Azimuth determining gyroscope

• US 4,503,718 A
• Filed: 04/02/1982
• Issued: 03/12/1985
• Est. Priority Date: 04/02/1982
• Status: Expired due to Fees

• Current Assignee: Loral Corporation (Newell Brands Inc.)
• Original Assignee: Sperry Corporation (Unisys Corporation)
• Inventors: Quermann, Thomas R.
• Primary Examiner(s): Bonck, Rodney H.
• Application Number:
  US06/365,052
• Time in Patent Office: 1,075 Days
• Field of Search: 74/5.46, 74/5.5, 74/5.6 E, 74/5.8, 74/5.41
• US Class Current: 74/5.46
• CPC Class Codes: G01C 19/38 with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
• CPC Class Codes: Y10T 74/125 by magnetic field
• CPC Class Codes: Y10T 74/1257 Damping
• CPC Class Codes: Y10T 74/1279 Electrical and magnetic
• CPC Class Codes: Y10T 74/1286 Vertical gyroscopes

Abstract

In an azimuth determining gyroscope, a mechanically balanced gimbal is suspended from a fixed case by a wire which passes through the generally tubular upper portion of the suspended gimbal. A spin motor and a wheel for rotating about a vertical axis are coupled to the lower portion of the suspended gimbal. The upper portion of the suspended gimbal has pickoff and torquer coils for measuring the position of the suspended gimbal with respect to the fixed case and for providing torque to the suspended gimbal. Leads to the spin motor are configured to act as azimuth restraint means between the suspended gimbal and the fixed case.

Claims

1. A gyroscope comprising:

a case;

mechanically balanced gimbal means having lower and upper surfaces;

means for suspending said gimbal means from said case;

a spin motor, coupled to said lower surface of said gimbal means, having a wheel coupled thereto for spinning about a vertical axis, and

means, coupled to said upper surface of said gimbal means, for measuring positions of said gimbal means with respect to said case and for providing torque to said gimbal means to precess said wheel, said measuring and torqueing means including;

a plurality of pickoff and torquer coil pairs disposed along orthogonal axes of said measuring and torqueing means; and

a plurality of plates, having magnets disposed therebetween coupled to said upper surface of said gimbal in a cooperating relationship with said pickoff and torquer coil pairs.

2. A gyroscope according to claim 1 further including means for restraining said gimbal.

3. A gyroscope according to claim 2 wherein said restraint means includes:

a plurality of terminals attached to said case and said gimbal means;

a plurality of flexible conductors coupling said terminals on said case to said terminals on said gimbal means; and

a rigid frame coupled to said conductors.

4. A gyroscope according to claim 3 wherein said restraint means further includes means for applying tension to said conductors.

5. A gyroscope according to claim 3 or 4 wherein each torquer coil is responsive to output signals from said pickoff coil paired therewith.

6. The gyroscope according to claim 5 further including means for reversing rotation direction of said spin motor.

7. A gyroscope according to claim 6 further including means for integrating output signals of said torquer coils and said pickoff coils.

8. A gyroscope according to claim 7 further including means for dividing said integrated output signals of said integrating means to obtain a ratio representative signal of integrated output signals.

9. A gyroscope according to claim 8 further including means responsive to said ratio representative signal for providing an angle representative signal.