Linear actuator control system for platform stabilization

• US 5,170,104 A
• Filed: 08/20/1991
• Issued: 12/08/1992
• Est. Priority Date: 08/20/1991
• Status: Expired due to Term

• Current Assignee: Tech Corporation Company Limited
• Original Assignee: Applied Industrial Technologies Incorporated
• Inventors: Laughlin, Darren
• Primary Examiner(s): Stephan, Steven L.
• Assistant Examiner(s): Rebsch, D. S.
• Application Number:
  US07/747,674
• Time in Patent Office: 476 Days
• Field of Search: 310/12, 310/13, 310/15, 310/51, 310/90, 318/135, 318/128, 318/649, 384/12, 384/118, 33/DIG. 1, 73/516 R, 73/517 R, 73/663
• US Class Current: 318/135
• CPC Class Codes: F16F 7/1011 by electromagnetic means
• CPC Class Codes: G03F 7/709 Vibration, e.g. vibration detection, compensation, suppression or isolation
• CPC Class Codes: H02K 33/18 with coil systems moving upon intermittent or reversed energisation thereof by interaction with a fixed field system, e.g. permanent magnets

Abstract

An inertial linear actuator for stabilizing a platform against vibration includes a movable coil having windings which may be energized, supported on an actuator guide for movement. The actuator guide is fixed to the platform and a current is supplied to the movable coil to generate a force for damping sensed vibrations on the platform surface. Permanent magnets parallel to the actuator guide, and a current in the movable coil results in a force being introduced between the movable coil and the stationary actuator guides. A control system on the platform supplies a feedback signal from an accelerometer coupled to the platform to drive electronics. The drive electronics produce a current having the magnitude and direction for creating the actuator force for damping the sensed disturbance.

Claims

1. An inertial actuator stabilizing system for stabilizing a platform against vibration comprising:

an actuator guide supported on said platform by first and second end pieces;

first, second and third rows of permanent magnets supported by said end pieces, about an axis of said actuator guide, and parallel to said actuator parallel to said axis and spaced therefrom;

a movable coil having windings coaxial with said actuator guide which slides over said actuator guide between said rows of magnets in response to a current flowing through said coil windings;

an accelerometer coupled to said platform for sensing acceleration forces applied to said platform; and

,

electronic means connected to said accelerometer for producing a current for said movable coil windings which generates a force on said movable coil having a direction opposite to said sensed acceleration forces.

2. The inertial actuator stabilizing system of claim 1 further comprising first and second position sensing windings located on opposite ends of said actuator guide, said position sensing windings supplying a current to said electronic means which produces a biasing current positioning said movable coil along said actuator guide.

3. The inertial actuator of claim 1 wherein said movable coil is disposed on a coil form which comprises an annular air plenum which connected to a source of air, and which discharges said air through a plurality of apertures facing said actuator guide, thereby forming an air bearing with said actuator guide.

4. The inertial actuator of claim 2 wherein said first and second position sensing windings are magnetically coupled with said movable coil, and differentially connected to provide a voltage having a magnitude and polarity which forces said movable coil to a central position along said actuator guide.

5. The inertial actuator of claim 2 further comprising a source of alternating current signal connected to said electronic means for providing a caging signal to said movable coil which is induced in said first and second position sensing windings.

6. The inertial actuator of claim 1 wherein said electronic means provides a low pass filter function for said accelerometer signal, having an 8th order filter function.

7. In a system for stabilizing a platform against acceleration forces applied to said platform, an inertial actuator comprising:

an actuator guide supported on said platform by first and second end pieces;

a plurality of rows of permanent magnets parallel to said actuator guide, and spaced apart therefrom along a common radius;

a movable coil having a plurality of windings coaxial to said actuator guide inside said common radius, said coil being freely slidable over said actuator guide in response to an electric current applied thereto; and

,

first and second position sensing coils on each end of said actuator guide, said sensing coils being connected together to provide a differential voltage having a polarity and magnitude proportional to the position of said movable coil.

8. The inertial actuator of claim 7 wherein said movable coil comprises:

an air plenum surrounding said actuator guide having an air inlet and a plurality of outlets facing said actuator guide, forming an air bearing with said actuator guide; and

,

a multi-turn winding wound about the exterior surface of said air plenum, having first and second ends adapted to receive said electric current.

9. The inertial actuator of claim 7 wherein said movable coil comprises:

a coil form surrounding said actuator guide, forming a sliding bearing with said actuator guide; and

,

a multi-turn winding surrounding said coil form, having first and second ends for receiving said current.

10. The inertial actuator of claim 7 wherein said first and second position sensing coils are magnetically coupled with said movable coil by said actuator guide.

11. The inertial actuator of claim 7 wherein each row of magnets comprises a linear array of a plurality of magnets parallel to the axis of said actuator guide.

12. An inertial actuator for generating a linear force comprising:

a cylindrical support having an axis aligned in a direction of a force to be generated;

a cylindrical coil form supported for sliding contact with said cylindrical support, said coil form including a coil winding having first and second ends, said first end in electrical contact with said cylindrical support;

a cylindrical brush coaxial with said support and coil form, having an inner surface in sliding contact with said coil winding second end;

a toroidal permanent magnet means having an axis coaxial with said cylindrical support, directing a magnetic flux through said coil; and

,

a cylindrical housing enclosing said cylindrical support, coil form and toroidal permanent magnet means, said housing being terminated at each end with first and second end pieces, forming a magnetic circuit with said cylindrical support and toroidal permanent magnet means.

13. An inertial actuator in accordance with claim 12 wherein said toroidal permanent magnet means comprises a plurality of toroidal magnets.

14. An inertial actuator in accordance with claim 12, further comprising position sensing means for determining the relative position of said cylindrical coil form and coil winding.

15. An inertial actuator in accordance with claim 14 wherein said position sensing means comprises first and second sensing windings at opposite ends of said cylindrical support differentially connected to provide a current proportional to the relative distance between said coil form and said ends of said cylindrical support.