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    CONTROL DEVICE FOR DRIVE DEVICE
    1.
    发明申请
    CONTROL DEVICE FOR DRIVE DEVICE 有权
    用于驱动装置的控制装置

    公开(公告)号：US20150137724A1

    公开(公告)日：2015-05-21

    申请号：US14550433

    申请日：2014-11-21

    Applicant: IHI AEROSPACE CO., LTD. ,  SINFONIA TECHNOLOGY CO., LTD.

    Inventor： Hitoshi OYORI ,  Yoshito OHTA ,  Keisuke ONISHI

    IPC: H02P5/00

    CPC classification number: H02P5/00 ,  G05B11/32 ,  G05B11/36 ,  G05B11/38 ,  G05B2219/40208 ,  G05B2219/42317

    Abstract: Multipliers 21a and 21b output values, which are obtained by multiplying a total drive command value Es by first and second gains G1 and G2, respectively, as first and second drive command values E1 and E2. Controllers 23a and 23b control first and second actuators (motors) 5 and 7, respectively, on the basis of the first and second drive command values. The detection values of the drive amounts of the actuators are denoted by Ef1 and Ef2, respectively, and the detection value of the drive amount of a driven body is denoted by Ef. A gain calculator 27 calculates the gains G1 and G2 on the basis of Ef1, Ef and Ef2. An upper limit value of Ef, which denotes the drive amount of the driven body, is denoted by Lmax. When Ef1, Ef2 or Ef approaches zero, the first gain G1 is brought close to (Ef1−Lmax/2)/(Ef−Lmax).

    Abstract translation: 乘法器21a和21b的输出值分别通过将总驱动指令值Es乘以第一和第二增益G1和G2作为第一和第二驱动指令值E1和E2获得。 控制器23a和23b分别基于第一和第二驱动指令值来控制第一和第二致动器（马达）5和7。 致动器的驱动量的检测值分别由Ef1和Ef2表示，驱动体的驱动量的检测值用Ef表示。 增益计算器27基于Ef1，Ef和Ef2来计算增益G1和G2。 表示被驱动体的驱动量的Ef的上限值由Lmax表示。 当Ef1，Ef2或Ef接近零时，第一增益G1接近（Ef1-Lmax / 2）/（Ef-Lmax）。

    MOTOR CONTROLLER
    2.
    发明申请
    MOTOR CONTROLLER 有权
    电机控制器

    公开(公告)号：US20150162857A1

    公开(公告)日：2015-06-11

    申请号：US14560406

    申请日：2014-12-04

    Applicant: SINFONIA TECHNOLOGY CO., LTD. ,  IHI AEROSPACE CO., LTD.

    Inventor： Yoshito OHTA ,  Keisuke ONISHI ,  Hitoshi OYORI

    IPC: H02P6/00

    CPC classification number: H02P6/002 ,  H02P6/28 ,  H02P21/22 ,  H02P29/0243

    Abstract: A 0-axis current calculator 7 configured to calculate a target value of the 0-axis current by setting the current of the open phase to be zero when one of the phases becomes open, or determines that the target value of the 0-axis current is zero when there is no open phase is provided. Based on the target values of the d-axis current and the q-axis current, the target value of the 0-axis current calculated by the 0-axis current calculator 7, and the d-axis current, the q-axis current, and the 0-axis current transformed by the d-q-0 transformer 8, the current supplied to each phase of the motor are controlled.

    Abstract translation: 0轴电流计算器7，被配置为当其中一个相位变为断开时，通过将开路相位的电流设置为零来计算0轴电流的目标值，或者确定0轴电流的目标值 当没有提供开放相位时为零。 基于d轴电流和q轴电流的目标值，由0轴电流计算器7计算的0轴电流的目标值和d轴电流，q轴电流， 和由dq-0变压器8变换的0轴电流，控制提供给电动机各相的电流。

    AIRCRAFT ELECTRIC ACTUATOR DRIVE APPARATUS
    4.
    发明申请
    AIRCRAFT ELECTRIC ACTUATOR DRIVE APPARATUS 有权
    飞机电动执行器驱动装置

    公开(公告)号：US20150060601A1

    公开(公告)日：2015-03-05

    申请号：US14470194

    申请日：2014-08-27

    Applicant: NABTESCO CORPORATION ,  IHI AEROSPACE CO., LTD.

    Inventor： Shingo NAKAGAWA ,  Yoichi YAMAMOTO ,  Hitoshi OYORI

    IPC: B64C13/50 ,  B64D41/00

    CPC classification number: B64C13/50 ,  B64D41/00 ,  Y02T50/44

    Abstract: An aircraft electric actuator drive apparatus has an electric actuator and a secondary power supply device. The electric actuator is driven using electric power from a main power unit provided in an aircraft. The secondary power supply device can temporarily supply electric power to the electric actuator while electric power from the main power unit is applied to the electric actuator.

    Abstract translation: 飞机电动执行机构驱动装置具有电动执行器和二次供电装置。 电动执行器使用设在飞机上的主动力单元的电力来驱动。 辅助电源装置能够将来自主电源单元的电力施加到电致动器的电动执行机构暂时供给电力。

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