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US4316394A Expired / Lapsed US ⏱️ 0.0 years remaining

Magnetically suspended free rotor gyroscope

Assignee: Honeywell Inc
•
Filing: 1980-02-11
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Granted: 1982-02-23
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Expires: 2000-02-11
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Abstract

Abstract A gyro rotor is freely suspended in a housing for simultaneous rotation about a spin axis and a pair of precession axes in turn orthogonal to the spin axis, by a pair of magnetic suspensions spaced along the spin axis. Each magnetic suspension comprises a magnetically permeable stator member and a cooperative magnetically permeable rotor member relatively arranged so as to define axially spaced annular magnetically permeable gaps. Each magnetic suspension includes a permanent magnet for producing a fixed or passive magnetic flux in each gap and an electromagnet coil for producing a controllable or active magnetic flux in each gap. The passive flux provides passive stabilized suspension of the rotor parallel to two of said axes, while the active flux provides active stabilized suspension of the rotor parallel to the third of said axes using a closed servo loop. The ratio of the axial distance between the annular magnetic gaps to the diameter thereof is such that the rotor tends to maintain its position upon tilt thereof; that is, the gyro exhibits substantially zero restoring spring rates about its sensing axes. By means of closed loop servo techniques including angular pick-offs and torquers, measures of rates of turn are provided in terms of torquer currents required to maintain the angular pick-off outputs at null values.

Inventors

  • 👤 James R. Dohogne

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 02:16
CPC Classifications
F; F16; F16C; F16C32/00; F16C32/04; F16C32/0406; F16C32/044; G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/16; G01C19/24; G01C19/28; F16C2370/00; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1229; Y10T74/1232; Y10T74/125; Y10T74/1261; Y10T74/1279

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 272 words
A free rotor gyroscopic rate sensor comprising: housing means having a housing axis, generally cylindrically rotor means adapted to spin about a spin axis in said housing normally coincident with said housing axis, magnetic suspension means coupled between said housing means and said rotor means for contactlessly suspending said rotor means in said housing means with said rotor axis normally coincident with said housing axis, said magnetic suspension means comprising, at least one pair of axially spaced magnetic flux gaps formed by at least one pair of magnetically permeable pole pieces on said housing means radially spaced from said spin axis and a cooperating pair of correspondingly axially and radially spaced pole pieces on said rotor means, and means for producing passive and active magnetic fluxes between said pole pieces, said active and passive magnetic fluxes supporting said rotor means in unstable equilibrium in a first direction relative to said spin axis and said passive magnetic flux supporting said rotor means in stable equilibrium in a second direction relative to said spin axis at right angles to said first direction, motive means coupled between said housing and rotor means for spinning said rotor means about said spin axis, the mean axial distance between said axially spaced gaps bearing a predetermined ratio to the mean radius of said spaced gaps, such that in response to relative tilting of said rotor spin axis and said housing means, the passive magnetic flux force tending to retain said rotor means in stable equilibrium in said second direction is substantially balanced by the passive magnetic flux force tending to destabilize said unstable equilibrium in said first direction.
Claim 2
Dependent Claim 272 words
A free rotor gyroscopic rate sensor comprising: housing means having a housing axis, generally cylindrically rotor means adapted to spin about a spin axis in said housing normally coincident with said housing axis, magnetic suspension means coupled between said housing means and said rotor means for contactlessly suspending said rotor means in said housing means with said rotor axis normally coincident with said housing axis, said magnetic suspension means comprising, at least one pair of axially spaced magnetic flux gaps formed by at least one pair of magnetically permeable pole pieces on said housing means radially spaced from said spin axis and a cooperating pair of correspondingly axially and radially spaced pole pieces on said rotor means, and means for producing passive and active magnetic fluxes between said pole pieces, said active and passive magnetic fluxes supporting said rotor means in unstable equilibrium in a first direction relative to said spin axis and said passive magnetic flux supporting said rotor means in stable equilibrium in a second direction relative to said spin axis at right angles to said first direction, motive means coupled between said housing and rotor means for spinning said rotor means about said spin axis, the mean axial distance between said axially spaced gaps bearing a predetermined ratio to the mean radius of said spaced gaps, such that in response to relative tilting of said rotor spin axis and said housing means, the passive magnetic flux force tending to retain said rotor means in stable equilibrium in said second direction is substantially balanced by the passive magnetic flux force tending to destabilize said unstable equilibrium in said first direction.
Claim 3
Dependent Claim 37 words
Apparatus as defined in claim 1 further comprising, pick-off means for sensing and providing a signal proportional to said relative tilt, and torquer means responsive to said tilt signal tending to reduce said tilt signal to zero.
Claim 4
Dependent Claim 51 words
Apparatus as defined in claim 2 wherein said predetermined ratio is defined as: ##EQU7## where L=the mean effective axial distance between said magnetic gaps, R=the mean effective radius of said magnetic gaps, K u =the magnetic stiffness in said first direction, and K r =the magnetic stiffness in said second direction.
Claim 5
Dependent Claim 16 words
Apparatus as described in claim 3 wherein said predetermined ratio is on the order of 2:1.
Claim 6
Dependent Claim 35 words
Apparatus set forth in claim 1 wherein said active magnetic fluxes stabilize said rotor means in said gaps in an axial direction and said passive magnetic fluxes stabilize said rotor means in said radial direction.
Claim 7
Dependent Claim 34 words
Apparatus as set forth in claim 1 wherein said active magnetic fluxes stabilize said rotor means in a radial direction and where said passive magnetic fluxes stabilize said rotor means in an axial direction.
Claim 8
Dependent Claim 209 words
A free rotor gyroscopic rate sensor including: housing means having a housing axis, generally cylindrical rotor means having a spin axis normally coincident with said housing axis, magnetic suspension means for suspending said rotor means in normally non-contacting relation within said housing means and including: at least one pair of annular, axially spaced magnetic flux gaps formed between a first pair of annular magnetically permeable pole pieces on said housing and a corresponding second pair of cooperating pole pieces on said rotor, means for producing passive magnetic fluxes between said first and second pair of magnetically permeable pole pieces and for producing destabilizing and stabilizing forces on said rotor means in axial and radial directions, respectively, and motive means for spinning said rotor means with respect to said housing means normally about said housing axis, the mean effective axial distance between said axially spaced gaps having a predetermined ratio to the mean effective radius of said spaced gaps such that, in response to tilting of said rotor means spin axis relative to said housing axis, the passive magnetic forces tending to stabilize said rotor means radially of said spin axis are substantially balanced by the passive magnetic forces tending to destabilize said rotor means axially of said spin axis.
Claim 9
Dependent Claim 209 words
A free rotor gyroscopic rate sensor including: housing means having a housing axis, generally cylindrical rotor means having a spin axis normally coincident with said housing axis, magnetic suspension means for suspending said rotor means in normally non-contacting relation within said housing means and including: at least one pair of annular, axially spaced magnetic flux gaps formed between a first pair of annular magnetically permeable pole pieces on said housing and a corresponding second pair of cooperating pole pieces on said rotor, means for producing passive magnetic fluxes between said first and second pair of magnetically permeable pole pieces and for producing destabilizing and stabilizing forces on said rotor means in axial and radial directions, respectively, and motive means for spinning said rotor means with respect to said housing means normally about said housing axis, the mean effective axial distance between said axially spaced gaps having a predetermined ratio to the mean effective radius of said spaced gaps such that, in response to tilting of said rotor means spin axis relative to said housing axis, the passive magnetic forces tending to stabilize said rotor means radially of said spin axis are substantially balanced by the passive magnetic forces tending to destabilize said rotor means axially of said spin axis.
Claim 10
Dependent Claim 146 words
A free rotor gyroscope rate sensor including: housing means having a housing axis, generally cylindric rotor means having a spin axis normally coincident with said housing means axis, magnetic suspension means for suspending said rotor means in normally non-contacting relation within said housing means and including: a first pair of annular magnetically permeable pole pieces on said housing means, and a second pair of annular magnetically permeable pole pieces on said rotor means, said first and second pairs of annular magnetically permeable pole pieces forming annular spaced apart gaps, the mean effective axial distance between said annular spaced apart gaps having a predetermined ratio to the mean effective radius of said annular spaced apart gaps such that the relative magnetic stiffnesses in the axial and radial direction across said gaps balance each other upon relative angular rotations of said rotor means normal to said spin axis.
Claim 11
Dependent Claim 146 words
A free rotor gyroscope rate sensor including: housing means having a housing axis, generally cylindric rotor means having a spin axis normally coincident with said housing means axis, magnetic suspension means for suspending said rotor means in normally non-contacting relation within said housing means and including: a first pair of annular magnetically permeable pole pieces on said housing means, and a second pair of annular magnetically permeable pole pieces on said rotor means, said first and second pairs of annular magnetically permeable pole pieces forming annular spaced apart gaps, the mean effective axial distance between said annular spaced apart gaps having a predetermined ratio to the mean effective radius of said annular spaced apart gaps such that the relative magnetic stiffnesses in the axial and radial direction across said gaps balance each other upon relative angular rotations of said rotor means normal to said spin axis.
Claim 12
Dependent Claim 13 words
Apparatus as described in claim 8 wherein said predetermined ratio is substantially 2:1.

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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) 1985-02-22 1985-08-24 1986-02-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1989-02-22 1989-08-24 1990-02-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1993-02-22 1993-08-24 1994-02-23 $7700.00 Window Closed / Lapsed

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