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US4568286A Expired / Lapsed US ⏱️ 0.0 years remaining

Flight simulator feel system

Assignee: BAE Systems PLC
•
Filing: 1984-10-03
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Granted: 1986-02-04
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Expires: 2004-10-03
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Abstract

Abstract Flight Simulator feel apparatus suitable for use with an elevator control column and a rudder bar is provided by a variably tensioned cable subjected to transverse deflection by movement of the control column or rudder bar as the case may be, whereby a variable control stiffness (feel) is achieved in a simple and effective manner.

Inventors

  • 👤 Donald J. Acklam

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 19:29
CPC Classifications
G; G09; G09B; G09B9/00; G09B9/02; G09B9/08; G09B9/28

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 101 words
Apparatus for applying a variable force to oppose movement of a member comprises, in combination, a fixed structure, an elongate tensioned element carried by the fixed structure having spaced end portions and an intermediate region therebetween, the intermediate region being capable of displacement away from a plane including the two end portions, means for providing a variable tension within the element by urging the end portions relatively apart, and engagement means being moveable with reference to the fixed structure in response to movement of said member and engaging the element intermediate its ends to thereby effect displacement away from said plane.
Claim 2
Dependent Claim 101 words
Apparatus for applying a variable force to oppose movement of a member comprises, in combination, a fixed structure, an elongate tensioned element carried by the fixed structure having spaced end portions and an intermediate region therebetween, the intermediate region being capable of displacement away from a plane including the two end portions, means for providing a variable tension within the element by urging the end portions relatively apart, and engagement means being moveable with reference to the fixed structure in response to movement of said member and engaging the element intermediate its ends to thereby effect displacement away from said plane.
Claim 3
Dependent Claim 59 words
Apparatus according to claim 1 wherein the variable tension providing means includes a lever arm pivoted to the fixed structure, one end portion of the tensioned element being carried by the lever arm and the other end portion being carried by the fixed structure, and tensioning means urging the lever arm such that tensioning within the element is effected.
Claim 4
Dependent Claim 24 words
Apparatus according to claim 2 wherein the tensioning means comprise a pneumatic actuator of the low friction diaphragm type carried by the fixed structure.
Claim 5
Dependent Claim 13 words
Apparatus according to claim 1 wherein said tensioned element is of flexible form.
Claim 6
Dependent Claim 60 words
Apparatus according to claim 1 wherein the moveable member comprises a control column pivoted to the fixed structure about an axis lying parallel to that plane including the two end portions of the tensioned element and the engagement means comprises a push pull rod lying generally normal to that plane and extending between the control column and the tensioned element.
Claim 7
Dependent Claim 55 words
Apparatus according to claim 4 wherein the moveable member comprises a control bar pivoted to the fixed structure about an axis lying within that plane including the two end portions of the tensioned element, and the engagement means comprise guide means for the tensioned element disposed remote from the axis carried by the control bar.
Claim 8
Dependent Claim 24 words
Apparatus according to claim 6 wherein the guide means comprise two pairs of rollers, the tension element extending between the rollers of each pair.
Claim 9
Dependent Claim 40 words
Apparatus according to claim 7 wherein the fixed structure includes rail means extending parallel to said plane on which the control bar can slide for adjustment purposes, the tension element itself sliding past the guide means as adjustment is effected.

References Cited (Backward Citations)

US2300004A Cited
US2514606A Cited
US2510174A Cited
US3517446A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-02-03 1989-08-05 1990-02-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-02-03 1993-08-05 1994-02-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-02-03 1997-08-05 1998-02-04 $7700.00 Window Closed / Lapsed

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