GAS TURBINE ENGINE FUEL SYSTEM
    1.
    发明申请
    GAS TURBINE ENGINE FUEL SYSTEM 审中-公开
    燃气涡轮发动机燃油系统

    公开(公告)号:US20160109133A1

    公开(公告)日:2016-04-21

    申请号:US14876352

    申请日:2015-10-06

    Abstract: A fuel system for a gas turbine engine, the gas turbine engine including a combustor having a pilot fuel injector and a main fuel injector, the fuel system including first and second variable flow fuel pumps configured to provide metered fuel flow to the pilot injector, and the main injector respectively; first and second variable speed electric motors configured to drive respective first and second fuel pumps; wherein each of the electric motors includes a polyphase motor including a stator having concentrated windings.

    Abstract translation: 一种用于燃气涡轮发动机的燃料系统,所述燃气涡轮发动机包括具有引燃燃料喷射器和主燃料喷射器的燃烧器,所述燃料系统包括构造成向所述先导喷射器提供计量燃料流的第一和第二可变流量燃料泵,以及 主喷油器分别; 第一和第二变速电动机,其构造成驱动相应的第一和第二燃料泵; 其中每个电动机包括具有集中绕组的定子的多相电动机。

    WIRELESS SIGNAL PROPAGATION APPARATUS
    2.
    发明申请
    WIRELESS SIGNAL PROPAGATION APPARATUS 有权
    无线信号传播设备

    公开(公告)号:US20140106665A1

    公开(公告)日:2014-04-17

    申请号:US14039443

    申请日:2013-09-27

    CPC classification number: H04B7/145 H01Q1/007 H01Q3/06 H01Q9/0407 H01Q9/30

    Abstract: There is provided apparatus for propagation of a wireless signal through a barrier comprising a first antenna for location on a first side of the barrier, a second antenna for location on a second side of the barrier and a waveguide. The waveguide comprises a conducting member passing through the barrier between the first and second sides. The conducting member is held within an insulator sleeve such that it is spaced from a surrounding metal wall of the waveguide. A wireless signal received by the waveguide on the first side of the barrier is transmitted through the barrier by Transverse Electro-Magnetic (TEM) mode propagation along the waveguide is re-radiated on the second side.

    Abstract translation: 提供了一种用于通过屏障传播无线信号的装置,包括用于在屏障的第一侧上定位的第一天线,用于位于屏障的第二侧上的第二天线和波导。 波导包括穿过第一和第二侧之间的阻挡层的导电构件。 导电构件保持在绝缘体套筒内,使得其与波导的周围金属壁间隔开。 波导在屏障的第一侧接收的无线信号通过横向电磁(TEM)传输通过屏障沿着波导的传播被再次辐射在第二面上。

    ELECTRICAL GENERATION ARRANGEMENT FOR AN AIRCRAFT
    3.
    发明申请
    ELECTRICAL GENERATION ARRANGEMENT FOR AN AIRCRAFT 有权
    航空器电气设备安装

    公开(公告)号:US20140338352A1

    公开(公告)日:2014-11-20

    申请号:US14069957

    申请日:2013-11-01

    Abstract: This invention relates to a multi-spool gas turbine engine, including: a first generator for providing electrical power to an electrical system, the generator being driveably connected to a first spool; a second generator for providing electrical power to the electrical system, the generator being driveably connected to a second spool; a disconnection device for disconnecting the second generator from the second spool; and, a controller configured to selectively operate the disconnection device under predetermined powered engine conditions.

    Abstract translation: 本发明涉及一种多阀芯燃气涡轮发动机,包括:第一发电机,用于向电气系统提供电力,发电机可驱动地连接到第一线轴; 用于向所述电气系统提供电力的第二发电机,所述发电机可驱动地连接到第二线轴; 断开装置,用于将第二发生器与第二卷轴断开; 以及控制器,被配置为在预定的动力发动机条件下选择性地操作所述断开装置。

    ELECTRICAL POWER GENERATOR FOR A GAS TURBINE ENGINE
    5.
    发明申请
    ELECTRICAL POWER GENERATOR FOR A GAS TURBINE ENGINE 有权
    燃气轮机发电机

    公开(公告)号:US20150244296A1

    公开(公告)日:2015-08-27

    申请号:US14608860

    申请日:2015-01-29

    Abstract: An aircraft electrical power generation system includes an AC generator having a rotor including a plurality of electromagnetic rotor-windings and stator including plurality of electrical stator-windings. The rotor mechanically coupled to a shaft of a gas turbine engine by transmission-system. The generator includes a frequency controller, a torque sensor determining a torque on the transmission-system by the generator and controller to operate the system in first and second modes. In first mode, the power output frequency of the generator controlled by the frequency controller within limits, and reduced idle signal going to a turbine engine controller. In second mode, the power output frequency of the generator not controlled by the frequency controller and increased idle signal going to the turbine engine controller. The controller operates the system in first mode when the torque is below a limit, and in second mode when the torque is above a limit.

    Abstract translation: 飞机发电系统包括具有转子的交流发电机,该转子包括多个电磁转子绕组和包括多个电定子绕组的定子。 转子通过传动系统机械联接到燃气涡轮发动机的轴。 发电机包括频率控制器,扭矩传感器,其通过发电机和控制器确定传动系统上的转矩,以在第一和第二模式下操作系统。 在第一模式中,由频率控制器控制的发电机的功率输出频率在限制内,并且减少空转信号进入涡轮发动机控制器。 在第二模式中,发电机的功率输出频率不受频率控制器控制,并且空载信号增加到涡轮发动机控制器。 当转矩低于极限时,控制器以第一模式运行系统,而当转矩高于极限时,控制器处于第二模式。

    METHOD OF CONTROLLING AN AIRCRAFT ELECTRICAL POWER GENERATION SYSTEM
    6.
    发明申请
    METHOD OF CONTROLLING AN AIRCRAFT ELECTRICAL POWER GENERATION SYSTEM 审中-公开
    控制飞机电力发电系统的方法

    公开(公告)号:US20140125121A1

    公开(公告)日:2014-05-08

    申请号:US14036721

    申请日:2013-09-25

    CPC classification number: B60R16/03 B64D2221/00 H02J4/00 H02J7/1446 Y02T50/54

    Abstract: A method of operating an electrical power generation system on an aircraft. The method includes assessing a required electrical power of the aircraft, assessing whether a first and a second electrical power source are able to provide the required electrical power in combination, assessing a predetermined condition, determining an operating mode of the first and second electrical power sources to match the predetermined condition, and operating the first and second electrical power sources according to the determined operating mode.

    Abstract translation: 一种在飞机上操作发电系统的方法。 该方法包括评估飞行器的所需电力,评估第一和第二电源是否能够组合提供所需的电力,评估预定条件,确定第一和第二电源的操作模式 以匹配预定条件,并且根据所确定的操作模式操作第一和第二电源。

    SUPERCONDUCTING ELECTRICAL SYSTEM
    7.
    发明申请
    SUPERCONDUCTING ELECTRICAL SYSTEM 有权
    超导电气系统

    公开(公告)号:US20130082518A1

    公开(公告)日:2013-04-04

    申请号:US13625490

    申请日:2012-09-24

    CPC classification number: B64D33/08 B64D2013/0614 E02D27/425 Y02E40/622

    Abstract: This invention relates to a superconducting electrical network, comprising: an electrical system including a plurality of superconducting electrical equipment; a cryogenic system including one or more refrigeration units for providing coolant to the plurality of superconducting electrical equipment; a controller configured to control the flow of coolant to the plurality of superconducting electrical equipment, wherein the controller is configured to isolate the supply of refrigerant to one or more of the plurality of electrical equipment upon demand and increase the flow of coolant to one or more of the non-isolated plurality of electrical equipment.

    Abstract translation: 本发明涉及一种超导电气网络,包括:包括多个超导电气设备的电气系统; 低温系统,包括用于向多个超导电气设备提供冷却剂的一个或多个制冷单元; 控制器,被配置为控制到多个超导电气设备的冷却剂流,其中控制器被配置为根据需要将制冷剂的供应隔离成多个电气设备中的一个或多个,并且将冷却剂的流量增加到一个或多个 的非隔离多个电气设备。

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