GB2153137A - Rapidly tunable laser - Google Patents

Rapidly tunable laser Download PDF

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Publication number
GB2153137A
GB2153137A GB08401257A GB8401257A GB2153137A GB 2153137 A GB2153137 A GB 2153137A GB 08401257 A GB08401257 A GB 08401257A GB 8401257 A GB8401257 A GB 8401257A GB 2153137 A GB2153137 A GB 2153137A
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United Kingdom
Prior art keywords
laser
output
grating
resonator
angle
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.)
Withdrawn
Application number
GB08401257A
Inventor
Denis Roderick Hall
Kenneth Samuel Lipton
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Laser Applications Ltd
Original Assignee
Laser Applications Ltd
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 Laser Applications Ltd filed Critical Laser Applications Ltd
Priority to GB08401257A priority Critical patent/GB2153137A/en
Publication of GB2153137A publication Critical patent/GB2153137A/en
Withdrawn legal-status Critical Current

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    • 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
    • H01S3/10Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating
    • H01S3/106Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating by controlling devices placed within the cavity
    • H01S3/1068Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating by controlling devices placed within the cavity using an acousto-optical device
    • 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
    • H01S3/10Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating
    • H01S3/105Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating by controlling the mutual position or the reflecting properties of the reflectors of the cavity, e.g. by controlling the cavity length
    • H01S3/1055Controlling the intensity, frequency, phase, polarisation or direction of the emitted radiation, e.g. switching, gating, modulating or demodulating by controlling the mutual position or the reflecting properties of the reflectors of the cavity, e.g. by controlling the cavity length one of the reflectors being constituted by a diffraction grating

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Optics & Photonics (AREA)
  • Lasers (AREA)

Abstract

A rapidly tunable laser producing a repeatable sequence of output frequencies comprises a dispersive element (14) within the resonant optical cavity so that only one wavelength can resonate at any instant, and an electrically controlled device (10) to vary this wavelength. In one embodiment device (10) is an an angle scanning device. As the scanning angle changes, the resonator is in alignment sequentially for wavelengths characteristic of each of a plurality of possible laser transitions. In an alternative embodiment the dispersive element is an acousto optic modulator device which is electrically controllable and may incorporate the rear reflector and grating. <IMAGE>

Description

SPECIFICATION Rapidly tunable laser The present invention is concerned with a rapidly tunable laser.
Many lasers can be caused to operate on more than one lasing transition by the use of suitable dispersive elements such as prisms or gratings positioned within the laser resonator.
One example is the carbon dioxide laser which has many rotational-vibrational transitions in two bands in the 9- um region of the spectrum. One may select any one of these transitions by suitably aligning the dispersive element to the precise angle with respect to the optic axis which minimises cavity losses for the wavelength of the desired transition.
Small adjustments to this angle will allow the laser output to be tuned from transition to transition, such as, for example, by the use of a precise micrometer movement on well known laser mirror mounts. Such wavelength changes are of necessity very slow. However, there are applications where the ability of the laser to scan very rapidly from line to line would be a distinct advantage.
It is an object of the present invention to provide a means by which such a laser may be tuned rapidly from line to line to produce a repeatable burst of sequential transition output.
In accordance with the present invention, this is achieved by the use of an electrically controlled angle scanning device which is arranged in a laser resonator between the laser mirror and a dispersive element, such as a diffraction grating or prism, such that as the scanning angle changes, the resonator is in alignment sequentially for wavelengths characteristic of each Of a plurality of possible laser transitions.
By this means, the laser output will consist of a sequence of rapid bursts, each burst consisting of a series of lines produced sequentially as the laser output sweeps across the available gain spectrum.
The invention is described further hereinafter, by way of example only, with reference to the accompanying drawings, in which: Figures 1 and 2 are schematic diagrams of two embodiments of rapidly tunable lasers in accordance with the present invention; and Figure 3 is a diagram showing a typical output from the laser arrangement of Fig. 1.
With reference to Fig. 1, the laser has a resonator designed to incorporate an electrically controlled angle scanning device 10 such as an electro-mechanical scanner, either of the linear or the resonant variety, or an acoustoptic deflector. Such devices are capable of scan rates of at least tens of kilohertz. This scanning device is disposed between the laser mirror 1 2 and a dispersive element 14, such as a diffraction grating or prism. The laser gain medium is indicated by the reference numeral 16.
As the scanner angle changes, the resonator will be in alignment sequentially for the wavelengths characteristic of each of the rotational vibrational transitions. Consequently, the output of the laser will consist of a sequence of pulses as illustrated in Fig. 3. Then, as the scanner reverses direction the output will be a mirror image of the first scan. In this way, bursts of radiation, each burst consisting of a series of lines produced sequentially at the laser output, sweeps across the available gain spectrum.
In the embodiment of Fig. 2, an acousto optic device 1 8 is used as the rear reflector and the grating, although these functions can be separated. A partially transmitting laser mirror 20 is disposed between the laser gain medium 16' and the modulator device 1 8.
The grating equation is: 2d sin < p = nA where d = grating spacing ss = incident angle A = wavelength By varying d and keeping < p constant, the output wavelength can be adjusted. The grating spacing can be adjusted by simply altering the input frequency to the acousto optic device 1 8. It will be noted that the relatively low reflection efficiencies achievable by using an acousto optic modulator 1 8 as a grating are counteracted by employing a three-mirror cavity.
These laser devices have many possible applications in remote surveillance such as trace gas or pollution detection or any system where a rapidly tuned frequency-agile laser is required.
1. A method of rapidly tuning a laser from line to line to produce a repeatable burst of sequential transition output by arranging an electrically controlled angle scanning device in a laser resonator between the laser mirror and a dispersive element of the resonator, such that as the scanning angle changes, the resonator is in alignment sequentially for wavelengths characteristic of each of a plurality of possible laser transitions.
2. A method as claimed in claim 1 in which the output wavelength conforms to the relation nA = 2d sin ss where A is the wavelength, d is the grating spacing and < p is the incident angle, and in which the grating spacing is adjusted by altering the input frequency to an acousto optic device serving as the angle scanning device.
3. Apparatus to perform the method of claim 1 in which the angle scanning device is an electro mechanical scanner of either the linear or resonant variety.
4. Apparatus as claimed in claim 3 in which the dispensive element is a diffraction
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (11)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Rapidly tunable laser The present invention is concerned with a rapidly tunable laser. Many lasers can be caused to operate on more than one lasing transition by the use of suitable dispersive elements such as prisms or gratings positioned within the laser resonator. One example is the carbon dioxide laser which has many rotational-vibrational transitions in two bands in the 9- um region of the spectrum. One may select any one of these transitions by suitably aligning the dispersive element to the precise angle with respect to the optic axis which minimises cavity losses for the wavelength of the desired transition. Small adjustments to this angle will allow the laser output to be tuned from transition to transition, such as, for example, by the use of a precise micrometer movement on well known laser mirror mounts. Such wavelength changes are of necessity very slow. However, there are applications where the ability of the laser to scan very rapidly from line to line would be a distinct advantage. It is an object of the present invention to provide a means by which such a laser may be tuned rapidly from line to line to produce a repeatable burst of sequential transition output. In accordance with the present invention, this is achieved by the use of an electrically controlled angle scanning device which is arranged in a laser resonator between the laser mirror and a dispersive element, such as a diffraction grating or prism, such that as the scanning angle changes, the resonator is in alignment sequentially for wavelengths characteristic of each Of a plurality of possible laser transitions. By this means, the laser output will consist of a sequence of rapid bursts, each burst consisting of a series of lines produced sequentially as the laser output sweeps across the available gain spectrum. The invention is described further hereinafter, by way of example only, with reference to the accompanying drawings, in which: Figures 1 and 2 are schematic diagrams of two embodiments of rapidly tunable lasers in accordance with the present invention; and Figure 3 is a diagram showing a typical output from the laser arrangement of Fig. 1. With reference to Fig. 1, the laser has a resonator designed to incorporate an electrically controlled angle scanning device 10 such as an electro-mechanical scanner, either of the linear or the resonant variety, or an acoustoptic deflector. Such devices are capable of scan rates of at least tens of kilohertz. This scanning device is disposed between the laser mirror 1 2 and a dispersive element 14, such as a diffraction grating or prism. The laser gain medium is indicated by the reference numeral 16. As the scanner angle changes, the resonator will be in alignment sequentially for the wavelengths characteristic of each of the rotational vibrational transitions. Consequently, the output of the laser will consist of a sequence of pulses as illustrated in Fig. 3. Then, as the scanner reverses direction the output will be a mirror image of the first scan. In this way, bursts of radiation, each burst consisting of a series of lines produced sequentially at the laser output, sweeps across the available gain spectrum. In the embodiment of Fig. 2, an acousto optic device 1 8 is used as the rear reflector and the grating, although these functions can be separated. A partially transmitting laser mirror 20 is disposed between the laser gain medium 16' and the modulator device 1 8. The grating equation is: 2d sin < p = nA where d = grating spacing ss = incident angle A = wavelength By varying d and keeping < p constant, the output wavelength can be adjusted. The grating spacing can be adjusted by simply altering the input frequency to the acousto optic device 1 8. It will be noted that the relatively low reflection efficiencies achievable by using an acousto optic modulator 1 8 as a grating are counteracted by employing a three-mirror cavity. These laser devices have many possible applications in remote surveillance such as trace gas or pollution detection or any system where a rapidly tuned frequency-agile laser is required. CLAIMS
1. A method of rapidly tuning a laser from line to line to produce a repeatable burst of sequential transition output by arranging an electrically controlled angle scanning device in a laser resonator between the laser mirror and a dispersive element of the resonator, such that as the scanning angle changes, the resonator is in alignment sequentially for wavelengths characteristic of each of a plurality of possible laser transitions.
2. A method as claimed in claim 1 in which the output wavelength conforms to the relation nA = 2d sin ss where A is the wavelength, d is the grating spacing and < p is the incident angle, and in which the grating spacing is adjusted by altering the input frequency to an acousto optic device serving as the angle scanning device.
3. Apparatus to perform the method of claim 1 in which the angle scanning device is an electro mechanical scanner of either the linear or resonant variety.
4. Apparatus as claimed in claim 3 in which the dispensive element is a diffraction grating or prism.
5. Apparatus to perform the method of claims 1 or 2 in which the angle scanning device is an acousto optic device.
6. Apparatus as claimed in claim 5 in which the acousto optic device is used as the rear reflector and grating of the dispersive element.
7. Apparatus as claimed in claims 5 or 6 in which a partiaily transmitting laser mirror is disposed between the laser gain medium and the acousto optic modulator device.
8. Apparatus as claimed in claim 6 in which the grating equation for the acousto optic modulator device is 2d sin + = nA, where d = grating spacing, < p = incident angle and A = wavelength.
9. Apparatus as claimed in any of claims 5 to 8 in which a three-mirror cavity is employed to counteract low reflection efficiency using the acousto optic modulator device.
10. Apparatus to produce a repeatable burst of sequential transition output from a laser constructed and arranged substantially as hereinbefore described with reference to Fig. 1 or Fig. 2 of the accompanying drawings.
11. A method of rapidly tuning a laser from line to line, substantially as hereinbefore described with reference to the accompanying drawings.
GB08401257A 1984-01-18 1984-01-18 Rapidly tunable laser Withdrawn GB2153137A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08401257A GB2153137A (en) 1984-01-18 1984-01-18 Rapidly tunable laser

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GB08401257A GB2153137A (en) 1984-01-18 1984-01-18 Rapidly tunable laser

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6959024B2 (en) 2002-02-28 2005-10-25 Picarro, Inc. Laser Tuning by spectrally dependent spatial filtering

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3774121A (en) * 1971-12-13 1973-11-20 Bell Telephone Labor Inc Wavelength selective laser apparatus
GB1338503A (en) * 1972-05-23 1973-11-28 British Aircraft Corp Ltd Wavelength modulation of a dye lacer
US3872407A (en) * 1972-09-01 1975-03-18 Us Navy Rapidly tunable laser
US3902137A (en) * 1974-10-29 1975-08-26 Us Navy Electro-optic diffraction grating tuned laser
US3931592A (en) * 1974-06-14 1976-01-06 The United States Of America As Represented By The Secretary Of The Navy Surface acoustic wave tuned laser
US3940713A (en) * 1974-11-11 1976-02-24 The United States Of America As Represented By The Secretary Of The Navy Stimulated Brillouin scattered (SBS) tuned laser
US3959739A (en) * 1975-02-03 1976-05-25 The United States Of America As Represented By The Secretary Of The Navy Electro-optic tuning of organic dye laser
US4028636A (en) * 1973-06-28 1977-06-07 The United States Of America As Represented By The Secretary Of The Navy Acousto-optical deflector tuned organic dye laser
US4118675A (en) * 1977-03-31 1978-10-03 The United States Of America As Represented By The Secretary Of The Navy Laser tuning with an acousto-optic lens
US4216440A (en) * 1978-08-28 1980-08-05 The United States Of America As Represented By The Secretary Of The Navy Surface acoustic wave tuning for lasers
GB2129201A (en) * 1982-09-30 1984-05-10 Honeywell Inc Rapidly tunable laser

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3774121A (en) * 1971-12-13 1973-11-20 Bell Telephone Labor Inc Wavelength selective laser apparatus
GB1338503A (en) * 1972-05-23 1973-11-28 British Aircraft Corp Ltd Wavelength modulation of a dye lacer
US3872407A (en) * 1972-09-01 1975-03-18 Us Navy Rapidly tunable laser
US4028636A (en) * 1973-06-28 1977-06-07 The United States Of America As Represented By The Secretary Of The Navy Acousto-optical deflector tuned organic dye laser
US3931592A (en) * 1974-06-14 1976-01-06 The United States Of America As Represented By The Secretary Of The Navy Surface acoustic wave tuned laser
US3902137A (en) * 1974-10-29 1975-08-26 Us Navy Electro-optic diffraction grating tuned laser
US3940713A (en) * 1974-11-11 1976-02-24 The United States Of America As Represented By The Secretary Of The Navy Stimulated Brillouin scattered (SBS) tuned laser
US3959739A (en) * 1975-02-03 1976-05-25 The United States Of America As Represented By The Secretary Of The Navy Electro-optic tuning of organic dye laser
US4118675A (en) * 1977-03-31 1978-10-03 The United States Of America As Represented By The Secretary Of The Navy Laser tuning with an acousto-optic lens
US4216440A (en) * 1978-08-28 1980-08-05 The United States Of America As Represented By The Secretary Of The Navy Surface acoustic wave tuning for lasers
GB2129201A (en) * 1982-09-30 1984-05-10 Honeywell Inc Rapidly tunable laser

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6959024B2 (en) 2002-02-28 2005-10-25 Picarro, Inc. Laser Tuning by spectrally dependent spatial filtering
US6970484B2 (en) 2002-02-28 2005-11-29 Picarro, Inc. Laser tuning by spectrally dependent spatial filtering

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