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1. 发明授权

US08648556B2 Device for control of a PMSM 有权
标题翻译：用于控制PMSM的装置
公开(公告)号：US08648556B2
公开(公告)日：2014-02-11
申请号：US13513362
申请日：2010-12-10
申请人： Guilhem Lejeune , Sebastien Vieillard
发明人： Guilhem Lejeune , Sebastien Vieillard
IPC分类号： H02P6/16 , H02P21/13 , H02P23/14
CPC分类号： H02P21/13 , H02P21/14 , H02P21/16 , H02P21/18 , H02P23/14
摘要： A permanent magnet synchronous machine (PMSM) includes a stator and rotor powered by an inverter. A device to control the PMSM includes a sensor to sample a measurement θm of the position of the rotor, a control unit to control an operating point of the PMSM according to the position of the rotor and settings, and an estimation unit to determine an estimate {circumflex over (θ)} of the rotor position. The device also includes a malfunction detector to detect a malfunction of the sensor and a switch to connect the control unit to the sensor so that the control unit receives the measured position θm of the rotor while the malfunction detector does not indicate any sensor malfunction, and otherwise to connect the control unit to the estimation unit so that the control unit receives the estimated position {circumflex over (θ)} of the rotor when the malfunction detector indicates a sensor malfunction.
摘要翻译：永磁同步电机（PMSM）包括由逆变器供电的定子和转子。用于控制PMSM的装置包括：传感器，用于对转子位置的测量点进行采样;控制单元，用于根据转子和设置的位置控制PMSM的工作点;以及估计单元，用于确定估计值转子位置的（θ）回转。该装置还包括用于检测传感器故障的故障检测器和用于将控制单元连接到传感器的开关，使得控制单元接收到转子的测量位置，同时故障检测器没有指示任何传感器故障，以及否则将控制单元连接到估计单元，使得当故障检测器指示传感器故障时，控制单元接收转子的估计位置（回旋（θ））。

2. 发明申请

US20130285615A1 MODULE FOR CONVERTING VOLTAGE BETWEEN A HIGH-VOLTAGE ELECTRICAL NETWORK OF AN AIRCRAFT AND AN ENERGY STORAGE ELEMENT 有权
标题翻译：用于在飞机高能电力网络和能源储存元件之间转换电压的模块
公开(公告)号：US20130285615A1
公开(公告)日：2013-10-31
申请号：US13976215
申请日：2011-12-22
申请人： Sebastien Vieillard , Laurent Bernard Brosson , Charif Karimi , Marc Henri Yues Pontrucher
发明人： Sebastien Vieillard , Laurent Bernard Brosson , Charif Karimi , Marc Henri Yues Pontrucher
IPC分类号： H02J7/00
CPC分类号： H02J7/0068 , H02J4/00 , H02J7/345 , H02M3/1584
摘要： A module converting voltage between a high-voltage electrical network and at least one energy storage element an aircraft, the conversion module configured to reversibly convert between a DC voltage of the high-voltage electrical network and a DC voltage of the energy storage element, the DC voltage of the energy storage element floating relative to the DC voltage of the high-voltage electrical network and centered relative to the mass of the aircraft, the module including an input module including two filters each capable of receiving a DC voltage, a first arm and a second arm including switches, and a mechanism controlling the switches, operating per cycle of a switching period and capable of controlling at least one first switch and at least one second switch identically but offset by a half-period, whereby the first switch is open when the second switch is closed and vice versa.
摘要翻译：一种将高压电网和至少一个能量存储元件之间的电压转换成飞行器的模块，所述转换模块被配置为在高压电网的直流电压和能量存储元件的直流电压之间可逆地转换，能量存储元件的直流电压相对于高压电网的直流电压而相对于飞行器的质量而相对于所述质量浮动，该模块包括一个包括两个能够接收直流电压的滤波器的输入模块，第一臂以及包括开关的第二臂，以及控制开关的机构，每个开关周期的周期操作，并且能够同时控制至少一个第一开关和至少一个第二开关，但偏移半个周期，由此第一开关是当第二个开关闭合时打开，反之亦然。

3. 发明申请

US20130229053A1 METHOD AND ARCHITECTURE FOR PROCESSING ELECTRICAL ENERGY REGENERATED FROM AN AIRCRAFT 有权
标题翻译：用于处理从飞机重新生产的电能的方法和架构
公开(公告)号：US20130229053A1
公开(公告)日：2013-09-05
申请号：US13885103
申请日：2011-11-22
申请人： Julien Rambaud , Sebastien Vieillard
发明人： Julien Rambaud , Sebastien Vieillard
IPC分类号： H02P3/14 , B60R16/03
CPC分类号： H02P3/14 , B60L7/20 , B60R16/0307 , H02P3/18 , Y02T10/642
摘要： A method and architecture processing electrical energy regenerated from an aircraft, to address drawbacks posed by customary solutions for dissipating low energy of resistors, conventionally ceramics, which require a significant volume of ceramic and an additional power converter. The method and architecture return energy to an electric generator to convert the energy into mechanical energy. The architecture includes a reversible electric generator, driven by a thermal machine and configured to deliver an AC voltage, electric actuators, and a voltage converter circuit with multiple links. The circuit includes AC voltage rectifiers for voltage originating from the generator and power converters arranged on the multiple links to drive as many electric actuators. The converter circuit also includes a mechanism for electrical energy inverse transmission applied to the generator operating in a motor mode.
摘要翻译：一种处理从飞行器再生的电能的方法和架构，以解决用于耗散电阻器的低能量的常规解决方案所带来的缺点，常规陶瓷需要大量陶瓷和额外的功率转换器。该方法和结构将能量返回到发电机以将能量转换成机械能。该架构包括由热机驱动并被配置为提供交流电压，电致动器和具有多个链路的电压转换器电路的可逆发电机。该电路包括用于来自发电机的电压的AC电压整流器和布置在多个链路上的功率转换器，以驱动尽可能多的电致动器。转换器电路还包括施加到以电动机模式工作的发电机的电能反向传输机构。

4. 发明授权

US09592907B2 Device for electrically powering an aircraft on the ground 有权
标题翻译：为地面上的飞机供电的装置
公开(公告)号：US09592907B2
公开(公告)日：2017-03-14
申请号：US14234541
申请日：2012-07-27
申请人： Sebastien Vieillard , Serge Berenger , Serge Thierry Roques , Pascal Dauriac
发明人： Sebastien Vieillard , Serge Berenger , Serge Thierry Roques , Pascal Dauriac
IPC分类号： B64D41/00 , B64C25/40 , H02J4/00
CPC分类号： B64C25/405 , B64D41/00 , H02J4/00 , Y02T50/44 , Y02T50/823
摘要： An electrical power supply device for an aircraft on the ground, the device including two electricity generators driven by an auxiliary power unit, wherein the first generator is connected by a selective connection/disconnection mechanism to an aircraft network and to an electrical taxiing network, and is configured to deliver either a first AC voltage to the aircraft network when it is connected to that network, or an AC voltage or a power to the taxiing network when it is connected to that network, and wherein the second generator is connected by the connection/disconnection mechanism to the aircraft network to deliver the first AC voltage to that network solely when the first generator is powering the taxiing network.
摘要翻译：一种用于地面上的飞行器的电力供应装置，该装置包括由辅助动力单元驱动的两个发电机，其中第一发电机通过选择性连接/断开机构连接到飞行器网络和电滑行网络，以及被配置为当其连接到所述网络时交付给所述飞行器网络的第一AC电压，或者当连接到所述网络时，所述AC电压或所述滑行网络的电力传递到所述滑行网络，并且其中所述第二发电机通过所述连接 /断开机构到飞行器网络，以便仅当第一发电机为滑行网络供电时将第一AC电压传送到该网络。

5. 发明申请

US20140138479A1 DEVICE FOR ELECTRICALLY POWERING AN AIRCRAFT ON THE GROUND 有权
标题翻译：用于电动地面上的飞机的装置
公开(公告)号：US20140138479A1
公开(公告)日：2014-05-22
申请号：US14234541
申请日：2012-07-27
申请人： Sebastien Vieillard , Serge Berenger , Serge Thierry Roques , Pascal Dauriac
发明人： Sebastien Vieillard , Serge Berenger , Serge Thierry Roques , Pascal Dauriac
IPC分类号： B64C25/40
CPC分类号： B64C25/405 , B64D41/00 , H02J4/00 , Y02T50/44 , Y02T50/823
摘要： An electrical power supply device for an aircraft on the ground, the device including two electricity generators driven by an auxiliary power unit, wherein the first generator is connected by a selective connection/disconnection mechanism to an aircraft network and to an electrical taxiing network, and is configured to deliver either a first AC voltage to the aircraft network when it is connected to that network, or an AC voltage or a power to the taxiing network when it is connected to that network, and wherein the second generator is connected by the connection/disconnection mechanism to the aircraft network to deliver the first AC voltage to that network solely when the first generator is powering the taxiing network.
摘要翻译：一种用于地面上的飞行器的电力供应装置，该装置包括由辅助动力单元驱动的两个发电机，其中第一发电机通过选择性连接/断开机构连接到飞行器网络和电滑行网络，以及被配置为当其连接到所述网络时交付给所述飞行器网络的第一AC电压，或者当连接到所述网络时，所述AC电压或所述滑行网络的电力传递到所述滑行网络，并且其中所述第二发电机通过所述连接 /断开机构到飞行器网络，以便仅当第一发电机为滑行网络供电时将第一AC电压传送到该网络。

6. 发明申请

US20110121891A1 ELECTRONIC CONTROL MODULE FOR A JFET TRANSISTOR 有权
标题翻译：用于JFET晶体管的电子控制模块
公开(公告)号：US20110121891A1
公开(公告)日：2011-05-26
申请号：US12871661
申请日：2010-08-30
申请人： Julien RAMBAUD , Sebastien Vieillard
发明人： Julien RAMBAUD , Sebastien Vieillard
IPC分类号： G05F1/10
CPC分类号： H03K17/0822 , H03K17/165
摘要： An electronic control module for a field effect transistor includes a gate, a drain and a source. The electronic control module includes: a control circuit including: a power supply able to provide a fixed potential to the gate of the field effect transistor; and an amplifier stage able to vary the potential of the source of the field effect transistor with relation to the potential of the gate of the field effect transistor; and a field effect transistor whose gate is connected to the fixed potential; and source is connected to the amplifier stage.
摘要翻译：用于场效应晶体管的电子控制模块包括栅极，漏极和源极。电子控制模块包括：控制电路，包括：能够向场效应晶体管的栅极提供固定电位的电源; 以及能够相对于场效应晶体管的栅极的电位改变场效应晶体管的源极的电位的放大器级; 以及栅极连接到固定电位的场效应晶体管; 源极连接到放大器级。

7. 发明授权

US09467077B2 Method and architecture for processing electrical energy regenerated from an aircraft 有权
标题翻译：用于处理从飞行器再生的电能的方法和结构
公开(公告)号：US09467077B2
公开(公告)日：2016-10-11
申请号：US13885103
申请日：2011-11-22
申请人： Julien Rambaud , Sebastien Vieillard
发明人： Julien Rambaud , Sebastien Vieillard
IPC分类号： B60L1/00 , B60L3/00 , H02G3/00 , H02P3/14 , B60L7/20 , H02P3/18 , B60R16/03
CPC分类号： H02P3/14 , B60L7/20 , B60R16/0307 , H02P3/18 , Y02T10/642
摘要： A method and architecture processing electrical energy regenerated from an aircraft, to address drawbacks posed by customary solutions for dissipating low energy of resistors, conventionally ceramics, which require a significant volume of ceramic and an additional power converter. The method and architecture return energy to an electric generator to convert the energy into mechanical energy. The architecture includes a reversible electric generator, driven by a thermal machine and configured to deliver an AC voltage, electric actuators, and a voltage converter circuit with multiple links. The circuit includes AC voltage rectifiers for voltage originating from the generator and power converters arranged on the multiple links to drive as many electric actuators. The converter circuit also includes a mechanism for electrical energy inverse transmission applied to the generator operating in a motor mode.
摘要翻译：一种处理从飞行器再生的电能的方法和架构，以解决用于耗散电阻器的低能量的常规解决方案所带来的缺点，常规陶瓷需要大量陶瓷和额外的功率转换器。该方法和结构将能量返回到发电机以将能量转换成机械能。该架构包括由热机驱动并被配置为提供交流电压，电致动器和具有多个链路的电压转换器电路的可逆发电机。该电路包括用于来自发电机的电压的AC电压整流器和布置在多个链路上的功率转换器，以驱动尽可能多的电致动器。转换器电路还包括施加到以电动机模式工作的发电机的电能反向传输机构。

8. 发明申请

US20140008972A1 ELECTRICAL POWER SUPPLY FOR AN AIRCRAFT 审中-公开
标题翻译：用于飞机的电力供应
公开(公告)号：US20140008972A1
公开(公告)日：2014-01-09
申请号：US14005674
申请日：2012-03-07
申请人： Eric De Wergifosse , Julien Rambaud , Sebastien Vieillard
发明人： Eric De Wergifosse , Julien Rambaud , Sebastien Vieillard
IPC分类号： B60R16/03
CPC分类号： B60R16/03 , B64D2221/00 , H02J4/00 , H02M5/458
摘要： A generation method performed by a generator module of an electricity network of an aircraft, the electricity network including a power supply line powered by the generator module, a DC bus powered from the power supply line via a rectifier, and at least one electrical actuator powered with AC from the DC bus via an inverter. The generation method includes: delivering an AC voltage as a function of a voltage setpoint and of a voltage measured in the on-board network; and determining the voltage setpoint as a function of an operating parameter of the actuator.
摘要翻译：由飞行器的电力网络的发电机模块执行的生成方法，所述电力网络包括由发电机模块供电的电源线，经由整流器从所述电源线供电的DC总线，以及至少一个电动致动器通过逆变器从直流总线交流。生成方法包括：根据电压设定点和在车载网络中测量的电压递送AC电压; 以及根据所述致动器的操作参数确定所述电压设定值。

9. 发明授权

US10128652B2 Stabilizing a DC electricity network 有权
公开(公告)号：US10128652B2
公开(公告)日：2018-11-13
申请号：US14344760
申请日：2012-09-12
申请人： Sebastien Vieillard , Pierre Magne , Farid Meibody-Tabar , Babak Nahid-Mobarakeh , Serge Pierfederici
发明人： Sebastien Vieillard , Pierre Magne , Farid Meibody-Tabar , Babak Nahid-Mobarakeh , Serge Pierfederici
IPC分类号： H02J3/14 , H02J1/00 , H02J1/14 , H02J3/16 , H02J3/24 , B60R16/03 , G06F17/10 , H02M3/02 , H03H7/01
摘要： A method of stabilizing a DC electricity network, the network including a DC voltage source powering electrical loads that are connected in parallel to terminals of the voltage source and each of which is to receive a current or voltage setpoint. The method stabilizes the network by regulating setpoints applied to the loads by a virtual stabilization impedance generated at terminals of each load, the virtual impedances being dimensioned to stabilize the network in desired operating points and in given configurations of the network including a state in which at least one load is inactive or has failed and a state in which the stabilization of a load is inactive. Each virtual impedance is generated by a non-linear regulation loop acting on the setpoint for the corresponding load.

10. 发明授权

US09062627B2 Method for controlling electric motors of a thrust reverser 有权
标题翻译：用于控制推力反向器的电动机的方法
公开(公告)号：US09062627B2
公开(公告)日：2015-06-23
申请号：US12527125
申请日：2008-01-25
申请人： Michel Philippe Dehu , Fabrice Henri Emile Metezeau , Eric Lecossais , Gilles Le Gouellec , Regis Meuret , Sebastien Vieillard
发明人： Michel Philippe Dehu , Fabrice Henri Emile Metezeau , Eric Lecossais , Gilles Le Gouellec , Regis Meuret , Sebastien Vieillard
IPC分类号： F02K1/76
CPC分类号： F02K1/763 , F05D2270/62 , Y02T50/671
摘要： The invention relates to a method for controlling an electric motor actuating a mobile hood provided in a thrust reverser for a turboreactor, said method being characterized in that it comprises steps of: determining the operating state of the electric motor; interrupting the supply of the electric motor if said motor is not in operation during a defined period of time; reactivating the electric motor after an idle period and repeating the previous steps or definitively stopping the motor if the steps have already been repeated a pre-defined number of times. The invention also relates to a method for managing the electrical supply of a motor provided in a device arranged in the vicinity of a turboreactor.
摘要翻译：本发明涉及一种用于控制电动马达的方法，该马达致动设置在用于涡轮反应器的推力反向器中的移动罩，所述方法的特征在于包括以下步骤：确定电动机的运行状态; 如果所述电机在限定的时间段内不工作，则中断电动机的供应; 在空闲时间之后重新激活电动机并重复前面的步骤，或者如果步骤已经重复了预先定义的次数，则确定地停止电动机。本发明还涉及一种用于管理设置在布置在涡轮反应器附近的装置中的马达的电力供应的方法。

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