ELECTRONIC DAMPING OF STEPPER MOTOR

    公开(公告)号:CA1155911A

    公开(公告)日:1983-10-25

    申请号:CA353784

    申请日:1980-06-11

    Applicant: IBM

    Abstract: ELECTRONIC DAMPING OF STEPPER MOTOR A damping control system for a three phase stepper motor. A reluctance velocity transducer is used for each of the three phases. The output of each of the transducers is proportional to the rotational velocity of the motor. Each of the transducers is rotationally phase shifted 3.75 with respect to one another and phased to the motor rotor rotationally such that the zero voltage crossings of the transducers correspond to the zero torque crossings of the motor. During damping or detenting of the motor the selected phase has current applied to it which is equal to a predetermined fixed value plus the feedback from its associated transducer. The windings on each side of the detent position have current applied to them which is proportional to the voltage from their respective feedback transducers. The voltage in each of the windings is amplified by a selected gain constant. The current in each of the windings is such that maximum torque is applied to drive the motor to the detent position with appropriate current reversals in the windings to damp out any kinetic energy in the rotor during detenting. AT9-78-032

    SOLENOID IMPACT PRINT HAMMER WITH UNIFORM FREE FLIGHT TIME

    公开(公告)号:CA1166511A

    公开(公告)日:1984-05-01

    申请号:CA374644

    申请日:1981-04-03

    Applicant: IBM

    Abstract: SOLENOID IMPACT PRINT HAMMER WITH UNIFORM FREE FLIGHT TIME In an impact printer including a print wheel having a plurality of selectable character type bearing elements for respectively printing a plurality of characters, said print wheel being rotatable for selectively positioning selected type elements in successive print positions, impact means impellable against the selected elements to drive said elements against the printing medium and means for impelling the impact means against said selected type element, the present invention provides the improvement comprising the combination of means for sensing the flight time of the impelled impact means until impact by sensing variations in the velocity of said impact means, means for comparing the sensed flight time to a predetermined ideal flight time, and means for selectively varying the amplitude of the current to the impelling means to adjust the sensed flight time to equal the ideal flight time. AT9-79-037

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