Directional gyro

• US 4,558,604 A
• Filed: 09/22/1982
• Issued: 12/17/1985
• Est. Priority Date: 02/02/1981
• Status: Expired due to Fees

• Current Assignee: TELDIX GmbH (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: TELDIX GmbH (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Auer, Werner
• Primary Examiner(s): Bonck, Rodney H.
• Application Number:
  US06/425,083
• Time in Patent Office: 1,182 Days
• Field of Search: 74/5.44, 74/5.45, 74/5.46, 74/5.5, 74/5.42, 74/5.9
• US Class Current: 74/5.44
• CPC Class Codes: G01C 19/34 for indicating a direction in the horizontal plane, e.g. directional gyroscopes
• CPC Class Codes: Y10T 74/1243 by weight
• CPC Class Codes: Y10T 74/1246 by friction
• CPC Class Codes: Y10T 74/1257 Damping
• CPC Class Codes: Y10T 74/1289 Horizontal gyroscopes

Abstract

The invention relates to a directional gyro having two mutually perpendicularly arranged gimbals. The first or outer gimbal is fastened to a frame by means of a trunnion having a perpendicular axis. This axis is provided with an angle pickup to determine the course angle. The second or inner gimbal is provided with a gyro motor comprising a stator and a rotor, with the rotor axis being held in a horizontal orientation by means of a verticality device. According to the invention, the verticality device comprises an element which displaces the center of gravity of the inner gimbal and is attached, for example, to this inner gimbal, and an element which damps the rotary movement about one of the gimbal axis and which is formed, for example, of a ball bearing subject to a defined friction or of a slip brush.

Claims

1. Directional gyro comprising:

a frame;

a first gimbal having a vertical axis and being mounted in said frame for rotation about said vertical axis;

a second gimbal having a precession axis which is perpendicular to said vertical axis and being mounted in said first gimbal for pivoting about said precession axis;

a gyro motor including a rotor having a spin axis, said gyro motor being mounted in said second gimbal with said spin axis being perpendicular to said precession axis;

a pickup means operatively associated with a said first gimbal for indicating an angle of rotation of said first gimbal relative to said frame; and

verticality means including a first means for displacing the center of gravity of said second gimbal to below said precession axis and a second means for damping the rotation of said first gimbal about said vertical said first and second means cooperating with each other to place said spin axis in a horizontal orientation.

2. Directional gyro according to claim 1, wherein said first means comprises a mass attached to said gimbal.

3. Directional gyro according to one of claims 1 and 2, wherein said second means comprises a bearing subject to a defined friction and positioned on said vertical axis.

4. Directional gyro according to one of claims 1 and 2, wherein said second means comprises a slip ring subject to a defined friction and positioned on said vertical axis.

5. Directional gyro according to claim 1, wherein said gyro is used for measuring changes in course within short periods of time.

6. Directional gyro according to claim 1, wherein said verticality means further includes third means for damping the pivoting of said second gimbal about said precession axis, said third means cooperating with said first and second means to place said spin axis in a horizontal position.

7. Directional gyro according to claim 6, wherein said third means comprises a bearing subject to a defined friction and positioned on said precession axis.

8. Directional gyro according to claim 6, wherein said third means comprises a slip ring subject to a defined friction and positioned on said precession axis.