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    • 5. 发明授权
    • Bi-stable pin actuator
    • US10297376B2
    • 2019-05-21
    • US15714119
    • 2017-09-25
    • The United States of America as represented by the Administrator of NASA
    • Joseph C. Church
    • H01F7/00H01F7/16
    • A bi-stable pin actuator includes a soft magnetic core and having a first central portion and a second central portion spaced apart from the first central portion. The first central portion has a first passage extending there-through and the second portion has a second passage extending there-through which is coaxial with the first passage. A first coil is wound about the first central portion and a second coil is wound about the second central portion. A pair of permanent magnets are located in the space between the first central portion and second central portion and attached to the core. An armature is movably positioned between and spaced apart from the permanent magnets. A pin is attached to the armature and extends into the first passage and second passages such that movement of the armature results in movement of the pin within the first passage and second passage. The armature moves between a first position wherein the armature is adjacent to the first central portion of the core and a second position wherein the armature is adjacent to the second central portion of the core. The armature is in one stable state when in the first position and in another of the stable state when in the second position. The magnets generate magnetic flux having a magnetic flux density sufficient to hold the armature in either of the stable states when neither of the coils is energized. When the armature is in the first stable state, only a first end of the pin protrudes from the core. When the armature is in the second stable state, only an opposite second end of the pin protrudes from the core. Energizing at least one of the coils generates a magnetic flux in one section of the actuator that opposes the magnetic flux holding the armature in a current stable state and supplements the magnetic flux in another section of the actuator so as to shift the armature into another stable state.