Airframe mounted electric motor driven lubrication pump control deoil system
    1.
    发明授权
    Airframe mounted electric motor driven lubrication pump control deoil system 有权
    机载电动机驱动润滑泵控制脱油系统

    公开(公告)号:US07871248B2

    公开(公告)日:2011-01-18

    申请号:US11708727

    申请日:2007-02-20

    申请人: Jim E. Delaloye

    发明人: Jim E. Delaloye

    摘要: A system for controlling lubricant displacement from a machine during turbomachine shutdown sequence includes a motor, a pump, a control valve, and a motor control unit. The motor is selectively energized from a power bus to rotate at a rotational speed and supply a drive force to the pump. The pump, in response to the drive force, draws fluid from a fluid and supplies the fluid to the machine. The control valve is movable between at least a first position, in which the control valve fluidly communicates the pump with a lubrication fluid source, and a second position, in which the control valve fluidly communicates the pump with a gaseous fluid source. During the shutdown sequence, the motor control unit controllably energizes the motor from the power bus to thereby control its rotational speed in accordance with a schedule that will displace at least a substantial volume of lubricant in the rotating machine with fluid from the gaseous fluid source.

    摘要翻译: 一种用于在涡轮机关闭序列期间控制来自机器的润滑剂位移的系统包括马达,泵,控制阀和马达控制单元。 电动机从电力总线选择性地通电,以转速旋转并向泵提供驱动力。 泵响应于驱动力从流体中吸取流体并将流体供应到机器。 所述控制阀可在至少第一位置和所述第二位置之间移动,在所述第一位置,所述控制阀将所述泵与润滑流体源流体连通,并且所述控制阀将所述泵与气态流体源流体连通。 在关机顺序期间,电动机控制单元可控制地从电力总线向电动机供电,从而根据将使来自气态流体源的流体在旋转机器中至少移动大量体积的润滑剂的时间表来控制其转速。

    Manuever-based aircraft gas turbine engine speed control system and method
    3.
    发明申请
    Manuever-based aircraft gas turbine engine speed control system and method 失效
    基于Manuever的飞机燃气轮机发动机转速控制系统及方法

    公开(公告)号:US20090099750A1

    公开(公告)日:2009-04-16

    申请号:US11707703

    申请日:2007-02-15

    IPC分类号: F02C9/00

    摘要: A system and method for controlling the rotational speed of a gas turbine engine in an aircraft includes appropriate devices and processes for determining a pressure of lubricant supplied to the turbine engine, and for determining a maneuver state of the aircraft. The rotational speed of the gas turbine engine is controlled based at least partially on the determined pressure and the determined maneuver state. Thus, if the aircraft is in a maneuver state that may cause a reduction or loss of lubricant to the gas turbine engine, the rotational speed of the gas turbine engine can be reduced to a magnitude sufficient to increase turbomachine tolerance to the reduced or no lubricant flow.

    摘要翻译: 用于控制飞行器中的燃气涡轮发动机的转速的系统和方法包括用于确定供应到涡轮发动机的润滑剂的压力以及用于确定飞行器的机动状态的适当装置和方法。 至少部分地基于确定的压力和确定的机动状态来控制燃气涡轮发动机的转速。 因此,如果飞机处于可能导致燃气涡轮发动机的润滑剂减少或损失的机动状态,则燃气涡轮发动机的转速可以减小到足以提高对减少的或不润滑的润滑剂的涡轮机公差 流。

    Gas turbine engine cold start mechanization
    4.
    发明授权
    Gas turbine engine cold start mechanization 失效
    燃气轮机发动机冷启动机械化

    公开(公告)号:US07690205B2

    公开(公告)日:2010-04-06

    申请号:US11231949

    申请日:2005-09-20

    IPC分类号: F02C7/26 F02C7/275

    摘要: An apparatus and method is provided to start gas turbine engines at cold start. A gearbox is not mechanically coupled to any accessory or to the starter-generator. Rather, a controller is used to route power to a starter-generator to rotate the turbine mainshaft to start the gas turbine engine. The controller prevents power to an accessory drive motor, until the starter-generator creates a positive torque. When a positive torque is reached, excess power is routed to the accessory drive motor, typically a brushless direct current motor.

    摘要翻译: 提供了一种在冷启动时启动燃气涡轮发动机的装置和方法。 齿轮箱不与任何附件或起动发电机机械耦合。 相反,控制器用于将动力路由到起动器发电机以使涡轮机主轴旋转以启动燃气涡轮发动机。 控制器防止附件驱动电机通电,直到起动发电机产生正转矩。 当达到正转矩时,多余的功率被路由到附件驱动电动机,通常是无刷直流电动机。

    Airframe mounted motor driven lubrication pump control system and method
    5.
    发明授权
    Airframe mounted motor driven lubrication pump control system and method 有权
    机身安装电机驱动润滑泵控制系统及方法

    公开(公告)号:US07571597B2

    公开(公告)日:2009-08-11

    申请号:US11339160

    申请日:2006-01-25

    申请人: Jim E. Delaloye

    发明人: Jim E. Delaloye

    IPC分类号: F02C7/06

    摘要: A system and method for precisely controlling lubricant supply flow to one or more rotating machines in an aircraft includes a motor, a pump, and a motor control unit. The motor is coupled to receive motor speed commands and, in response to the commands, rotates at the commanded motor speed and supplies a drive force to the pump. The pump, upon receipt of the drive force, draws lubricant from a lubricant source and supplies it to a rotating machine. The motor control unit determines a scheduled lubricant supply pressure based at least in part on lubricant temperature, rotating machine rotational speed, and one or more aircraft operating conditions, and to supplies the motor speed commands to the motor that cause the pump to supply lubricant at the scheduled lubricant supply pressure.

    摘要翻译: 用于精确地控制飞机中的一个或多个旋转机器的润滑剂供应流的系统和方法包括马达,泵和马达控制单元。 电动机被耦合以接收电动机速度命令,并且响应于这些命令以指令的电动机转速旋转并向泵提供驱动力。 泵在接收到驱动力后,从润滑剂源中吸取润滑剂并将其提供给旋转机器。 电动机控制单元至少部分地基于润滑剂温度,旋转机器旋转速度和一个或多个飞行器操作条件来确定预定的润滑剂供应压力,并且将电动机速度命令提供给电动机,使得泵在 预定的润滑油供应压力。

    Active gas turbine lubrication system flow control
    6.
    发明授权
    Active gas turbine lubrication system flow control 失效
    主动燃气轮机润滑系统流量控制

    公开(公告)号:US07506724B2

    公开(公告)日:2009-03-24

    申请号:US10897782

    申请日:2004-07-23

    申请人: Jim E. Delaloye

    发明人: Jim E. Delaloye

    IPC分类号: F01M1/00

    摘要: A lubrication system is provided for an aircraft turbine machine, the lubrication system being controlled by a closed-loop logic arrangement, wherein the oil pressure of a lubricant circulated therein is monitored and altered according to attitude data, acceleration data, operating mode data, or some combination thereof contained in a signal received from an airframe flight controller and according to a oil pressure signal and an oil temperature signal. The logic responsively provides a supply pump speed control signal, according to a predetermined target oil pressure value selected to correspond to the data contained in the signals. The target value may be continuously compared to the present oil pressure value and the present oil pressure adjusted by sending a motor control signal to the supply pump and a valve flow control signal to a flow control valve that conditionally allows oil from the outlet side of the supply pump to be fed back to its inlet side.

    摘要翻译: 提供一种用于飞机涡轮机的润滑系统,润滑系统由闭环逻辑装置控制,其中在其中循环的润滑剂的油压根据姿态数据,加速度数据,操作模式数据或 其一些组合包含在从机身飞行控制器接收的信号中,并且根据油压信号和油温信号。 该逻辑响应地提供供应泵速度控制信号,根据预定的目标油压值被选择以对应于包含在信号中的数据。 目标值可以与当前油压值和通过向供给泵发送电动机控制信号而调节的当前油压以及向流量控制阀的阀流量控制信号进行持续比较,该流量控制阀有条件地允许从出口侧的油 供应泵被反馈到其入口侧。

    Maneuver based aircraft gas turbine engine speed control
    7.
    发明授权
    Maneuver based aircraft gas turbine engine speed control 失效
    机动飞机燃气轮机发动机转速控制

    公开(公告)号:US07725236B2

    公开(公告)日:2010-05-25

    申请号:US11707703

    申请日:2007-02-15

    IPC分类号: G06F19/00

    摘要: A system and method for controlling the rotational speed of a gas turbine engine in an aircraft includes appropriate devices and processes for determining a pressure of lubricant supplied to the turbine engine, and for determining a maneuver state of the aircraft. The rotational speed of the gas turbine engine is controlled based at least partially on the determined pressure and the determined maneuver state. Thus, if the aircraft is in a maneuver state that may cause a reduction or loss of lubricant to the gas turbine engine, the rotational speed of the gas turbine engine can be reduced to a magnitude sufficient to increase turbomachine tolerance to the reduced or no lubricant flow.

    摘要翻译: 用于控制飞行器中的燃气涡轮发动机的转速的系统和方法包括用于确定供应到涡轮发动机的润滑剂的压力以及用于确定飞行器的机动状态的适当装置和方法。 至少部分地基于确定的压力和确定的机动状态来控制燃气涡轮发动机的转速。 因此,如果飞机处于可能导致燃气涡轮发动机的润滑剂减少或损失的机动状态,则燃气涡轮发动机的转速可以减小到足以提高对减少的或不润滑的润滑剂的涡轮机公差 流。

    Electric Motor Driven Lubrication Pump Control System And Method That Accomodates Turbomachine Windmill Operation
    8.
    发明申请
    Electric Motor Driven Lubrication Pump Control System And Method That Accomodates Turbomachine Windmill Operation 有权
    电机驱动的润滑泵控制系统和容纳涡轮机风车操作的方法

    公开(公告)号:US20100023169A1

    公开(公告)日:2010-01-28

    申请号:US11774083

    申请日:2007-07-06

    申请人: Jim E. Delaloye

    发明人: Jim E. Delaloye

    IPC分类号: G05D7/06 F04B49/06

    摘要: A system and method are provided to selectively control lubricant supply flow to one or more rotating machines in an aircraft when the rotating machines are windmilling. A controller determines if the rotating machines are windmilling. When the rotating machines are windmilling, the controller at least selectively energizes an electric motor driven lubrication pump, to thereby supply lubricant to the windmilling turbomachine.

    摘要翻译: 提供了一种系统和方法,用于当旋转机器是风车时选择性地控制到飞行器中的一个或多个旋转机器的润滑剂供应流。 控制器确定旋转机器是否是风车。 当旋转机器是风车时,控制器至少选择性地激励电动机驱动的润滑泵,从而向风力涡轮机提供润滑剂。

    ELECTRIC MOTOR DRIVEN LUBRICATION PUMP AND LUBRICATION SYSTEM PROGNOSTIC AND HEALTH MANAGEMENT SYSTEM AND METHOD
    9.
    发明申请
    ELECTRIC MOTOR DRIVEN LUBRICATION PUMP AND LUBRICATION SYSTEM PROGNOSTIC AND HEALTH MANAGEMENT SYSTEM AND METHOD 审中-公开
    电动马达驱动润滑泵和润滑系统预防与健康管理系统及方法

    公开(公告)号:US20090299535A1

    公开(公告)日:2009-12-03

    申请号:US11835540

    申请日:2007-08-08

    申请人: Jim E. Delaloye

    发明人: Jim E. Delaloye

    CPC分类号: F01D25/20 F02C7/06

    摘要: An aircraft lubrication supply system health and prognostic system and method includes supplying a pressure signal representative of lubricant pressure, a temperature signal representative of lubricant temperature, a speed signal representative of motor rotational speed, and one or more aircraft condition signals representative of one or more aircraft operating conditions to a system characterization model of at least portions of the lubrication supply system. Simulation response data representative of at least the pressure signal, the temperature signal, and the speed signal are generated, and lubrication supply system health is determined based, at least in part, on the simulation response data.

    摘要翻译: 飞机润滑供应系统健康和预测系统和方法包括提供代表润滑剂压力的压力信号,代表润滑剂温度的温度信号,代表电机转速的速度信号和代表一个或多个的一个或多个飞行器状态信号 至少部分润滑供应系统的系统表征模型的飞机操作条件。 产生代表至少压力信号,温度信号和速度信号的模拟响应数据,并且至少部分地基于模拟响应数据来确定润滑供应系统健康状况。

    Airframe mounted electric motor driven lubrication pump control deoil system
    10.
    发明申请
    Airframe mounted electric motor driven lubrication pump control deoil system 有权
    机载电动机驱动润滑泵控制脱油系统

    公开(公告)号:US20080196383A1

    公开(公告)日:2008-08-21

    申请号:US11708727

    申请日:2007-02-20

    申请人: Jim E. Delaloye

    发明人: Jim E. Delaloye

    摘要: A system for controlling lubricant displacement from a machine during turbomachine shutdown sequence includes a motor, a pump, a control valve, and a motor control unit. The motor is selectively energized from a power bus to rotate at a rotational speed and supply a drive force to the pump. The pump, in response to the drive force, draws fluid from a fluid and supplies the fluid to the machine. The control valve is movable between at least a first position, in which the control valve fluidly communicates the pump with a lubrication fluid source, and a second position, in which the control valve fluidly communicates the pump with a gaseous fluid source. During the shutdown sequence, the motor control unit controllably energizes the motor from the power bus to thereby control its rotational speed in accordance with a schedule that will displace at least a substantial volume of lubricant in the rotating machine with fluid from the gaseous fluid source.

    摘要翻译: 一种用于在涡轮机关闭序列期间控制来自机器的润滑剂位移的系统包括马达,泵,控制阀和马达控制单元。 电动机从电力总线选择性地通电,以转速旋转并向泵提供驱动力。 泵响应于驱动力从流体中吸取流体并将流体供应到机器。 所述控制阀可在至少第一位置和所述第二位置之间移动,在所述第一位置,所述控制阀将所述泵与润滑流体源流体连通,并且所述控制阀将所述泵与气态流体源流体连通。 在关机顺序期间,电动机控制单元可控制地从电力总线向电动机供电,从而根据将使来自气态流体源的流体在旋转机器中至少移动大量体积的润滑剂的时间表来控制其转速。