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US3883788A Expired / Lapsed US ⏱️ 0.0 years remaining

Gyroscope orientation controller

Assignee: Sperry Sun Well Surveying Co
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Filing: 1973-10-26
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Granted: 1975-05-13
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Expires: 1993-10-26
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Abstract

Abstract A gyroscope control system for maintaining a gyroscope rotor in a predetermined orientation utilizes the earth''s gravity vector as a reference. A gravity sensitive mercury switch is placed on the gyroscope''s rotor gimbal such that its conducting state changes when the rotor varies from the predetermined orientation. The mercury switch and a capacitor in series with the switch are connected into the rotor motor power circuit. The power circuit includes a power source that produces a square wave that acquires a ringing characteristic due to circuit impedance. The mercury switch switches the capacitor into the rotor motor circuit whenever the rotor varies from the predetermined location, thereby changing the amplitude of the ringing characteristic. An amplitude detection circuit measures the ringing amplitude and generates a control signal, which causes a reversible torque motor to re-orient the rotor.

Inventors

  • 👤 Jr Roy E Storey

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 17:03
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/30; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1229; Y10T74/1261

Claims Analysis

Total Claims: 29
Claim 1
Independent Claim 78 words
In a gyroscope for use in a borehole survey instrument, a rotor orienting system, comprising: means for providing to the gyroscope rotor motor a power signal having an impulse characteristic; means for producing a ringing characteristic in the power signal; means for varying the state of a parameter of the ringing characteristic; means for detecting the state of the parameter; and means for orienting the rotor in response to the state of the parameter of the ringing characteristic.
Claim 2
Dependent Claim 78 words
In a gyroscope for use in a borehole survey instrument, a rotor orienting system, comprising: means for providing to the gyroscope rotor motor a power signal having an impulse characteristic; means for producing a ringing characteristic in the power signal; means for varying the state of a parameter of the ringing characteristic; means for detecting the state of the parameter; and means for orienting the rotor in response to the state of the parameter of the ringing characteristic.
Claim 3
Dependent Claim 16 words
The system of claim 1 wherein the means for providing a power signal is a generator.
Claim 4
Dependent Claim 12 words
The system of claim 2 wherein the generator produces a square wave.
Claim 5
Dependent Claim 17 words
The system of claim 1 wherein the means for producing a ringing characteristic is an impedance load.
Claim 6
Dependent Claim 12 words
The system of claim 4 wherein the impedance load is a capacitor.
Claim 7
Dependent Claim 21 words
The system of claim 1 wherein the means for varying a parameter of the ringing characteristic is a variable resistor means.
Claim 8
Dependent Claim 13 words
The system of claim 6 wherein the variable resistor means is a switch.
Claim 9
Dependent Claim 12 words
The system of claim 7 wherein the switch is a mercury switch.
Claim 10
Dependent Claim 47 words
The system of claim 1 wherein the means for detecting the state of the parameter comprises: means for removing the ringing characteristic from the power signal; means for isolating the parameter from other parameters of the ringing characteristic; and means for measuring the state of the parameter.
Claim 11
Dependent Claim 22 words
The system of claim 9 wherein the means for removing the ringing characteristic from the power signal is a frequency sensitive filter.
Claim 12
Dependent Claim 16 words
The system of claim 10 wherein the frequency sensitive filter comprises: a transformer; and a capacitor.
Claim 13
Dependent Claim 15 words
The system of claim 9 wherein the means for isolating the parameter is a rectifier.
Claim 14
Dependent Claim 12 words
The system of claim 12 wherein the rectifier is a bridge rectifier.
Claim 15
Dependent Claim 19 words
The system of claim 9 wherein the means for measuring the state of the parameter is a level detector.
Claim 16
Dependent Claim 12 words
The system of claim 1 wherein the orienting means is a motor.
Claim 17
Dependent Claim 13 words
The system of claim 1 further including means for controlling the orienting means.
Claim 18
Dependent Claim 124 words
In a gyroscope, a rotor orienting system, comprising: a square wave power generator in circuit with the rotor motor; a capacitor in the power circuit, whereby a ringing characteristic, having an amplitude different from that which naturally occurs may be produced in the power signal; a mercury switch on the rotor gimbal and connected in series with the capacitor, whereby the amplitude of the ringing characteristic may be altered when the rotor changes orientation; a transformer in the power circuit; a filtering capacitor in circuit with the transformer; a bridge rectifier in circuit with the transformer; a level detector in circuit with the bridge rectifier; a motor controller in circuit with the bridge rectifier; and an orienting motor in circuit with the bridge rectifier.
Claim 19
Dependent Claim 124 words
In a gyroscope, a rotor orienting system, comprising: a square wave power generator in circuit with the rotor motor; a capacitor in the power circuit, whereby a ringing characteristic, having an amplitude different from that which naturally occurs may be produced in the power signal; a mercury switch on the rotor gimbal and connected in series with the capacitor, whereby the amplitude of the ringing characteristic may be altered when the rotor changes orientation; a transformer in the power circuit; a filtering capacitor in circuit with the transformer; a bridge rectifier in circuit with the transformer; a level detector in circuit with the bridge rectifier; a motor controller in circuit with the bridge rectifier; and an orienting motor in circuit with the bridge rectifier.
Claim 20
Dependent Claim 76 words
In a gyroscope for use in a borehole survey instrument, apparatus for produCing a datum on a square wave power signal to control the orientation of the rotor, comprising: an impedance load, whereby a ringing characteristic different from that which naturally occurs may be imposed on the square wave; and switch means in circuit with the impedance load, whereby the ringing characteristic of the square may be varied when the orientation of the rotor gimbal varies.
Claim 21
Dependent Claim 76 words
In a gyroscope for use in a borehole survey instrument, apparatus for produCing a datum on a square wave power signal to control the orientation of the rotor, comprising: an impedance load, whereby a ringing characteristic different from that which naturally occurs may be imposed on the square wave; and switch means in circuit with the impedance load, whereby the ringing characteristic of the square may be varied when the orientation of the rotor gimbal varies.
Claim 22
Dependent Claim 12 words
The apparatus of claim 18 wherein the impedance load is a capacitor.
Claim 23
Dependent Claim 13 words
The apparatus of claim 19 wherein the switch means is a mercury switch.
Claim 24
Dependent Claim 88 words
In a gyroscope for use in a borehole survey, instrument, a rotor tilt control system, comprising: a square wave power signal generator in circuit with the rotor motor; an impedance load in the power circuit, whereby a ringing characteristic may be imposed on the power signal; a directionally sensitive switch in circuit with the impedance load; a filter in the power circuit tuned to the frequency of the ringing characteristic; a voltage rectifier in circuit with the filter; and a voltage level detector in circuit with the rectifier.
Claim 25
Dependent Claim 88 words
In a gyroscope for use in a borehole survey, instrument, a rotor tilt control system, comprising: a square wave power signal generator in circuit with the rotor motor; an impedance load in the power circuit, whereby a ringing characteristic may be imposed on the power signal; a directionally sensitive switch in circuit with the impedance load; a filter in the power circuit tuned to the frequency of the ringing characteristic; a voltage rectifier in circuit with the filter; and a voltage level detector in circuit with the rectifier.
Claim 26
Independent Claim 61 words
A method of controlling the orientation of a gyroscope rotor whose motor is powered by a signal having an impulse characteristic, comprising the steps of: sensing variation of the rotor from a predetermined orientation; altering a parameter of a ringing characteristic in the power signal; and regulating the orientation of the rotor in response to the parameter of the ringing characteristic.
Claim 27
Independent Claim 61 words
A method of controlling the orientation of a gyroscope rotor whose motor is powered by a signal having an impulse characteristic, comprising the steps of: sensing variation of the rotor from a predetermined orientation; altering a parameter of a ringing characteristic in the power signal; and regulating the orientation of the rotor in response to the parameter of the ringing characteristic.
Claim 28
Independent Claim 66 words
A method of orienting a gyroscope rotor that is powered by a signal having an impulse characteristic, comprising the steps of: sensing variation of the rotor from a predetermined orientation; altering the amplitude of a ringing characteristic in the power signal in response to the variations; sensing the amplitude of the ringing characteristic; and precessing the rotor in response to the amplitude of the ringing characteristic.
Claim 29
Independent Claim 66 words
A method of orienting a gyroscope rotor that is powered by a signal having an impulse characteristic, comprising the steps of: sensing variation of the rotor from a predetermined orientation; altering the amplitude of a ringing characteristic in the power signal in response to the variations; sensing the amplitude of the ringing characteristic; and precessing the rotor in response to the amplitude of the ringing characteristic.

References Cited (Backward Citations)

US2625046A Cited
US3225229A Cited
US3375421A Cited
US3704406A Cited
US3704407A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-05-12 1978-11-11 1979-05-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-05-12 1982-11-11 1983-05-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-05-12 1986-11-11 1987-05-13 $7700.00 Window Closed / Lapsed

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