Abstract:
A method for treating an article with a plasma jet is disclosed. The method involves rotating an article ( 30 ) with a surface ( 32 ) to be treated about an axis (Ha), wherein the rotation defines a rotation radius extending from the axis. The article surface is contacted with the plasma jet ( 10 ) to form a plasma jet footprint ( 11 ) having a predetermined dimension on the article surface. The plasma jet footprint is moved along the rotation radius in the radial direction according to a velocity profile along the rotation radius so as to apply heat to the article surface to obtain a desired temperature distribution profile on the article surface along the rotation radius. The method provides a means for controlling the temperature of the article uniformly in a temperature range from about 30° C. and 1200° C. to allow different treatment applications to be performed on the article. The control of article temperature as described allows for uniform treatment processes, such as polymer ablation, etching, deposition and thermal treatment, of the article material itself by injecting different gasses into the plasma jet.

Description:
BACKGROUND 
     1. Field of the Invention 
     The present invention relates to a method for treating the surface of articles, such as silicon wafers, with a plasma jet. More particularly, the present invention relates to a method for moving a plasma jet tool relative to the surface of an article being treated by the plasma jet tool. 
     2. Description of the Prior Art 
     A plasma jet is a confined and very intensive heat source. Typically, plasma jet tools have a cross section or footprint which is significantly less than the cross sectional area of a surface of an article, such as a silicon wafer, being treated by the plasma jet. Prior art plasma jet treatment of articles typically involves the production of a plasma jet which is directed at the article&#39;s surface. While the plasma jet is directed at the article&#39;s surface, the plasma jet is moved relative to the surface, usually by linear scanning, such as an X-Y linear scan. 
     Such prior art plasma jet treatment methods using linear scanning can result in damage caused by local overheating of the surface. In the case of silicon wafers, local overheating can result in crystal structure defects, wafer melting, high temperature gradient induced stresses, and breakage. Also, with prior art plasma jet wafer treatment methods, providing uniformity of plasma jet treatment to wafers of differing dimension can be problematic. 
     More specifically, several deficiencies in prior art linear scanning methods include low throughput and high potential for wafer damage. Every linear movement of the plasma jet across the wafer produces hot lanes at the wafer surface with cold surfaces adjacent thereto. The hot lanes tend to produce high temperature gradients, which in turn causes stress in the wafer. In order to avoid high temperature gradients, a delay must be made between adjacent hot lanes to allow for partial cooling of a previous hot lane and lowering of temperature gradients to avoid wafer surface overheating or thermal stress induced wafer damage. As many linear scan movements have to be made to treat the entire wafer surface with sufficient delays to prevent thermal damage to the wafer, resulting wafer treatment throughput suffers. 
     The linear scan methods of the prior art also have the drawback that surface treatment quality suffers due to redeposition on the wafer surface caused by the contact of etch products with cold wafer surface near a hot lane. 
     SUMMARY OF THE INVENTION 
     The present invention relates to a method for treating a surface of an article with a plasma jet. According to the method, an article having a surface to be treated and a plasma jet is provided. The article is rotated about an axis so as to define a rotation radius. The plasma jet is contacted with the surface of the article so as to have a plasma jet footprint of predetermined dimension. The plasma jet is moved along the rotation radius of the article according to a velocity profile so that the surface of the article is heated to obtain a desired temperature distribution profile on the article surface as measured along the rotation radius. 
     It is one object of the present invention to provide a method which can achieve a relatively high process throughput without increasing potential article damager. 
     The foregoing and other objects, features, and advantages will become apparent from the detailed description of the preferred embodiments invention as illustrated in the accompanying drawings. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     The drawings, which are not drawn to scale, include: 
     FIG. 1, which is a schematic diagram of a plasma jet apparatus for carrying out the method of the present invention; 
     FIG. 2, which is a schematic diagram of an alternative plasma jet apparatus embodiment for carrying out the method of the present invention; 
     FIG. 3, which is a plan view of a circular wafer-like article, illustrating the footprint of a plasma jet applied thereto; and 
     FIG. 4, which is a graph showing the relationship of removal thickness of a polymer by ablation for a given velocity. 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     Referring to FIGS. 1 and 2, a plasma jet  10  is produced by plasma jet generator  20  of any known type, which is located in a plasma jet process chamber (not shown). The ambient gas pressure of the plasma jet process chamber is maintained at about atmospheric pressure. In FIGS. 1 and 2, the plasma jet generator  20  is preferably oriented so that the plasma jet  10  is directed upwards, relative to the force of gravity, towards a wafer-like article  30 , such as a silicon wafer, which is held in position on holder  40 . The article  30  may be secured to the holder  40  by a vacuum chuck or any other known article holding means. Article  30  having a surface to be treated  32  is oriented on the holder  40  such that the surface  32  faces the plasma jet  10 , which as illustrated in FIGS. 1 and 2, is a generally downward orientation. Generally, during processing with the plasma jet, the holder  40  is rotated by motor  50  with revolution frequency f. Also, the article  30  is positioned on the holder  40  so that the rotation axis Ha of the holder  40  is coincident with the articles&#39;s inertial center or rotational axis Wa. 
     As will be explained in more detail below, the revolution frequency f of the article  30  about axis Wa, and corresponding duration, is chosen to be less than the time it takes for the temperature of a point on the surface heated at the beginning of a revolution to cool to the temperature the surface point had just before the beginning of the revolution of the article. Under these processing conditions, only a gradual heating of every point on the surface  32  of the article  30  is caused by the crossing of the plasma jet over the surface  32  of the article  30  during rotation thereof. By simultaneously moving the plasma jet along the articles&#39; rotation radius and changing the rotation frequency of the wafer, high temperature gradients and thermal stress damage can be avoided. 
     The duration of the cooling of a point on the surface  32  of an article  30 , such as a silicon wafer, may be estimated by using well-known theory of non-stationary heat conductivity. For example, assuming that article  30  is a silicon wafer with thickness less than about 1 mm, has uniform temperature distribution in volume due to high heat conductivity and that it is cooled mainly by convectional heat transfer to ambient gas with constant temperature T o  from both sides, the wafer&#39;s cooling may be described by the equation          m                 C                 h                     δ        (         T   s          (   t   )       -     T   0       )         δ                 t         =     2        α        (         T   s          (   t   )       -     T   0       )                                
     where: m=Si density; 
     C=Si heat capacitance; 
     h=wafer thickness; 
     Ts(t)=wafer surface temperature; 
     To=ambient gas temperature; and 
     α=heat transfer coefficient. 
     Assuming that just before beginning of revolution (i+1), the temperature of wafer surface was T i  and during the beginning of (i+1) revolution the wafer surface was heated up to temperature T i+1 , then from the equation (1) the wafer revolution duration for which wafer surface temperature decreases from T i+1  back to T i  may be estimated:          t   max     =           m                 C                 h       2                 α            ln        (           T   s          (   t   )       -     T   0           T     i   +   1       -     T   0         )         =         m                 C                 h       2                 α            ln        (         T   i     -     T   0           T     i   +   1       -     T   0         )                                  
     According to the method of the present invention, the duration of every wafer revolution should be chosen so that the temperature of the wafer surface caused by heating from the plasma jet is less than t max  and frequency f of wafer rotation should be chosen f&gt;f min =1/t max . 
     According to the method of the present invention, the plasma jet  10  may be directed at an angle to the article&#39;s surface  32 . The angle between plasma jet  10  and the surface  32  influences the conditions of plasma flowing along surface  32 . Referring to FIG. 3, when the angle of the plasma jet  10  directed at the surface  32  of the wafer  30  is 90°, in other words, when the angle of the plasma jet  10  is normal to the surface  32 , the plasma spot or plasma footprint  11  on the surface  32  tends to be symmetrical and the plasma properties within plasma footprint  11  on the surface  32  are more uniform than when the plasma jet is directed at the wafer surface at an angle which is less than 90°. Preferably, in the method of the present invention, the plasma jet  10  is directed at the surface  32  in a normal orientation so as to provide the uniform footprint  11 . 
     Referring to FIGS. 1 through 3, according to the present invention, the plasma jet  10  is moved relative to the surface  32  typically between a first surface point having maximum rotation radius R max  and a second wafer surface point having a smaller rotation radius R min . Movement of the plasma jet  10  may be done with any trajectory along the surface  32  because only the velocity vector component directed along the wafer rotation radius R is important for realization of this method. The relative movement of the plasma jet may be done by supporting the plasma jet on a rail  70  and connecting the generator  20  to a worm gear or screw transmission  80  which is driven by motor  60 . The rail  70  is placed parallel to surface  32  and along wafer rotation radius R. 
     Because the plasma jet footprint  11  has limited cross sectional dimension d in the plane of the surface  32 , it is convenient to determine the instaneous position of the plasma jet  10  relative to the surface  32  by the measuring or noting the distance between the article rotation axis Wa and the plasma jet axis Ja. Referring to FIGS. 1 and 2, the plasma jet  10  starts interacting with the surface  32  at the point of maximum rotation radius R max  when it is located at position (R+d/2). Due to the rotation of the motor  60 , the plasma jet generator  20  is moved along surface  32  and the plasma jet spot or footprint  11  on the surface  32  is moved towards the article surface points that have a minimal rotation radius, R min . 
     There are two possible variations of movement of the article  30  relative to the plasma jet  10  and the two variations depend on the article type and location of its rotation axis Wa. Referring to FIG. 1, the first variant occurs when the rotation axis Wa is located out of the article  30  and at a distance which is more than d/2 from the outer edge  33  of the article  30 , or when the article  30  has an opening  34  with a dimension which is more than plasma jet footprint  11  dimension d and the wafer&#39;s rotation axis is located within the opening  34  at a distance which is more than d/2 from its inner edge  36 . In these cases, minimal rotation radius R min  is more than half the plasma jet&#39;s footprint&#39;s  11  dimension (d/2). Complete treatment of surface  32  is achieved after reaching a distance which is less than R min +d/2 between rotation axis Wa and plasma jet footprint axis Ja. When the plasma jet  10  reaches its limit, it may be either turned off or moved further and stopped in the range between 0 and R min −d/2 without incurring damage to the article  30 . 
     Referring to FIG. 2, in the second variant, the rotation axis Wa is located out of the article  30  and positioned less than d/2 from the outer edge  33  of the article  30  or the article has an opening  34  having a cross sectional dimension which is larger than the plasma jet footprint  11  dimension d and the article rotation axis Wa is located within the opening  34  and distanced less then d/2 from the inner edge  36  or the article has an opening  34  with a dimension which is less than plasma jet footprint  11  dimension d or no opening at all (R min =0). In these cases minimal rotation radius R min  is less than half the plasma jet footprint&#39;s dimension (d/2). Complete treatment of article surface  32  is achieved after reaching a location which is less than (R min +d/2) between article rotation axis Wa and plasma jet footprint axis Ja. Then the plasma jet has to be either turned off or moved back toward wafer points with R max  and stopped at the distance which is greater than (R min +d/2) between the article rotation axis Wa and plasma jet axis Ja. In the later case wherein the plasma jet is not turned off, the article surface  32  is actually treated twice. 
     Relative movement velocity v(R) is changed by controlling the frequency of motor  50  having a shaft  55  which is connected to holder  40  to cause holder  40  to rotate. The velocity of the plasma jet  10  relative to the article  30  around any rotation radius R is given by 2πfR, and is chosen to be greater than the velocity providing the plasma jet shift in the radial direction of the article, v(R). For one revolution of the article, the heat input from the plasma jet around the rotation radius spreads in the article material due to heat conductivity for a duration time equal to a revolution, t rev . From the theory of non-stationary heat conductivity the heat spreading length I heat  for duration t rev  of wafer revolution may be estimated as:          l   heat     =     3          at   rev                 a   =     λ   mc                            
     where: 
     λis the heat conductivity of wafer material. 
     The requirement for not developing a radial thermal gradient gives the condition: 
     
       
         v(R)t rev &gt;l heat   
       
     
     or          v        (   R   )       &gt;     3          a     t   rev                                  
     For R&lt;d/2, the maximum velocity in the radial direction v max (R) is given by the requirement for uniform treatment, that the plasma jet shift in the radial direction be less than the plasma jet dimension D over the duration of one revolution, t rev . 
     The plasma jet foot print  11  on the wafer surface has dimension d, which is about several centimeters and non-uniform distribution of heat flux. That distribution may be measured by calorimeter or any other known means. 
     Referring to FIG. 3, from the theory of non-stationary heat conductivity, the temperature of an article wafer at a point with coordinate (R, W o ) may be described by differential equation:                m                 C                 h                     δ        (     Δ                   T        (   t   )         )         δ                 t         =         q   pl          (       ρ        (   t   )       ,     ϕ        (   t   )         )       -       q   cool          (     R   ,       W   0        Δ                   T        (   t   )           )                 (*   )                                
     where: 
     ΔT(t)=T s (t)−T o ; 
     T s (t) is article surface temperature at the point (R,W o ) and is less than temperature of article surface material damage; 
     T o  is the ambient gas temperature; 
     q p1 (ρ(t), ρ(t)) is the heat flux distribution from the plasma jet in polar coordinates with instantaneous center at point=0; and 
     q cool (R, Wo, ΔT(t)) is the cooling heat flux at wafer surface point with coordinates (R, W o ). 
     The article is rotated around the axis through the point R=0 and at the same time the distance r(t) between wafer rotation axis and plasma jet center is changed due to relative plasma jet to article movement, v(R) and consequently so: 
     
       
         ρ(t)=R 2 −r 2 (t)−2Rr(t)cos(W(t)+W o )  (**) 
       
     
     
       
         φ(t)=arctan(Rsin(W(t)+W(t)+W o )/(r(t)−Rcos(W(t)+W o ))) 
       
     
     Solution of the equations (*) and (**) by routine numeric integration allows the determination of function r(t) and W(t) which provides a method for achieving required article surface temperature at every article surface point for concrete given conditions. Relative movement velocity function is determined by differentiation of r(t). 
     For practical use the relative movement velocity function may be found by routine experimental procedure. For simplicity the rotation frequency f is fixed and the article  30  is to be heated from initial temperature To the temperature T w (R). In step  1 , the velocity v(R) is chosen arbitrarily from the range limited by the above mentioned conditions and may be taken as constant. In step  2 , one plasma jet pass along the article surface  32  is made. In step  3 , the temperature distribution T heat (R) along article&#39;s radius R is measured. In step  4 , the real temperature distribution T heat (R) is compared with desirable T w (R) and if difference between T heat (R) and T w (R) is unacceptable then the velocity function is changed according to the relation v(R)=((T heat (R)−T o )/(T w (R)−T o ))v(R) and the procedure is repeated from Step  2 . If the difference between T heat (R) and T w (R) is acceptable then the procedure is stopped and found optimal velocity function v opt (R) may be used for article treatment. 
     This procedure may be extended to a general iterative procedure to obtain an optimal velocity function, v opt (R). For each iteration, a new velocity function, v i+1 (R) can be obtained from the previous velocity function v i (R); the measured temperature profile across the wafer, T heat,i (R), obtained when executing the velocity function V i (R); and the previously measured temperature profile, T heat,i−1 (R), obtained when executing the velocity function v i−1 (R): 
     
       
         v i+1 (R)=(T heat,i (R)−T heat,i−1 (R))/T w (R)−T heat,i−1 (R))V i (R)  (iii) 
       
     
     These iterations can be repeated until the measured temperature at all points, T heat,i (R) is acceptably close to the desired temperature T w (R). The velocity function for this iteration can then be used for the temperature treatment process and is an optimum velocity function, v opt (R). 
     In practice, to prevent damage to the article surface  30  due to thermal stress, the temperature distribution after every pass will be constant to within some acceptable temperature difference, T d . The temperature of all points on surface  32 , at all radii, should be within an acceptable temperature difference of the surface point with minimum rotation radius or T w (R)=T(R min )±T d . 
     Having determined v opt (R), the velocity function, v* opt (R), to change the article temperature from T w (R) to another desired temperature T* w (R) may be obtained by: 
     
       
         v* opt (R)=((T* w (R)−T 0 /T w (R)−T 0 )v opt (R)  (iv) 
       
     
     The temperature to which the article should be heated depends on application requirements, for example: 
     1000-1100° C. for poly-Si layer recrystallization; 
     900-1000° C. for activation of ion implanted dopants; 
     500-600° C. for reflowing BPSG; and so on. 
     Plasma jet treatment may be used for thin polymer film removal or polymer photo resist stripping from the article surface. For these applications, the relative movement velocity along article rotation radius is chosen less then velocity providing heating polymer film surface on article surface up to polymer ablation temperature. Specific polymer ablation temperature is usually very close to polymer melting temperature and may be obtained from handbooks on polymer properties. The value v abl (R) which provides that article temperature T abl  is determined from equation (*) or from experimental data and relation that follows from equation (iv): 
     
       
         v abl (R)=((T abl −T o )/(T w −T o ))*v opt (R), 
       
     
     where: v opt (R) is the relative movement velocity known from the experiments providing wafer heating to the temperature T w . 
     If the polymer ablation temperature is unknown then the v abl (R) may be found experimentally by the following procedure. For given inert gas plasma jet parameters, the polymer removal thickness Δh is measured for different values v(R). A typical plot Δh versus v(R) is shown at FIG.  4 . The v abl (R) is the value where the curve has sharp slope change. 
     The velocity v abl (R) is threshold for starting of polymer ablation. All velocity values v(R)&lt;v abl (R) provide polymer ablation and removal without dependence on whether the plasma jet consists of chemical reactants or not. The smaller v(R), the greater removal thickness during each pass. 
     To provide uniform ablation removal of the polymer within the article, the relative movement velocity v(R) (v(R)&lt;V abl (R)) along article rotation radius Wa is changed depending on the distance between plasma jet footprint  11  at the article surface  32  and article rotation axis Wa so that the removal thickness of the polymer at article surface points at all rotation radii be equal to removal thickness at article surface points at the minimum rotation radius. 
     For practical use, the velocity function for the relative movement of the plasma jet relative to the axis of rotation of the article  30  may be determined directly from measured polymer ablation removal by the following steps. First, the velocity v(R) is chosen from the range v(R)&lt;v abl (R); it may be taken as the velocity function that provides uniform heating of the article. Second, one plasma jet pass over the article is made. Third, the polymer thickness removal Δh(R) is measured along the article radius in steps Δr. An average polymer thickness removal Δh av  can then be calculated: 
     
       
         Δh av =(Δr/R max )ΣΔh(R i ) 
       
     
     Fourth, the measured polymer removal Δ(R) is compared to the average removal Δh(R); if the difference between Δh av  and Δh(R) is unacceptable, a new velocity function v*(R) is recalculated according to the function v*(R)=(Δh(R)/Δh av )v(R). If the difference between Δh av  and Δh(R) is acceptable, then the procedure is stopped and then an optimum velocity function v opt (R)=v(R) may be used for polymer removal. In general, an iterative procedure similar to that described for determining an optimum velocity profile for temperature treatment, equation (iii), could be used for repeated iterations with measured polymer removal. 
     To obtain the desired polymer removal thickness Δh des  the velocity v des (R) may be obtained as: 
     v des (R)=(Δh des /Δh av )*v opt (R). 
     If the polymer layer thickness H to be removed is more than the removal thickness Δh for one pass, the treatment is repeated until complete polymer removal is achieved. The minimal necessary quantity N of required passes may be estimated as: N=H/Δh. 
     Referring to FIG. 4, note that for velocity values v(R)&gt;v abl (R), removal by ablation with an inert gas plasma jet is insignificant. In the case that the plasma jet contains chemically active reactants, such as oxygen or hydrogen, then the polymer is removed by the plasma jet by chemical reactions, commonly referred to as ashing, but with a much lower rate than is possible by ablation removal. 
     For providing plasma etching of article material or other materials on the article&#39;s surface  32 , a reactant which is able to produce volatile chemical substance with the material components is added to plasma jet. The greater the reactant concentration in the plasma jet  10 , the greater the etching rate. The reactant may be fluorine containing gas (freon, SF 6 , NF 3 , etc.) for etching Si, poly-Si, SiO 2 , Si 3 N 4 , other Si-based materials, M o , Ti, W, Cr. It may be chlorine containing gas (CCl 4 ) for etching Aluminum. It may be oxygen or hydrogen for etching polymers such as photo resists, or polyimide. 
     To provide uniform etch removal of the material within the article  30 , the relative movement velocity of the plasma jet  10  along the article&#39;s rotation radius R is changed depending on the distance between the plasma jet footprint  11  at the article surface  32  and the article rotation axis Wa to provide a removal thickness of wafer surface material at wafer surface points at all rotation radii be equal to removal thickness at the wafer surface point with minimal rotation radius. During one plasma jet pass along the wafer, the etch removal rate and etch uniformity are determined by the relative movement velocity function v etch (R) for given plasma jet parameters and reactant concentration. For practical use the velocity of function v etch (R) may be found by an experimental procedure provided by the following steps. In the first step, the velocity v etch (R) may be taken as the velocity function providing uniform heating of the article. In the second step, one plasma jet pass along through the wafer is made. In the third step, etch removal thickness Δh(R) along article radius is measured in steps Δr. Average material removal thickness Δh av  is calculated as          Δ                   h   av       =         Δ                 r       R   max              ∑       R   i     =     R   min           R   i     =     R   max              Δ                   h        (     R   i     )                                    
     In the fourth step, the real etch removal thickness Δh(R) is compared with Δh av  and if the difference between Δh(R) and Δh av  is unacceptable then a new velocity function v* etch (R) is calculated according to the relation v* etch (R)=(Δh(R)/Δh av )v etch (R) and the procedure is repeated from the second step. If the difference between Δh(R) and Δh av  is acceptable then the procedure is stopped and the optimal velocity function v opt (R) may be used for uniform etching. 
     To obtain the etch removal thickness desired Δh des , the velocity v des (R) may be obtained from the function v des (R)=(Δh des /Δh av )v etch (R). Again, as described for determining the velocity function for heat treatment, a general iterative procedure similar to equation (iii) can be used to determine an optimum velocity profile for etching. 
     If the material layer thickness H etch  to be removed is more then removal thickness Δh for one pass, the treatment is repeated until necessary etch depth is reached. The minimal necessary quantity N of the passes may be estimated as: 
     N=H etch /Δh. 
     If the etching is conducted through a polymer photo resist mask, the velocity function for relative movement of the plasma jet should be chosen to be more than the ablation threshold velocity for the polymer material to avoid ablation removal of the polymer mask. 
     To conduct plasma enhanced chemical deposition of a thin layer on a wafer surface at least one reactant gas which is able to produce a nonvolatile chemical substance on the wafer surface is added to the plasma jet  10 . As an example, adding SiH 4  to the plasma jet  10  allows deposition of amorphous or poly Si if the plasma jet and process chamber ambient gases are inert. If a mixture of SiH 4  or silica organic substance vapor and oxygen is added to the plasma jet, silicon oxide film is deposited onto wafer surface. 
     For uniform material deposition the relative movement velocity v dep (R) along wafer rotation radius is changed depending on distance between plasma jet at the wafer surface and wafer rotation axis to provide a deposited layer thickness at wafer surface points at all rotation radii that is equal to the deposited layer thickness at wafer surface point with minimal rotation radius. 
     In practice, the velocity function v dep (R) may be found by routine experimental procedure by the following steps. In the first step, the velocity v dep (R) may be taken as velocity providing uniform heating of the wafer. In the second step, one plasma jet pass along through the wafer is made. In the third step, material deposition thickness Δh(R) along wafer radius is measured in increments Δr. The average deposition thickness Δh av  is calculated as          Δ                   h   av       =         Δ                 r       R   max              ∑       R   i     =     R   min           R   i     =     R   max              Δ                   h        (     R   i     )                                    
     In the fourth step, the real deposition thickness Δh(R) is compared with Δh av  and if the difference between Δh(R) and Δh av  is unacceptable then a new velocity function V*dep is calculated according to the relation v* dep (R)=(Δh(R)/Δh av )v dep (R) and the procedure is repeated from the second step. If the difference between Δh(R) and Δh av  is acceptable then the procedure is stopped and found optimal velocity function v opt (R) may be used further for uniform deposition. 
     To achieve desirable deposition thickness Δhd des  the velocity v des (R) may be obtained from the function: v des (R)=(Δh des /Δh av )*v dep (R). Again, as described for determining the velocity function for heat treatment, a general iterative procedure similar to equation (iii) can be used to determine an optimum velocity profile for deposition. 
     If the material layer thickness H dep  to be deposited is more than the deposition thickness Δh for one pass, the treatment steps are repeated until necessary layer thickness is reached. The minimum necessary quantity N of passes may be estimated as: 
     N=H dep /Δh. 
     The methods described for article processing by heating, polymer ablation, etching and deposition may be combined to give multiple processes in a single run. The key factor is control of and capability to change the article temperature described in the above sections. Such an application is to pattern a polysilicon film through a photo resist mask, and then strip the mask in a single process: (1) pattern a polysilicon film by etching the film through a pattern photoresist mask at a low temperature, high average velocity, v(R)&gt;V abl (R), and (2) follow by stripping the photoresist mask by an ablative process using inert gas, no chemically reactive gasses, at a higher temperature, lower average velocity, V(R)&lt;V abl . 
     As will be understood from the foregoing description, according to the present invention, the method may be employed for several plasma jet operations. It is to be understood that the embodiments described herein are merely illustrative of the principles of the invention. Various modifications may be made thereto by persons skilled in the art which will embody the principles of the invention and fall within the spirit and scope thereof. Hence, the present invention is deemed limited only by the appended claims and the reasonable interpretation thereof.