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US4193059A Expired / Lapsed US ⏱️ 0.0 years remaining

Attitude indicator comparator warning system

Assignee: United States Department of the Air Force
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Filing: 1978-06-15
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Granted: 1980-03-11
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Expires: 1998-06-15
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Abstract

Abstract The indications of attitude indicators at two different indicating locations that are indicating the same parameter but actuated from different sources, are monitored for the same indication by electrically interconnecting two transolvers that are mechanically coupled to the respective attitude indicator at each location. A monitor, at one indicating location, furnishes the excitation for the transolver at the other location and by the magnitudes of the sine and cosine outputs of the local transolver furnishes flag indication of any system defects of either indicator at each location.

Inventors

  • 👤 Richard L. Harris

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 20:32
CPC Classifications
G; G08; G08C; G08C19/00; G08C19/38; G08C19/46

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 180 words
An attitude indicator comparator warning system comprising: a. a first attitude indicator indicating an attitude parameter, and having a motor drive actuated from a first sensing system; b. a second attitude indicator indicating the same attitude parameter, and having a motor drive actuated from a second sensing system; c. a first transolver having a stator winding and a rotor winding: d. a second transolver having a stator winding and a rotor winding; e. means for coupling the said rotor of the first transolver to the said motor drive in the said first attitude indicator; f. means for coupling the said rotor of the second transolver to the said motor drive of the said second attitude indicator; g. means for interconnecting the said stator winding of the first transolver with the said stator winding of the second transolver; and h. a comparator warning monitor providing excitation to the rotor of the said first transolver and cooperating with the rotor of the said second transolver and providing a flag output responsive to the output from the rotor of the said second transolver.
Claim 2
Dependent Claim 180 words
An attitude indicator comparator warning system comprising: a. a first attitude indicator indicating an attitude parameter, and having a motor drive actuated from a first sensing system; b. a second attitude indicator indicating the same attitude parameter, and having a motor drive actuated from a second sensing system; c. a first transolver having a stator winding and a rotor winding: d. a second transolver having a stator winding and a rotor winding; e. means for coupling the said rotor of the first transolver to the said motor drive in the said first attitude indicator; f. means for coupling the said rotor of the second transolver to the said motor drive of the said second attitude indicator; g. means for interconnecting the said stator winding of the first transolver with the said stator winding of the second transolver; and h. a comparator warning monitor providing excitation to the rotor of the said first transolver and cooperating with the rotor of the said second transolver and providing a flag output responsive to the output from the rotor of the said second transolver.
Claim 3
Dependent Claim 262 words
An attitude indicator comparator warning system for a first attitude indicator and a second attitude indicator, the said first and second attitude indicators indicating the same parameter and having indicator drive motors energized from separate sources and with each indicator having an electrically actuated flag indicator, the said warning system comprising: a. a first transolver coupled to the said motor drive of the said first attitude indicator and having an electrical excitation input and an electrical output; b. a second transolver coupled to the said motor drive of the said second attitude indicator and having an electrical input and a sine and cosine electrical output; c. means for interconnecting the said electrical output of the first transolver with the electrical input of the said second transolver; d. a comparator warning monitor having an excitation output, a sine input, a cosine input, and a flag excitation output; e. means for connecting the said excitation output from the said monitor to the said excitation input of the said first transolver; f. means for connecting the sine output from the said second transolver to the said sine input of the said monitor, and connecting the said cosine output from the said second transolver to the said cosine input of the said monitor; and g. means for connecting the said flag excitation output of the said monitor to the said electrically actuated flag indicator of both the said first and said second attitude indicators whereby the said flag indication is responsive to the said sine output and the said cosine output from the said second transolver.
Claim 4
Dependent Claim 262 words
An attitude indicator comparator warning system for a first attitude indicator and a second attitude indicator, the said first and second attitude indicators indicating the same parameter and having indicator drive motors energized from separate sources and with each indicator having an electrically actuated flag indicator, the said warning system comprising: a. a first transolver coupled to the said motor drive of the said first attitude indicator and having an electrical excitation input and an electrical output; b. a second transolver coupled to the said motor drive of the said second attitude indicator and having an electrical input and a sine and cosine electrical output; c. means for interconnecting the said electrical output of the first transolver with the electrical input of the said second transolver; d. a comparator warning monitor having an excitation output, a sine input, a cosine input, and a flag excitation output; e. means for connecting the said excitation output from the said monitor to the said excitation input of the said first transolver; f. means for connecting the sine output from the said second transolver to the said sine input of the said monitor, and connecting the said cosine output from the said second transolver to the said cosine input of the said monitor; and g. means for connecting the said flag excitation output of the said monitor to the said electrically actuated flag indicator of both the said first and said second attitude indicators whereby the said flag indication is responsive to the said sine output and the said cosine output from the said second transolver.
Claim 5
Dependent Claim 124 words
The warning system as claimed in claim 2 wherein the said first and second attitude indicators provide a trim adjustment and the said means for interconnecting the said electrical output of the said first transolver with the said electrical input of the said second transolver includes a first differential syncro electrically connected to the said first transolver output and a second differential syncro electrically connected to the said input of the second transolver and the said first differential syncro mechanically cooperating with the said trim adjustment of the first indicator and the said second differential syncro mechanically cooperating with the said trim adjustment of the second indicator, whereby differences in trim adjustment in the said first indicator and the said second indicator are compensated.
Claim 6
Dependent Claim 107 words
The warning system as claimed in claim 2 wherein the said first and second attitude indicators provide a trim adjustment and the said monitor provides a first trim adjustment input and a second trim adjustment input, the said attitude warning system including a first potentiometer cooperating mechanically with the first attitude indicator trim adjustment and electrically connected to the first trim adjustment input of the said monitor and a second potentiometer mechanically cooperating with the second attitude indicator trim adjustment and electrically connected to the second trim adjustment input of the said monitor, whereby differences in trim adjustment in the said first and second indicators are compensated.

References Cited (Backward Citations)

US2432772A Cited
US2428402A Cited
US2596698A Cited
US2794975A Cited
US2810119A Cited
US2950460A Cited
US3094691A Cited
US3534349A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-03-11 1983-09-10 1984-03-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-03-11 1987-09-10 1988-03-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-03-11 1991-09-10 1992-03-11 $7700.00 Window Closed / Lapsed

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