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US4427388A Expired / Lapsed US ⏱️ 0.0 years remaining

Yoke mover

Assignee: United States Department of the Air Force
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Filing: 1982-08-11
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Granted: 1984-01-24
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Expires: 2002-08-11
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Abstract

Abstract A servomechanical controller for inputting prerecorded flight data to an aircraft flight simulator is provided which comprises a pair of servomotors operatively interconnected to a single output shaft connected to the flight simulator control wheel, one motor controlling simulated pitch to the wheel by imparting axial movement to the shaft, and the other motor controlling simulated roll by imparting rotation to the shaft, transducer means for sensing both angular and axial position of the shaft, and a force sensor for sensing torque and axial load on the shaft. The controller is configured for accepting analog or digital prerecorded electronic command inputs and translating those inputs to the flight simulator.

Inventors

  • 👤 Dana R. Hope

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 11:45
CPC Classifications
G; G09; G09B; G09B9/00; G09B9/02; G09B9/08; G09B9/28

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 194 words
A servomechanical controller for inputting electronically prerecorded commands to a flight simulator having a wheel and column type control, comprising: a. an output shaft operatively interconnected to said wheel to provide pitch control to said wheel in response to axial movement of said shaft, and roll control to said wheel in response to rotative movement of said shaft; b. first means, operatively interconnected to said shaft, to impart axial movement to said shaft in response to electronic inputs thereto; c. second means, operatively interconnected to said shaft to impart rotative movement to said shaft in response to electronic inputs thereto; d. first transducer means sensing the axial position of said shaft and providing an output signal thereof; e. second transducer means sensing the angular position of said shaft and providing an output signal thereof; f. a force sensor for sensing the torque and axial load on said shaft and providing output signals thereof; and g. electrical means operatively interconnecting said first means, second means, first and second transducer means, and force sensor for providing said electronic inputs to said first and second means in response to said electronically prerecorded commands and said output signals.
Claim 2
Dependent Claim 194 words
A servomechanical controller for inputting electronically prerecorded commands to a flight simulator having a wheel and column type control, comprising: a. an output shaft operatively interconnected to said wheel to provide pitch control to said wheel in response to axial movement of said shaft, and roll control to said wheel in response to rotative movement of said shaft; b. first means, operatively interconnected to said shaft, to impart axial movement to said shaft in response to electronic inputs thereto; c. second means, operatively interconnected to said shaft to impart rotative movement to said shaft in response to electronic inputs thereto; d. first transducer means sensing the axial position of said shaft and providing an output signal thereof; e. second transducer means sensing the angular position of said shaft and providing an output signal thereof; f. a force sensor for sensing the torque and axial load on said shaft and providing output signals thereof; and g. electrical means operatively interconnecting said first means, second means, first and second transducer means, and force sensor for providing said electronic inputs to said first and second means in response to said electronically prerecorded commands and said output signals.
Claim 3
Dependent Claim 17 words
The controller as recited in claim 1 wherein said first and second means comprises servo controlled motors.

References Cited (Backward Citations)

US3024539A Cited
US3496651A Cited
US3493906A Cited
US3601733A Cited
US4227319A Cited
US4236325A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-01-23 1987-07-25 1988-01-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-01-23 1991-07-25 1992-01-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-01-23 1995-07-25 1996-01-24 $7700.00 Window Closed / Lapsed

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