake force. A cap assembly is coupled to the end of the actuator and is configured to engage an aircraft brake element and supply the commanded brake force to one or more aircraft wheels. The cap assembly is constructed of a low thermal conductivity material and has thermal resistance grooves formed therein. The cap assembly is also configured to compensate for certain undesired tangential movements that may occur during an aircraft brake cycle.

    摘要翻译： 飞机制动器致动系统包括用于选择性地移动到对应于所命令的制动力的位置的致动器。 盖组件联接到致动器的端部并且构造成接合飞行器制动元件并将命令的制动力提供给一个或多个飞行器轮。 盖组件由低导热性材料构成，并且在其中形成有热阻槽。 盖组件还被配置为补偿在飞机制动循环期间可能发生的某些不期望的切向运动。

    MODULAR, HARNESSLESS ELECTROMECHANICAL ACTUATION SYSTEM ASSEMBLY
    7.
    发明申请
    MODULAR, HARNESSLESS ELECTROMECHANICAL ACTUATION SYSTEM ASSEMBLY 有权
    模块化，无线电动执行系统总成

    公开(公告)号：US20090114763A1

    公开(公告)日：2009-05-07

    申请号：US12133175

    申请日：2008-06-04

    申请人： Kellan Geck ,  George Woessner ,  Dwayne M. Benson ,  Bulent Sarlioglu

    发明人： Kellan Geck ,  George Woessner ,  Dwayne M. Benson ,  Bulent Sarlioglu

    IPC分类号： B64C9/00 ,  H02K7/00 ,  H02K7/06

    CPC分类号： F42B10/64 ,  H02K7/116 ,  H02K11/0094 ,  H02K11/33 ,  H02K16/00

    摘要： A modular electromechanical actuation system assembly is provided that includes an electronic control unit housing having a plurality of motor receptacles and a plurality of battery receptacles formed in an outer surface thereof. Each of the motor receptacles has an associated motor electrical interface, and each of the battery receptacles has an associated battery electrical interface. An electronic control unit is disposed within the electronic control unit housing and is electrically coupled to each of the motor electrical interfaces and each of the battery electrical interfaces. A plurality of motors are supported, one each, within one of the motor receptacles, and a plurality of batteries are supported, one each, within one of the battery receptacles.

    摘要翻译： 提供了一种模块化机电致动系统组件，其包括具有多个马达插座的电子控制单元壳体和形成在其外表面中的多个电池插座。 每个电动机插座具有相关联的电动机电接口，并且每个电池插座具有相关联的电池电接口。 电子控制单元设置在电子控制单元壳体内并且电耦合到每个电动机电接口和每个电池电接口。 多个电动机在一个电动机插座内分别被支撑，多个电池分别在一个电池插座内被支撑。