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1. 发明申请

WO2010068426A1 ELECTRIC ENERGY STORAGE INTEGRATED WITHIN OR PROXIMATE TO ELECTRICALLY DRIVEN FLIGHT CONTROL ACTUATORS 审中-公开
标题翻译：集成在或靠近电动驾驶飞行控制执行器的电力存储
公开(公告)号：WO2010068426A1
公开(公告)日：2010-06-17
申请号：PCT/US2009/065679
申请日：2009-11-24
申请人： GE AVIATION SYSTEMS LLC , HUANG, Hao , KARIPIDES, David, Dimitri , RADUN, Arthur, Vorwerk
发明人： HUANG, Hao , KARIPIDES, David, Dimitri , RADUN, Arthur, Vorwerk
IPC分类号： H02P27/08 , B64C13/50 , H02M3/158
CPC分类号： H02P27/08 , H02M3/1582 , Y10T29/49002
摘要： An apparatus for use with a flight control actuator and method for assembling the same is provided. The apparatus includes a motor drive system (100) and a control unit. The motor drive system (100) includes a capacitor-based energy storage (120) configured to store and provide energy within or proximate to the actuator. The control unit is coupled to the motor drive system and is configured to facilitate managing power within or proximate to the actuator.
摘要翻译：提供了一种用于飞行控制致动器的装置及其组装方法。该装置包括电机驱动系统（100）和控制单元。马达驱动系统（100）包括基于电容器的能量存储器（120），其被配置为在致动器内或附近存储和提供能量。控制单元耦合到马达驱动系统并且被配置为便于在致动器内部或附近管理动力。

2. 发明申请

WO2010138234A1 METHOD AND APPARATUS FOR ELECTRICAL BUS CENTERING 审中-公开
标题翻译：电气总线中心的方法和装置
公开(公告)号：WO2010138234A1
公开(公告)日：2010-12-02
申请号：PCT/US2010/028473
申请日：2010-03-24
申请人： GENERAL ELECTRIC COMPANY , KARIPIDES, David, Dimitri , ZHOU, Rui , RADUN, Arthur, Vorwerk , HUANG, Hao
发明人： KARIPIDES, David, Dimitri , ZHOU, Rui , RADUN, Arthur, Vorwerk , HUANG, Hao
IPC分类号： H02M7/487 , H02M1/00
CPC分类号： H02M7/487 , H02M1/00
摘要： A bus centering device for use in an aircraft electrical power distribution system that includes a positive bus rail, a negative bus rail, and a ground is described. The device includes a central node, a first and second switching component configured to couple the central node to the positive rail and the negative rail for a first and second predetermined duty cycle, respectively. The device includes an inductive component coupled between the central node and ground, and is configured to maintain a voltage at the central node substantially equal to ground, wherein a voltage between the positive rail and the central node is maintained substantially equal to a voltage between the negative rail and the central node. The device includes a first and second current limiting device configured to maintain a continuity of current from the inductive component when the first and second switching components are turned off.
摘要翻译：描述了一种用于包括正母线，负母线和地面的飞机配电系统的总线定心装置。该装置包括中央节点，第一和第二开关部件，其被配置成分别将第一和第二预定占空比将中心节点耦合到正轨和负轨。该装置包括耦合在中心节点和地之间的电感部件，并且被配置为将中心节点处的电压基本上保持等于接地，其中正轨和中心节点之间的电压基本上等于负轨和中心节点。该装置包括第一和第二限流装置，其被配置为当第一和第二开关部件关闭时保持来自电感部件的电流的连续性。

3. 发明申请

WO2010126654A1 SYSTEM AND METHOD FOR TRANSFERRING POWER BETWEEN AN AIRCRAFT POWER SYSTEM AND ENERGY STORAGE DEVICES 审中-公开
标题翻译：用于传输飞机动力系统和能量储存装置之间的动力的系统和方法
公开(公告)号：WO2010126654A1
公开(公告)日：2010-11-04
申请号：PCT/US2010/027094
申请日：2010-03-12
申请人： GE AVIATION SYSTEMS LLC , RADUN, Arthur, Vorwerk
发明人： RADUN, Arthur, Vorwerk
IPC分类号： H02J1/16 , H02J7/14 , H02J7/34
CPC分类号： H02J7/1423 , B64D2221/00 , H02J1/16 , H02J7/1492 , H02J7/345 , Y10T307/615
摘要： A method for transferring power in an aircraft between an energy storage device and a power system. The method includes determining an amount of power required by the power system, determining a predetermined amount of power from a generator, comparing the power required by the power system to the predetermined power of the generator, and transferring power to the energy storage device from the power system or to the power system from the energy storage device based on the comparing.
摘要翻译：一种用于在能量存储装置和电力系统之间的飞行器中传递动力的方法。该方法包括确定电力系统所需的功率量，确定来自发电机的预定功率量，将电力系统所需的功率与发电机的预定功率进行比较，以及从电力系统电力系统或电力系统从储能装置上进行比较。

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