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    Ram air thermal management system
    7.
    发明授权
    Ram air thermal management system 有权

    公开(公告)号：US09840967B2

    公开(公告)日：2017-12-12

    申请号：US14132716

    申请日：2013-12-18

    申请人： Rolls-Royce North American Technologies, Inc.

    发明人： Douglas J. Snyder ,  Kenneth M. Pesyna

    IPC分类号： F01N5/02 ,  F02C7/18 ,  F02K3/115 ,  F02C7/14

    CPC分类号： F02C7/185 ,  F02C7/14 ,  F02K3/115 ,  F05D2260/601 ,  Y02T50/671 ,  Y02T50/675

    摘要： An aircraft may have a heat generating component and an engine, at least one of which generates a heat load, and a thermal management system to cool the heat load. The engine may have a duct and an engine fan configured to draw an inlet air stream into an inlet portion of the duct, where at least a portion of the inlet air stream may be used as an engine air stream. The thermal management system may include a cooling circuit configured to circulate a fluid through the heat load such that at least a portion of it may be transferred to the fluid, a heat exchanger configured to enable heat transfer between the fluid and a cooling air stream, and a pumping device. The pumping device may be configured to draw the cooling air stream through the heat exchanger and into a portion of the engine air stream.

    Compact actuation system for flow nozzle
    8.
    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

    申请人： Rolls-Royce North American Technologies, Inc.

    发明人： Kenneth M. Pesyna

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

    CPC分类号： 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

    摘要： 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.

    摘要翻译： 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。

    HEAT EXCHANGER INTEGRATED WITH A GAS TURBINE ENGINE AND ADAPTIVE FLOW CONTROL
    9.
    发明申请
    HEAT EXCHANGER INTEGRATED WITH A GAS TURBINE ENGINE AND ADAPTIVE FLOW CONTROL 有权
    热交换器与气体涡轮发动机和自适应流量控制集成

    公开(公告)号：US20140271116A1

    公开(公告)日：2014-09-18

    申请号：US14107412

    申请日：2013-12-16

    申请人： Rolls-Royce North American Technologies, Inc.

    发明人： Douglas J. Snyder ,  Kenneth M. Pesyna ,  Anthony F. Pierluissi

    IPC分类号： F02C7/12

    CPC分类号： F02C7/12 ,  F01D25/12 ,  F02C7/14 ,  F02C7/141 ,  F02C7/18 ,  F02K3/06 ,  F05D2260/20 ,  Y02T50/675

    摘要： One embodiment of an engine may include an enclosure surrounding an engine having an engine centerline, and the enclosure defining a passage for a cold-side airflow. The engine may also include one or more contiguous heat exchangers having a cold side inlet surface receiving a cold-side airflow. The heat exchanger may be disposed within the passage, such that a surface normal relative to the cold side inlet surface is offset by at least 30 degrees from the engine centerline.

    摘要翻译： 发动机的一个实施例可以包括围绕具有发动机中心线的发动机的外壳，并且外壳限定用于冷侧气流的通道。 发动机还可以包括一个或多个连续的热交换器，其具有接收冷侧气流的冷侧入口表面。 热交换器可以设置在通道内，使得相对于冷侧入口表面法线的表面与发动机中心线相抵离至少30度。

    RAM AIR THERMAL MANAGEMENT SYSTEM
    10.
    发明申请
    RAM AIR THERMAL MANAGEMENT SYSTEM 有权
    RAM空气管理系统

    公开(公告)号：US20140246170A1

    公开(公告)日：2014-09-04

    申请号：US14132716

    申请日：2013-12-18

    申请人： Rolls-Royce North American Technologies, Inc.

    发明人： Douglas J. Snyder ,  Kenneth M. Pesyna

    IPC分类号： F02C7/18

    CPC分类号： F02C7/185 ,  F02C7/14 ,  F02K3/115 ,  F05D2260/601 ,  Y02T50/671 ,  Y02T50/675

    摘要： An aircraft may have a heat generating component and an engine, at least one of which generates a heat load, and a thermal management system to cool the heat load. The engine may have a duct and an engine fan configured to draw an inlet air stream into an inlet portion of the duct, where at least a portion of the inlet air stream may be used as an engine air stream. The thermal management system may include a cooling circuit configured to circulate a fluid through the heat load such that at least a portion of it may be transferred to the fluid, a heat exchanger configured to enable heat transfer between the fluid and a cooling air stream, and a pumping device. The pumping device may be configured to draw the cooling air stream through the heat exchanger and into a portion of the engine air stream.

    摘要翻译： 飞机可以具有发热部件和发动机，其中至少一个产生热负荷，以及用于冷却热负荷的热管理系统。 发动机可以具有管道和发动机风扇，其构造成将入口空气流抽吸到管道的入口部分中，其中入口空气流的至少一部分可以用作发动机空气流。 热管理系统可以包括冷却回路，其被配置为使流体循环通过热负荷，使得其中至少一部分可以被传递到流体;热交换器，其配置成使流体和冷却空气流之间的热传递， 和泵送装置。 泵送装置可以被配置成将冷却空气流抽吸通过热交换器并进入发动机气流的一部分。