SE7908117L - RING LASER - Google Patents

RING LASER

Info

Publication number
SE7908117L
SE7908117L SE7908117A SE7908117A SE7908117L SE 7908117 L SE7908117 L SE 7908117L SE 7908117 A SE7908117 A SE 7908117A SE 7908117 A SE7908117 A SE 7908117A SE 7908117 L SE7908117 L SE 7908117L
Authority
SE
Sweden
Prior art keywords
laser
plane
mirror
length
ring laser
Prior art date
Application number
SE7908117A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE449664B (en
Inventor
Jr D C Grant
T J Hutchings
Original Assignee
Litton Systems Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Litton Systems Inc filed Critical Litton Systems Inc
Publication of SE7908117L publication Critical patent/SE7908117L/en
Publication of SE449664B publication Critical patent/SE449664B/en

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • G01C19/64Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
    • G01C19/66Ring laser gyrometers
    • G01C19/661Ring laser gyrometers details
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/05Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
    • H01S3/08Construction or shape of optical resonators or components thereof
    • H01S3/081Construction or shape of optical resonators or components thereof comprising three or more reflectors
    • H01S3/083Ring lasers
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/05Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
    • H01S3/08Construction or shape of optical resonators or components thereof
    • H01S3/081Construction or shape of optical resonators or components thereof comprising three or more reflectors
    • H01S3/083Ring lasers
    • H01S3/0835Gas ring lasers

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Electromagnetism (AREA)
  • Optics & Photonics (AREA)
  • Power Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Plasma & Fusion (AREA)
  • Lasers (AREA)
  • Gyroscopes (AREA)

Abstract

In an optical resonator arrangement, particularly a ring laser gyroscope, a concave mirror 22 and at least one planar mirror 24, 26, 28 are used to guide a laser beam 14, the plane of one of the mirrors being inclined at an angle of between 1 and 3 arc minutes with respect to the plane of the or each other mirror. The laser is tuned by translating the concave mirror substantially in its own plane (which may be inclined itself in one embodiment) so as to alter the length of the laser path. One of mirrors 26 preferably has an aperture for suppressing off-axis modes of oscillation, and this mirror must be translated in its own plane during tuning to realign the aperture to suppress the off-axis modes. Such a ring laser gyroscope may be made very small: the length of each side of the laser path may be less than an inch in length. <IMAGE>
SE7908117A 1978-10-02 1979-10-01 PROCEDURE FOR REGULATING LASER BAN'S LENGTH IN AN OPTICAL RESONATOR AND OPTICAL RESONATOR FOR EXECUTION OF THE PROCEDURE SE449664B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US94735578A 1978-10-02 1978-10-02

Publications (2)

Publication Number Publication Date
SE7908117L true SE7908117L (en) 1980-04-03
SE449664B SE449664B (en) 1987-05-11

Family

ID=25486010

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7908117A SE449664B (en) 1978-10-02 1979-10-01 PROCEDURE FOR REGULATING LASER BAN'S LENGTH IN AN OPTICAL RESONATOR AND OPTICAL RESONATOR FOR EXECUTION OF THE PROCEDURE

Country Status (9)

Country Link
JP (2) JPS584475B2 (en)
CA (1) CA1133615A (en)
CH (1) CH651157A5 (en)
DE (1) DE2939804A1 (en)
FR (1) FR2438357A1 (en)
GB (1) GB2032169B (en)
IL (1) IL57936A (en)
IT (1) IT1164049B (en)
SE (1) SE449664B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4519708A (en) * 1981-05-20 1985-05-28 Raytheon Company Mode discrimination apparatus
IL70499A (en) * 1982-12-27 1988-06-30 Litton Systems Inc Laser cathode
US4672623A (en) * 1985-08-16 1987-06-09 Honeywell Inc. Cathode construction for a laser

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3390606A (en) * 1965-03-01 1968-07-02 Honeywell Inc Control apparatus
US3462708A (en) * 1966-11-29 1969-08-19 Sperry Rand Corp Ring laser having a piezoelectric reflector external to the closed loop to cancel a frequency modulation within the loop
US3503005A (en) * 1967-10-17 1970-03-24 Honeywell Inc Ring laser which is biased to permit two equal intensity transition frequencies to be generated in opposite directions
US3581227A (en) * 1968-04-18 1971-05-25 Honeywell Inc Adjustable, thin membrane mirror for use in the stabilization of ring lasers
US3824487A (en) * 1972-05-08 1974-07-16 United Aircraft Corp Unstable ring laser resonators
CA1085031A (en) * 1976-11-08 1980-09-02 Litton Systems, Inc. Laser gyro with phased dithered mirrors
US4115004A (en) * 1976-11-15 1978-09-19 Litton Systems, Inc. Counterbalanced oscillating ring laser gyro

Also Published As

Publication number Publication date
JPS5910078B2 (en) 1984-03-06
CH651157A5 (en) 1985-08-30
SE449664B (en) 1987-05-11
FR2438357A1 (en) 1980-04-30
IL57936A (en) 1982-07-30
GB2032169A (en) 1980-04-30
GB2032169B (en) 1982-09-22
FR2438357B1 (en) 1984-02-17
JPS5821385A (en) 1983-02-08
JPS5548989A (en) 1980-04-08
DE2939804A1 (en) 1980-04-10
IT1164049B (en) 1987-04-08
CA1133615A (en) 1982-10-12
JPS584475B2 (en) 1983-01-26
IT7950401A0 (en) 1979-09-28

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