The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 10, 1984

Filed:

Mar. 25, 1982
Applicant:
Inventors:

Bernard J O'Connor, Eastchester, NY (US);

Joseph P Pierry, Park Ridge, NJ (US);

Michael J Lanni, Ridgewood, NJ (US);

Assignee:

The Bendix Corporation, Teterboro, NJ (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01C / ;
U.S. Cl.
CPC ...
33325 ; 33326 ;
Abstract

A gyrocompass has a gimbal (18;218) rotatable about an upright axis (22;222) and a gyro (10;210) rotatably mounted in this gimbal (18;218) about an inner axis (16;216) transverse to the upright axis (22;222). The gyrocompass also includes a level sensor (30,32;230,232) supported by the gimbal (18;218) for providing a level signal signifying the tilt of the upright axis (22;222) from vertical. Also included is a controller (50) connected to the level sensor (30,32;230,232). The controller includes equipment (50) responsive to the level signal for rotating the gimbal (18;218) into an initial position (SP(1)) at which the level signal has a predetermined value. A method employing the foregoing apparatus includes the steps of rotating the gimbal (18;218) until the level sensor (30,32;230,232) indicates the inner axis (16;216) is horizontal. Another step is measuring the torque applied to the gyroscope (10;210) by the horizontal component of rotation of the earth with the spin axis (SA1;SA) of the gyroscope (10;210) rotated about the inner axis (16;216) into a horizontal position. Other steps are rotating the gimbal (18;218) 180 degrees and remeasuring the torque applied to the gyroscope (10;210) by the horizontal component of rotation of the earth with the spin axis (SA1;SA) of the gyroscope (10;210) rotated about the inner axis (16;216) into a horizontal position.


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