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    CONTROL OF LOAD REJECTION
    3.
    发明申请
    CONTROL OF LOAD REJECTION 有权
    负载控制

    公开(公告)号：US20130043680A1

    公开(公告)日：2013-02-21

    申请号：US13589263

    申请日：2012-08-20

    Applicant: Martin Liebau ,  Peter Marx ,  Sami Hashmi

    Inventor： Martin Liebau ,  Peter Marx ,  Sami Hashmi

    IPC: F02C9/18 ,  H02P9/04

    CPC classification number: F01D17/105 ,  F01D21/14 ,  F02C9/18 ,  F05D2270/56

    Abstract: A control system is provided for a power generating system having a gas turbine, a flue gas exhaust stage and a blow-off valve assembly. The gas turbine includes a compression stage, a combustion stage and a driveshaft. The blow-off valve assembly is configured to selectively provide fluid communication between the combustion stage and the flue gas exhaust stage. The control system includes a controller configured to output a signal causing the blow-off valve assembly to provide the fluid communication in response to a sudden de-loading of the gas turbine.

    Abstract translation: 提供了一种用于具有燃气轮机，烟道气排放台和排气阀组件的发电系统的控制系统。 燃气轮机包括压缩级，燃烧级和驱动轴。 排气阀组件构造成选择性地提供燃烧阶段和烟气排放阶段之间的流体连通。 控制系统包括控制器，该控制器被配置为输出使得吹扫阀组件响应于燃气轮机的突然卸载而提供流体连通的信号。

    TWO SERVOVALVE THRUST REVERSER ACTUATOR SYSTEM
    4.
    发明公开
    TWO SERVOVALVE THRUST REVERSER ACTUATOR SYSTEM 审中-公开

    公开(公告)号：US20240287948A1

    公开(公告)日：2024-08-29

    申请号：US18175102

    申请日：2023-02-27

    Applicant: Woodward, Inc.

    Inventor： William Ernest Stone ,  Joseph Thomas Kopecek

    IPC: F02K1/76 ,  F02K1/62

    CPC classification number: F02K1/763 ,  F02K1/62 ,  F02K1/766 ,  F05D2220/323 ,  F05D2270/56 ,  F05D2270/64

    Abstract: The subject matter of this specification can be embodied in, among other things, an engine assembly having a nacelle surrounding an engine, and a thrust reverser coupled to the nacelle and having a thrust-reversing element movable relative to the nacelle between a stowed and deployed position, a first hydraulic actuator configured to move the thrust-reversing element between the stowed position and deployed position, the first hydraulic actuator being connected to a fluid source and a return reservoir, and a second hydraulic actuator configured to move the thrust-reversing element between the stowed and deployed position, the second hydraulic actuator being connected to the fluid source and the return reservoir, and a control system having an electrohydraulic servo valve operable to selectively route fluid between the fluid source, the second hydraulic actuator, and the return reservoir, and a controller configured to operate the electrohydraulic servo valve.

    Steam valve and steam turbine
    5.
    发明授权
    Steam valve and steam turbine 有权

    公开(公告)号：US09670794B2

    公开(公告)日：2017-06-06

    申请号：US14894245

    申请日：2014-02-19

    Applicant: MITSUBISHI HEAVY INDUSTRIES COMPRESSOR CORPORATION

    Inventor： Daisuke Takemura

    IPC: F16K31/12 ,  F01D17/14 ,  F16K31/44

    CPC classification number: F01D17/145 ,  F05D2220/31 ,  F05D2230/31 ,  F05D2260/30 ,  F05D2260/57 ,  F05D2260/60 ,  F05D2270/56 ,  F05D2270/58 ,  F05D2270/64 ,  F16K31/163 ,  F16K31/44

    Abstract: A steam valve includes: a valve main body which has, on the inside thereof, a flow path through which steam flows, and has a valve seat formed in a portion of the flow path; a valve body which comes into contact with the valve seat, thereby shutting off the flow path, and is separated from the valve seat, thereby opening the flow path; a valve shaft which is connected to the valve body, extends in an upward direction from the valve body, and moves up and down, thereby bringing the valve body into contact with the valve seat and separating the valve body from the valve seat; a hydraulic drive unit which is disposed to be separated in a horizontal direction from the valve main body, at a position which does not overlap the valve main body in a case of being viewed from above, and has a drive rod which is driven forward and backward by oil pressure; a first link unit which connects the drive rod and the valve shaft and transmits the forward and backward drive of the drive rod to the valve shaft, thereby moving the valve shaft up and down; a second link unit connected to the valve main body; and a connection unit which connects the second link unit and the first link unit and transmits a movement of the valve main body in the horizontal direction to the first link unit through the second link unit.

    VALVE FOR CONTROLLING HEAT EXCHANGES IN AN OIL CIRCUIT
    6.
    发明申请
    VALVE FOR CONTROLLING HEAT EXCHANGES IN AN OIL CIRCUIT 有权
    用于控制油路中的热交换器的阀

    公开(公告)号：US20140014198A1

    公开(公告)日：2014-01-16

    申请号：US13938925

    申请日：2013-07-10

    Applicant: SNECMA

    Inventor： Huguette de Wergifosse

    IPC: F16K49/00

    CPC classification number: F16K49/00 ,  F02C7/06 ,  F02C7/224 ,  F05D2260/606 ,  F05D2260/98 ,  F05D2270/303 ,  F05D2270/3062 ,  F05D2270/56 ,  G05D23/1393 ,  G05D23/1925 ,  Y02T50/671 ,  Y10T137/6579

    Abstract: A valve for regulating the temperature of an oil flow, includes a first inlet channel, a second inlet channel and an outlet channel, the second inlet channel and the outlet channel being capable of cooperating with a temperature regulator. One of the inlet channels includes an oil flow regulator controlled by a computer by generation of an electrical set value respecting a control law configured within the computer, the control law being slaved by an oil flow temperature sensor, the electrical set value controlling opening and closing of the regulator, the regulation law generating an alternation of open and closed states of the flow regulator so as to achieve a required average temperature of the oil flow over a given period.

    Abstract translation: 用于调节油流温度的阀包括第一入口通道，第二入口通道和出口通道，第二入口通道和出口通道能够与温度调节器配合。 其中一个入口通道包括由计算机控制的油流调节器，通过产生相对于在计算机内构成的控制规律的电气设定值，控制律由油流温度传感器驱动，电气设定值控制打开和关闭 调节规则产生流量调节器的开启和关闭状态的交替，以便在给定时间段内实现所需的油流平均温度。

    CONTROL APPARATUS FOR AEROPLANE GAS TURBINE ENGINE
    7.
    发明申请
    CONTROL APPARATUS FOR AEROPLANE GAS TURBINE ENGINE 有权
    机载涡轮发动机的控制装置

    公开(公告)号：US20110046863A1

    公开(公告)日：2011-02-24

    申请号：US12861292

    申请日：2010-08-23

    Applicant: Makoto Tezuka

    Inventor： Makoto Tezuka

    IPC: G06F19/00

    CPC classification number: F02C9/46 ,  F01D21/02 ,  F01D21/14 ,  F02C9/40 ,  F05D2270/56

    Abstract: An apparatus for controlling an aeroplane gas turbine engine has various sensors and devices for operating the engine, and two control channels each calculating a command value for controlling operation of the engine based on signals outputted from the sensors. In each of the control channels, it is determined whether any of the sensors and devices is abnormal based on the signals to determine a failure level of the control channel concerned with a numerical value. The failure level is compared with that of the other control channel and based thereon, the command value calculated by the control channel of smaller failure level is sent to the devices. With this, even when both control channels are failed, the engine control can be continued with taking the failure level into account.

    Abstract translation: 用于控制飞机燃气涡轮发动机的装置具有用于操作发动机的各种传感器和装置，以及两个控制通道，每个控制通道基于从传感器输出的信号计算用于控制发动机的运行的命令值。 在每个控制通道中，基于用于确定与数值有关的控制信道的故障等级的信号，确定传感器和设备中的任一个是否异常。 将故障等级与其他控制信道的故障等级进行比较，基于此，由故障级别较小的控制信道计算出的命令值发送到设备。 由此，即使在两个控制通道都失败的情况下，可以考虑故障等级来继续发动机控制。

    Pressure regulator
    8.
    发明申请
    Pressure regulator 失效
    压力调节器

    公开(公告)号：US20060218911A1

    公开(公告)日：2006-10-05

    申请号：US11167642

    申请日：2005-06-27

    Applicant: Daniel Bickley

    Inventor： Daniel Bickley

    IPC: F16D31/02

    CPC classification number: F02C7/232 ,  F02C9/263 ,  F05D2270/301 ,  F05D2270/56 ,  F05D2270/64 ,  G05D16/2093 ,  Y10T137/7798

    Abstract: A pressure regulator comprises a housing, a metering spool movable within the housing to control the degree of opening of a metering orifice of the regulator, a first inlet through which hydraulic fluid at high pressure is supplied to said metering orifice, a first pressure chamber within the housing and containing hydraulic fluid at a reference pressure (Pref) to which one end of said metering spool is exposed, compression spring means within said first pressure chamber and acting at one end against said one end of said metering spool, an outlet from the housing downstream of said metering orifice, for hydraulic fluid at regulated pressure (Preg) from said metering orifice, a second pressure chamber containing hydraulic fluid at said regulated pressure Preg to which the opposite end of said metering spool is exposed, such that the metering position of the metering spool relative to the housing is a position of equilibrium between the force of the spring and Pref acting on one end of said metering spool and Preg acting on the other end of the metering spool, said equilibrium position changing to maintain a predetermined pressure difference (Pdiff) between Pref and Preg, and the regulator further including an abutment against which the opposite end of said compression spring means reacts and a third pressure chamber containing hydraulic fluid at a control pressure (Pcon) acting on said abutment, whereby the value of Pcon, can be changed to adjust the position of said abutment relative to the housing of the regulator to change the pre-load of said compression spring means thereby to adjust the value of Pdiff.

    Abstract translation: 压力调节器包括壳体，计量阀芯，其可在壳体内移动以控制调节器的计量孔口的开度;第一入口，通过该第一入口将高压液压流体供应到所述计量孔;第一压力室， 所述壳体和所述液压流体在所述计量阀芯的一端暴露于所述基准压力（P＆lt;＆lt;＆gt;＆gt;）处，所述压缩弹簧装置在所述第一压力室内并且在一端作用于所述第一压力 所述计量阀芯，来自所述计量孔口下游的壳体的出口，用于来自所述计量孔口的处于调节压力（P reg）的液压流体;第二压力室，包含处于所述调节压力P 所述计量阀芯的相对端暴露于其中，使得计量阀芯相对于壳体的计量位置是弹簧的力之间的平衡位置 作用在所述计量阀芯的一端上的作用在计量阀芯的另一端上的泵和P ，所述平衡位置改变以保持预定的压力差（ 并且调节器还包括所述压缩弹簧装置的相对端反应的支座，以及 第三压力室，其包含作用在所述基台上的控制压力（P SUB）的液压流体，由此可以改变P < 相对于调节器的壳体的邻接以改变所述压缩弹簧装置的预加载，从而调节P 的值。

    Control apparatus particularly for a plurality of compressor bleed valves of a gas turbine engine
    9.
    发明授权
    Control apparatus particularly for a plurality of compressor bleed valves of a gas turbine engine 失效
    控制装置特别适用于气体涡轮发动机的压缩机排气阀的大量

    公开(公告)号：US3848636A

    公开(公告)日：1974-11-19

    申请号：US28940472

    申请日：1972-09-15

    Applicant: BENDIX CORP

    Inventor： MCCOMBS H

    IPC: F04D27/02 ,  F17D3/00

    CPC classification number: F02C9/52 ,  F02C9/18 ,  F04D27/0223 ,  F04D27/023 ,  F05D2270/56 ,  Y10T137/86485 ,  Y10T137/86606 ,  Y10T137/87201 ,  Y10T137/87845

    Abstract: Control apparatus for programmed control of a plurality of gas turbine engine compressor air bleed valves in response to a plurality of control input signals representing engine operating conditions including variable conditions related to engine power output. The control inputs are sensed and/or computed and scheduled to provide accurate and reliable control over a plurality of compressor air bleed valves by means including a hydraulic programmer with a three dimensional compressor rise scheduling cam and adjustable hydraulic timers.

    Abstract translation: 控制装置，用于响应于多个控制输入信号来编程控制多个燃气涡轮发动机压缩机排气阀，所述多个控制输入信号表示包括与发动机功率输出有关的可变条件的发动机运行状态。 控制输入​​被感测和/或计算和调度，以通过包括具有三维压缩机上升调度凸轮和可调节液压定时器的液压编程器的装置来提供对多个压缩机排气阀的精确和可靠的控制。

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