Heat controlling apparatus for a detector of a CT machine and a detector

    公开(公告)号:US09817133B2

    公开(公告)日:2017-11-14

    申请号:US15043245

    申请日:2016-02-12

    CPC classification number: G01T1/2018

    Abstract: A heat controlling apparatus for a detector of a CT machine and a detector. The heat controlling apparatus comprises: a heat conducting frame, which is disposed at a side where a chip on a circuit board in the detector is located; a heater, which thermally contacts with the heat conducting frame and is used for heating the heat conducting frame; a heat dissipating member, which is connected with the heat conducting frame and used for dissipating heat produced by the detector; and a heat isolating member, which is wrapped at a periphery of a collimator of the detector, the heat conducting frame and the heater.

    POWER SYSTEM AND METHODS OF ASSEMBLING THE SAME
    67.
    发明申请
    POWER SYSTEM AND METHODS OF ASSEMBLING THE SAME 审中-公开
    电力系统及其组装方法

    公开(公告)号:US20170051670A1

    公开(公告)日:2017-02-23

    申请号:US14829411

    申请日:2015-08-18

    Abstract: A power system is provided. The power system includes a gas turbine assembly having a compressor, a combustor, and a turbine coupled in serial flow arrangement. The compressor has a compressor inlet. The power system also includes an electrostatic precipitation system coupled to the gas turbine assembly upstream from the compressor inlet. The compressor is oriented to receive working gases discharged from the electrostatic precipitation system to facilitate removing entrained matter from the working gases flowing into the compressor inlet.

    Abstract translation: 提供电力系统。 电力系统包括具有压缩机,燃烧器和以串联流动方式联接的涡轮机的燃气轮机组件。 压缩机具有压缩机入口。 电力系统还包括与压缩机入口上游的燃气轮机组件相连的静电沉淀系统。 压缩机被定向为接收从静电沉淀系统排出的工作气体,以便于从流入压缩机入口的工作气体中除去夹带的物质。

    GAS TURBINE ENGINE LIQUID FUEL SUPPLY SYSTEM AND METHOD
    68.
    发明申请
    GAS TURBINE ENGINE LIQUID FUEL SUPPLY SYSTEM AND METHOD 审中-公开
    燃气涡轮发动机液体燃料供应系统及方法

    公开(公告)号:US20160341429A1

    公开(公告)日:2016-11-24

    申请号:US14717570

    申请日:2015-05-20

    CPC classification number: F23R3/36 F02C3/30 F02C7/22 F02C7/222 F02C7/224 F02C9/40

    Abstract: A method of supplying liquid fuel in a gas turbine engine is provided and includes sealing a fuel manifold with a fluid in the fuel manifold. The method also includes initiating routing of a liquid fuel from a liquid fuel supply structure to the fuel manifold. The method further includes displacing the fluid disposed in the fuel manifold with the liquid fuel. The method yet further includes routing the liquid fuel and the fluid into a combustor.

    Abstract translation: 提供了一种在燃气涡轮发动机中供应液体燃料的方法,并且包括用燃料歧管中的流体密封燃料歧管。 该方法还包括启动将液体燃料从液体燃料供应结构路由到燃料歧管。 该方法还包括用液体燃料置换设置在燃料歧管中的流体。 该方法还包括将液体燃料和流体路由到燃烧器中。

    GAS TURBINE SYSTEM AND METHOD
    69.
    发明申请
    GAS TURBINE SYSTEM AND METHOD 审中-公开
    气体涡轮机系统和方法

    公开(公告)号:US20160273456A1

    公开(公告)日:2016-09-22

    申请号:US14768431

    申请日:2013-10-16

    Abstract: A fuel supply system includes a first fuel gas compressor coupled to a fuel gas compressor shaft and configured to pressurize a fuel for a gas turbine system. A clutch is coupled to the fuel gas compressor shaft and is configured to selectively engage the fuel gas compressor shaft with a turbine shaft of the gas turbine system. An electromechanical machine is configured to operator as a motor to drive the fuel gas compressor shaft or to operate as a generator driven by the turbine shaft to generator power, based on an operating condition of the gas turbine system.

    Abstract translation: 燃料供应系统包括耦合到燃料气体压缩机轴并被配置为对燃气轮机系统的燃料加压的第一燃料气体压缩机。 离合器联接到燃料气体压缩机轴并且构造成选择性地将燃料气体压缩机轴与燃气轮机系统的涡轮轴接合。 机电机构被配置为基于燃气轮机系统的操作条件,作为电动机操作以驱动燃料气体压缩机轴或作为由涡轮机轴驱动的发电机运行以发电机功率。

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