US4651576A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Gyroscope having temperature controlling arrangement
Assignee: BAE Systems PLC
•
Filing: 1984-10-12
•
Granted: 1987-03-24
•
Expires: 2004-10-12
Abstract
Abstract Gyroscopes, particularly those with permanent magnet torquers, may be temperature sensitive. A temperature signal may be derived and used to correct the temperature dependent parameters such as gyro scale factor. Herein, instead of or in addition to such correction, it is proposed to regulate the gyro temperature by varying the torquer signals and hence controlling the power dissipated in the torquer coils. The torquer signals may comprise positive- and negative-going pulses of fixed amplitude and having respective durations appropriate to produce the required torquing effect. Then, the dissipated power can be controlled by varying the durations of the inter-pulse dead-zones.
Inventors
- 👤 Paul D. Luke
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 11:34
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/30; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1229; Y10T74/1232; Y10T74/125; Y10T74/1261; Y10T74/1279
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
80 words
A gyroscope comprising: a gyro wheel, at least one gyro rate feedback loop incorporating a permanent magnet torquer having torquer coils, and a magnet temperature regulating loop including means for deriving a signal indicative of the temperature of the torquer, and control means, connected to the temperature signal deriving means and said gyro rate feedback loop, for regulating the torquer temperature by varying the torque inducing signals fed to the torquer to vary the power dissipated in the torquer coils.
Claim 2
Dependent Claim
80 words
A gyroscope comprising: a gyro wheel, at least one gyro rate feedback loop incorporating a permanent magnet torquer having torquer coils, and a magnet temperature regulating loop including means for deriving a signal indicative of the temperature of the torquer, and control means, connected to the temperature signal deriving means and said gyro rate feedback loop, for regulating the torquer temperature by varying the torque inducing signals fed to the torquer to vary the power dissipated in the torquer coils.
Claim 3
Dependent Claim
114 words
Gyroscope apparatus comprising: a gyroscope including a gyro wheel, sensing means for sensing relative movement of the gyro wheel and the gyroscope, and permanent magnet torquer means for controlling said relative movement, a control circuit, connected to said sensing means and said torquer means, for supplying signals to drive the torquer means, said signals being positive-going and negative-going current pulses having a dead zone period therebetween and having respective durations controlled to vary the torque applied to the wheel, and temperature regulating means, connected to said control circuit, for forming a temperature signal indicative of the temperature of said torquer means and for controlling in dependence upon the said temperature signal the dead-zone period.
Claim 4
Dependent Claim
114 words
Gyroscope apparatus comprising: a gyroscope including a gyro wheel, sensing means for sensing relative movement of the gyro wheel and the gyroscope, and permanent magnet torquer means for controlling said relative movement, a control circuit, connected to said sensing means and said torquer means, for supplying signals to drive the torquer means, said signals being positive-going and negative-going current pulses having a dead zone period therebetween and having respective durations controlled to vary the torque applied to the wheel, and temperature regulating means, connected to said control circuit, for forming a temperature signal indicative of the temperature of said torquer means and for controlling in dependence upon the said temperature signal the dead-zone period.
References Cited (Backward Citations)
US3264528A
Cited
US3843945A
Cited
US3939403A
Cited
US4225812A
Cited
EP0009347A1
Cited
GB2117118A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-03-23 | 1990-09-22 | 1991-03-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-23 | 1994-09-22 | 1995-03-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-23 | 1998-09-22 | 1999-03-24 | $7700.00 | Window Closed / Lapsed |