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1.发明授权Power system comprising several synchronous machines synchronously self-controlled by a converter and control method for such a system 有权电力系统包括由转换器同步自控的多个同步电机和用于这种系统的控制方法公开(公告)号：US07538501B2
公开(公告)日：2009-05-26
申请号：US11689835
申请日：2007-03-22
IPC分类号： H02P1/54
CPC分类号： H02P6/04
摘要： A power system including at least two self-controlled synchronous machines operating in parallel synchronously, a central three-phase converter to which all these machines are connected in parallel, at least two rotor position sensors. The system also includes at least one control module that receives phase currents from each synchronous machine, signals output from position sensors, and a required reference torque value and that powers the three-phase central converter so as to slave the phase currents for each machine as a function of the required reference torque.
摘要翻译： 包括至少两个同时并行运行的自控同步电机的电力系统，所有这些机器并联连接的中心三相转换器，至少两个转子位置传感器。 该系统还包括至少一个控制模块，其接收来自每个同步电机的相电流，从位置传感器输出的信号和所需的参考转矩值，并为三相中央转换器供电，从而将每台机器的相电流作为 所需参考扭矩的函数。
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2.发明申请公开(公告)号：US20070262644A1
公开(公告)日：2007-11-15
申请号：US11689821
申请日：2007-03-22
IPC分类号： H02J1/00
CPC分类号： H02J1/10 , B64D2221/00 , H02J4/00 , Y02T50/54 , Y10T307/313 , Y10T307/391
摘要： The invention relates to a power supply system for several user systems onboard an aircraft. This system comprises at least two power supply electronics (10, 11) and means of connecting these at least two power supply electronics to at least two user systems (12, 13, 14, 15), characterised in that these connecting means comprise a network of connecting contactors (16, 17; 32, 33) from each power supply electronics with at least two user systems not performing similar functions but technologically compatible such that these power supply electronics supply these user systems at different times.
摘要翻译： 本发明涉及一种用于飞机上的多个用户系统的电源系统。 该系统包括至少两个电源电子设备（10,11）以及将这些至少两个电源电路连接到至少两个用户系统（12,13,14,15）的装置，其特征在于，这些连接装置包括网络 将来自每个电源电子设备的接触器（16,17; 32,33）与不具有相似功能但技术上相容的至少两个用户系统连接，使得这些电源电子设备在不同时间提供这些用户系统。
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3.发明申请POWER SYSTEM COMPRISING SEVERAL SYNCHRONOUS MACHINES SYNCHRONOUSLY SELF-CONTROLLED BY A CONVERTER AND CONTROL METHOD FOR SUCH A SYSTEM 有权包含由转换器同步控制的几个同步机器的电力系统和这种系统的控制方法公开(公告)号：US20070273310A1
公开(公告)日：2007-11-29
申请号：US11689835
申请日：2007-03-22
IPC分类号： H02P5/00
CPC分类号： H02P6/04
摘要： The invention relates to a power system comprising at least two self-controlled synchronous machines (MS1, MS2) operating in parallel synchronously, a central three-phase converter (20; 50) to which all these machines are connected in parallel, at least two rotor position sensors (23, 24; 45, 46, 47, 48), characterised in that it comprises at least one control module (25; 30, 31; 53, 54, 55, 56) that receives phase currents from each synchronous machine, signals output from position sensors (23, 24), and a required reference torque value (Cref) and that powers the three-phase central converter (20) so as to slave the phase currents for each machine as a function of the required reference torque (Cref). The invention also concerns a control method for such a system.
摘要翻译： 本发明涉及一种电力系统，包括至少两个同时并行操作的自控同步电机（MS 1，MS 2），所有这些机器并联连接的中心三相转换器（20; 50） 至少两个转子位置传感器（23,24; 45,46,47,48），其特征在于，其包括至少一个控制模块（25; 30,31; 53,54,55,56），其接收来自每个 同步机，位置传感器（23,24）输出的信号和所需的参考转矩值（Cref），并为三相中央转换器（20）供电，从而使每个机器的相电流为 所需参考扭矩（Cref）。 本发明还涉及这种系统的控制方法。
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4.发明授权公开(公告)号：US07939962B2
公开(公告)日：2011-05-10
申请号：US11689821
申请日：2007-03-22
CPC分类号： H02J1/10 , B64D2221/00 , H02J4/00 , Y02T50/54 , Y10T307/313 , Y10T307/391
摘要： The invention relates to a power supply system for several user systems onboard an aircraft. This system comprises at least two power supply electronics (10, 11) and means of connecting these at least two power supply electronics to at least two user systems (12, 13, 14, 15), characterised in that these connecting means comprise a network of connecting contactors (16, 17; 32, 33) from each power supply electronics with at least two user systems not performing similar functions but technologically compatible such that these power supply electronics supply these user systems at different times.
摘要翻译： 本发明涉及一种用于飞机上的多个用户系统的电源系统。 该系统包括至少两个电源电子设备（10,11）以及将这些至少两个电源电路连接到至少两个用户系统（12,13,14,15）的装置，其特征在于，这些连接装置包括网络 将来自每个电源电子设备的接触器（16,17; 32,33）与不具有相似功能但技术上相容的至少两个用户系统连接，使得这些电源电子设备在不同时间提供这些用户系统。
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5.发明申请公开(公告)号：US20050099746A1
公开(公告)日：2005-05-12
申请号：US10626254
申请日：2003-07-23
申请人： Sebastien Vergnat , Etienne Foch
发明人： Sebastien Vergnat , Etienne Foch
摘要： The invention relates to a device for protection against overcurrents in an electrical energy distribution cabinet which receives electrical energy supplied by at least one generator and which distributes this energy to at least two loads, which comprises: switching means (20), means (23; C) for calculating the absolute value of the difference between at least one current entering the said cabinet and at least one corresponding current leaving the said cabinet, for at least one harmonic of these currents, comparison means (24) which control the opening of the switching means (20) if this absolute value is greater than a predetermined threshold (S).
摘要翻译： 本发明涉及一种用于防止电能分配柜中的过电流的装置，其接收由至少一个发电机提供的电能并将该能量分配给至少两个负载，该装置包括：开关装置（20），装置（23; C）用于计算进入所述机壳的至少一个电流与离开所述机壳的至少一个对应电流之间的差的绝对值，对于这些电流的至少一次谐波，控制开关的比较装置（24） 如果该绝对值大于预定阈值（S），则切换装置（20）。
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公开(公告)号：US4789119A
公开(公告)日：1988-12-06
申请号：US117586
申请日：1987-11-06
申请人： Roger Bellego , Etienne Foch
发明人： Roger Bellego , Etienne Foch
CPC分类号： B64D45/0005 , B64C13/36 , B64D2045/001
摘要： This invention relates to a system for controlling the high-lift flaps of an aircraft subjected to the blast of at least one engine. The system includes reversible hydraulic jacks for actuating the flaps arranged so that each flap is actuated by a jack and each of the two chambers of one jack are connected to the corresponding chamber of the other jack, as well as to an orifice in a hydraulic fluid distributing unit, so that the supply and exhaust of the corresponding chambers of the jacks are respectively simultaneous. The high-lift flaps are connected by a mechanical torsional connection which allows a dissymetry of position of the high-lift flaps in extended position. A safety system is also provided to block the high-lift flaps in position as soon as the extent of dissymetry of position between the high-lift flaps in extended position reaches a predetermined threshold.
摘要翻译： 本发明涉及一种用于控制经受至少一个发动机爆炸的飞行器的高升力襟翼的系统。 该系统包括用于致动翼片的可逆液压千斤顶，其布置成使得每个翼片由千斤顶致动，并且一个千斤顶的两个腔室中的每一个连接到另一个千斤顶的相应室以及液压流体中的孔口 分配单元，使得千斤顶的相应室的供应和排放分别同时进行。 高提升襟翼通过机械扭力连接连接，允许高升襟翼的位置偏离延伸位置。 一旦安全系统被提供，一旦伸出位置的高提升襟翼之间的位置偏差程度达到预定的阈值，就可以将高升襟翼阻挡在适当位置。
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公开(公告)号：US20110198918A1
公开(公告)日：2011-08-18
申请号：US12294435
申请日：2007-03-13
申请人： Olivier Langlois , Etienne Foch
发明人： Olivier Langlois , Etienne Foch
CPC分类号： B64D41/00 , B64D41/007 , B64D2041/002 , B64D2221/00 , F03D9/12 , F03D9/25 , F03D9/32 , F05B2220/50 , Y02E10/725 , Y02E60/16 , Y02T50/44 , Y02T50/54
摘要： A device and a method for emergency electricity supply on board an aircraft, able to supply a part of the aircraft's electrical power circuit. The device includes a synchronous machine with separate excitation, associated with a flywheel, and an auxiliary device to set the flywheel in rotation and to maintain rotation of the flywheel.
摘要翻译： 一种用于飞机上的紧急电力供应的装置和方法，能够提供飞机电力电路的一部分。 该装置包括具有与飞轮相关联的单独激励的同步机，以及用于将飞轮旋转并保持飞轮旋转的辅助装置。
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8.发明申请DEVICE AND METHOD FOR GENERATING A BACK-UP ELECTRICITY SUPPLY ON BOARD AN AIRCRAFT 审中-公开在飞机上生成备用电源的装置和方法公开(公告)号：US20100270858A1
公开(公告)日：2010-10-28
申请号：US12294246
申请日：2007-03-07
申请人： Etienne Foch , Olivier Langlois
发明人： Etienne Foch , Olivier Langlois
IPC分类号： B60L1/00
CPC分类号： B64D41/00 , B64D13/06 , B64D2013/0618 , B64D2013/0644 , B64D2221/00 , F01D15/10 , F02C6/08 , F05D2220/76 , Y02T50/44 , Y02T50/54 , Y02T50/56 , Y02T50/671
摘要： A device and a method to generate electricity on board an aircraft, including plural generators and plural air-conditioning units having an outside air intake. This device includes a control to command air-conditioning units as emergency generators and a storage device.
摘要翻译： 一种在飞机上发电的装置和方法，包括多个发电机和具有外部空气入口的多个空调机组。 该装置包括用于指令空调机组作为应急发电机和存储装置的控制。
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9.发明授权Device for supplying electrical power to an aircraft and for electrically starting a jet engine on board an aircraft 有权用于向飞行器提供电力并在飞机上电喷射喷气发动机的装置公开(公告)号：US07638890B2
公开(公告)日：2009-12-29
申请号：US11868828
申请日：2007-10-08
申请人： Jean-Louis Lando , Etienne Foch , Xavier Roboam , Dominique Alejo
发明人： Jean-Louis Lando , Etienne Foch , Xavier Roboam , Dominique Alejo
CPC分类号： F02C7/26 , F01D15/10 , Y02T50/671
摘要： This invention relates to a device for supplying electrical power to an aircraft and for electrically starting a jet engine on board an aircraft, including a multi-phased starter-generator, a multi-phased transformer-rectifier unit, a multi-phased DC-AC converter, a multi-phased rectifier unit, and at least one three-phase inverter, wherein the number of phases is equal to or greater than 5.
摘要翻译： 本发明涉及一种用于向飞行器提供电力并且用于电动启动飞机上的喷气发动机的装置，包括多相起动发电机，多相变压器整流器单元，多相DC-AC 转换器，多相整流器单元和至少一个三相逆变器，其中相数等于或大于5。
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10.发明申请公开(公告)号：US20080174177A1
公开(公告)日：2008-07-24
申请号：US12013082
申请日：2008-01-11
申请人： Olivier LANGLOIS , Etienne Foch , Lucien Prisse , Xavier Roboam
发明人： Olivier LANGLOIS , Etienne Foch , Lucien Prisse , Xavier Roboam
CPC分类号： H02J1/14 , B64D2221/00 , H02J1/08 , H02J1/12 , Y02T50/54 , Y10T307/305 , Y10T307/344
摘要： The invention relates to a system and a method for supplying power to an aircraft comprising several generators supplying alternating current to several different primary electrical master boxes (10, 11, 12 and 13), the various aircraft loads being connected to each of these master boxes. This system comprises conventional master boxes (10, 11, 12 and 13) which supply power loads and at least one master box (40, 41) devoted to actuator loads, this at least one devoted master box being connected to conventional master boxes.
摘要翻译： 本发明涉及一种用于向飞行器供电的系统和方法，包括向多个不同的主电主箱（10,11,12和13）提供交流电的多个发电机，各种飞机负载连接到这些主箱中的每一个 。 该系统包括提供动力负载的常规主箱（10,11,12和13）以及致力于致动器负载的至少一个主箱（40,41），该至少一个专用主箱连接到常规主箱。
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