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US3826575A Expired / Lapsed US ⏱️ 0.0 years remaining

High performance ring laser gyroscope with magneto-optical bias

Assignee: United States Department of the Navy
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Filing: 1973-06-25
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Granted: 1974-07-30
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Expires: 1993-06-25
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Abstract

Abstract A ring laser gyroscope capable of producing an output signal at low rates of angular rotation. A differential magneto-optical bias system eliminates the requirement of extreme stability in the bias system.

Inventors

  • 👤 J Walter

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 16:03
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/58; G01C19/64; G01C19/66; G01P; G01P3/00; G01P3/42; G01P3/56; G01P3/60; H; H01; H01S; H01S3/00; H01S3/05; H01S3/08; H01S3/081; H01S3/083

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 188 words
A ring laser rotational rate sensor having a differential bias system to prevent low angular rate lock-in, comprising: a first laser cavity forming a closed loop path containing a lasing medium in said closed loop path for producing a first pair of counter-rotating light beams in said path, a second laser cavity located in the plane described by said first laser cavity forming a second closed loop path containing a second lasing medium in said second closed loop path for producing a second pair of counter-rotating light beams in said path with at least one light beam of each of said first and second closed loop paths being substantially parallel and separated by short distance, means for producing magNeto-optical rotation of light beams disposed to have said parallel light beams pass therethrough, and first and second photodetector and retroreflector means receiving respectively said first and second laser cavity light beam pair for producing outputs corresponding respectively to frequency differences between said first and second pair of counter-rotating light beams, said outputs indicating angular rotation of said first and second laser cavities about an axis perpendicular to said plane.
Claim 2
Dependent Claim 188 words
A ring laser rotational rate sensor having a differential bias system to prevent low angular rate lock-in, comprising: a first laser cavity forming a closed loop path containing a lasing medium in said closed loop path for producing a first pair of counter-rotating light beams in said path, a second laser cavity located in the plane described by said first laser cavity forming a second closed loop path containing a second lasing medium in said second closed loop path for producing a second pair of counter-rotating light beams in said path with at least one light beam of each of said first and second closed loop paths being substantially parallel and separated by short distance, means for producing magNeto-optical rotation of light beams disposed to have said parallel light beams pass therethrough, and first and second photodetector and retroreflector means receiving respectively said first and second laser cavity light beam pair for producing outputs corresponding respectively to frequency differences between said first and second pair of counter-rotating light beams, said outputs indicating angular rotation of said first and second laser cavities about an axis perpendicular to said plane.
Claim 3
Dependent Claim 35 words
The apparatus of claim 1 wherein the light beams passing through said magneto-optical rotation means are separated by a distance at least equal to or greater than the diameter of one of said light beams.
Claim 4
Dependent Claim 20 words
The apparatus of claim 2 wherein said means for producing magneto-optical rotation of said light beams is a Faraday cell.
Claim 5
Dependent Claim 18 words
The apparatus of claim 3 wherein said Faraday cell comprises an optical medium having a large Verdet constant.
Claim 6
Dependent Claim 62 words
The apparatus of claim 1 wherein each of said first and second output producing means comprises a photodetector and a retroreflector both disposed outside of the associated laser cavity, and a reflecting surface in each of said first and second laser cavities is partially reflective and transmits a portion of said light beams to the photodetector for that cavity via said retroreflector.
Claim 7
Dependent Claim 107 words
A ring laser rotational rate sensor having a stable differential bias system to prevent low angular rate lock-in, comprising, a pair of closed-loop laser cavities disposed adjacent to one another in the same plane with at least one light path of one cavity parallel to but separated from one light path of the other cavity, magneto-optical bias means disposed to have said parallel light paths pass therethrough, and a pair of detection means cooperating with said pair of laser cavities for producing output signals upon detecting frequency differences present in said pair of laser cavities, said output signals being indicative of rotation of said laser cavities plane.
Claim 8
Dependent Claim 107 words
A ring laser rotational rate sensor having a stable differential bias system to prevent low angular rate lock-in, comprising, a pair of closed-loop laser cavities disposed adjacent to one another in the same plane with at least one light path of one cavity parallel to but separated from one light path of the other cavity, magneto-optical bias means disposed to have said parallel light paths pass therethrough, and a pair of detection means cooperating with said pair of laser cavities for producing output signals upon detecting frequency differences present in said pair of laser cavities, said output signals being indicative of rotation of said laser cavities plane.
Claim 9
Dependent Claim 20 words
The apparatus of claim 6 wherein said parallel light paths are separated by at least one laser light beam diameter.
Claim 10
Dependent Claim 19 words
The apparatus of claim 7 wherein said magneto-optical bias means comprises a Faraday cell having a large Verdet constant.
Claim 11
Dependent Claim 20 words
The apparatus of claim 8 wherein said pair of detection means are located external to said pair of laser cavities.

References Cited (Backward Citations)

US3373650A Cited
US3468608A Cited
US3600095A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-07-29 1978-01-28 1978-07-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-07-29 1982-01-28 1982-07-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-07-29 1986-01-28 1986-07-30 $7700.00 Window Closed / Lapsed

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