Patent US4947697A successfully refreshed from Google Patents.
US4947697A
Expired / Lapsed
US
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System for measuring force versus position of a flight controller in an aircraft or flight simulator
Assignee: CAE Electronics Ltd
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Filing: 1989-06-28
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Granted: 1990-08-14
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Expires: 2009-06-28
Abstract
Abstract A six-axis force transducer is mounted on the flight controller and provides three independent orthogonal linear force components of the applied force and three independent orthogonal torque components of the applied force. Change in position is measured by a motorized spool connected to a high resolution shaft encoder. A small diameter thread is wound around the spool via a mechanically driven threading device. The free end of the thread is connected to a fixed point in the cockpit. The output of the transducer and the shaft encoder are fed to a microprocessor which calculates net force, in accordance with well known formula, and net position, from calibration data.
Inventors
- 👤 Robert W. Prentice
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 03:39
CPC Classifications
G; G01; G01L; G01L5/00; G01L5/16; G01L5/22; G01L5/223
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
81 words
A system for measuring the change in position, resulting from an applied force, of an aircraft or flight simulator flight controller, with respect to a fixed aircraft or flight simulator reference position; said system comprising: means for measuring said change in position; means for measuring said applied force comprising a six-axis force transducer to provide three independent orthogonal linear force components and three independent orthogonal torque components; and means for calculating the net applied force resulting from said six measured forces.
Claim 2
Independent Claim
81 words
A system for measuring the change in position, resulting from an applied force, of an aircraft or flight simulator flight controller, with respect to a fixed aircraft or flight simulator reference position; said system comprising: means for measuring said change in position; means for measuring said applied force comprising a six-axis force transducer to provide three independent orthogonal linear force components and three independent orthogonal torque components; and means for calculating the net applied force resulting from said six measured forces.
Claim 3
Dependent Claim
45 words
A system as defined in claim 1 wherein the output of said means for measuring said change in position is connected to said means for calculating, and wherein the output of said means for measuring said applied force is connected to said means for calculating.
Claim 4
Dependent Claim
30 words
A system as defined in claim 2 wherein said means for measuring said change and wherein said means for measuring said applied force are both mounted on said flight controller.
Claim 5
Dependent Claim
40 words
A system as defined in claim 3 wherein said means for measuring said change comprises a motorized spool connected to a high resolution shaft encoder; a small diameter thread being wound on said spool via a mechanically driven threading device.
Claim 6
Dependent Claim
30 words
A system as defined in claim 4 wherein the free end of said thread is connected to a fixed point in the cockpit of the aircraft or the flight simulator.
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) | 1993-08-13 | 1994-02-12 | 1994-08-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-08-13 | 1998-02-12 | 1998-08-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-08-13 | 2002-02-12 | 2002-08-14 | $7700.00 | Window Closed / Lapsed |