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125 条记录 (耗时 0.013 秒)

    Optimal thrust control of an aircraft engine
    1.
    发明授权
    Optimal thrust control of an aircraft engine 有权

    公开(公告)号：US10711734B2

    公开(公告)日：2020-07-14

    申请号：US16377488

    申请日：2019-04-08

    申请人： UNITED TECHNOLOGIES CORPORATION

    发明人： Chaohong Cai ,  Timothy J. Crowley ,  Mark E. Lacour ,  David Lei Ma

    IPC分类号： F02K1/17 ,  F02C9/50 ,  F02C9/54 ,  F02C9/00

    摘要： A control system for a gas turbine engine, a method for controlling a gas turbine engine, and a gas turbine engine are disclosed. The control system may include a nozzle scheduler for determining an exhaust nozzle position goal based on a nozzle schedule of exhaust nozzle positions related to flight conditions. The control system may further include a control module for determining a control command for the gas turbine engine. The control command may include, at least, a fuel flow command and an exhaust nozzle position command and the control command may be based on, at least, the exhaust nozzle position goal and an estimated thrust value. The control system may further include an actuator for controlling the gas turbine engine based on the control command.

    Device for controlling a variable section nozzle of an aircraft
    2.
    发明授权
    Device for controlling a variable section nozzle of an aircraft 有权
    用于控制飞机的可变部分喷嘴的装置

    公开(公告)号：US09488131B2

    公开(公告)日：2016-11-08

    申请号：US13864553

    申请日：2013-04-17

    申请人： AIRBUS OPERATIONS (S.A.S)

    发明人： Guillaume Bulin ,  Patrick Oberle ,  Nicolas Devienne

    IPC分类号： F02K3/06 ,  F02K1/15 ,  F02K1/16 ,  F02K1/17 ,  F02K3/075 ,  F02C9/48 ,  F02K1/09

    CPC分类号： F02K3/06 ,  F02C9/48 ,  F02K1/09 ,  F02K1/15 ,  F02K1/16 ,  F02K1/17 ,  F02K3/075 ,  F05B2270/1031 ,  Y02T50/671

    摘要： A control device for controlling a variable section nozzle of an aircraft power plant, the variable section nozzle including one or several movable parts capable of modifying the nozzle section and connected by a mechanical transmission chain to an actuator. The control device includes a system for regulating the power plant connected to a control member configured to control the actuator. The control device includes a single control member, an immobilization unit configured to immobilize all the movable parts which are deactivated only when the regulation system controls the positional change of the movable part or parts and a determination unit configured to determine the actual position of the movable part or parts.

    摘要翻译： 一种用于控制飞机发电厂的可变部分喷嘴的控制装置，所述可变部分喷嘴包括能够修改喷嘴部分并通过机械传动链连接到致动器的一个或多个可移动部件。 控制装置包括用于调节连接到被配置为控制致动器的控制构件的发电厂的系统。 控制装置包括单个控制构件，固定单元，其被配置为固定仅当调节系统控制可移动部件的位置变化时停用的所有可移动部件，以及确定单元，其被配置为确定可移动部件的实际位置 部分或部分。

    Control devices for gas turbine power plants
    3.
    发明授权
    Control devices for gas turbine power plants 失效
    气体涡轮发电厂控制装置

    公开(公告)号：US3719047A

    公开(公告)日：1973-03-06

    申请号：US3719047D

    申请日：1971-02-03

    申请人： SNECMA

    发明人： BRIOTET J ,  RAVAGLI A

    IPC分类号： F02K1/17 ,  F02K11/00

    CPC分类号： F02K1/17

    摘要： A control device for a gas turbine power plant of the type comprising a compressor, a combustion chamber supplied with air coming from the compressor and with fuel, a turbine supplied with combustion gases coming from the combustion chamber, and a nozzle which discharges the combustion gases coming from the turbine, said control device comprising means for metering the fuel flow to the combustion chamber and means for varying the crosssectional area of the nozzle, wherein the means for varying the cross-sectional area of the nozzle is controlled as a function of the fuel flow rate C delivered to the combustion chamber, the static air pressure P2 at exit from the compressor, and the static gas pressure Ps at the turbine exit, so that at least under certain conditions of operation, an output quantity defined by the expression c/( Beta Ps - Ps ), in which Beta designates a constant coefficient of reduction, has a desired predetermined value.

    摘要翻译： 一种用于燃气轮机发电厂的控制装置，其类型包括压缩机，供应有来自压缩机的空气和燃料的燃烧室，提供有来自燃烧室的燃烧气体的涡轮机和排出燃烧气体的喷嘴 所述控制装置包括用于计量到燃烧室的燃料流的装置和用于改变喷嘴的横截面面积的装置，其中用于改变喷嘴的横截面积的装置被控制为一个功能 输送到燃烧室的燃料流量C，从压缩机出口的静态空气压力P2和涡轮机出口处的静态气体压力Ps，使得至少在某些操作条件下，由 表示c /（βPs-Ps），其中β表示常数的还原系数，具有期望的预定值。