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    Controllable variable fan outlet guide vanes
    1.
    发明授权
    Controllable variable fan outlet guide vanes 有权

    公开(公告)号：US11802490B2

    公开(公告)日：2023-10-31

    申请号：US17412218

    申请日：2021-08-25

    Applicant: Rolls-Royce Corporation

    Inventor： Christopher D. Hall ,  William B. Bryan ,  Daniel E. Molnar, Jr.

    IPC: F01D17/16 ,  F01D7/02 ,  F01D17/06

    CPC classification number: F01D17/162 ,  F01D7/02 ,  F01D17/06 ,  F05D2240/12 ,  F05D2250/90 ,  F05D2260/56

    Abstract: A fan assembly includes a fan duct, an inlet fan, and an outlet guide vane assembly. The inlet fan includes blades adapted to force fan exit air toward an aft end of the fan duct. The outlet guide vane assembly is located in the fan duct downstream of the inlet fan and is configured to adjust a direction of the fan exit air received from the blades. The outlet guide vane assembly includes a first plurality of outlet guide vanes including a first outlet guide vane configured to rotate to a first angle so as to redirect the fan exit air in a first direction and a second outlet guide vane configured to rotate to a second angle so as to redirect the fan exit air in a second direction. The second outlet guide vane is located at a different circumferential position than the first outlet guide vane.

    Electric Track Lock
    4.
    发明申请
    Electric Track Lock 有权
    电动轨道锁

    公开(公告)号：US20160363098A1

    公开(公告)日：2016-12-15

    申请号：US14735865

    申请日：2015-06-10

    Applicant: Woodward, Inc.

    Inventor： Joseph Thomas Kopecek

    IPC: F02K1/76 ,  F16H25/04

    CPC classification number: F02K1/766 ,  B64D29/06 ,  F02K1/72 ,  F02K1/763 ,  F05D2260/56 ,  G05G5/08 ,  G05G5/18 ,  Y02T50/671

    Abstract: The subject matter of this specification can be embodied in, among other things, a track lock assembly that includes a pawl assembly comprising a pawl arm extending from a pawl axis and configured to engage a slot in a slider assembly, a cam arm extending from the pawl axis and having a pawl cam, and a compliant member, and a position lock assembly comprising a first lock arm extending from a lock axis and an actuator configured to urge rotation of the first lock arm between a lock locked position and a lock unlocked position, the first lock arm configured to engage and retain the cam arm in a pawl locked position when the first lock arm is in the lock locked position and disengage the cam arm in the lock unlocked position such that the compliant member is able to urge the pawl assembly to a pawl unlocked position.

    Abstract translation: 本说明书的主题可以包括一种轨道锁组件，其包括棘爪组件，所述棘爪组件包括从棘爪轴线延伸并构造成接合滑块组件中的狭槽的棘爪臂， 棘爪轴并具有棘爪凸轮和柔顺构件，以及位置锁定组件，其包括从锁定轴线延伸的第一锁定臂和构造成促使第一锁定臂在锁定锁定位置和锁定解除位置之间的旋转的致动器 所述第一锁定臂构造成当所述第一锁定臂处于所述锁定位置时将所述凸轮臂接合并保持在棘爪锁定位置，并且所述凸轮臂在所述锁定解锁位置中脱离，使得所述柔顺构件能够推动所述棘爪 组装到棘爪解锁位置。

    Compact actuation system for flow nozzle
    5.
    发明授权
    Compact actuation system for flow nozzle 有权
    紧凑的流动喷嘴致动系统

    公开(公告)号：US09464594B2

    公开(公告)日：2016-10-11

    申请号：US14209749

    申请日：2014-03-13

    Applicant: Rolls-Royce North American Technologies, Inc.

    Inventor： Kenneth M. Pesyna

    IPC: F02K1/12 ,  F02K1/15 ,  F02K3/075 ,  F02K3/077 ,  F02K3/115 ,  F02K1/80

    CPC classification number: F02K1/1223 ,  F02K1/1207 ,  F02K1/1238 ,  F02K1/15 ,  F02K1/80 ,  F02K3/075 ,  F02K3/077 ,  F02K3/115 ,  F05D2250/411 ,  F05D2260/50 ,  F05D2260/56 ,  F05D2270/051 ,  F05D2270/66 ,  Y02T50/671

    Abstract: Embodiments may include an actuation system for an exhaust nozzle of a gas turbine engine. The actuation system may comprise a plurality of flap assemblies including a plurality of convergent flaps movable between first and second convergent positions and a plurality of divergent flaps movable between first and second divergent positions. Each of the plurality of divergent flaps may extend from a respective one of the plurality of convergent flaps. The system may further include a first sync ring rotatably carried by an engine body and configured to synchronously move the divergent flaps between the first and second divergent positions and a second sync ring rotatably carried by the engine body and configured to synchronously move the convergent flaps between the first and second convergent positions. A method may translate rotation of the sync ring to movement of a vehicle surface between radially outward and inward positions.

    Abstract translation: 实施例可以包括用于燃气涡轮发动机的排气喷嘴的致动系统。 致动系统可以包括多个翼片组件，其包括可在第一和第二收敛位置之间移动的多个收敛翼片和可在第一和第二发散位置之间移动的多个发散翼片。 多个发散片中的每一个可以从多个收敛片中的相应一个延伸。 该系统可以进一步包括第一同步环，该第一同步环由发动机本体可旋转地承载并且构造成在第一和第二发散位置之间同步地移动发散翼片，以及第二同步环，该第二同步环由发动机主体可转动地支撑并且构造成使收敛翼片在 第一和第二收敛位置。 一种方法可以将同步环的旋转转移到径向向外和向内位置之间的车辆表面的移动。

    Dual-Cam Bellcrank Mechanism
    6.
    发明申请
    Dual-Cam Bellcrank Mechanism 有权
    双凸轮钟形机构

    公开(公告)号：US20160258385A1

    公开(公告)日：2016-09-08

    申请号：US14635625

    申请日：2015-03-02

    Applicant: The Boeing Company

    Inventor： Alex C. Lumbab

    IPC: F02K1/15 ,  B05B1/04 ,  F16H25/18

    CPC classification number: F02K1/15 ,  B05B1/04 ,  F02K1/763 ,  F05D2260/56 ,  F16H25/18 ,  Y02T50/672

    Abstract: A method and system for imparting a linear motion to a flexible shaft is disclosed. The system includes a bellcrank having a first arm, a second arm, and a first pivot pin therebetween. The system further includes an actuating device coupled to the first arm and configured to apply a force to cause the bellcrank to rotate about the first pivot pin. Still further, the system includes a second pivot pin coupled to a rod-end of the flexible shaft and further coupled to a slotted hole on the second arm. Yet still further, the system includes a follower surface on the rod-end of the flexible shaft and configured to slide on a cam surface machined on the second arm. Upon application of the force to the first arm, the flexible shaft moves in a substantially linear motion.

    Abstract translation: 公开了一种用于向柔性轴施加直线运动的方法和系统。 该系统包括具有第一臂，第二臂和第一枢转销之间的曲拐。 所述系统还包括联接到所述第一臂并且构造成施加力以使所述曲拐围绕所述第一枢转销旋转的致动装置。 此外，该系统包括联接到柔性轴的杆端的第二枢转销，并且还连接到第二臂上的开槽孔。 而且，该系统还包括在柔性轴的杆端上的随动表面，并且构造成在加工在第二臂上的凸轮表面上滑动。 在向第一臂施加力时，柔性轴以基本线性的运动移动。

    COMPONENT ARRANGEMENT OF A GAS TURBINE
    7.
    发明申请
    COMPONENT ARRANGEMENT OF A GAS TURBINE 审中-公开
    气体涡轮机的组件布置

    公开(公告)号：US20160032777A1

    公开(公告)日：2016-02-04

    申请号：US14805496

    申请日：2015-07-22

    Applicant: MTU Aero Engines AG

    Inventor： Stefan Sasse

    IPC: F01D25/24

    CPC classification number: F01D25/243 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2260/37 ,  F05D2260/56

    Abstract: The present invention relates to a component arrangement of a gas turbine, this arrangement having a first gas turbine component, in particular a first wall segment (10) of a gas turbine duct casing; a second gas turbine component that can be joined thereto, in particular a second wall segment (20) of a gas turbine duct casing, with a flange (21), which is particularly bent; and an eccentric clamping element (30), which is mounted rotatably about an axis of rotation (A) on the first gas turbine component and has an eccentric contour portion (31), whose radial distance (r) to the axis of rotation varies by an angle (φ) about the axis of rotation, in order to press the flange (21) of the second gas turbine component (20) against the first gas turbine component, in particular to clamp it between the first gas turbine component and the eccentric contour portion (31).

    Abstract translation: 本发明涉及一种燃气轮机的部件布置，该装置具有第一燃气轮机部件，特别是燃气轮机管壳体的第一壁段（10）; 能与其连接的第二燃气涡轮机部件，特别是燃气轮机管道壳体的第二壁部分（20），其具有特别弯曲的凸缘（21）; 以及偏心夹紧元件（30），其围绕第一燃气轮机部件的旋转轴线（A）可旋转地安装，并且具有偏心轮廓部分（31），其偏心轴线的径向距离（r） 围绕旋转轴线的角度（＆phgr），以便将第二燃气轮机部件（20）的凸缘（21）压靠第一燃气轮机部件，特别是将其夹紧在第一燃气轮机部件和 偏心轮廓部分（31）。

    ACTUATOR MOUNTED TO TORQUE BOX
    8.
    发明申请
    ACTUATOR MOUNTED TO TORQUE BOX 有权
    执行器安装到扭矩箱

    公开(公告)号：US20150219017A1

    公开(公告)日：2015-08-06

    申请号：US14684689

    申请日：2015-04-13

    Applicant: United Technologies Corporation

    Inventor： Bernard W. Pudvah ,  Eugene C. Gasmen ,  Stanley Wiecko

    IPC: F02C9/22 ,  F16H21/44

    CPC classification number: F02C9/22 ,  F01D17/162 ,  F04D29/563 ,  F05D2250/312 ,  F05D2250/313 ,  F05D2260/31 ,  F05D2260/56 ,  F16H21/44 ,  Y10T74/18888 ,  Y10T74/20012

    Abstract: An actuator system mounted to a gas turbine engine that communicates mechanical power for positioning variable guide vanes within the gas turbine engine. The actuator system includes a torque box having components for communicating mechanical power to the variable guide vanes for positioning the vanes and an actuator mechanically coupled to provide mechanical power to the components of the torque box used to communicate the provided mechanical power to the inlet guide vanes. The actuator is mounted to the torque box via an elongate fastener extending in one direction and another elongate fastener extending in another direction.

    Abstract translation: 安装到燃气涡轮发动机的致动器系统，其传达用于在燃气涡轮发动机内定位可变导向叶片的机械动力。 致动器系统包括具有用于将机械动力传递到用于定位叶片的可变导向叶片的部件的扭矩盒，以及致动器，其机械联接以向用于将所提供的机械动力传递到入口导向叶片的扭矩箱的部件提供机械动力 。 致动器通过沿一个方向延伸的细长紧固件安装在转矩箱上，另一个细长紧固件沿另一个方向延伸。

    Turbine yokeplate flyweights to improve RAT startup
    9.
    发明授权
    Turbine yokeplate flyweights to improve RAT startup 有权
    涡轮机yokeplate flyweights来改善RAT启动

    公开(公告)号：US09045983B2

    公开(公告)日：2015-06-02

    申请号：US12907728

    申请日：2010-10-19

    Applicant: David Everett Russ

    Inventor： David Everett Russ

    IPC: F01D7/02 ,  B64D41/00

    CPC classification number: F01D7/02 ,  B64D41/007 ,  F05D2220/34 ,  F05D2260/52 ,  F05D2260/56 ,  F05D2260/71 ,  F05D2260/77 ,  F05D2260/79 ,  Y02T50/671 ,  Y02T50/673

    Abstract: A turbine having a cam follower operable to control turbine blade pitch in association with a position thereof is provided and includes an axially movable plate, a rotational and axially movable flyweight and a system operably coupled to the plate and the flyweight whereby, at low RPMs, the system prevents flyweight rotation such that the plate and the flyweight position the cam follower at a first position, at medium RPMs, the system permits flyweight rotation such that the plate and the flyweight position the cam follower at a second position, and, at high RPMs, the system prevents further flyweight rotation and permits initial axial movement of the plate and the flyweight such that the plate and the flyweight position the cam follower at a third position.

    Abstract translation: 提供了具有可操作以与其位置相关联地控制涡轮机叶片间距的凸轮从动件的涡轮机，并且包括可轴向移动的板，可旋转和可轴向移动的飞轮和可操作地联接到板和飞轮的系统， 该系统防止飞行重量的旋转，使得板和飞行重量将凸轮从动件定位在第一位置，以中等RPMs，系统允许飞行重复旋转，使得板和飞行重量将凸轮从动件定位在第二位置，并且在高 RPM，系统防止进一步的飞行重量旋转并且允许板和飞重的初始轴向运动，使得板和飞轮将凸轮从动件定位在第三位置。

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