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1. 发明申请

US20100018806A1 ELECTRIC MOTOR DRIVEN LUBRICATION PUMP STARTUP CONTROL SYSTEM AND METHOD 有权
标题翻译：电动马达驱动润滑泵启动控制系统及方法
公开(公告)号：US20100018806A1
公开(公告)日：2010-01-28
申请号：US12181195
申请日：2008-07-28
申请人： Jim Delaloye , Matthew Christopher
发明人： Jim Delaloye , Matthew Christopher
IPC分类号： F01M5/00
CPC分类号： F01M5/025 , F01M2001/0215
摘要： A system and method are provided for controlling an electric motor driven lubrication supply pump that is supplied with electrical power from a power bus, and that supplies lubricant to a rotating machine that is at least part of a vehicle subsystem. A determination is made that the subsystem is being started-up. Moreover, one or more lubricant parameters, power bus electrical state, and one or more lubricant load states are determined. The electrical power supplied from the power bus to the electric motor is varied, based on the one or more lubricant parameters, the power bus electrical state, and the one or more lubricant load states.
摘要翻译：提供了一种系统和方法，用于控制从电力总线提供电力的电动机驱动的润滑供给泵，并且向作为车辆子系统的至少一部分的旋转机械供应润滑剂。确定子系统正在启动。此外，确定一个或多个润滑剂参数，功率总线电状态和一个或多个润滑剂负载状态。基于一个或多个润滑剂参数，电力总线电气状态和一个或多个润滑剂负载状态，从电力总线供应到电动机的电力是不同的。

2. 发明授权

US08201662B2 Electric motor driven lubrication pump control system and method for turbomachine windmill operation 有权
标题翻译：电机驱动润滑泵控制系统及涡轮机风车运行方法
公开(公告)号：US08201662B2
公开(公告)日：2012-06-19
申请号：US12174553
申请日：2008-07-16
申请人： Jim Delaloye , Matthew Christopher
发明人： Jim Delaloye , Matthew Christopher
IPC分类号： F01D25/18 , F01D17/06 , F01D21/02 , F01M9/00 , F01B25/06 , F03B15/06 , F04D15/00 , F04D27/00 , F03D3/06
CPC分类号： F01D25/20 , F02C7/06 , F05D2220/34 , F05D2270/09 , F05D2270/304
摘要： A system and method are provided to selectively control lubricant supply flow to a rotating machine that is installed in an aircraft having ram air turbine that is movable between at least a deployed position and a stowed position. A controller determines at least when the ram air turbine is in the deployed position, and determining when rotational speed of the rotating machine exceeds a predetermined value. The electric motor driven lubrication pump is at least selectively energized to control the measured lubricant pressure to a predetermined minimum pressure at least when the ram air turbine is deployed and the rotational speed exceeds the predetermined value.
摘要翻译：提供了一种系统和方法，用于选择性地控制向安装在具有可在至少展开位置和收起位置之间移动的冲压式空气涡轮机的飞行器中的旋转机器的润滑剂供应流。控制器至少确定冲压式空气涡轮机处于展开位置时，确定旋转机械的转速何时超过预定值。所述电动机驱动的润滑泵至少选择性地通电以至少在所述冲压式空气涡轮机展开并且所述转速超过所述预定值时将所测量的润滑剂压力控制到预定的最小压力。

3. 发明授权

US09151193B2 Electric motor driven lubrication pump startup control system and method 有权
标题翻译：电机驱动润滑泵起动控制系统及方法
公开(公告)号：US09151193B2
公开(公告)日：2015-10-06
申请号：US12181195
申请日：2008-07-28
申请人： Jim Delaloye , Matthew Christopher
发明人： Jim Delaloye , Matthew Christopher
IPC分类号： F01M5/00 , F01M5/02 , F01M1/02
CPC分类号： F01M5/025 , F01M2001/0215
摘要： A system and method are provided for controlling an electric motor driven lubrication supply pump that is supplied with electrical power from a power bus, and that supplies lubricant to a rotating machine that is at least part of a vehicle subsystem. A determination is made that the subsystem is being started-up. Moreover, one or more lubricant parameters, power bus electrical state, and one or more lubricant load states are determined. The electrical power supplied from the power bus to the electric motor is varied, based on the one or more lubricant parameters, the power bus electrical state, and the one or more lubricant load states.
摘要翻译：提供了一种系统和方法，用于控制从电力总线提供电力的电动机驱动的润滑供给泵，并且向作为车辆子系统的至少一部分的旋转机械供应润滑剂。确定子系统正在启动。此外，确定一个或多个润滑剂参数，功率总线电状态和一个或多个润滑剂负载状态。基于一个或多个润滑剂参数，电力总线电气状态和一个或多个润滑剂负载状态，从电力总线供应到电动机的电力是不同的。

4. 发明申请

US20090045014A1 ELECTRIC MOTOR DRIVEN LUBRICATION PUMP CONTROL SYSTEM AND METHOD FOR TURBOMACHINE WINDMILL OPERATION 有权
标题翻译：电动马达驱动润滑泵控制系统及涡轮机风机运行方法
公开(公告)号：US20090045014A1
公开(公告)日：2009-02-19
申请号：US12174553
申请日：2008-07-16
申请人： Jim Delaloye , Matthew Christopher
发明人： Jim Delaloye , Matthew Christopher
IPC分类号： F01M9/00
CPC分类号： F01D25/20 , F02C7/06 , F05D2220/34 , F05D2270/09 , F05D2270/304
摘要： A system and method are provided to selectively control lubricant supply flow to a rotating machine that is installed in an aircraft having ram air turbine that is movable between at least a deployed position and a stowed position. A controller determines at least when the ram air turbine is in the deployed position, and determining when rotational speed of the rotating machine exceeds a predetermined value. The electric motor driven lubrication pump is at least selectively energized to control the measured lubricant pressure to a predetermined minimum pressure at least when the ram air turbine is deployed and the rotational speed exceeds the predetermined value.
摘要翻译：提供了一种系统和方法，用于选择性地控制向安装在具有可在至少展开位置和收起位置之间移动的冲压式空气涡轮机的飞行器中的旋转机器的润滑剂供应流。控制器至少确定冲压式空气涡轮机处于展开位置时，确定旋转机械的转速何时超过预定值。所述电动机驱动的润滑泵至少选择性地通电以至少在所述冲压式空气涡轮机展开并且所述转速超过所述预定值时将所测量的润滑剂压力控制到预定的最小压力。

5. 发明申请

US20060054406A1 Active gas turbine lubrication system flow control 失效
公开(公告)号：US20060054406A1
公开(公告)日：2006-03-16
申请号：US10897782
申请日：2004-07-23
申请人： Jim Delaloye
发明人： Jim Delaloye
IPC分类号： F01D25/18
CPC分类号： F01D25/20 , F01D25/18 , Y10T137/0753
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.

6. 发明申请

US20070169997A1 Airframe mounted motor driven lubrication pump control system and method 有权
标题翻译：机身安装电机驱动润滑泵控制系统及方法
公开(公告)号：US20070169997A1
公开(公告)日：2007-07-26
申请号：US11339160
申请日：2006-01-25
申请人： Jim Delaloye
发明人： Jim Delaloye
IPC分类号： F01D25/18
CPC分类号： F01D25/18 , F04B49/20 , F04B2205/05 , F04D15/0066 , F05D2270/303 , F05D2270/304
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，并将电动机速度命令提供给电动机，该电动机使得泵在预定的润滑油供应压力。

7. 发明申请

US20070234739A1 Gas turbine engine cold start mechanization 失效
标题翻译：燃气轮机发动机冷启动机械化
公开(公告)号：US20070234739A1
公开(公告)日：2007-10-11
申请号：US11231949
申请日：2005-09-20
申请人： Jim Delaloye , Joe Keck , Barry Kingery
发明人： Jim Delaloye , Joe Keck , Barry Kingery
IPC分类号： F02C9/00
CPC分类号： F02C7/275 , F01D19/00 , F05D2260/40 , F05D2260/85
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。

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