CONTAMINANT IDENTIFICATION AND CONCENTRATION DETERMINATION BY MONITORING THE WAVELENGTH OF THE OUTPUT OF AN INTRACAVITY LASER

Abstract: A method and apparatus for detecting the presence of a specific concentration of gaseous species within a calibrated range in a gas sample is disclosed. The ILS gas detection system (10) of the present invention simply comprises an ILS laser (12), a wavelength-selective optical element (52), and an optical detector (16). However, the potential or operational wavelength bandwidth of the ILS laser (12) is preferably entirely included within one of the absorption bands or regions assigned to the intracavity gaseous species being monitored. Thus, within the calibrated range, the presence of the gaseous species changes the output laser wavelength or output intensity at the specific wavelength of the ILS laser (12). Consequently, only the wavelength of the output or the output intensity at the specific wavelength of the ILS laser (12) need be monitored in order to quantitatively determine the concentration of the absorbing gaseous species within a calibrated range when using the ILS method of the present invention.

Description: CONTAMINANT IDENTIFICATION AND CONCENTRAΗON DETERMINATION BY MONITORING THE WAVELENGTH OF THE OUTPUT OF AN INTRACAVITY LASER 0 CROSS-REFERENCE TO RELATED APPLICATION This application is related to the application Serial Number 09/165,884, filed on even date herewith. That application concerns a method for detecting the presence of a specific concentra- 5 tion of gaseous species in a gas sample using an ILS laser without any external wavelength- selective element(s) whereby the total output intensity is used to determine gaseous species concentrations. The present application is directed to the use of an ILS laser with a wavelength- selective element for measuring changes in the spectral output of the laser. 0 TECHNICAL FIELD This invention relates, generally, to the detection of contaminants in gases, and more particularly, to the high sensitivity detection of gaseous molecules, atoms, radicals, and/or ions by laser techniques generally termed intracavity laser spectroscopy. 5 BACKGROUND OF THE INVENTION A laser in its simplest form can be schematically illustrated as including a gain medium that is located between two mirrors. Light within the laser cavity is reflected back and forth be- 0 tween the mirrors, each time passing through the gain medium, which produces optical gain. The mirror coating on the first mirror may be totally reflective, while the mirror coating on the second mirror may be partially reflective, thereby permitting some light to escape from the laser cavity. The spatial region between the reflective surfaces of the mirrors defines the laser resonator or cavity, and in the context of the present invention relates to the so-called "mtracavity region". The intensity of the laser output is a function of both the wavelength region over which the gain medium operates and the reflectivity of the resonator elements. Normally this output is broad and without sharp, distinctive spectral features. The identification of gaseous species, e.g., atoms, molecules, radicals, or ions, via laser spectroscopy requires that the laser output be m a wavelength region where the species absorbs. In conventional applications of lasers to the detection of gaseous species, laser radiation is used to excite a gas sample that is external to the laser in order to produce a secondary signal such as loni- zation or fluorescence. Alternatively, in conventional absorption spectroscopy, laser light is passed through a gas sample that is situated outside of the laser and attenuation that vanes with wavelength is monitored. Some twenty years ago, another detection methodology, mtracavity laser spectroscopy (ILS) was first explored; see, e.g., G. Atkinson, A. Laufer, M. Kurylo, "Detection of Free Radicals by an mtracavity Dye Laser Technique", 59 Journal Of Chemical Physics, pp. 350-354, July 1, 1973. In ILS, a laser itself is used as the detector. The gas sample to be analyzed is inserted mto the optical cavity of a multimode, homogeneously broadened laser. Atkinson et al, supra, showed that by placing gaseous molecules, atoms, radicals, and/or ions in either their ground or excited states mside the optical cavity, the laser output can be altered. In particular, the absorption spectrum of the mtracavity species appears in the spectral output of the laser. Distinct absorption features in the laser output anse from the mtracavity losses introduced by the gaseous species that are absorbing. (As used herein, an absorption feature corresponds to a series of consecutive wavelengths where the light intensity reaches a single local minimum in light intensity in a plot of light intensity versus wavelength.) In a multimode laser, mtracavity absorption losses compete with the laser gam via the normal mode dynamics. As a result, attenuation can be observed in the laser output intensity at wavelengths where the stronger mtracavity absorption features compete effectively against the gam of the laser. The more intense the absorption features, the larger the decrease m the laser output intensity at those wavelengths. By inserting the absorbing gaseous species mside the laser resonator, ILS can provide a detection sensitivity that is enhanced over conventional spectroscopy methods. The enhanced de- tection sensitivity of ILS techniques derives from the non-linear competition between (1) the gam produced m the laser gam medium and (2) the absorber loss(es). As a result, ILS can be utilized to detect both weak absorption and/or extremely small absorber concentrations. Each gaseous species in the optical cavity can be uniquely identified by its respective absorption spectrum or signature. Additionally, the intensity of a specific absorption feature or fea- tures in the spectral signature can be used to determine the concentration of the gaseous species once the sensor is appropriately calibrated. (As used herein, the term "spectral signature" corresponds to the wavelength plotted against absorption intensity or absorbance that uniquely identifies the gaseous species.) The spectral signature of the gaseous species can be obtained by dispersing the output of the ILS laser with respect to wavelength. Two detection schemes are typically employed to disperse the output of the ILS laser and thereby obtain the spectral signature of the gaseous species. The output of the ILS laser can be passed through a fixed-wavelength, dispersive spectrometer, and the specific spectral region that is resolved by this spectrometer can be recorded using a mul- tichannel detector; see U.S. Patent No. 5,747,807, issued May 5, 1998, to G.H. Atkinson et al entitled "Diode Laser-Pumped Laser System for Ultra-sensitive Gas Detection via mtracavity Laser Spectroscopy (ILS)". Alternatively, a spectrometer that can be scanned in wavelength can be employed to selectively resolve different spectral regions that are recorded with a single channel detector, supra. Prior art ILS detection systems employ ILS lasers having a spectral bandwidth that is substantially broad relative to the bandwidth of the absorption features in the absorption spectrum of the intracavity species to be detected; see U.S. Patent No. 5,689,334, issued November 18, 1997, to G.H. Atkinson et al entitled "Intracavity Laser Spectroscope for High Sensitivity Detection of Contaminants". In particular, the laser systems possess an operational wavelength bandwidth that is at least three times as broad as the absorption features of the gaseous species being monitored. Prior art methods of performing ILS, however, while successfully demonstrated in the laboratory, are too large and complex for many commercial applications. In particular, the requirement for a spectrometer fixed in wavelength used in conjunction with a diode array detector or a tunable spectrometer with a single channel detector or a computer to analyze the absorption features, adds to the size and complexity of the detection system. In contrast, the constraints of commercial reality dictate that a gas detector be conveniently sized, relatively inexpensive, and reliable. Thus, what is needed is a methodology that significantly reduces (1) the complexity of ILS measurements and (2) the size of ILS instrumentation, for example, by eliminating the need for a computer. SUMMARY OF THE INVENTION In accordance with the present invention, a method for detecting the presence of a specific concentration of a gaseous species m a gas sample is disclosed. The method compnses: (a) determining that the gaseous species has at least one absorbing band of consecutive wavelengths and determining the concentration of the gaseous species withm a calibrated range, (b) providing an ILS laser comprising- (l) a laser cavity; and (n) a gam medium, wherein the ILS laser is configured to operate only at wavelengths entirely included withm the band of consecutive wavelengths where the gaseous species is absorbing, and the absorption induced by the gaseous species is large enough to change the wavelength or plurality of wavelengths of the laser withm the calibrated range; (c) situating the gam medium such that an output beam from the gam medium is directed through the gas sample that is contained m the laser cavity prior to exiting the laser cav- ity, (d) situating a detector so as to detect the output exiting the ILS laser to quantify either the absolute wavelength or the wavelength relative to a selected wavelength standard (filter or fixed portion of a wavelength dispersive optic); and (e) situating a wavelength-selective optical element outside of the ILS laser and between the ILS laser and the detector such that the output exiting the ILS laser must first pass through the wavelength-selective optical element before reaching the detector, the wavelength- selective optical element only transmitting light having a wavelength within a portion of the output wavelength of the ILS laser. Additionally, a gas detection system for detecting the presence of a specific concentration within the calibrated range of a gaseous species in a gas sample, is provided wherein the gaseous species absorbs light withm at least one single band of consecutive wavelengths and thereby changes the output wavelength exiting the ILS laser by a specific amount The gas detection system compnses- (a) an ILS laser compnsmg (l) a laser cavity; and (n) a gam medium, wherein the ILS laser being configured to operate only at wavelengths entirely included withm the band of consecutive wavelengths where the gaseous species is absorbing and the absorption in- duced by the gaseous species is large enough to change the output wavelength of the laser or the intensity at a specific wavelength within a calibrated range; (b) a container for containing the gas sample in the laser cavity, the container allowing an output beam emanating from the gain medium to pass through the gas sample prior to exiting the laser cavity; (c) a detector for quantifying the absolute laser output power at a specific wavelength; and (d) a wavelength-selective optical element located outside of the ILS laser and between the ILS laser and the detector such that the output exiting the ILS laser must first pass through the wavelength-selective optical element before reaching the detector, the wavelength- selective optical element only transmitting light having a wavelength within a portion of the output wavelength of the ILS laser. In accordance with the present invention, the present inventors have devised a commercially viable contaminant sensor system that is smaller, simpler, and less expensive to construct than any ILS laser system disclosed in prior art. In the present mvention, only a portion of the wavelength output is utilized. As used herein, the portion that is utilized may be any part of the bandwidth that is less than the full output bandwidth. Other objects, features, and advantages of the present mvention will become apparent upon consideration of the following detailed description and accompanying drawings, in which like reference designations represent like features throughout the Figures. BRIEF DESCRIPTION OF THE DRAWINGS The drawings referred to in this description should be understood as not being drawn to scale except if specifically noted. FIG. la is a cross-sectional view depicting a prior art gas detection system comprising an ILS laser, a spectrometer assembly, an optical detector, and a computer for analyzing electrical output from the optical detector; FIG. lb, on coordinates of intensity and wavelength, is a plot of the spectrally resolved output of the prior art ILS laser both (i) when absorbing gaseous species are present in the laser cavity and (ii) when the absorbing gaseous species are not present within the laser cavity; FIG. 2a is a cross-sectional view depicting a gas detection system of the present invention comprising an ILS laser, a wavelength-selective optical element, and an optical detector; FIGS. 2b, on coordinates of wavelength and concentration, is a plot of the output wavelength of the ILS laser of the present invention for two different operational conditions of the ILS laser; FIG. 3 is a schematic representation of another embodiment of the ILS laser of the present invention; and FIG 4, on coordinates of laser mtensity/water absorption (in arbitrary units) and wavelength (in nanometers), is a graph showing the absorption spectrum for high concentrations of water vapor over the wavelengths of 1450 to 1455 nanometers DESCRIPTION OF PREFERRED EMBODIMENTS Reference is now made in detail to a specific embodiment of the present invention, which illustrates the best mode presently contemplated by the inventor for practicing the invention Alternative embodiments are also bnefly descnbed as applicable. The present invention is directed to extremely high sensitivity detection of gaseous species using an ILS sensor. The term "gaseous species" as used herein refers to molecular, atomic, radical, and/or ionic species that may be present in gaseous materials such as those that are used in the fabncation of silicon films. Accordingly, the ILS gas detection system of the present invention may be used to detect the presence of a contaminant (e.g , water) m a gaseous matenal (e.g , mtro- gen). Alternatively, ILS detection may be used to determine if a gas line (e.g., nitrogen gas line) has been sufficiently purged of the gaseous matenal (i.e., nitrogen) FIGS la and lb schematically illustrate the prior art method of performing ILS detection Specifically, in FIG. la, a cross-section of an ILS gas detection system 10 is shown comprising an ILS laser 12, a spectrometer assembly 14, an optical detector 16, and a computer 18 for analyzing electrical output from the optical detector The ILS laser 12 depicted in FIG. la includes a gam medium 20 and a gas sample cell 22 that are situated withm an optical resonator 24 defined by the entire optical path length between mirrors 26 and 28 It will be appreciated that the ILS laser 12 additionally requires a pumping source (not shown), such as an optical pumping source that delivers optical radiation to the gam medium 20 to thereby drive the ILS laser 12 FIG. la shows that laser light generated withm the gam medium 20 is directed to the gas sample cell 22 and passes through the gas sample therein. As described above, gaseous species withm the optical resonator or laser cavity 24 and, m particular, withm the gas sample cell 22, may introduce absorption losses if absorption features are located in the wavelength region where the ILS laser 12 operates. Accordingly, the output beam 32 of the ILS laser 12 can be analyzed to identify the presence of an absorbing gaseous species within the laser cavity 24 by determining if the output beam exiting the ILS laser contains absorption features identical to those in the spectral signature of the gaseous species. It will be noted that the spectral signature contains information on intensity and wavelength. As used herein, an absorption feature corresponds to an absorption line, i.e., a region of consecutive wavelengths observable in a plot of light intensity versus wavelength that includes and surrounds a single local minimum in light intensity (i.e., where absorption reaches a maximum). Each absoφtion line has a finite wavelength bandwidth and a point where the absoφtion reaches a maximum (or the output intensity reaches a minimum). With respect to the present invention, absoφtion features are important because all the wavelengths that make up the absorbing feature are wavelengths where the gaseous species is absorbing. Additionally, as used herein, the term "absoφtion band" is defined as a single uninterrupted wavelength region in the absoφtion spectrum wherein absoφtion occurs at each wave- length. Accordingly, if an absoφtion spectrum contains two absoφtion lines, A, and A 2 , separated by region, B, where no absoφtion is observed, then two absorbing lines, A, and A 2 , correspond to separate absoφtion bands. If, however, the two absoφtion lines A, and A 2 , are only separated by a local absoφtion minimum (or local maximum in intensity), then the two absorbing lines, A, and A 2 , correspond to a single absoφtion band. Since the concentration of the absorbing species will affect the absoφtion spectrum, then the number of absorbing bands in an absoφtion spectrum will vary with concentration. For example, absoφtion lines that are separate and distinct at a first concentration, may at a second, higher concentration, come together and coalesces to form a single absoφtion band. It will be appreciated that the temperature, the generation time, and the pumping power will also affect the output spectrum and the measured absoφtion spectrum. Accordingly, the number of absorbing bands in a measured absoφtion spectrum will also vary with temperature, generation time, and pumping power. To analyze the spectral output of the ILS laser 12, the ILS output beam 32 from the ILS laser is sent to the spectrometer assembly 14, which disperses the output beam with respect to wavelength. In FIG. la, diffraction gratings 38 and 40 are employed to disperse the output beam 32 exiting the ILS laser 12. Lenses 34 and 36 expand the output beam 32 prior to incidence on the diffraction gratings 38 and 40. Lens 42 focuses the output of the spectrometer assembly 14 onto the optical detector 16. In one prior art method, (1) the spectrometer assembly 14 contains a dispersive optical element that can be scanned with respect to wavelength, and (2) the optical detector 16 comprises a single channel detector. FIG. la depicts this scanning dispersive optical element as a diffraction grating 38. The spectral signature of the gaseous species in the laser cavity 24 is obtained by scanning the dispersive optical element (grating 38) while the light transmitted through the spectrometer as- sembly 14 passes through an appropriate aperture 46 placed in front of the (single channel) optical detector 16. (Aperture 46 may simply comprise a slit.) The intensity of the light transmitted through the spectrometer assembly 14 is measured by the optical detector 16 as diffraction grating 38 is scanned. The optical detector 16 outputs an electrical signal to indicate this intensity. (For example, the electrical signal may be proportional to the ILS laser intensity.) Additionally, the spectrometer sends an electronic signal to the computer 18 that indicates the respective wavelength. In this manner, the computer 18 correlates the intensity determined by the optical detector 16 with the wavelength as determined by the spectrometer assembly 14. Thus, the spectrometer assembly 14 and the optical detector 16 are operated in conjunction with the computer 18 to enable the spectral distribution of the output beam 32 emanating from the ILS laser 12 to be meas- ured. FIG. lb schematically illustrates the sort of data obtained from prior art ILS detection methods. Curve 48 represents a typical spectrally dispersed ILS laser output spectrum (or absoφtion spectrum) obtained by scanning the wavelength and measuring the intensity of the light transmitted through the spectrometer assembly 14. At wavelengths where absoφtion features are located, the intensity of the ILS laser 12 is attenuated. Arrows 49 indicate six such absoφtion features. (Curve 50 depicts the spectral distribution of the ILS laser 12 absent any absorbing gaseous species.) The computer 18 can use the absoφtion spectrum shown in curve 48 to identify the gaseous species. In particular, the absoφtion spectrum comprising numerous absoφtion features within the output spectrum of the ILS laser 12 is measured and compared with the known spectral signature of the gaseous species to be monitored. The positions and relative intensities of the specific absoφtion features of the gaseous species can be utilized to uniquely identify the gaseous species to be detected. The concentration or amount of the intracavity gaseous species within the laser cavity 24 can be determined from the magnitude of the absoφtion feature(s) found in the ab- soφtion spectrum when the magnitudes are previously calibrated with known concentrations. In an alternative prior art method, (1) the output beam 32 emanating from the ILS laser 12 is passed through a spectrometer having fixed dispersive optical elements (i.e., gratings 38 and 40 are not scanned), and (2) the optical detector 16 comprises a multichannel detector array. The spectral region over which the ILS laser 12 operates is produced by the spectrometer assembly 14 and is displaced spatially across the (multichannel array) optical detector 16. The aperture 46 (if any) that is placed in front of the optical detector 16 is large enough to allow illumination of a plurality of detectors in the detector array such that multiple wavelengths are simultaneously tracked by the multiple detectors in the detector array. Accordingly, the specific spectral region that is resolved by the spectrometer assembly 14 is simultaneously measured with the (multichannel array) optical detector 16. The computer 18 operates the (multichannel array) optical detector 16 and reads the intensity measured from the multiple detectors therein. Additionally, the spectrometer assembly 14 sends an electronic signal to the computer 18 that indicates the wavelength resolved by the spectrometer assembly 14. The computer 18 is programmed to convert the electronic signals from the (multichannel array) optical detector 16 and the spectrometer assembly 14 mto intensity and wavelength, respectively. In this manner, the computer correlates the intensity determined by the optical detector 16 with the wavelength as determined by the spectrometer assembly 14. Thus, the spectrometer assembly 14 and the (multichannel array) optical detector 16 are operated m conjunction with the computer 18 to measure and record the spectral distnbution of the output beam 32 emanating from the ILS laser 12. An absoφtion signature similar to that shown in FIG. lb may be produced. As described above, the spectral signature is used to identify the gaseous species in the laser cavity 24. The computer records the measured absoφtion bands comprising numerous absoφ- tion features or lines withm the output spectrum of the ILS laser 12 and compares them with the known spectral signature of the gaseous species to be monitored. The concentration of the mtracavity species can be determined from the magnitude of the absoφtion feature(s) found in the spectral signature once the magnitudes are calibrated using known concentrations. It will be appreciated, however, that these prior art methods require the computer 18 to ef- fectively generate a plot of intensity versus wavelength by measuring and recording the intensity at a plurality of wavelengths including the wavelengths corresponding to the absoφtion features as well as the wavelength regions surrounding the absoφtion features where absoφtion is minimal. The method of the present invention, in contrast, is conceptually much simpler than these prior art approaches. Rather than monitoring the distribution of intensities over a plurality of wavelengths, the method of the present invention involves only determining the output produced by the ILS laser 12 during operation, i.e., producing light, withm a portion of the total output bandwidth. The method of the present invention essentially utilizes the change in laser output withm a portion of the bandwidth over which the ILS laser 12 is operating. Thus, absoφtion fea- tures that were measured m pnor art methods by dispersing the laser output are utilized in the present method to affect the output wavelength or intensity at a specific wavelength of the ILS laser 12 Measuring and recording multiple absoφtion features withm the spectrum of the ILS laser 12 is not necessary The method of the present invention is conceptually different from the pnor art method for ILS gas detection in another respect; namely, the ILS laser 12 used m the present invention preferably has a bandwidth comparable to the bandwidth of the relevant absoφtion feature(s) Pnor art methods of ILS detection employ an ILS laser 12 that has a spectral bandwidth that is substantially larger than the bandwidth of the individual absoφtion features associated with the mtracavity species to be detected. In particular, prior art ILS lasers 12 preferably possess an operational bandwidth that is at least three times as broad as the absoφtion features of the gaseous species being monitored Several reasons tend to favor the use of ILS lasers 12 having a bandwidth that is substantially broad relative to the bandwidth of the absoφtion features produced by the gaseous species As descnbed above, the vanous absoφtion features in the spectral signature aid the computer 18 in identifying the particular gaseous species to be detected. Thus, prior art methods of identifying absorbing gaseous species rely on ILS lasers 12 having a spectral bandwidth that is large enough to include more than one absoφtion feature. Additionally, an ILS laser 12 having multiple longitudinal modes is most advantageous since the enhanced detection sensitivity of ILS techniques de- rives mainly from the non-lmear gam versus loss competition of a multimode laser. Consequently, prior art methods employ ILS lasers 12 that have a spectral bandwidth that is large enough to include multiple longitudinal modes. The ILS laser 12 of the first embodiment of the present invention, however, preferably has an operational bandwidth that is comparable to or smaller than the bandwidth of one of the ab- soφtion bands associated with the mtracavity gaseous species being monitored Additionally, to successfully employ the method of the present invention, the operational bandwidth of the ILS laser 12 must be tuned to directly overlap the absoφtion band. (As discussed above an absoφtion band may include a single absoφtion feature or a plurality of consecutive absoφtion features ) The potential or operational bandwidth (Δv laser ) of the ILS laser 12, is defined by the wavelength region over which the gam medium 20 can operate, the spectral charactenstics of the mirrors 26 and 28, and the wavelength regions over which each of the optical elements withm the optical cavity 24 are transmitting. In particular, Δv laser is defined by the convolution of the bandwidth of the gam medium 20 and the mirrors 26 and 28, as well as the bandwidth of any other separate mtracavity optical elements, e.g., pellicle or birefringent tuner within the laser cavity 24 Preferably, the ratio of the operational bandwidth of the ILS laser 12, to the bandwidth of the overlapped portion of the absoφtion band (compnsmg, for example, an absoφtion feature or a plurality of consecutive absoφtion features) is one to one More preferably, the operational bandwidth of the ILS laser 12 is (1) sufficiently broad to maintain multimode operation but (2) suffi- ciently narrow to overlap only the absoφtion band associated with the gaseous species of interest. The overlapped portion of the absoφtion band is hereinafter denoted, W abs , and its bandwidth, Δv abs . As descnbed above, using an ILS laser 12 having a sufficiently broad bandwidth to allow multimode operation preserves the enhanced detection sensitivity that is attainable with ILS However, since the operational bandwidth of the ILS laser 12 is sufficiently narrow to overlap only the absoφtion band associated with the gaseous species to be detected, then the output of a particular wavelength from the laser will be quantitatively altered as the concentration of the gaseous species changes. When the overlapped portion of the bandwidth of the absorbing gaseous species, Δv abs , and the bandwidth of the ILS laser 12, Δv laser , are comparable (i.e., W abs entirely overlaps W laser ), then absoφtion from the mtracavity gaseous species can limit the amount of light generated by the laser at a specific wavelength, thereby causing the output wavelength to shift to another value more favored by the gam properties and reflectivities and transmittances of the ILS laser. The ILS laser 12 cannot operate as efficiently m wavelength regions where absoφtion losses are found. If the absorbing gaseous species is present, then the only region where the ILS laser 12 can operate is occupied by the absoφtion band, which frustrates the operation of the laser at a specific wavelength With higher concentrations of the gaseous species, the absoφtion loss will be higher and the task of generating enough light (or gam) m the gam medium 20 to overcome the loss at a spe- cific wavelength becomes more difficult. Thus, as the concentration of the mtracavity gaseous species increases, the wavelength of the light output from the ILS laser 12 will change. The intensity of the light output at a particular wavelength as a function of mtracavity absorber concentration can be used to calibrate the ILS sensor. This idea can be extended to the special case where at a sufficiently high concentration of absorbing gaseous species, the ILS laser 12 cannot reach threshold at all and will fail to operate. No light output at any wavelength will be produced by the ILS laser Consequently, only the intensity of the output at a particular wavelength of the ILS laser 12 need be monitored in order to quantitatively determine the concentration of the absorbing gaseous species when using the ILS method of the present invention. FIGS. 2a and 2b schematically illustrate the method and apparatus of the present invention, which is directed to detecting gaseous species in a gas sample. In particular, FIG. 2a shows a cross-section of an ILS gas detection system 10 constructed in accordance with the present invention and FIG. 2b, on coordinates of wavelength and intensity, is a plot showing the output wave- length of the ILS laser of the present invention for two different operational conditions of the ILS laser The ILS gas detection system 10 of the present invention simply compnses an ILS laser 12, wavelength-selective optical element 52, and an optical detector 16 to quantify either the output wavelength or the relative change m laser output at a particular wavelength. The ILS laser 12, as depicted in the embodiment of the present invention that is shown in FIG 2a, includes a gam medium 20 and a gas sample cell 22, each of which are situated withm an optical resonator 24 formed between mirrors 26 and 28 Although the laser cavity 24 shown in FIG. 2a is a linear cavity, it will be appreciated that alternative cavity designs can be employed m accordance with the present invention. Such alter- native cavity designs are acceptable as long as the potential (or operational) wavelength bandwidth of the ILS laser 12, Δv laser , is comparable to, i.e., matches one-to-one, or fits withm, the overlapped portion of the bandwidth, Δv abs , of the absoφtion band feature associated with the gaseous species to be detected. The wavelength-selective optical element 52 shown in FIG. 2a compnses a metallized pellicle that acts as a thm high-reflectance Fabry-Perot etalon that provides the required narrowband tuning. The metallization increases the finesse of the etalon and narrows the bandwidth thereby creating a narrow-band bandpass filter. Examples of other wavelength-selective optical elements 52 that may be suitably employed in the present invention include optical bandpass filters, diffraction gratings, prisms, electro-optic bandpass filters, filters operating on polarization properties, filters operating on non-lmear optical properties, and combinations thereof. It will be appreciated that the potential (or operational) wavelength band, W laser , (and bandwidth, Δv laser ) of the ILS laser 12 depends on the gam medium 20 and any optical coatings formed on the optical components that are situated withm the laser cavity 24 as well as any optical coatings formed on mirrors 26 and 28. Accordingly, the gam medium and any coatings on the op- tical components that are used in the ILS laser 12, e.g., mirrors 26 and 28, or windows on the gas sample cell 22, or coatings on crystal 20, can be designed to narrow and tune the potential (or operational) bandwidth, W laser , of the ILS laser to overlap only the absoφtion band associated with the gaseous species to be monitored in the manner described above For the ILS laser 12 depicted in FIG. 2a, the potential (or operational) wavelength band of the ILS laser 12, W laser , is defined by the convolution of the wavelength band over which the gam medium 20 can operate, the wavelength band over which the mirrors 26 and 28 are reflecting, the wavelength band over which mirror 28 is transmitting, as well as the wavelength band over which any of the other intracavity optical elements (e.g., wavelength-selective optical elements) withm the laser cavity 24 are transmitting It will be further appreciated that the ILS laser 12 requires a pumping source (not shown) to dnve the ILS laser at or slightly above its threshold. For example, an optical pumping source may be employed that delivers optical radiation to the gain medium 20. FIG. 2a shows that laser light generated withm the gam medium 20 is directed to the gas sample cell 22 and passes through the gas sample therein. As descnbed above, gaseous species withm the laser cavity 24 and, in particular, withm the gas sample cell 22, may introduce absoφtion losses In accordance with the present mvention, however, the potential bandwidth, Δv laser , of the ILS laser 12 is comparable to the bandwidth, Δv abs , of the overlapped portion, W abs , of the ab- soφtion band associated with the gaseous species being monitored. Thus, absoφtion from the intracavity gaseous species will change the output wavelength of the ILS laser 12, and hence the output intensity at a particular wavelength. Therefore, to determine the concentration of the gaseous species, the ILS laser 12 must be calibrated withm well-defined operating conditions. The output beam 32 that emanates from the laser is detected directly by an optical detector 16 after passing through the wavelength-selective element 52. In its simplest form, the optical detector 16 comprises a single channel detector such as a photodiode, a photoconductor, or a photomultipher tube. Other detectors may suitably be employed in the present invention. The only requirement for the optical detector 16 is that the detector must be able to sense the ILS laser beam 32 and produce a resultant electrical signal. Accord- mgly, an electrical output terminal 54 extending from the optical detector 16 is depicted in FIG 2a. The gas detection system 10 of the present invention differs from the prior art system that is shown in FIG. la m that no computer 18 is employed. The gas detection system 10 depicted in FIG. 2a also does not require a multichannel detector array Additionally, the gas detection system 10 of the present invention may optionally include an additional wavelength-selective optical element 52' withm the laser cavity 24 that narrows and tunes the operational bandwidth of the ILS laser 12 to coincide only with the absoφtion band associated with the gaseous species to be detected. It will be appreciated that since ILS offers increased sensitivity beyond pnor art methods, weak transitions previously not measured may become measurable for the first time with the gas detection system 10 of the present invention. Knowledge of where to tune the ILS laser 12 must be obtained from spectroscopic studies of the gaseous species of interest that show the spectral loca- tion of various absoφtion features. An understanding of how to optically control the wavelength and operational bandwidth of the ILS laser 12 is also required to match the spectral output of the laser with the absoφtion feature (or features). Additionally, to eliminate the possibility of spectral interferences that could lead to false positive readings, spectroscopic studies are required for any additional gaseous species that are likely to be present in a given gas sample. If such additional gaseous species are not to be detected, the spectral output of the ILS laser 12 must be tuned away from any absorbing feature that is produced by these other gaseous species. Potential contnbutions from absoφtion features arising from other gaseous species will then be absent in the wavelength region where the ILS laser 12 emits light. Thus, the operational wavelength of the ILS laser 12 must be chosen (1) to coincide with an absoφtion feature(s) associated with the gaseous species to be detected and (2) to avoid spectral interference from gaseous species that are not of interest. If the foregoing requirements are satisfied, then the spectral interaction with the ILS laser 12 output will be traceable only to absoφtion from the gaseous species to be monitored. Accordingly, the ILS laser 12 output wavelength, when calibrated, will accurately measure the concentration of the monitored gaseous spe- cies. The identity of the gaseous species is known because the selected spectral bandpass of the wavelength-selective optical element 52 is chosen to coincide with a specific portion of the output wavelengths of the ILS laser 12 where only that gaseous species contributes to a change in output intensity. The concentration of the gaseous species is known by calibrating the output wavelength or intensity at a particular wavelength corresponding to the bandpass of the wavelength-selective optical element 52 under well-defined operating conditions with a known concentration of gaseous species in the laser cavity 24. This concentration depends on a specific set of operational parameters that includes temperature, pressure, laser gam, generation time (t g ), i.e., the period over which mtracavity mode competition is permitted to occur, and any other parameter that alters the output wavelength of the ILS laser 12. It will be appreciated that these operational parameters must be held constant to ensure that the gas detection system 10 remains calibrated. Alternatively, varying these operational parameters will change the calibrated sensitivity of the gas detection system, thus enabling multiple calibrations under different well-defined operational conditions to increase the dynamic range of the gas detection system. Regardless, knowledge of the specific operational parameters that affect the output intensity of the ILS laser 12 is required to design a gas detection system 10 that maintains calibration over extended use. Referring now to FIG. 2b, the output intensity of the ILS laser 12 is shown versus wave- length for two different operational conditions. Curve 56 corresponds to the ILS laser 12 operating at a particular concentration with a particular laser output wavelength. Curve 58 corresponds to the ILS laser 12 operating at a different contaminant concentration with a different laser output wavelength Referring now to FIG. 3, a separate embodiment of the present invention is shown. In accordance with the present invention, the potential (or operational) wavelength bandwidth (Δv la ser ) of the ILS laser 12 depicted in FIG. 3 is narrow enough to coincide exclusively with an absoφtion band or region (W abs ) associated with the gaseous species to be monitored. As discussed above, the term "absoφtion band" is defined as a single uninterrupted wavelength region in the absoφtion spectrum wherein absoφtion occurs at each wavelength. Ac- cordmgly, if an absoφtion spectrum contains two absoφtion lines, A, and A 2 , separated by region, B, where no absoφtion is observed, then two absorbing lines, A, and A 2 , correspond to separate absoφtion bands. If, however, the two absoφtion lines, A, and A 2 , are only separated by a local absoφtion minimum (or local maximum in intensity), then the two absorbing lines, A, and A 2 , correspond to a single absoφtion band. In accordance with the present invention, the gas detection system 10 depicted m FIG. 3 comprises an ILS laser 12, a wavelength-selective optical element 52, and an optical detector 16 The ILS laser 12 includes a gam medium 20 that is located withm the laser cavity 24 defined by mirrors 26 and 28. The laser cavity 24 is a linear cavity and the gam medium 20 compnses an ion- doped crystal. The first mirror 26 is formed by depositing a reflective coating on one end 60 of the ion-doped crystal. The second mirror 28 comprises a curved reflector. As in FIG. 2a, an optional wavelength-selective optical element 52' may be included withm the laser cavity 24 Although the laser cavity 24 shown m FIG. 3 is a linear cavity, it will be appreciated that alternative cavity designs can be employed in accordance with the present invention. Such alternative cavity designs are acceptable as long as the operational bandwidth, Δv laser , of the ILS laser 12 is comparable to, i.e., matches one-to-one, or fits withm, the bandwidth of the overlapped portion of the absoφtion band associated with the gaseous species to be detected. In this second embodiment of the present invention, the ion-doped crystal used as a gam medium 20 is a Tm 3+ ,Tb 3+ :YLF crystal. It will be appreciated, however, that other ion-doped crystals may be employed as is suited to the particular use contemplated. Accordingly, it is not intended that the ion-doped crystals specifically disclosed herein, including those listed below, are to be exhaustive. A sampling of ion-doped crystals that can be suitably employed m the method and apparatus of the present invention include Cr:Tm:Ho:YAG, Cr 4+ :YSO, Cr 4+ :YAG, Cr 4+ :YSAG, Er 3+ :GSGG, Er^YSGG, Er^YLF, Er 3+ :Yb 3+ :glass, Ho 3+ :YSGG, Ho 3+ :Tm 3+ :LUAG, Tm 3+ :Ho 3+ :YLF, Tm 3+ :Ho 3+ :YAG, Tm 3+ :Ca Y SOAP, Tm 3+ :YLF, Tm 3+ :glass, Tm 3+ :Ca La SOAP, Tm 3+ :YOS, Tm 3+ :YSGG, Tm 3+ :YAG, Tm 3+ :YN0 4 , Yb 3+ :YAG, Cr:Forstente, Er:Yb:Glass, C0 2 :MgF 2 , Cr^ZnSe, and Cr 2+ :ZnS/ZnSe/ZnTe. Other matenals, whether gas, liquid, or solid, may also be used as the gam medium 20. FIG. 3 additionally shows a gas sample cell 22 located withm the laser cavity 24. The gas sample cell 22 isolates the gas sample from the laser components. It will be appreciated that the gas sample cell 22 is not required for gas samples that are non-corrosive, in which case, the gas sample may be contained withm the entire laser cavity 24. The gas sample cell 22 is provided with an mlet conduit 62 and an outlet conduit 64. Re- spective cell windows 66 and 68 are mounted on the distal ends of the gas sample cell 22 and permit beam 70 to pass through the gas sample to be analyzed. Windows 66 and 68 also seal the gas sample cell 22. In the event that gas sample cell 22 is present withm chamber 72 containing the ILS laser 12, it is necessary that the gaseous species that are to be detected are removed or eliminated from the chamber. By removing the gaseous species from the chamber 72, the system response obtained through use of the gas detection system 10 accurately indicates the presence and amount of the gaseous species contained withm the gas sample cell 22. After purging or evacuating the chamber 72 of gaseous species, the gas sample is fed mto the gas sample cell 22 through inlet conduit 62 and outlet conduit 64 (for example, when the gas sample comprises corrosive gas). However, in such cases where the gas sample does not chemically react with the laser components, the gas sample may be communicated into the chamber 72. As discussed above, the ILS laser 12 requires a pumping source 74 to excite the gam medium 20. Optical excitation of the ion-doped crystal gam medium 20 is provided by the pumping source 74, which comprises a semiconductor diode laser 76 It should be appreciated that pumping source 74 may compnse any suitable optical pumping source, either coherent or incoherent, continuous or pulsed, that will drive the ILS laser 12. For example, pumping source 74 may alternatively comprise a solid state crystal laser (e.g., Νd:YAG), a gas laser, one or more flashlamps, fiber laser, or any other pumping source that is suitable for pumping the ILS laser 12. FIG. 3 shows the semiconductor diode laser 76 being powered by an electrical power supply 78 and being cooled by a thermoelectric cooler 80. The semiconductor laser diode 76 and the thermoelectric cooler 80 are mounted m a heatsmk 82 provided to dissipate heat generated by the semiconductor diode laser. Use of a semiconductor diode laser 76 as a pumping source 74, however, typically requires use of a beam shaping optics 84 to facilitate optical matching between the semiconductor diode laser 76 and the ILS laser 12. Examples of beam modification optics include diffractive optics, refractive optics, gradient index optics wherein the refractive index varies axially, gradient index optics wherein the refractive index vanes radially, micro-optics, and combinations thereof. FIG. 3 shows the beam shaping optics 84 comprising macroscopic optics, which include a pair of anamoφhic pnsms 86 and a pair of lenses 88. Alternatively, a beam expanding telescope or micro-optics that are placed with several micrometers of the semiconductor diode laser 76 may be employed. FIG. 3 further shows a first modulator 90 inserted between the beam shaping optics 84 and the gain medium 20. The first modulator 90 is powered and controlled by a modulator dnver 92. The first modulator 90 alternatively attenuates and transmits the pumping beam 96 emanating from the semiconductor diode laser 76 and thereby periodically prevents the pumping beam from pumping the gam medium 20. In this manner, the first modulator 90 causes the pumping beam 96 to reproducibly pump the gam medium 20 such that the ILS laser 12 will be switched on and off. A second modulator 94 is inserted in the path of the output beam 32 exiting the ILS laser 12. The second modulator 94 alternatively attenuates and transmits the output beam 32 exiting the laser cavity 24 and thereby penodically samples the output beam from the ILS laser 12 by passing the output to the optical detector 16. The second modulator 94 is synchronized to the first modulator 90 so that the first modu- lator 90 penodically allows the total intensity of the pumping beam 96 to reach the gam medium 20 while the second modulator 94 periodically allows the total intensity of the output beam 32 to reach the optical detector 16. Use of both modulators, 90 and 94, provides control over the length of time during which the gam in the gam medium 20 is competing with the absoφtion loss produced by the gaseous species. In particular, the value of t g , generation time, can be adjusted by employing the two modulators, 90 and 94. As used herein, generation time is defined as the penod over which mode competition occurs before measurement withm the ILS laser 12. (Alternatively, the generation time, t g , can be varied without the use of the first modulator 90 and/or the second modulator 94 by pulsing the output of the pumping source 74 thereby causing the pump beam 96 to alternate between a low intensity and a high intensity value to bring the gain medium 20 alternately below and above (or at) threshold.) It will be appreciated that interruption in pumping can be achieved utilizing a variety of means, including, but not limited to using a mechanically operated chopper, an electro-optic or acousto-optic modulator, and a shutter. Alternatively, the electrical power supplied to the pumping source 74 (e.g., semiconductor diode laser 76) can be varied, thereby causing the output of the semiconductor diode laser to fluctuate between high and low intensity levels that periodically bring the gain medium 20 just above and below the threshold required for laser operation. It will be further appreciated that although the second modulator 94 comprises an acousto- optic modulator, other devices such as a mechanically operated chopper or a shutter may be suitably employed in the method and apparatus of the present invention. Alternatively, instead of employing the second modulator 94, optical detector 16 may be alternately switch on and off to periodically sample the output of ILS laser 12. FIG. 3 depicts the output beam 32 from the ILS laser 12 being directed to the optical de- tector 16 through the wavelength-selective element 52. It will be appreciated that the light output from the ILS laser 12 can alternatively be transmitted via an optical fiber link, i.e., an optical fiber or an optical fiber bundle, to a remote site where the optical detector 16 is located. As discussed above, the potential (or operational) wavelength band, W laser , of the ILS laser 12 of the present invention preferably is narrow enough to coincide exclusively with a single ab- soφtion band or region in the absoφtion spectrum of the gaseous species to be monitored. For the ILS laser 12 shown in FIG. 3, wherein the gain medium 20 comprises Tm +3 , Tb +3 :YLF, the wavelength bandwidth directly overlaps a single absoφtion band in the absoφtion spectrum of water vapor. Absoφtion data for water vapor was obtained using an ILS laser 12 similar to that shown schematically in FIG. 3 except that first modulator 90 was not employed. Rather, the electrical power to the semiconductor diode laser 76 was modulated instead. Additionally, a spectrometer assembly 14 similar to that shown in Fig. la was required to disperse the output of the ILS laser 12 to thereby produce the plot depicted in FIG. 4. The ILS laser 12, however, comprised an ion- doped crystal made of Tm +3 , Tb +3 :YLF that was optically excited with the semiconductor diode laser 76. FIG. 4 shows a plot of normalized laser intensity/water absoφtion versus wavelength for a high concentration of water vapor in nitrogen gas. FIG. 4 displays the spectral signature of water vapor for the wavelength region between 1450 to 1455 nanometers in wavelength. Water absoφtion lines at 1452.5 and 1452.1 nanometers are indicated by arrows 98 and 100, respectively. These two absoφtion lines are considered absoφtion features separated by a local minimum in absoφtion. These two absoφtion lines have coalesced to thereby form a single absoφtion band or region that coincides within the bandwidth of the diode pumped Tm +3 , Tb +3 :YLF. FIG. 4 depicts the bandwidth of the diode laser-pumped Tm +3 , Tb +3 :YLF ILS laser to be roughly comparable to (actually slightly larger than) the water absoφtion band created by the two water absoφtion lines. At high enough concentrations, the absoφtion band or region comprising these two lines will entirely overlap and encompass (i.e., be at least as large as) the operational bandwidth of the ILS laser 12. Accordingly, output wavelength from the ILS laser 12 will be changed or the output of the ILS laser changed at a particular wavelength. When the potential or operational bandwidth, Δv laser , of the ILS laser 12 is comparable to the bandwidth, Δv abs , of the overlapped portion of the absoφtion band assigned to the intracavity gaseous species being monitored, the method and apparatus of the present invention can be utilized both to identify and to measure the concentration of the gaseous species. Utilization of the method of the present invention results in an ILS gas detection system 10 that is substantially smaller, simpler, less expensive, and easier to use than prior art ILS sensors that rely on mapping the wavelength distribution of the output of the ILS laser 12. As a consequence of its smaller size, lower cost, and operational simplicity, the gas detection system 10 of the present invention can be directed to a completely distinct set of applications in gas detection. Thus, a method and apparatus has been disclosed for detecting the presence of a concentration of gaseous species within a calibrated range. It will be readily apparent to those skilled in this art that various modifications may be made in the design and arrangement of the elements set forth herein without departing from the scope of the invention as expressed in the appended claims. Moreover, the application of gas detection system 10, as well as the location of the ILS gas detector, e.g., in a semiconductor fabrication assembly, can vary as may be desired. For example, the specific placement of the various elements within the ILS chamber 72 and gas detector system 10 itself may be modified so long as their configuration and placement suitably enables optical excitation of ILS laser 12 in a readily reproducible manner. These and other modifications in the design, arrangement, and application of the present invention as now known or here- after devised by those skilled in the art are contemplated by the appended claims.

Claims: CLAIMS What Is Claimed Is. 1. A gas detection system (10) for detecting the presence of a specific concentration of gaseous species in a gas sample withm a calibrated range, said gaseous species absorbing light withm at least one single band of consecutive wavelengths, said system comprising- (a) an ILS laser (12) compnsing: (I) a laser cavity (24); and (n) a gam medium (20) compnsing an ion-doped crystal, said ILS laser (12) being configured to operate only at wavelengths entirely included with said band of consecutive wavelengths where said gaseous species is absorbing and said absoφtion induced by said gaseous species is large enough to change the output wavelength of the laser (12) or the intensity at a specific wavelength withm a calibrated range; (b) a container (22) for containing said gas sample in said laser cavity, said container (22) allowing an output beam (32) emanating from said gam medium (20) to pass through said gas sample prior to exiting said laser cavity (24); (c) a detector (16) for quantifying the absolute laser output power at a specific wavelength; and (d) a wavelength-selective optical element (52) located outside of said ILS laser (12) and between said ILS laser (12) and said detector (16) such that said output (32) exiting said ILS laser (12) must first pass through said wavelength-selective optical element (52) before reaching said detector (16), said wavelength-selective optical element (52) only transmitting light having a wavelength withm a portion of the output wavelength of said ILS laser (12). 2. The gas detection system (10) of Claim 1 wherein said ILS laser (12) is configured to operate only withm one single region of consecutive wavelengths 3 The gas detection system (10) of Claim 1 wherein said ILS laser (12) comprises com- ponents that prevent said ILS laser (12) from operating at wavelengths outside said band where said gaseous species is absorbing. 4. The gas detection system (10) of Claim 3 wherein an additional wavelength-selective optical element (52') is located withm said laser cavity (24), said wavelength-selective optical element (52') preventing said ILS laser (12) from operating at wavelengths outside said band where said gaseous species is absorbing. 5. The gas detection system (10) of Claim 3 wherein said gam medium (20) has a band- width that is narrow enough to prevent said ILS laser (12) from operating at wavelengths outside said band where said gaseous species is absorbing or has an optical coating thereon that prevents said ILS laser (12) from operating at wavelengths outside said band where said gaseous species is absorbing 6. The gas detection system (10) of Claim 3 wherein said container (22) comprises a gas sample cell (22) located withm said laser cavity (24), said gas sample cell (22) having windows (66, 68) that allow said output beam (32) from said gain medium (20) to pass through said gas sample, at least one of said windows (66, 68) having an optical coating thereon that prevents said ILS laser (12) from operating at wavelengths outside said band where said gaseous species is ab- sorbing. 7. The gas detection system (10) of Claim 3 wherein said laser cavity (24) is formed from at least two mirrors (26, 28) and at least one of said mirrors (26, 28) has an optical coating thereon that prevents said ILS laser (12) from operating at wavelengths outside said band where said gase- ous species is absorbing. 8 The gas detection system (10) of Claim 1 wherein an optical pumping source (74) delivers optical radiation to said gam medium (20) to thereby drive said ILS laser (12). 9. The gas detection system (10) of Claim 1 wherein said band where said gaseous species is absorbing compnses either (a) a single absoφtion feature and said ILS laser (12) has an operational bandwidth that is wide enough to maintain multimode operation and narrow enough to overlap only wavelengths m said single absoφtion feature or (b) a plurality of absoφtion features and said ILS laser (12) has an operational bandwidth that is wide enough to maintain multimode operation and narrow enough to overlap only wavelengths in at least one of said absoφtion features. 10. A method for detecting the presence of a specific concentration of gaseous species m a gas sample withm a calibrated range employing said gas detection system (10) of Claim 1, said method comprising (a) determining that said gaseous species absorbs light within at least one single band of consecutive wavelengths when said gaseous species is present in said gas sample in quantities within the calibrated range; (b) providing said ILS laser (12) of Claim 1; (c) situating said gain medium (20) such that said output beam (32) from said gain medium (20) is directed through said gas sample that is contained in said laser cavity (24) prior to exiting said laser cavity (24); (d) situating said detector (16) so as to detect the output intensity exiting said ILS laser (12) to thereby quantify the output power at a specific wavelength; and (e) situating said wavelength-selective optical element (52) outside of said ILS laser (12) and between said ILS laser (12) and said detector (16) such that said output (32) exiting said ILS laser (12) must first pass through said wavelength-selective optical element (52) before reaching said detector (16), said wavelength-selective optical element (52) only transmitting light having a wavelength within a portion of the output wavelength of said ILS laser (12).

Inventors: ATKINSON GEORGE H, PILGRIM JEFFREY S, ATKINSON, GEORGE, H., PILGRIM, JEFFREY, S.
Applicants: INNOVATIVE LASERS CORP, INNOVATIVE LASERS CORPORATION
Application year: 1999
Main classification: G01N21
IPC codes: G01J3, G01N21, H01S3