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US4361760A Expired / Lapsed US ⏱️ 0.0 years remaining

Two-degree-of-freedom gyro with radiant energy pickoffs

Assignee: United States Department of the Army
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Filing: 1980-10-29
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Granted: 1982-11-30
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Expires: 2000-10-29
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Abstract

Abstract A two-degree-of-freedom gyro that uses a combination of fiber optics and iant energy sensors for low torque gimbal/housing position sensors. The mode of operation of the gyro is a sustained rotor displacement type instrument. The radiant energy type pickoffs eliminate gimbal wiring, slip rings, and wiper environmental problems.

Inventors

  • 👤 Aubrey Rodgers

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 03:35
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/28; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1261; Y10T74/1264

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 217 words
A two-degree-of-freedom gyro utilizing transmitted/reflected radiant energy as wide angle pickoffs comprising: a. a housing; b. an outer gimbal carried in said housing, said outer gimbal having a pair of shafts extending from opposite sides thereof for support of said outer gimbal in said housing, the first of said pair of shafts being hollow, the second of said pair of shafts having a flat reflective surface thereon; c. an inner gimbal carried in said housing in concentric relation with said outer gimbal; d. a rotor carried in said inner gimbal, said rotor having a reflective/non-reflective pattern on the outer surface thereof; e. a first source of light for directing radiant energy against said flat surface of said shaft; f. detector means carried in said housing adjacent said flat surface of said shaft for receiving reflected radiant energy from said flat surface for providing a signal indicative of the position of said shaft relative to said housing; g. a second source of light for directing radiant energy against said reflective/non-reflective pattern; h. filter optics means carried in said hollow shaft for directing radiant energy from said second light source to said reflective/non-reflective pattern and for directing reflected radiant energy away from said reflective/non-reflective pattern; and i. sensor means for receiving said reflected radiant energy from said reflective/non-reflective pattern.
Claim 2
Dependent Claim 217 words
A two-degree-of-freedom gyro utilizing transmitted/reflected radiant energy as wide angle pickoffs comprising: a. a housing; b. an outer gimbal carried in said housing, said outer gimbal having a pair of shafts extending from opposite sides thereof for support of said outer gimbal in said housing, the first of said pair of shafts being hollow, the second of said pair of shafts having a flat reflective surface thereon; c. an inner gimbal carried in said housing in concentric relation with said outer gimbal; d. a rotor carried in said inner gimbal, said rotor having a reflective/non-reflective pattern on the outer surface thereof; e. a first source of light for directing radiant energy against said flat surface of said shaft; f. detector means carried in said housing adjacent said flat surface of said shaft for receiving reflected radiant energy from said flat surface for providing a signal indicative of the position of said shaft relative to said housing; g. a second source of light for directing radiant energy against said reflective/non-reflective pattern; h. filter optics means carried in said hollow shaft for directing radiant energy from said second light source to said reflective/non-reflective pattern and for directing reflected radiant energy away from said reflective/non-reflective pattern; and i. sensor means for receiving said reflected radiant energy from said reflective/non-reflective pattern.

References Cited (Backward Citations)

US2959060A Cited
US3277304A Cited
US3399347A Cited
US3328595A Cited
US3422686A Cited
US3499332A Cited
US3836260A Cited
US3915019A Cited
US3940609A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1985-11-29 1986-05-31 1986-11-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-11-29 1990-05-31 1990-11-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-11-29 1994-05-31 1994-11-30 $7700.00 Window Closed / Lapsed

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