Electrostatic rate gyroscope

• US 4,061,043 A
• Filed: 03/29/1976
• Issued: 12/06/1977
• Est. Priority Date: 03/29/1976
• Status: Expired due to Term

• Current Assignee: Kearfott Guidance and Navigation Corporation
• Original Assignee: John Callender Stiles
• Inventors: Stiles, John Callender
• Primary Examiner(s): Scott, Samuel
• Assistant Examiner(s): Ferrell, Don E.
• Application Number:
  US05/671,257
• Time in Patent Office: 617 Days
• Field of Search: 74/5, 74/5 R, 74/5 F, 74/5.1, 74/5.37, 74/5.4, 74/5.41, 74/5.42, 74/5.5, 74/5.6 A, 74/5.6 B, 74/5.6 C, 74/5.6 D, 74/5.6 E, 74/5.6 R, 74/5. 7
• US Class Current: 74/5.60D
• CPC Class Codes: G01C 19/16 Suspensions; Bearings
• CPC Class Codes: G01C 19/24 using magnetic or electrostatic fields
• CPC Class Codes: G01C 19/28 Pick-offs, i.e. devices for taking-off an indication of the displacement of the rotor axis
• CPC Class Codes: G01C 19/42 for indicating rate of turn; for integrating rate of turn
• CPC Class Codes: Y10T 74/12 Gyroscopes
• CPC Class Codes: Y10T 74/1236 by plural diverse forces
• CPC Class Codes: Y10T 74/1275 Electrical
• CPC Class Codes: Y10T 74/1286 Vertical gyroscopes

Abstract

A two-axis rate gyroscope of the captured type is provided having a cylindrical rotor with one or more inwardly projecting flanges. The rotor is disposed within a sealed toroidal cavity in a rotor housing and the interior of the cavity is evacuated to a "hard" vacuum. An electrostatic suspension system restrains the rotor from translatory movement along the gyroscope spin axis and two axes perpendicular thereto so that a virtually frictionless spin bearing is provided for the rotor. The suspension system functions to prevent relative angular rotation between the rotor and the rotor housing about two precession axes. The rotor housing is mounted on a flexure joint which prevents translatory movement of the housing along three orthogonal axes but permits rotational movement of the housing about the two precession axes. Vibrating beam force transducer means exert a reaction force on the housing which prevents rotation of the housing about the two precession axes in response to input rates applied to the gyroscope, so that the electrical output signals of the transducer means are a function of the input rates applied to the gyroscope. The rotor housing, flexure joint, rotor and vibrating beam force transducers are disposed within a sealed casing which may be evacuated separately from the toroidal cavity within the rotor housing, so that the toroidal cavity may be easily evacuated to the higher degree of vacuum required for a frictionless rotor spin bearing. The cylindrical rotor structure permits the use of a simplified electrostatic suspension system in which the suspension electrodes also function as rotor displacement sensing electrodes.

Claims

1. A gyroscope having a spin axis and at least one input axis comprising

a rotor housing having a toroidal cavity therein concentrically disposed about said spin axis;

mounting means for mounting said rotor housing to permit rotation thereof about at least one precession axis;

a rotor having a cylindrical body portion with projecting flange means thereon concentrically disposed within said cavity about said spin axis;

electrostatic suspension means for suspending said rotor within said cavity to permit rotor rotation about said spin axis and to prevent relative angular rotation between said housing and said rotor about said one precession axis, so that said housing rotates with said rotor about said precession axis in response to an input rate applied to said input axis; and

force transducer means coupled to said housing for exerting a force on said housing to prevent rotation thereof about said precession axis and for producing an output signal in response to said force, whereby said output signal is responsive to said applied input rate.

2. A gyroscope as claimed in claim 1 wherein said force tranducer means comprises vibrating beam force transducer means of the type having at least one resonator beam which produces an electrical output signal having a frequency which is a function of the mechanical stress produced in said resonator beam by the force being sensed.

3. A gyroscope as claimed in claim 2 wherein said toroidal cavity is a sealed evacuable cavity adapted to be evacuated to a high degree of vacuum.

4. A gyroscope as claimed in claim 3 wherein said rotor housing and said vibrating beam force transducer means are disposed within a sealed evacuable casing which is adapted to be evacuated separately from said sealed toroidal cavity.

5. A gyroscope as claimed in claim 4 wherein

said casing is made of a non-electrically conductive and non-magnetic material,

said rotor has at least the surface thereof formed of an electrically conductive material, and

means are mounted exteriorly of said casing for generating a rotating magnetic field within said rotor housing about said spin axis to induce eddy currents in said rotor and produce rotor spin torque.

6. A gyroscope as claimed in claim 1 wherein

at least a portion of the surface areas of sid rotor body portion and flange means comprise electrically conductive material, and

said electrostatic suspension means comprises

displacement sensing means for sensing the displacement of said rotor from a null position within said cavity, and

suspension electrode means responsive to the output of said displacement sensing means for exerting an electrostatic force on said rotor to return said rotor to said null position.

7. A gyroscope as claimed in claim 6 wherein said suspension electrode means comprise suspension electrodes disposed on the walls of said rotor housing defining said cavity.

8. A gyroscope as claimed in claim 7 wherein said suspension electrodes comprise

a first set of radially disposed suspension electrodes located on the housing cavity wall adjacent one side of said rotor flange means,

a second set of radially disposed suspension electrodes located on the housing cavity wall adjacent the other side of said rotor flange means in radial alignment with the electrodes of said first set, so that the electrodes of said second set cooperate with the electrodes of said first set to form radially disposed electrode pairs which control translatory movement of said rotor along said spin axis and relative angular rotation between said housing and said rotor about two perpendicular axes which are each perpendicular to said spin axis, and

a third set of radially disposed suspension electrodes located on the housing cavity wall adjacent said rotor body portion, the electrodes of said third set cooperating with each other to form radially disposed electrode pairs with the electrodes of each such pair being located on diametrically opposite sides of said rotor, so that said third set of electrodes controls translatory movement of said rotor along said two perpendicular axes.

9. A gyroscope as claimed in claim 8 wherein said displacement sensing means comprise a separate rotor displacement sensing circuit for each of said radially disposed electrode pairs, said rotor displacement sensing circuit comprising

a capacitance bridge detector circuit having two of the arms thereof formed by the capacitances between said rotor and the pair of suspension electrodes associated with the sensing circuit,

means for coupling said bridge circuit to an alternating current source for energization thereby, so that the output of said bridge circuit is an amplitude modulated alternating current signal having an amplitude and phase respectively representing the magnitude and direction of the rotor displacement from said null position with respect to said associated pair of suspension electrodes, and

detector demodulator circuit means having an input coupled to the output of said bridge circuit and an output coupled across said associated pair of suspension electroes for demodulating said bridge circuit output signal to produce a direct current control signal for said associated electrode pair having a magnitude and polarity to return the rotor to said null position.

10. A gyroscope as claimed in claim 1 wherein said rotor flange means comprise first and second annular flanges projecting from opposite ends of said rotor body portion, each of said flange means being substantially perpendicular to said rotor body portion so that said rotor has a substantially C-shaped cross-sectional area.

11. A gyroscope as claimed in claim 10 wherein said toroidal cavity has a substantially rectangular cross-sectional area.

12. A gyroscope as claimed in claim 1 wherein said rotor flange means comprises an annular flange projecting from the central portion of said rotor body portion, said flange being substantially perpendicular to said rotor body portion so that said rotor has a substantially T-shaped cross-sectional area.

13. A gyroscope as claimed in claim 12 wherein said toroidal cavity has a substantially T-shaped cross-sectional area.

14. A gyroscope as claimed in claim 1 wherein

said mounting means comprises a support rod extending along said spin axis and having a necked-down portion of gradually decreasing circular cross-sectional area to form a flexure joint hving two degrees of rotational freedom about axes perpendicular to said spin axis,

said rotor housing is fixedly mounted on one end of said support rod, and

the center-of-gravity of said rotor housing and rotor lies in said flexure joint. formed of an electrically conductive material, and

means are mounted exteriorly of said casing for generating a rotating magnetic field within said rotor housing about said spin axis to induce eddy currents in said rotor and produce rotor spin torque.

15. A gyroscope having a spin axis and two input axes comprising

a rotor housing having a sealed evacuable toroidal cavity therein;

means for mounting the rotor housing with said cavity concentrically disposed about the spin axis and oriented in the plane defined by said input axes, said mounting means having two degrees of freedom to permit rotation of said housing about both of the gyroscope precession axes;

a rotor having a cylindrical body portion concentrically disposed within said cavity about the spin axis and annular flange means projecting from said body portion, said flange means being substantially perpendicular to said body portion;

electrostatic suspension means comprising a plurality of suspension electrodes disposed on the walls of said cavity adjacent said rotor body portion and flange means for suspending said rotor within said cavity to permit rotor rotation about said spin axis and prevent relative angular rotation between said housing and said rotor about said precession axes, so that the housing rotates with the rotor about said precession axes in response to input rates applied to said input axes; and

vibrating beam force transducer means connected to said housing for exerting a restraining force thereon to prevent housing rotation about said precession axes, said transducer means being of the type having at least one resonator beam which produces an electrical output signal having a frequency which is a function of the mechanical stress produced in the beam by the reaction force exerted by the transducer means.

16. A gyroscope as claimed in claim 15 wherein said rotor housing comprises a wheel-like structure having

a central hub portion connected to said mounting means for support thereby,

an annular rim portion concentrically disposed about said hub portion and containing said toroidal cavity, and

a plurality of support arms interconnecting said rim portion and said hub portion.