Scanning system for mapping gas flow uniformity in a laser
RIGHTS OF THE GOVERNMENT 
     The invention described herein may be manufactured and used by or for the Government of the United States for all governmental purposes without the payment of any royalty. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     The present invention broadly relates to measurement of operating characteristics of lasers and, more particularly, is concerned with a scanning system for mapping the degree of uniformity of gas flow in the laser cavity. 
     2. Description of the Prior Art 
     The short operating duration of a large Air Force O 2  -I laser, for instance, a period of approximately 30 seconds in length, has made it difficult to achieve a complete understanding of the operating characteristics of the laser. Such understanding is a necessary prerequisite to scaling this laser to higher powers. 
     Particularly, the spatial concentration profile of O 2  molecules and I atoms, as represented by the degree of gas flow uniformity, in the laser cavity is a subject of great concern. Instrumentation presently available is not readily adaptable for use in measuring gas flow in lasers of this type. Consequently, the need exists for a technique for accurately mapping the degree of gas flow uniformity throughout the laser cavity which is relatively easy and inexpensive to carry out. 
     SUMMARY OF THE INVENTION 
     The present invention provides a scanning system designed to satisfy the aforementioned needs. The invention integrates commercially available components to provide a low cost scanning system that maps the spatial concentrations of excited diatomic oxygen molecules and iodine atoms in the gas flow of a large O 2  -I laser. The system can obtain two maps of the gas flow field during the course of a single run cycle. Each map is a graph of a series of electrical voltage output measurements generated by the scanning system which are proportional to the radiation emitted respectively by the O 2  molecules and I atoms in the flowing gas in the laser cavity. A series of spaced transmissive windows, defined by spaced non-transmissive plates disposed along the laser cavity, identify the positions where the voltage output measurements were taken along the laser cavity. 
     Accordingly, the present invention is directed to a scanning system for mapping the degree of gas flow uniformity in a laser cavity, which comprises the combination of: (a) radiation detecting means disposed adjacent a side of the laser cavity in radiation receiving relation thereto for generating a signal proportional to the level of radiation received by the detecting means from the laser cavity, the radiation level being indicative of the concentration of gas flow in the laser cavity; (b) means for moving the detecting means through successive positions along the laser cavity side; and (c) means for identifying portions of the signal which correspond to radiation received at the successive positions of the detecting means along the side of the laser cavity and, thereby, to the concentration of gas flow in the laser cavity adjacent the successive positions therealong. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a fragmentary side elevational view of a scanning system embodying the principles of the present invention. 
     FIG. 2 is a fragmentary top plan view of a series transmissive windows of the scanning system defined along a side of the laser cavity of FIG. 1 as seen along line 2--2. 
     FIG. 3 is an enlarged fragmentary end view of a carriage of the scanning system as seen along line 3--3. 
     FIGS. 4 and 5 are maps in the form of graphs depicting measurements of the distribution of O 2  and I along the laser cavity. 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     Referring now to the drawings, and more particularly to FIG. 1, there is shown the preferred embodiment of the scanning system of the present invention, being generally designated 10. The scanning system 10 is operable for mapping the degree of uniformity of gas flow along lasing axis 11 in the cavity 12 of a laser. 
     The scanning system 10 includes radiation detecting means 14 disposed adjacent a side of housing 16 defining the laser cavity 12 in a radiation receiving relationship with respect to the cavity 12. The detecting means 14 is preferably comprised by an infrared liquid nitrogen-cooled intrinsic GE detector 18 which is a component commercially available, and a pinhole collimator 20 which takes the form of an Al tube with a 1/2&#34; internal diameter and a 3&#34; length. Detector 18 which receives radiation scattered from laser cavity 12 via collimator 20 generates an output signal on data line 22 which is fed to a computer (not shown). The signal is proportional to the level of scattered radiation received by the detector 18 from the laser cavity 12. The scattered radiation level is, in turn, indicative of the concentration of O 2  molecules and I atoms in the gas flow along axis 11 in the laser cavity 12. 
     The scanning system 10 further includes means, generally designates 24 for moving the detecting means 14 through successive positions along the side of housing 16 parallel to axis 11 of laser cavity 12. The moving means 24 includes mounting means 26, guiding means 28 and driving means 30. 
     The mounting means 26 preferably takes the form of a carriage 32 comprised by a flat platform 34 supported by front and rear pairs of casters 36, 38 attached to the underside of the platform by brackets 40. Each of the casters 36, 38 has a central circumferential groove 42 (FIG. 3) formed therein. 
     The detector 18 and collimator 20 are mounted at a central location on the platform by any suitable means. For instance, the collimator 20 may be attached to the lower end of the detector 18 which extends through a suitable opening 44 in the platform 34, with the detector, in turn, mounted in its vertical orientation of FIG. 1 by a concentric sleeve 47 fixed to the upper side of the platform and into the central bore of which the detector 18 is threadably secured: 
     For moving the carriage 32 along the side of housing 16 defining of the laser cavity 12, a linear path of movement is defined by the guiding means 28, preferably in the form of a pair of 3/4&#34; angle tracks 46, and a motive force for moving the carriage 32 along the tracks 46 is provided by the driving means 30. As seen in FIG. 3, the tracks 46 are aligned parallel to one another along the side 16 of the laser cavity 12 and are adapted to be received in the respective grooves 42 of the casters 36, 38. The driving means 30 includes an elongated screw 48 which is drivingly coupled to bracket 50 which, in turn, is rigidly attached to the upper side of the platform 34. Also, a drive motor 52 is operatively connected to the screw for rotatably driving the same. Rotation of the screw 48 in a given direction thus causes movement of the carriage 32 along the linear path defined by tracks 46. Reverse rotation of the screw moves the carriage 32 in the opposite direction. The outer end of the screw 48 and the opposite ends of the motor are supported by brackets 54 in the desired position above the laser cavity 12 and carriage 32. The screw and drive motor are components adapted from a conventional garage door opener. 
     Finally, the scannning system 10 includes means, generally designated 56, for identifying portions of the signal generated by the detector 18 with successive positions of the detector along the side of housing 16 defining laser cavity 12 where radiation generating the signal was received by the detector. In such manner, the concentration of gas flow in the laser cavity and the corresponding portions of the cavity where the successive measurements were taken may be readily determined. Means 56 preferably takes the form of a series of non-transmissive strips or plates 58 mounted in equally spaced apart relationship along a pair of support rails 60. Radiation transmissive windows 62 are defined between the plates 58. 
     Data taken from the scanning system and recorded on a computer is shown in FIGS. 4 and 5. The data in FIG. 4 shows the average of ten sample points taken at each transmissive window. The data is a composite of several tests where the excited oxygen emission was observed. The labels on the horizontal axis referred to the window position numbers. FIG. 5 shows the same type of data for excited iodine atom emission where only one-half of the laser cavity has been mapped (windows 9 through 16). 
     It is thought that the improved scanning system of the present invention and many of its attendant advantages will be understood from the foregoing description and it will be apparent that various changes may be made in the form, construction and arrangement of the parts thereof without departing from the spirit and scope of the invention or sacrificing all of its material advantages the form hereinbefore described being merely a preferred or exemplary embodiment thereof.