CA1271551A - Large volume gaseous electric discharge system - Google Patents

Abstract

Abstract of the Disclosure Large Volume Gaseous Electric Discharge System A laser system having a high power output and a large volume gaseous discharge has a plurality of electrodes at each end of a channel to establish a plurality of discharges and a housing arranged to provide a continuous recirculating lasing gas flow through the channel. An ejector connected to a main circulating pump is fixed to discharge into the recirculating lasing gas flow adjacent the channel to mix lasing gas streams and cause diffusion of the gas and thereby provide a uniform plasma flow in the channel. In one embodiment, magnets are arranged to surround the channel to eliminate thermal instabilities, if they arise, and to further homogenize the lasing gas streams and insure their uniformity.

Description

~7~L551 Description Larqe Volume Gaseous Electric Dischar~e System Technical Field This invention relates generally to a method and an apparatus for controlling gas flow within a laser channel to provide a uniform large volume plasma, and more particularly, to a method and apparatus for providing a mixed and diffused gas flow via recirculation of only a portion of the gas at a velocity substantially higher than that of the remaining gas flow.

Backqround Art One of the problems encountered when a laser system is designed for use in an industrial environment is the compactness, size and reliability of the system.
Lasing action is obtained by subjecting a gas filled vessel or channel to an electric discharge to form a plasma. The electrons provided by the discharge collide with active gas molecules thereby exciting them to higher energy levels, from which they descend to lower energy levels and emit excess energy in the form of photons or light quanta. The density of particles in the higher energy level must exceed that in the lower energy level to achie~e optical gain. The addition of helium to a mixture of carbon dioxide and nitrogen has been found to yield increased output.
An electrical discharge having a large cross sectional area which will uniformly fill large volume cavities regardless of size or shape is mandatory if powerful and reliable lasers suitable for industrial applications are to be developed. An electrical discharge is normally very restricted in diameter because 7~

the temperature in different parts of the discharge is not uniform. This results in lower density and higher current at the inside of the plasma column, thus constricting the column. Individually ballasting a plurality of electrodes offers a partial solution by spreading the emission, but the streams tend to recombine. Judicious use and design of aerodynamic forces to control the ion and electron distribution in a large volume discharge have achieved some success and have resulted in a degree o~ compactness and reduction in size for the same power output, as measured against the very long discharge systems known in the prior art.
Lasers have been used to reduce production costs in those applications requiring cutting, welding, drilling, heat treating, and other processes. However, according to industry publications, laser sales are only about three percent of the machine tool industry.
Industrial application of lasers has been limited in the past because of the limitations of poor reliability, poor beam quality, large size, and heavy weight. ~hese problems, coupled with the high cost of lasers per watt of output, have caused the machine tool industry and other industries, which can use lasers, to proceed very slowly in their implementation. As an example of the size and weight problem, current high power (1 kw and up), continuous wave lasers measure about 22 feet long by 7 feet wide by 5.5 feet high and weigh several tons.
Improved reliability would enable industry to utilize lasers on production lines. Improved beam quality would make industry applications such as hardening or softening of metals, or adhering materials economical~ Miniaturization of structure would open the field of robotics to new applications. Lower costs would mean other equipment could be replaced by lasers.

U.S. Patent 3,581,146 issued May 25, 1971, to A. E~ Hill relates to a method of ballasting a gaseous discharge-tube system wherein a plurality of tubes are excited from a single power source.
U.S. Patent 3,735,2~4 issued May 22, 1973, to A. E. Hill teaches the use of aerodynamic forces to control the spatial distribution of charge in a laser system to obtain a uniform plasma.
U.S. Patent 3,795,838 issued March 5, 1974, to A. E. Hill also shows the use of aerodynamic forces to obtain uniform plasma in a laser system. It is important to note that both this and the previously mentioned patent obtain the desired uniform plasma by recirculation of the entire lasing medium. Accordingly, a portion of the gains obtained in reduced laser size and weight are offset by the necessity oE the large volume compressors.
Refsrence is made to the following publications for those relationships and definitions used herein:
"An investigation of Ejector Design by Analysis and Experiment" by Keenan, Neumann, and Lustwerk; Journal of Applied Mechanics; September 1950; page 299;
"Gaseous Conductors - Theory and Engineering Applications"; James D. Cobine Ph.D.; Dover Publications, Inc., 1958 Edition; and "Basic Data of Plasma Physics" by Sanborn C.
Brown, M.I.T. Press; 1959 Edition.
The present invention is directed to overcoming one or more of the problems as set forth above.

Disclosure of the Invention In accordance with one aspect of the present invention, a laser system having a high power output is comprised of a housing, a gas lasing medium in the housing, a laser channel in the housing, and means for ' ~7i5~1 providing continuous recirculating flow of the gas lasing medium through the channel. A plurality of electrodes are positioned at the upstream end of the housing adjacent one end of the channel, and a plurality of electrodes are positioned at the downstream end of the housing adjacent the other end of the channel. A source of elactrical power connects the electrodes for establishing and maintaining discharges in the channel, and means draws forth a beam of light energy from the channel. A diffusing means provides a uniform plasma flow in the channel and a pressure rise to balance the pressure drop from recirculating flow through the channel. The diffusing means is comprised of an ejector disposed downstream from each respective upstream electrode for mi~ing and diffusing gas streams into the laser channel.
In accordance with another aspect of the present invention, a laser system having a high power output comprises a housing having a gas lasing medium therein, a laser channel in the housing. A means provides continuous recirculating flow of the gas lasing medium through the channel. An electrode is positioned at one end of the channel. An electrode is positioned at the other end of the channel and a source of electrical power is connected to the electrodes for establishing and maintaining discharges in the channel. A means provides a plasma flow in the laser channel, and means surrounding the laser channel generates magnetic fields to cross couple thermal and attachment instabilities.
In accordance with another aspect of the present invention, a laser system for providing a uniform large volume gaseous discharge comprises a housing and a laser channel in fluidic communication with the housing and forming a primary recirculating gas flow path through ~7~l55~L

the housing and the laser ~hannel. A gaseous lasing medium is contained within the housing and laser channel.
A means pressurizes only a portion of the gaseous lasing medium and delivers the pressurized portion of the gaseous lasing medium via a secondary recirculating gas flow path into the lasing channel at a preselected velocity substantially greater than the velocity of the primary recirculating gas.
Thus the large pump previously needed for state of the art lasers is sharply reduced in size, weight, and capacity, leading to higher system efficiency, lower manufa~turing costs, lower input energy requirements, and lower cost per watt of output. The laser has high reliability and exceptionàl beam quality at high power.
Brief Description of the Drawin~s Fig. l is a schematic view of a gas laser embodying the present invention;
Fig. 2 is a sectional view of an ejector diffusing a plurality of lasing gas streams;
Fig. 3 is a sectional view of the ejector of Fig. 2 showing the blending of lasing gas streams;
Fig. 4 is a sectional view of the ejector of Fig. 2 showing the radial component of gas stream and showing the uniform velocity distribution of the lasing gas; and Figs. 5 through 8 are longitudinal sectional views of the laser showing four different means for applying magnetic fields to the lasing gas stream.
Best Mode for Carryinq Out the Invention As more fully disclosed hereinafter, this embodiment provides for mixing and pumping lasing gas streams in a laser having a primary, recirculating, gas ~ ~7~5~j~

stream. Fig. 1 shows a gas laser having the structure shown in more detail in Figs. 2, 3 and 4. The laser assembly has a c~lindrical housing 10 sealed to end walls 12 and 14 to form an enclosed housing. A laser channel 16 is disposed concentric with housing 10, and mirror 18 and output coupler 20 are fixed at opposite ends of the channel. Channel 16 is joined to a frustoconical member 22 having a plurality of equally spaced, cylindrical passages or tubes 24,26 forme~ at an acute angle with the axis of symmetry of the channel and serving as mixing tubes 2~,26 for the gas streams. Main nozzles 28,30 are fixed adjacent each respective mixing tube. Hollow electrodes 32,34 are positioned within and concentric with each respective main nozzle 28,30 and are connected to a source of high voltage electrical power 50 through conductors 56 to provide ths electric discharge for lasing action.
A diffusing means provides a uniform plasma flow in the laser channel 16 to provide a pressure rise to balance the pressure drop from recirculating flow through the laser channel 16. The diffusing means pressurizes only a portion of the gaseous lasing medium and delivers the pressurized portion into the laser channel 16 at a preselected velocity substantially greater than the velocity of the primary recirculating gas. The diffusing means includes a plurality of ej~ctors annularly distributed about the laser channel 16 and a pump 64 fluidicly connected between the primary gas flow stream and the ejectors. Each ejector introduces a secondary gas stream to effect diffusion, turbulence, a pressure rise, and an increase in mass flow. Ballast for the discharge streams may be provided by the device shown in U.S. Patent 3,581,146 identified above. It has been found that an exceptional and unusual characteristic of 1.~7~lS5~

the ejector contributes significantly to the turbulence and diffusion of the lasing gas streams. The ejectors include the primary nozzle 28,30 and the associated mixing tube 26,24. As the high velocity secondary gas stream emerges from the ejector nozzle 28,30 it enters the mixing tube 24,26, which is of a generally cylindrical form, and the gas from the primary recirculating stream is thus entrained by massive collisions between gas molecu]es. Vortices result from the collisions and these vortices blend the several streams homogeneously. The angular velocities of the vortices diminish as the blencled gases progress downstream. An aerodynamic contour is formed at the exit area of the mixing tube to develop a radial components of flow to the blended gas streams. This yields a homogeneous longitudinal flow in the laser channel with uniform radial velocity distribution.
Figs. 2, 3, and 4 show the profile of the mixing tubes 24,26 and, more specifically, the aerodynamic contour formed at the exit area. As viewed in section the tubes 24,26 terminate on one side in a reverse ogee 29 comprising a first curve 31 blending into a second curve 33. The first surface 31 is curved at a first preselected radius in a direction extending radially outward from the longitudinal center of the mixing tube 24, and the second surface (33) is curved at a second preselected radius in a direction radially inward toward the longitudinal center of the mixing tube 24. The second curved surface 33 is positioned intermediate the laser channel 1~ and the first curved surface 31. A radius section 35, opposite the reverse ogee 29, registers with the second curve. This aerodynamic contour is material in the development of a radial component in the gas stream as it exits the mixing - - ~2715~i1 tube. The reaction of the gas stream with the exit contour results in an homogeneous gas flow stream in the contour area and the laser channel with microturbulent, uniform velocity distribution as shown by the flow arrows and wave front profile. Unless the velocity distribution is uniform in cross section, those regions which flow more slowly will become preferentially heated, and these hotter regions become less dense. This leads to an optical disturbance of the laser beam, and can ultimately produce an electric arc.
Laser channel 16 is interrupted as shown by reference characters 40 and 42 to allow recirculation of gas through the housing and into the mixing tubes 24,26, as shown by the flow arrows. Hollow electrodes 44 and 46 are connected to electrical source 50 to complete the discharge circuit. The arrows in Figs. 1, 2, 3, and 4 illustrate the gas streams flow. The primary stream is the recirculating stream which flows through channel 16, out interruptions 40 and 42, through the volume between channel 16 and housing 10 and is entrained by the ejectors which introduce a high velocity secondary gas stream and vortices into th~ mixing tubes as seen in Fig.
3. A series of cylindrical finned heat exchangers, shown generally by numeral 48, are positioned adjacent the interruptions 40,42 to control the lasing gas temperature. Helium under pressure in tanks 52 and 54 is fed to electrodes 32,34,44,46 through piping 56,58.
A lasing gas bleed system for optimum continuous and predictable results is provided to remove impurities including, for example, oil, carbon monoxide, and hydrocarbons from the lasing gas. The system comprises an exhaust pump 60 connected to housing 10 by pipe 62 and having another exhaust pipe 63 leading to an appropriate storage vessel (not shown). A

:~2~

positive-displacement circulating pump 64 is connected to housing 10 by pipe 66 and heat exchanger 68 substantially as shown. Nitrogen gas and carbon dioxide gas under pressure are held in tanks 70 and 72 and are connected to piping 74 and thence to primary nozzles 32 and 34. A
catalytic converter 67 co~verts by chemical reaction any CO formed in the system to CO2. An electric heating system (not shown) is provided to maintain the gas temperature at the proper level for the converter 67 to function. A molecular sieve 69 is provided to prevent the gas from being poisoned by impurities.
A plurality of annu~Lar magnets 80, shown as permanent magnets, embrace laser channel 16 and are longitudinally spaced thsreon for a purpose to be explained.

Industrial Applicability In the operation of the device the circulating pump 64 establishes a pressure to create a high velocity lasing gas flow through catalytic converter 67, heat exchanger 68, piping 74, the annular array of primary nozzles 28,30, and the annular array of mixing tubes 24,26 into the laser channel 16. Flow continues through the laser channel 16, out the interruptions 40,42, around the vanes 76,78, past khe heat exchanger 48, and back into mixing tubes 24,26 in a recirculating mode flow substantially as shown by the arrows~ The operation of the ejector in mixing and diffusing the lasing gas streams results in a uniform, large volume gaseous discharge in the laser channel. Referring now to Figs. 2 and 3 it will be seen that very high velocity gas emerges from each primary nozzle 28,30 and enters its respective mixing tube 24,26. As represented in the figures a relatively conical boundary layer of gas enters the ~7~
-- ~o --mixing tube and flares outwardly in the tube as it progresses down its length. The gas molecules from the recirculating primary gas stream are entrained by the boundary layer's mass velocity. Gas vortices result from the collisions between gas stream molecules traveling at different velocities and the vortices intimately mix and blend the streams. The annular velocity of the vortices diminish as the blended gas stream move downstream and result in complete difEusion of the gas streams and a homoyeneous and uniform gas mixture. In one example of the system the cross sectional area ratio of each respective mixing tube to the throat of each respective primary nozzle is about 27.5 to 1. It is contemplated that other ratios can be used without departing from the scope of the invention; the stated ratio has been shown - to be advantageous.
The laser beam output emerges through the output coupler 20 substantially parallel to the primary gas stream. By a rearrangement of the optical system, the beam output can be made to emerge transverse to the longitudinal axis of channel 16. This system is well and truly shown and illustrated in Fig. 12 of U.S. Patent 3,795,838 identified above. In the present embodiment, a horizontally distributed ejector pump array is substituted for the nozzle block shown in Fig. 12 of the patent.
In the closed cycle or recirculating lasing gas mode, contamination of the lasing gas by oil, dust, impurities, ozone, carkon monoxide or chemical reactions within the system gives rise to serious attachment instability problems and will affect system power output and reliability by poisoning the gas. The catalytic converter 67 and molecular sieve 69 prevent the gas from being poisoned. Heat exchanger 68 dissipates heat and :L~7:1551 thereby cools the lasing gas to optimum temperature. ~n exhaust pump 60 and its associated plumbing 10,62,63 is provided to allow the composition of the lasing gas to be monitored, as by taking periodic samples, so that the optimum gas mixture can be maintained if necessary by introducing fresh gas from tanks 52,54,70,72.
Referring now to Figs. 5 to 8 inclusive, it has been found that in the design of an industrial laser wherein continuity of operation and reliability are material factors, the addition of a magnetic field which interacts with the plasma flowstream insures a homogeneous discharge plasma by inhibiting the growth of thermal instabilities within the discharge. Thermal instabilities are incipient arcs which align with the flowstream and unless controlled prevent a laser from delivering its full power output. If an arc develops it could burn and destroy the laser optical system and will short circuit the laser cavity. Thus, Figs. 5 to 8 illustrate various embodiments of a means surrounding the laser channel 16 for generating magnetic fields to cross couple thermal and attachment instabilities.
Fig. 5 shows the static magnetic field produced by ~he permanent magnets 80 with poles opposed. In this example, the interaction of the field with the flowstream does no work and neither adds nor subtracts energy from the system. The lines of force produce a static resultant undulating magnetic field which rises and falls in strength or intensity in the direction of plasma flow.
As the lasing gas flows it reacts with the undulating magnetic field thus produced and changes the electron flow pattern by giving the electrons a velocity component at right angles to the flow, causing migration of charged particles and mixing of hot and colder regions to prevent ~L ~' t~ r~
~7 the growth of thermal instabilities. A more uniform plasma results.
Fig. 6 shows another embodiment wherein a static magnetic field is produced by D.C. excited electromagnets 78. The field reacts with the lasing gas as in the preceding example and thus changes the electron - flow pattern to yield an homogeneous plasma. It follows, however, that the magnetic field produced by the voltage source 82 is variable in intensity and can be controlled externally by controlling the applied D.C. voltage.
The embodiment shown in Fig. 7 has an elongate electromagnet ~4 embracing a substantial segment of the channel 16. When excited by a D.C. voltage source 83 an axially uniform distributed magnetic field results which prevents development of thermal instabilities by distributing the magnetic lines of force in the direction of the lasing gas flowstream. The action of this field will prevent thermal instabilities by guiding the charged particles in substantially parallel paths in the laser channel.
The Fig. 8 embodiment shows an oscillator 86 which superimposes an A.C. field upon the D.C. field from power supply 85. The interaction of the two energy sources with the [distributed coil] electromagnet ~4 creates an undulating magnetic field at right angles to the direction of lasing gas flow. The work to compress and expand the field is s~pplied by the oscillator and causes a radial direction of motion of charged particles to homogenize the gas. To avoid standing wave-patterns, the oscillator frequency must exceed the gas flow-through time several fold.
The principles described above have been embodied in a 5\kw laser. It has been found that the level of plasma control obtained removes constraints on ~L~71551 -13- 8297-~97 the laser geometry so that large volume cavities can be uniformly filled with plasma, and one can thus design an optimum optical system. Very large and sturdy optical mirrors can now be used/
resulting in a lower flux density and thus preventing warping and destruction from heat. The technology eliminates the necessity for very delicate, fragile, and expensive op-tical systems which are not necessarily adaptable to industrial use.
It is expected that the use of plasma control to uni-formly fill a large volume cavity will allow a 5/kw laser having dimensions of approximately two feet by two feet by one foot, thereby enabling use on a robot arm.
There has been described a high power laser gaseous discharge system which has high reliability and exceptional beam quality at high power, but at reduced size and weight. It will be apparent to those skilled in the art that changes may be made in the construction and arrangements without departing from the scope of the invention as defined in the appended claims. Other aspects, objects, and advantages of this invention can be obtained from a study of the drawings, the disclosure and the appended claims.

Claims (40)

Claims

1. A laser system having a high power output comprising a housing, a gas lasing medium in the housing, a laser channel in the housing, means for providing continuous recirculating flow of the gas lasing medium through the channel, a plurality of electrodes at the upstream end of the housing adjacent one end of the channel, a plurality of electrodes at the downstream end of the housing adjacent the other end of the channel, a source of electrical power connected to the electrodes for establishing and maintaining discharges in the laser channel 16, diffusing means for providing a uniform plasma flow in the channel and for providing a pressure rise to balance the pressure drop from recirculating flow through the channel, the diffusing means comprising an ejector disposed downstream from each respective upstream electrode for mixing and diffusing gas streams into the laser channel, and means to draw forth a beam of light energy from said channel.

2. A laser system, as set forth in claim 1, wherein each ejector comprises a primary nozzle and a mixing tube, each primary nozzle being connected to a source of lasing gas pressure external to the housing.

3. A laser system, as set forth in claim 2, including a heat exchanger disposed external to the housing and being in fluidic communication with the primary nozzle.

4. A laser system, as set forth in claim 2, wherein each mixing tube has an aerodynamic contour formed at its exit area.

5. A laser system, as set forth in claim 4, wherein the aerodynamic contour comprises a reverse ogee curve on one side of the mixing tube and a radius section on the other side to impart a radial component to the gas stream flow upon exit.

6. A laser system, as set forth in claim 1, including means surrounding the laser channel to generate magnetic fields to cross couple thermal and attachment instabilities.

7. A laser system, as set forth in claim 6, wherein the magnetic field generating means comprises a plurality of annular permanent magnets spaced longitudinally on the laser channel 16 and embracing the channel.

8. A laser system, as set forth in claim 6, wherein the magnetic field generating means comprises a plurality of electromagnets spaced longitudinally on the laser channel, and a source of D.C. voltage connected to the the electromagnets.

9. A laser system, as set forth in claim 1, wherein each electrode has a passage formed therein and is disposed in concentric relation within each of the primary nozzles and is connected to a source of helium gas to introduce metastable helium atoms into the gas streams.

10. A laser system, as set forth in claim 2, wherein the cross sectional area ratio of each respective mixing tube to the throat of each respective primary nozzle is about 27.5 to 1.

11. A laser system, as set forth in claim 1 wherein the means to draw forth a beam of light energy from the laser channel comprises a pair of mirrors disposed in mutually facing relation and fixed one at each end of the laser channel to direct an output beam in a direction parallel to the laser channel.

12. A laser system, as set forth in claim 1, wherein the means to draw forth a beam of light energy from the laser channel comprises an optical system arranged to direct the beam in a direction transverse to lasing gas flow and in a direction transverse to the laser channel.

13. A laser system, as set forth in claim 1, wherein the source of electric power includes means for providing independant current regulation of each electrode.

14. A laser system, as set forth in claim 1, including a heat exchanger disposed intermediate the laser channel and the housing whereby the continuous recirculating flow of the gas lasing medium passes through the heat exchanger.

15. A method of mixing lasing gas streams for pumping a CO2 laser having a plurality of parallel discharges between electrodes to give a uniform large volume gaseous discharge in a laser channel, comprising the steps of:
guiding a primary lasing gas stream in a recirculating path wherein a pressure drop results;

introducing a secondary lasing gas stream at a higher pressure into the the first gas stream to effect diffusion of the streams, a pressure rise equal to the recirculating path pressure drop, and an increase in mass flow through the channel.

16. A method, as set forth in claim 15, including the step of introducing a third gas stream of helium through the electrodes to introduce metastable helium atoms into the gas streams and to inhibit metal sputtering.

17. A laser system having a high power output comprising a housing having a gas lasing medium therein, a laser channel in the housing, means for providing continuous recirculating flow of the gas lasing medium through the channel, an electrode at one end of the channel, an electrode at the other end of the channel, a source of electrical power connected to the electrodes for establishing and maintaining discharges in the laser channel, means for providing a plasma flow in the channel, and means surrounding the laser channel for generating magnetic fields to cross couple thermal and attachment instabilities.

18. A laser system, as set forth in claim 17, wherein the magnetic field means includes a plurality of annular permanent magnets spaced longitudinally along the laser channel.

19. A laser system, as set forth in claim 18, wherein each of the permanent magnets is positioned adjacent the permanent magnet of opposing polarity.

20. A laser system, as set forth in claim 17, wherein the magnetic field means includes a plurality of electromagnets spaced longitudinally along the laser channel, and a source of D.C. voltage connected to the electromagnets.

21. A laser system, as set forth in claim 20, wherein each of the electromagnets is connected to the source in opposing polarity so that adjacent electromagnets are of opposing polarity.

22. A laser system, as set forth in claim 17, wherein the magnetic field means includes an electromagnet positioned about a substantial segment of the laser channel.

23. A laser system, as set forth in claim 22, wherein the electromagnet is connected to a D.C. voltage source.

24. A laser system, as set forth in claim 23, including an oscillator connected in series intermediate the electromagnet and the D.C. voltage source.

25. A laser system, as set forth in claim 24, wherein the oscillator operates at a frequency directly related to the rate of the recirculating flow.

26. A laser system for providing a uniform large volume gaseous discharge, comprising:
a housing;
a laser channel being in fluidic communication with the housing and forming a primary recirculating gas flow stream through the housing and the laser channel;

a gaseous lasing medium contained within the housing and laser channel; and means for pressurizing only a portion of the gaseous lasing medium and delivering the pressurized portion of the gaseous lasing medium via a secondary recirculating gas flow stream into the laser channel at a preselected velocity substantially greater than the velocity of the primary recirculating gas.

27. A laser system, as set forth in claim 26, wherein the means includes at least one ejector having a mixing tube connected intermediate the laser channel and housing forming a portion of both the primary and secondary gas flow streams, a primary nozzle fixed adjacent to the mixing tube and adapted for delivering the secondary gas flow into the mixing tube, and a pump fluidicly connected between the primary gas flow stream and the primary nozzle.

28. A laser system, as set forth in claim 27, wherein the means includes a plurality of ejectors equally spaced about the laser channel and having a plurality of mixing tubes and primary nozzles connected to the pump.

29. A laser system, as set forth in claim 27, wherein the ratio of the cross sectional areas of the mixing tube and nozzle 30 have a ratio of approximately 27.5 to 1.

30. A laser system, as set forth in claim 27, including the laser channel having an axis of symmetry substantially parallel to the primary gas flow stream wherein the mixing tubes opens into the laser channel at an acute angle with the axis of symmetry.

31. A laser system, as set forth in claim 30, wherein the mixing tube includes an aerodynamic contour on an inner surface of the mixing tube adjacent the opening into the laser channel.

32. A laser system, as set forth in claim 31, wherein the aerodynamic contour includes the inner surface of the mixing tube having a reverse ogee adjacent the downstream connection of the mixing tube and laser channel and a radius section opposed to the reverse ogee adjacent the upstream connection of the mixing tube and laser channel.

33. A laser system, as set forth in claim 32, where the reverse ogee includes the inner surface of the mixing tube having first and second curved surfaces, the first surface being curved at a first preselected radius in a direction extending radially outward from the longitudinal center of the mixing tube, and the second surfaced being curved at a second preselected radius in a direction radially inward toward the longitudinal center of the mixing tube, the second curved surface being intermediate the laser channel and the first curved surface.

34. A laser system, as set forth in claim 27, wherein the primary nozzle includes a hollow electrode disposed in concentric relation within the primary nozzle and connected to a source of electrical power and a source of helium gas whereby the metastable helium atoms inhibit metal sputtering of the electrode.

35. A laser system, as set forth in claim 34, including a hollow electrode adjacent the end wall and connected to the source of electrical power and to a source of helium gas whereby the metastable helium atoms inhibit metal sputtering of the electrode.

36. A laser system, as set forth in claim 26, wherein the secondary gas flow stream includes a catalytic converter.

37. A laser system, as set forth in claim 26, wherein the secondary gas flow stream includes a molecular sieve.

38. A laser system, as set forth in claim 26, wherein the secondary gas flow stream includes a heat exchanger.

39. A laser system, as set forth in claim 38, wherein the heat exchanger includes a first heat exchanger disposed intermediate the laser channel and the housing and forming a portion of both the primary and secondary gas flow streams.

40. A laser system, as set forth in claim 39, wherein the heat exchanger includes a second heat exchanger disposed external to the housing and forming a portion of only the secondary gas flow stream.