GB2185846A - Ring laser - Google Patents

Ring laser Download PDF

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Publication number
GB2185846A
GB2185846A GB08601741A GB8601741A GB2185846A GB 2185846 A GB2185846 A GB 2185846A GB 08601741 A GB08601741 A GB 08601741A GB 8601741 A GB8601741 A GB 8601741A GB 2185846 A GB2185846 A GB 2185846A
Authority
GB
United Kingdom
Prior art keywords
ring laser
passage
block
electrodes
passages
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
GB08601741A
Other versions
GB2185846B (en
Inventor
William Gillies Mcnaught
Iain Edward Ross
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ferranti International PLC
Original Assignee
Ferranti PLC
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 Ferranti PLC filed Critical Ferranti PLC
Priority to GB8601741A priority Critical patent/GB2185846B/en
Priority to DE19873700844 priority patent/DE3700844A1/en
Priority to FR8700428A priority patent/FR2593650B1/en
Priority to CA000527771A priority patent/CA1309155C/en
Priority to JP1151987A priority patent/JPS62217683A/en
Publication of GB2185846A publication Critical patent/GB2185846A/en
Application granted granted Critical
Publication of GB2185846B publication Critical patent/GB2185846B/en
Expired legal-status Critical Current

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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
    • H01S3/09Processes or apparatus for excitation, e.g. pumping
    • H01S3/097Processes or apparatus for excitation, e.g. pumping by gas discharge of a gas laser
    • H01S3/0975Processes or apparatus for excitation, e.g. pumping by gas discharge of a gas laser using inductive or capacitive excitation
    • 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

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  • 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

A ring laser comprises a block (10) of dielectric material in which are formed a number of passages (11) defining a polygonal path enclosing a gaseous active medium. Two electrodes (16) are arranged external to the passage parallel to and on opposite sides of part or all of at least one of the passages (11). In operation the electrodes (10) are capacitively coupled to the gaseous active medium to produce an electric discharge therein transverse to the direction of the passage by the application to electrodes (16) of a high-frequency alternating voltage. <IMAGE>

Description

SPECIFICATION Ring laser Ring lasers are used as angular rate sensors primarily, though not exclusively in inertial navigation applications. Basically a ring laser comprises two laser beams which travel in opposite directions around the same closed loop path. Commonly the path is generally triangular in form. Rotation rates about an axis perpendicular to the plane of the ring laser resonant cavity are measured by detecting the beat frequency which occurs due to a frequency difference between the counterrotating beams resulting from the rotation.
A commonly-used form of ring laser designed for such a purpose is described in US Patent No. 3,390,606 and its British equivalent No. 1,142,962. The ring laser shown therein comprises a solid block of dielectric material in which three passages have been formed to provide a triangular passage through the block. Mirrors are provided at the points where pairs of passages intersect, and one of the mirrors also forms part of the detection means. The passages are filled with a suitable gas or gas mixture and an electric discharge is produced in the gas between anode and cathode electrodes which extend into the lasing gas.
Such an arrangement for producing an electric discharge in the gas has a number of disadvantages. One of these has been the need to provide an excitation power supply producing a dc running voltage of between 500 and 1,000 volts, with a striking voltage of up to 3,000 volts. Such a power supply has of necessity been large in size. In addition the presence of anode and cathode electrodes causes sputtering and gas flow effects. Other problems also occur.
It is an object of the present invention to provide a ring laser in which the above problems are avoided.
According to the present invention there is provided a ring laser which includes a block of dielectric material having formed therein at least one passage defining a closed polygonal path lying in one plane within the block, a gaseous active medium contained within the said passage, and two electrodes arranged external to the passage parallel to and on opposite sides of at least part of said passage and being, in use, capacitively coupled to the gaseous active medium by the dielectric material, whereby laser action is included in the gaseous active medium to produce an electric discharge therein transverse to the direction of the passage by the application of a high-frequency alternating voltage between said two electrodes.
The invention will now be described with reference to the accompanying drawings, in which: Figure 1 shows a simplified plan view of a ring laser according to a first embodiment of the invention; Figure 2 shows a part-sectioned side view of the ring laser of Fig. 1; Figure 3 shows a circuit diagram of a power supply suitable for the ring laser of Fig. 1; and Figure 4 shows a plan view according-to a second embodiment of the invention.
Referring now to Figs. 1 and 2 the ring laser is made from a block 10 of a dielectric material such as a glass-ceramic material having high thermal stability. Conveniently the block 10 may be in the shape of a truncated triangle as shown in Fig. 1. Three passages 11 are bored through the block 10 parallel to the three sides of the triangle. The three passages emerge through the truncated corners of the block. Each of these corners carries a mirror 12 mounted so that laser radiation emerging from one passage is reflected along the next passage so that the radiation follows a closed path through the passages. Two of the mirrors may be fully reflecting whilst the third is partially transmitting and is associated with a detector 13 which produces an electrical output on a cable 14.
As shown in Figs. 1 and 2 two grooves 15 are machined into the block respectively above and below on of the passages 11. At the bottom of each of the grooves 15 is located a metal electrode 16 to which may be applied a high-frequency alternating excitation voltage from a suitable power supply.
In the centre of block 10 may be located a dither mechanism, represented by the reference 17, which is able to oscillate the block through a small angle about an axis 18, this being the axis about which the ring laser is able to sense angular movements. Such dither mechanisms are well-known and need not be described here.
In operation, the application of a suitable high-frequency alternating voltage between the two electrodes 16 causes excitation of the laser gaseous active medium, usually a Helium Neon mixture, contained in the passage 11 located between the electrodes. This excitation is transverse to the direction of the passage 11 and produces an electric discharge in the gas, resulting in laser action taking place.
This produces laser beams travelling in both directions around the closed path defined by the passages 11 and the mirrors 12.
The use of a transverse high-frequency alternating voltage to excite the laser has a number of benefits. It is not necessary to insert electrodes into the passages 11, and hence the problems caused by such electrodes are avoided.
Transverse capacitive coupling of high-frequency alternating power into the discharge through the glass-ceramic walls between the electrodes allows a much reduced drive voltage to be used compared with known longi tudinally excited ring lasers. Typically, for a ring laser having a bore of 3mm the drive voltage may be of the order of 5-10 volts at a frequency of between 10MHZ and 5GHZ.
Capacitive ballasting exists so that no ballast resistors are required and hence the power consumption is much less. The frequency range referred to lies within the main communications band and hence components are readily available to enable small low cost power supplies to be produced. A power supply suitable for the purpose is shown in Fig.
3.
As shown in Fig. 3 the power supply circuit is very simple, comprising a radio-frequency oscillator 30 operable to produce an alternating signal at the required frequency. This signal is amplified by amplifier 31 to provide the necessary voltage level and is coupled to the ring laser shown schematically at 32 by an impedance matching network 33.
The laser illustrated in Fig. 1 has electrodes associated with one of the three passages 11 formed in the block. Excitation may be provided on either or both of the other passages if necessary, depending upon the bore of the passage and gain required for satisfactory operation. Fig. 4 show a plan view of 15 a ring laser having two pairs of electrodes.
The ring laser is not operated as a waveguide laser.
The electrodes need not necessarily be located in grooves in the dielectric material, though this is one way of reducing the thickness of material between the electrodes and the passage. If a material of sufficient strength was available the block could be made sufficiently thin for the electrodes to be formed on its surface. Alternatively the thickness of the material may be reduced by using other configurations.
A number of other advantages arise from the use of transverse high-frequency alternating excitation of the laser. The discharge in the gas occurs substantially between the two electrodes, unlike the dc longitudinally-excited ring laser. This means that the discharge occurs well away from the mirrors avoiding the risk of mirror damage due to ultra-violet radiation or ion bombardment. Construction is simpler than with the dc-excited ring laser leading to a lower manufacturing cost. The only vacuum seals required are for the three mirror ports and a gas fill port. Glass-ceramic materials are particularly suitable as they remain stable, having zero or very small coefficients of thermal expansion, over a very wide temperature range, from -500C to 400"C.
Various examples of such materials are known by the trade names Zerodur, Cervit and ULE.

Claims (9)

1. A ring laser which includes a block of dielectric material having formed therein at least one passage defining a closed polygon path lying in one plane within the block, a gaseous active medium contained within the said passage, and two electrodes arranged external to the passage parallel to and on opposite sides of at least part of said passage and being, in use, capacitively coupled to the gaseous active medium to produce electric discharge therein transverse to the direction of the passage by the application of a high-frequency alternating voltage between said two electrodes.
2. A ring laser as claimed in Claim 1 in which the block of dielectric material contains three passages defining a substantially triangular close path.
3. A ring laser as claimed in Claim 1 in which the said two electrodes are associated with one only of said passages.
4. A ring laser as claimed in any one of Claims 1 to 3 in which one at least of said two electrodes is located in a groove extending from the surface of the block of dielectric material towards the said passage.
5. A ring laser as claimed in any one of Claims 2 to 4 in which the said block carries three mirrors each positioned at the intersection of two of said passages so as to reflect laser radiation emerging from on passage into the adjacent passage.
6. A ring laser as claimed in only one of the preceding claims in which the block of dielectric material is made from a glass-ceramic material.
7. A ring laser as claimed in any one of Claims 1 to 6 in which the gaseous active medium is a mixture of Helium and Neon.
8. A ring laser as claimed in any one of Claims 1 to 7 in which the frequency of the high-frequency alternating voltage is in the range from 10 MHz to 5GHZ.
9. A ring laser substantially as herein described with reference to the accompanying drawings.
GB8601741A 1986-01-24 1986-01-24 Ring laser Expired GB2185846B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB8601741A GB2185846B (en) 1986-01-24 1986-01-24 Ring laser
DE19873700844 DE3700844A1 (en) 1986-01-24 1987-01-14 RING LASER
FR8700428A FR2593650B1 (en) 1986-01-24 1987-01-16 LASER IN RING.
CA000527771A CA1309155C (en) 1986-01-24 1987-01-21 Ring laser
JP1151987A JPS62217683A (en) 1986-01-24 1987-01-22 Ring laser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8601741A GB2185846B (en) 1986-01-24 1986-01-24 Ring laser

Publications (2)

Publication Number Publication Date
GB2185846A true GB2185846A (en) 1987-07-29
GB2185846B GB2185846B (en) 1989-12-20

Family

ID=10591887

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8601741A Expired GB2185846B (en) 1986-01-24 1986-01-24 Ring laser

Country Status (5)

Country Link
JP (1) JPS62217683A (en)
CA (1) CA1309155C (en)
DE (1) DE3700844A1 (en)
FR (1) FR2593650B1 (en)
GB (1) GB2185846B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5056102A (en) * 1989-05-15 1991-10-08 Honeywell Inc. Getter assembly
US5059028A (en) * 1989-02-03 1991-10-22 Gec Ferranti Defence Systems Limited Ring laser gyroscope having means for maintaining the beam intensity
GB2220098B (en) * 1988-06-22 1992-09-09 Litton Systems Inc Ring laser gyroscope
US5196905A (en) * 1988-06-22 1993-03-23 Litton Systems, Inc. Radio frequency excited ring laser gyroscope
CN105806327A (en) * 2015-01-15 2016-07-27 霍尼韦尔国际公司 Radio frequency ring laser gyroscope including multiple electrode system and impedance matching circuit

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8728831D0 (en) * 1987-12-10 1988-01-27 British Aerospace Ring laser gyroscopes
GB8728829D0 (en) * 1987-12-10 1988-01-27 British Aerospace Ring laser gyroscopes
DE3905549A1 (en) * 1989-02-23 1990-08-30 Marinescu Marlene Gas-discharge arrangement
CA2022329C (en) * 1989-12-26 1995-03-28 Bruce C. Grover Dual helix rf discharge with single driver for ring laser gyroscope
DE4017188A1 (en) * 1990-05-29 1991-12-05 Bodenseewerk Geraetetech GAS RING LASER
DE4124407A1 (en) * 1991-07-23 1993-01-28 Wb Laser Wegmann Baasel Laser Ring laser with polygonal beam path in resonator - uses reflection and output mirrors and deflection elements with two or more mutually offset polygonal beam paths to achieve high output power
US5381436A (en) * 1993-05-28 1995-01-10 Honeywell, Inc. Ring laser gyro employing radio frequency for pumping of gain medium

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1271889A (en) * 1969-05-09 1972-04-26 Comp Generale Electricite Ring laser
GB1594047A (en) * 1978-05-31 1981-07-30 Litton Systems Inc Ring laser gyroscopes
EP0065699A2 (en) * 1981-05-11 1982-12-01 Mitsubishi Denki Kabushiki Kaisha A silent discharge-type laser device
GB2126777A (en) * 1982-07-30 1984-03-28 Leroy Vernon Sutter A laser bore and electrode structure

Family Cites Families (4)

* 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
US3772611A (en) * 1971-12-27 1973-11-13 Bell Telephone Labor Inc Waveguide gas laser devices
FR2530087B1 (en) * 1982-07-09 1986-02-14 Telecommunications Sa GAS WAVEGUIDE LASER GENERATOR AND METHOD FOR MANUFACTURING THE WAVEGUIDE
US4596018A (en) * 1983-10-07 1986-06-17 Minnesota Laser Corp. External electrode transverse high frequency gas discharge laser

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1271889A (en) * 1969-05-09 1972-04-26 Comp Generale Electricite Ring laser
GB1594047A (en) * 1978-05-31 1981-07-30 Litton Systems Inc Ring laser gyroscopes
EP0065699A2 (en) * 1981-05-11 1982-12-01 Mitsubishi Denki Kabushiki Kaisha A silent discharge-type laser device
GB2126777A (en) * 1982-07-30 1984-03-28 Leroy Vernon Sutter A laser bore and electrode structure

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2220098B (en) * 1988-06-22 1992-09-09 Litton Systems Inc Ring laser gyroscope
US5196905A (en) * 1988-06-22 1993-03-23 Litton Systems, Inc. Radio frequency excited ring laser gyroscope
US5059028A (en) * 1989-02-03 1991-10-22 Gec Ferranti Defence Systems Limited Ring laser gyroscope having means for maintaining the beam intensity
US5056102A (en) * 1989-05-15 1991-10-08 Honeywell Inc. Getter assembly
CN105806327A (en) * 2015-01-15 2016-07-27 霍尼韦尔国际公司 Radio frequency ring laser gyroscope including multiple electrode system and impedance matching circuit
EP3048419A1 (en) * 2015-01-15 2016-07-27 Honeywell International Inc. Radio frequency ring laser gyroscope including a multiple electrode system and an impedance matching circuit
US9759565B2 (en) 2015-01-15 2017-09-12 Honeywell International Inc. Radio frequency ring laser gyroscope including a multiple electrode system and an impedance matching circuit
CN105806327B (en) * 2015-01-15 2020-09-29 霍尼韦尔国际公司 Radio frequency ring laser gyroscope including multiple electrode system and impedance matching circuit

Also Published As

Publication number Publication date
GB2185846B (en) 1989-12-20
CA1309155C (en) 1992-10-20
FR2593650B1 (en) 1993-08-13
FR2593650A1 (en) 1987-07-31
JPS62217683A (en) 1987-09-25
DE3700844A1 (en) 1987-07-30

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940124