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    Actuation system with redundant motor actuators
    1.
    发明公开
    Actuation system with redundant motor actuators 审中-公开
    驱动系统具有冗余马达的致动器

    公开(公告)号：EP1863154A3

    公开(公告)日：2009-01-21

    申请号：EP07109327.2

    申请日：2007-05-31

    申请人： Honeywell International Inc.

    发明人： Potter, Calvin C ,  Wingett, Paul T. ,  Hanlon, Casey ,  Morris, John T.

    IPC分类号： H02K21/24

    CPC分类号： H02K21/24 ,  B64C13/42 ,  H02K16/00 ,  H02K2213/06

    摘要： A multi-redundant motor (200) may be used to implement a relatively small, lightweight redundant actuator assembly package. The motor (200) is implemented as a brushless DC motor (200) and includes N-number of stators (202) and M-number of rotors (204). Each stator (202) has a plurality of independent stator coils (216) disposed thereon, and N is an integer greater than two. Each permanent magnet rotor (204) is disposed between, and is spaced axially apart from, two of the stators (202). Each rotor (204) has a plurality of magnetic dipoles (224) disposed thereon, and M is an integer equal to (N-1).

    Flight control surface actuation system with redundantly configured and lockable actuator assemblies
    3.
    发明公开
    Flight control surface actuation system with redundantly configured and lockable actuator assemblies 有权
    BettertigungsystemfürFlugzeugsteuerflächenmit redundantkonfiguriertenSchliessbetätigungsvorrichtungen

    公开(公告)号：EP1721825A1

    公开(公告)日：2006-11-15

    申请号：EP06113583.6

    申请日：2006-05-05

    申请人： Honeywell International Inc.

    发明人： Wingett, Paul T ,  Potter, Calvin C ,  Hanlon, Casey ,  Benson, Dwayne M

    IPC分类号： B64C13/00 ,  B64C13/42

    CPC分类号： B64C13/42 ,  B64C13/00

    摘要： A flight control surface actuator assembly (120) includes a pair of flight control surface actuators (206, 208) and a pivot arm (212). One of the flight control surface actuators (208) is coupled to a flight control surface (202) and a static airframe structure (215), the other flight control surface actuator (206) is coupled to the flight control surface (202) and the pivot arm (212). The pivot arm (212) coupled to the static airframe structure (215) and is configured to pivot relative to the second flight control surface actuator (126) and the static airframe structure (215).

    摘要翻译： 飞行控制表面致动器组件（120）包括一对飞行控制表面致动器（206,208）和枢转臂（212）。 飞行控制表面致动器（208）中的一个联接到飞行控制表面（202）和静态机身结构（215），另一个飞行控制表面致动器（206）联接到飞行控制表面（202），并且 枢转臂（212）。 枢转臂（212）联接到静态机身结构（215）并且构造成相对于第二飞行控制表面致动器（126）和静止机身结构（215）枢转。

    Actuation system with redundant motor actuators
    6.
    发明公开
    Actuation system with redundant motor actuators 审中-公开
    防盗系统

    公开(公告)号：EP1863154A2

    公开(公告)日：2007-12-05

    申请号：EP07109327.2

    申请日：2007-05-31

    申请人： Honeywell International Inc.

    发明人： Potter, Calvin C ,  Wingett, Paul T. ,  Hanlon, Casey ,  Morris, John T.

    IPC分类号： H02K21/24

    CPC分类号： H02K21/24 ,  B64C13/42 ,  H02K16/00 ,  H02K2213/06

    摘要： A multi-redundant motor (200) may be used to implement a relatively small, lightweight redundant actuator assembly package. The motor (200) is implemented as a brushless DC motor (200) and includes N-number of stators (202) and M-number of rotors (204). Each stator (202) has a plurality of independent stator coils (216) disposed thereon, and N is an integer greater than two. Each permanent magnet rotor (204) is disposed between, and is spaced axially apart from, two of the stators (202). Each rotor (204) has a plurality of magnetic dipoles (224) disposed thereon, and M is an integer equal to (N-1).

    摘要翻译： 多冗余电动机（200）可用于实现相对较小，重量轻的冗余致动器组件封装。 电动机（200）被实现为无刷直流电动机（200），并且包括N个定子（202）和M个转子（204）。 每个定子（202）具有多个独立的定子线圈（216），其中N是大于2的整数。 每个永磁转子（204）设置在两个定子（202）之间并且与两个定子（202）轴向间隔开。 每个转子（204）上设置有多个磁偶极子（224），M是等于（N-1）的整数。