US4425040A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Ring laser gyroscope cluster for strapped down navigation
Assignee: Kearfott Guidance and Navigation Corp
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Filing: 1981-01-29
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Granted: 1984-01-10
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Expires: 2001-01-29
Abstract
Abstract An inertial measurement unit using body dithered ring laser gyroscopes in which the individual ring laser gyroscopes are firmly attached to a common dithered structure and provisions made to cancel the reaction moment from the dithered structure by a passive resonator. The stable element, to which both the dithered structure and the passive resonator are attached with torsion springs, also serves as a non-vibrating foundation for strapped down accelerometers. The resulting structure contains fewer parts, has lower fabricating cost and permits a smaller package size than a conventional inertial measurement unit with individually body dithered ring laser gyroscopes.
Inventors
- 👤 Bo H. G. Ljung
- 👤 George R. Gamertsfelder
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 19:29
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/58; G01C19/64; G01C19/66; G01C19/68; G01C19/70
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
223 words
A ring laser gyroscope cluster for strapped down navigation comprising: a stable element having a dither axis; a common support structure having an axis of symmetry coaxial with the dither axis and having a rotationally symmetrical inner surface and having an outer surface adapted for orthogonally mounting first, second and third ring laser gyroscopes; first, second and third ring laser gyroscopes mounted to the outside of said support structure and peripherally spaced around the dither axis; first spring means mounting said common support structure to said stable element in a resilient manner and symmetrically disposed about the dither axis; and electromechanical transducer means for dithering said common support structure relative to said stable element, wherein said first, second and third gyroscopes have respectively first, second and third gyroscope axes of symmetry, said three gyroscope axes being peripherally spaced 120 degrees apart, and said three gyroscope axes being arranged to intersect the dither axis at a gyroscope common intersection point disposed axially outwardly of the common support structure, and said three gyroscope axes being disposed at the same angle to the dither axis, for rendering said ring laser gyroscopes insensitive to the differential thermal air currents, and for increasing the sensitivity of the combined output of the ring laser gyroscope cluster, and for ease of manufacture and overhaul of the ring laser gyroscope cluster.
Claim 2
Dependent Claim
223 words
A ring laser gyroscope cluster for strapped down navigation comprising: a stable element having a dither axis; a common support structure having an axis of symmetry coaxial with the dither axis and having a rotationally symmetrical inner surface and having an outer surface adapted for orthogonally mounting first, second and third ring laser gyroscopes; first, second and third ring laser gyroscopes mounted to the outside of said support structure and peripherally spaced around the dither axis; first spring means mounting said common support structure to said stable element in a resilient manner and symmetrically disposed about the dither axis; and electromechanical transducer means for dithering said common support structure relative to said stable element, wherein said first, second and third gyroscopes have respectively first, second and third gyroscope axes of symmetry, said three gyroscope axes being peripherally spaced 120 degrees apart, and said three gyroscope axes being arranged to intersect the dither axis at a gyroscope common intersection point disposed axially outwardly of the common support structure, and said three gyroscope axes being disposed at the same angle to the dither axis, for rendering said ring laser gyroscopes insensitive to the differential thermal air currents, and for increasing the sensitivity of the combined output of the ring laser gyroscope cluster, and for ease of manufacture and overhaul of the ring laser gyroscope cluster.
Claim 3
Dependent Claim
90 words
The arrangement and means according to claim 1, and further including a passive vibration damper resiliently coupled to said stable element, and wherein said damper comprises an inertial body and second spring means, and second spring means being connected to said inertial body and to said stable element, said inertial body and said second spring means each being symmetrically disposed about the dither axis, and wherein said damper is tuned to the dither frequency and has characteristics such as to cause said stable element to be at a neutral point.
Claim 4
Dependent Claim
95 words
The arrangement according to claim 1, and further including first, second and third accelerometers orthogonally mounted to said stable element, whereby said accelerometers will be at a neutral point, and wherein said first, second and third accelerometers have respectively first, second and third accelerometer axes of symmetry, said three accelerometer axes being peripherally spaced 120 degrees apart about the dither axis, and said three accelerometer axes being arranged to intersect the dither axis at an accelerometer common intersection point, and said three accelerometer axes each being disposed at the same angle to the dither axis.
Claim 5
Dependent Claim
63 words
The arrangement according to claim 1, and further including: non-compensating beam combiners associated with each of said ring laser gyroscopes; at least one compensating beam combiner associated with said gyroscopes; a dual photo detector associated with each beam combiner for sensing the outputs of said beam combiners; and means having as inputs the outputs of said photo detectors and providing three compensated outputs.
Claim 6
Dependent Claim
136 words
The arrangement according to claim 4, wherein said means provided comprise: (a) a first summing junction having as inputs the outputs of the photo detector associated with the compensated and uncompensated beam combiners of said first gyroscope, said compensated output providing the output for said first gyroscope and the output of said first summing junction providing a correction signal; (b) a second summing junction having as inputs said correction signal and the output from the photo detector associated with the uncompensated beam combiner of said second gyroscope, the output of said summing junction being the second gyroscope output; and (c) a third summing junction having as inputs the output of the photo detector associated with the uncompensated beam combiner of said third gyroscope and said correction signal and providing at its output, the third gyroscope output.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-01-09 | 1987-07-11 | 1988-01-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-01-09 | 1991-07-11 | 1992-01-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-01-09 | 1995-07-11 | 1996-01-10 | $7700.00 | Window Closed / Lapsed |