GB247265A - Gyroscope compasses - Google Patents
Gyroscope compassesInfo
- Publication number
- GB247265A GB247265A GB2666724A GB2666724A GB247265A GB 247265 A GB247265 A GB 247265A GB 2666724 A GB2666724 A GB 2666724A GB 2666724 A GB2666724 A GB 2666724A GB 247265 A GB247265 A GB 247265A
- Authority
- GB
- United Kingdom
- Prior art keywords
- coils
- phase
- axis
- compass
- casing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/34—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
- G01C19/38—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
Abstract
247,265. Swinburne, J. Aug. 17, 1925. Gyroscopic compasses. - In a compass with a balanced gyro - casing, controlled by a level or plummet the tilting of which relatively to the casing operates a relay y controlling means for exerting torques around both the horizontal and the vertical axes, the level &c. also controls a creeping gear for slowly applying a uni-diirectional torque which remains until it is reduced or removed by the resulting tilt of the casing. This creeping gear is employed to apply corrections for changes of latitude and may be applied to a compass having an horizontal axis, or to a compass in which the axis is maintained parallel to that of the earth. The Figures show the application of the invention to a compass of the latter type, the gyro-casing A being pivoted about an horizontal axis B in the plummet element C which is pivoted in the vertical ring G. Secured by arms T to the element C is a plummet H carrying coils I in a magnetic field J. When the coils move within the field a current is induced in them, and this induced current is utilized to operate the torque-applying means and the creeping gear as indicated in Fig. 4. The gyroscope is driven by two phase cuirrent : the coils J are in phase 1 and when' the coils I are displaced a pressure is induced in phase 2. The coils I are in series with coils K, L in the field of a magnet M which is excited by phase 2 so that the current through the coils K, L produces a torque around the horizontal axis. The coils I also supply current to one phase of a two-phase motor N, the other phase being excited so as to produce a torque about the vertical axis. The creeping gear is operated by a two-phase motor F also receiving current from the coils I and operating through reducing gear a pinion gearing with a rack secured to the casing A to vary slowly the tilt of the gyro-axis, equilibrium being reached when this axis is parallel to that of the earth. In the case of a compass in which the gyro-axis is horizontal, the motor F may operate a rheostat in order to vary continuously the current passing through one of the coils K, L.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2666724A GB247265A (en) | 1925-08-17 | 1925-08-17 | Gyroscope compasses |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2666724A GB247265A (en) | 1925-08-17 | 1925-08-17 | Gyroscope compasses |
Publications (1)
Publication Number | Publication Date |
---|---|
GB247265A true GB247265A (en) | 1926-02-18 |
Family
ID=10247260
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2666724A Expired GB247265A (en) | 1925-08-17 | 1925-08-17 | Gyroscope compasses |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB247265A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3254419A (en) * | 1962-10-31 | 1966-06-07 | Bendix Corp | Gyroscopic compass system |
US3596366A (en) * | 1967-01-13 | 1971-08-03 | Tokyo Keiki Seizosho Co Ltd | Gyroscopic instrument |
GB2222676A (en) * | 1988-09-07 | 1990-03-14 | Israel Aircraft Ind Ltd | Navigational gyroscope with mounting means |
-
1925
- 1925-08-17 GB GB2666724A patent/GB247265A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3254419A (en) * | 1962-10-31 | 1966-06-07 | Bendix Corp | Gyroscopic compass system |
US3596366A (en) * | 1967-01-13 | 1971-08-03 | Tokyo Keiki Seizosho Co Ltd | Gyroscopic instrument |
US3699657A (en) * | 1967-01-13 | 1972-10-24 | Tokyo Keiki Seizosho Co Ltd | Gyroscopic instrument |
GB2222676A (en) * | 1988-09-07 | 1990-03-14 | Israel Aircraft Ind Ltd | Navigational gyroscope with mounting means |
US5074159A (en) * | 1988-09-07 | 1991-12-24 | Israel Aircraft Industries Ltd. | Gyroscopic sensor lock for navigation apparatus |
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