Patent US3913406A successfully refreshed from Google Patents.
US3913406A
Expired / Lapsed
US
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Digital pulse rebalance accelerometer
Assignee: United States Department of the Army
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Filing: 1973-08-02
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Granted: 1975-10-21
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Expires: 1993-08-02
Abstract
Abstract The pulse rebalance accelerometer is an acceleration sensing device for measuring vehicle motion and includes a free floating proof mass which is rotated or spun on the acceleration sensitive axis. The proof mass is rotated on hydrodynamic bearings which provide frictionless support for axial motion of the mass. A capacitance type pickoff is located at each end of the rotation shaft and sense displacement of the proof mass, thereby controlling the amount of electrical pulses which feed into torquers to restore the proof mass to the center position. The amount of pulses required to restore the proof mass is proportional to the magnitude of the applied acceleration.
Inventors
- 👤 James V Johnston
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 14:48
CPC Classifications
G; G01; G01P; G01P15/00; G01P15/02; G01P15/08; G01P15/13; G01P15/132
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
349 words
A digital pulse rebalance accelerometer for measuring acceleration of a body and comprising: a housing assembly having an elongated inner cylindrical chamber, a primary motor winding disposed around a portion of the inner wall of the chamber for developing a rotational electromagnetic field across said chamber, rotor means having a longitudinal axis coaxial with said chamber and disposed within said chamber for unencumbered rotation and translation, an air gap encompassing said rotor for isolating said rotor from surrounding housing structure, a hysteresis motor ring disposed around a central portion of said rotor and disposed within the plane of said rotationaL electromagnetic field for rotating said rotor, first and second split cup, capacitive, pick-offs encompassing respective first and second end portions of said rotor for responding to changes in capacitance at respective rotor ends, first and second torque coils adjacent respective pick-offs and disposed around the inner annular surface of the chamber encompassing a portion of said rotor for coupling electromagnetic energy to respective ends of said rotor, said rotor being constrained only by the hydrodynamic air gap and electromagnetic forces, said rotor ends having, respectively, a magnetic metal ring forming the terminal end portion for changing the capacitance of said split cups in response to longitudinal motion of the rotor and for providing motor restoration forces in response to electromagnetic energy coupled through said torque coils, a power supply for activating said primary motor winding and thereby imparting rotation to the rotor, differential means coupled to said first and second capacitance pick-off cups for providing differential output pulses in proportion to change in capacitance at the rotor ends indicative of changes in velocity of the housing assembly, a first oscillator and clipper amplifier serially connected between said first capacitive cups and said differential means, a second oscillator and clipper amplifier serially connected between said second capacitive cups and said differential means; and wherein said first clipper amplifier has an output coupled to said second torque coil for coupling electromagnetic energy thereto, and said second amplifier has an output coupled to said first torque coil for coupling energy pulses thereto.
Claim 2
Dependent Claim
349 words
A digital pulse rebalance accelerometer for measuring acceleration of a body and comprising: a housing assembly having an elongated inner cylindrical chamber, a primary motor winding disposed around a portion of the inner wall of the chamber for developing a rotational electromagnetic field across said chamber, rotor means having a longitudinal axis coaxial with said chamber and disposed within said chamber for unencumbered rotation and translation, an air gap encompassing said rotor for isolating said rotor from surrounding housing structure, a hysteresis motor ring disposed around a central portion of said rotor and disposed within the plane of said rotationaL electromagnetic field for rotating said rotor, first and second split cup, capacitive, pick-offs encompassing respective first and second end portions of said rotor for responding to changes in capacitance at respective rotor ends, first and second torque coils adjacent respective pick-offs and disposed around the inner annular surface of the chamber encompassing a portion of said rotor for coupling electromagnetic energy to respective ends of said rotor, said rotor being constrained only by the hydrodynamic air gap and electromagnetic forces, said rotor ends having, respectively, a magnetic metal ring forming the terminal end portion for changing the capacitance of said split cups in response to longitudinal motion of the rotor and for providing motor restoration forces in response to electromagnetic energy coupled through said torque coils, a power supply for activating said primary motor winding and thereby imparting rotation to the rotor, differential means coupled to said first and second capacitance pick-off cups for providing differential output pulses in proportion to change in capacitance at the rotor ends indicative of changes in velocity of the housing assembly, a first oscillator and clipper amplifier serially connected between said first capacitive cups and said differential means, a second oscillator and clipper amplifier serially connected between said second capacitive cups and said differential means; and wherein said first clipper amplifier has an output coupled to said second torque coil for coupling electromagnetic energy thereto, and said second amplifier has an output coupled to said first torque coil for coupling energy pulses thereto.
Claim 3
Dependent Claim
29 words
An accelerometer as set forth in claim 1 and further comprising a crystal oscillator coupled to said first and second variable oscillator for providing a fundamental oscillating frequency thereto.
References Cited (Backward Citations)
US2869851A
Cited
US2591921A
Cited
US3109310A
Cited
US3132520A
Cited
US3111036A
Cited
US3068704A
Cited
US3175404A
Cited
US3558946A
Cited
US3702073A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1978-10-20 | 1979-04-21 | 1979-10-21 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1982-10-20 | 1983-04-21 | 1983-10-21 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1986-10-20 | 1987-04-21 | 1987-10-21 | $7700.00 | Window Closed / Lapsed |