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US5621171A Expired / Lapsed US ⏱️ 0.0 years remaining

Method for actively balancing a vibration structure gyroscope sensing element structure

Assignee: BAE Systems PLC
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Filing: 1996-04-05
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Granted: 1997-04-15
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Expires: 2016-04-05
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Abstract

Abstract A vibrating structure gyroscope sensing element structure of ring-like or substantially cylindrical form made of ferromagnetic material is actively balanced by applying a variable strength magnetic field across a predetermined section of the circumference of the sensing element structure differentially to shift the resonant frequency of one or the other of the primary and secondary vibration modes (1,2) thereof by an amount sufficient to bring the two mode resonant frequencies into balance.

Inventors

  • 👤 Christopher Fell

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-03 07:49
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/56; G01C19/567

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 75 words
A method for actively balancing a Vibrating Structure Gyroscope sensing element structure of ring-like or substantially cylindrical form made of ferromagnetic material, in which a variable strength magnetic field is applied across a predetermined section of the circumference of the sensing element structure differentially to shift the resonant frequency of one or the other of the primary and secondary vibration modes thereof by an amount sufficient to bring the two mode resonant frequencies into balance.
Claim 2
Independent Claim 75 words
A method for actively balancing a Vibrating Structure Gyroscope sensing element structure of ring-like or substantially cylindrical form made of ferromagnetic material, in which a variable strength magnetic field is applied across a predetermined section of the circumference of the sensing element structure differentially to shift the resonant frequency of one or the other of the primary and secondary vibration modes thereof by an amount sufficient to bring the two mode resonant frequencies into balance.
Claim 3
Dependent Claim 16 words
Method according to claim 1 in which the magnetic field is applied to the primary mode.
Claim 4
Dependent Claim 24 words
Method according to claim 2, in which the magnetic field applied reduces the mode resonant frequency of vibration in proportion to the field strength.

References Cited (Backward Citations)

US4951508A Cited
US4793195A Cited
GB2266588A Cited
US5445007A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 2000-04-14 2000-10-14 2001-04-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2004-04-14 2004-10-14 2005-04-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2008-04-14 2008-10-14 2009-04-15 $7700.00 Window Closed / Lapsed

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