Abstract:
A semiconductor filter is provided to operate in conjunction with a differential pressure transducer. In one embodiment, a method comprises receiving, at a filter having a plurality of apertures, a pressure, wherein the pressure includes a static pressure component and a dynamic pressure component; filtering, by the plurality of apertures, at least a portion of the dynamic pressure component of the pressure, wherein a diameter of each of the plurality of apertures is such that the plurality of apertures filters at least the portion of the dynamic pressure component of the pressure; outputting, from the filter, a filtered pressure; and wherein the filtered pressure is used to determine the dynamic pressure component of the pressure.

Description:
RELATED APPLICATION 
     This application is a continuation claiming priority under 35 U.S.C. §120 to co-pending U.S. patent application Ser. No. 13/657,525, filed Oct. 22, 2012, entitled “LOW PASS FILTER SEMICONDUCTOR STRUCTURES FOR USE IN TRANSDUCERS FOR MEASURING LOW DYNAMIC PRESSURES IN THE PRESENCE OF HIGH STATIC PRESSURES,” which is a continuation of U.S. patent application Ser. No. 12/938,141, filed Nov. 2, 2010, now U.S. Pat. No. 8,307,713, issued Nov. 13, 2012, entitled “LOW PASS FILTER SEMICONDUCTOR STRUCTURES FOR USE IN TRANSDUCERS FOR MEASURING LOW DYNAMIC PRESSURES IN THE PRESENCE OF HIGH STATIC PRESSURES,” which is a continuation of U.S. patent application Ser. No. 11/716,138, filed Mar. 9, 2007, now U.S. Pat. No. 7,823,455, issued Nov. 2, 2010, entitled “LOW PASS FILTER SEMICONDUCTOR STRUCTURES FOR USE IN TRANSDUCERS FOR MEASURING LOW DYNAMIC PRESSURES IN THE PRESENCE OF HIGH STATIC PRESSURES,” which is a continuation of U.S. patent application Ser. No. 11/100,652, filed Apr. 7, 2005, now U.S. Pat. No. 7,188,528, issued Mar. 13, 2007, entitled “LOW PASS FILTER SEMICONDUCTOR STRUCTURES FOR USE IN TRANSDUCERS FOR MEASURING LOW DYNAMIC PRESSURES IN THE PRESENCE OF HIGH STATIC PRESSURES,” which is a continuation-in-part of U.S. patent application Ser. No. 10/830,796, filed Apr. 23, 2004, now U.S. Pat. No. 7,107,853, issued Sep. 19, 2006, entitled “PRESSURE TRANSDUCER FOR MEASURING LOW DYNAMIC PRESSURES IN THE PRESENCE OF HIGH STATIC PRESSURES,” all of which are assigned to Kulite Semiconductor Products, Inc., the assignee herein, and all of which are hereby incorporated by reference in their entirety as if fully set forth below. 
    
    
     FIELD OF THE INVENTION 
     The invention relates to pressure transducers for measuring low dynamic pressures in the presence of high static pressures, and more particularly to improved low pass filter structures employed with such transducers. 
     BACKGROUND 
     During the testing of jet engines and in many other environments, it is often desirable to measure both the static pressure and the dynamic pressure. The static pressure, in most instances, is usually very high and the dynamic pressure is much lower. The dynamic pressure is also associated with a distinct frequency which occurs at a relatively high rate, for example, five thousand (5,000) cycles/second or greater. In this manner, the dynamic pressure may typically be twenty (20) times less than the static pressure. Hence, to measure static pressure, one requires a transducer with a relatively thick diaphragm so that it can stand the high static pressure. On other hand, such thick diaphragms have a poor response to low pressure. Therefore, to measure static pressure and dynamic pressure is extremely difficult unless one uses a thick diaphragm in conjunction with a thin diaphragm. However, if one uses a thin diaphragm, then this diaphragm will rupture upon application of the high static pressure, which also contains the dynamic pressure. One can think of the dynamic pressure as a relatively high frequency fluctuation on top of a relatively high constant static pressure. Thus, as one can ascertain, using a thick diaphragm to measure dynamic and static pressure is not a viable solution. 
     U.S. Pat. No. 6,642,594 (the “&#39;594 patent”), entitled “SINGLE CHIP MULTIPLE RANGE PRESSURE TRANSDUCER DEVICE”, which issued on Nov. 4, 2003 to A. D. Kurtz, the inventor herein and is assigned to Kulite Semiconductor Products, Inc., the assignee herein, discloses problems with transducers responsive to large pressures utilized to measure low pressures. Thus, pressure transducer adapted to measure relatively large pressures typically suffer relatively poor resolution or sensitivity when measuring relatively low pressures. This is because, as a span of the sensor increases, the resolution or sensitivity of that sensor at the low end of the span decreases. An example of various piezoresistive sensors are indicated in the aforementioned &#39;594 patent wherein different transducers have thinned regions having the same thickness, but different planar dimensions. In this manner, the thinned regions will deflect a different amount upon application of a common pressure thereto, whereby when excited each of the circuits provides an output indicative of the common pressure of a different operating range. 
     As indicated above, during the testing of jet engines there is a very high static pressure, which, for example, may be one hundred (100) psi. Present with the static pressure is a low dynamic pressure, which may exhibit frequencies in the range of five thousand hertz (5,000 Hz) and above. As indicated, using a high-pressure sensor to measure the static pressure will yield an extremely poor response to the dynamic pressure because of the small magnitude of dynamic pressure which can be, for example, about five (5) psi. Therefore, it is desirable to use a relatively rugged pressure transducer having a thick diaphragm to measure static pressure and to utilize another transducer on the same chip having a thinned diaphragm to measure dynamic pressure. Because the thinned transducer is exposed to static pressure both on the top and bottom sides, the static pressure cancels out and does not, in any manner, cause the thinned diaphragm to deflect. As described herein, both static and a dynamic pressure may be applied to the rear side of the diaphragm by a reference tube of substantial length. This reference tube, as will be explained, is a helical structure and has a low resonant frequency. In this manner, when a small dynamic pressure is applied because of the low internal frequency of the tube, the sensor will respond to the static pressure only. The thinned diaphragm should be stopped for pressures in excess of twenty five (25) psi, or some higher number than the desired dynamic pressure. The long reference tube can be made by taking a tubular structure and wrapping it such that it looks like a coil or spring. One end would be inserted into the transducer and other end would be exposed to pressure. In this manner, one can implement a transducer for simultaneously measuring a low dynamic pressure in the presence of a high static pressure. Alternative transducer structures and methods for measuring low dynamic pressure in the presence of high static pressure are also desired. 
     SUMMARY 
     A semiconductor filter is provided to operate in conjunction with a differential pressure transducer. The filter receives both a high and relatively low frequency static pressure attendant with a high frequency low dynamic pressure at one end, and operates to filter the high frequency dynamic pressure to provide only the static pressure at the other filter end. A differential transducer receives both dynamic and static pressure at one input port and receives the filtered static pressure at the other port where the transducer provides an output solely indicative of dynamic pressure. The filter in one embodiment has a series of etched channels directed from an input end to an output end. The channels are etched pores of extremely small diameter and operate to attenuate or filter the dynamic pressure. In another embodiment, a spiral tubular groove is formed between a silicon wafer and a glass cover wafer. An input port of the groove receives both the static and dynamic pressure with an output port of the groove providing only static pressure. The groove filters attenuate dynamic pressure to enable the differential transducer to provide an output only indicative of dynamic pressure by cancellation of the static pressure. 
    
    
     
       BRIEF DESCRIPTION OF THE FIGURES 
         FIG. 1  is a partial cross sectional view of a pressure transducer for measuring low dynamic pressures in the presence of high static pressures. 
         FIG. 2  is a partial cross sectional view of a pressure transducer for measuring low dynamic pressures in the presence of high static pressures employing a semiconductor attenuator according to an embodiment of the present invention. 
         FIG. 3  is a series of top views showing alternate pore configurations useful for the semiconductor attenuator of  FIG. 2 . 
         FIG. 4  is a partial cross sectional view of a pressure transducer responding to dynamic and static pressures employing a semiconductor helical structure operating as an attenuator. 
         FIG. 5A  shows a top view of the semiconductor attenuator utilized in  FIG. 4 . 
         FIG. 5B  shows a cross sectional view of the semiconductor attenuator utilized in  FIG. 4  taken through line B-B of  FIG. 5A . 
     
    
    
     DETAILED DESCRIPTION 
     Referring to  FIG. 1 , there is shown a pressure transducer which basically consists of two leadless peizoresistive sensors  20  and  21  mounted on header pins in accordance with the methods disclosed in Kulite U.S. Pat. No. 5,955,771, entitled “SENSORS FOR USE IN HIGH VIBRATIONAL APPLICATIONS AND METHODS FOR FABRICATING THE SAME,” which issued on Sep. 21, 1999 to A. D. Kurtz et al., the inventor herein and assigned to Kulite Semiconductor Products, Inc., the assignee herein. This patent is incorporated herein by reference. 
     Shown in  FIG. 1  are two separate transducers  20  and  21 , which are fabricated by the same process as according to the teachings of the above-noted co-pending application and patent. The difference between the two transducer or sensor structures is that the sensor structure on the left has a diaphragm  20  which is thicker than the diaphragm  21  of the sensor structure on the right. Both sensors receive on their top surfaces a pressure indicative of the static pressure (P s ) plus the dynamic pressure (P d )(P s +P d ). As indicated, the static pressure (P s ) may be of a relatively high value and, for example, could be one hundred (100) psi or more. The dynamic pressure (P d ) appears as a ripple on top of the static pressure (P s ) and is characterized by a relatively high frequency on the order of magnitude of five thousand hertz (5,000 Hz) and above and a low value of five (5) psi or less. Both sensors receive the combination of the static plus the dynamic pressure shown in  FIG. 1 . Sensor  20 , as indicated, has a thicker diaphragm and responds mainly to the static pressure to produce at the output pins  15 ,  16  associated therewith, a voltage proportional to the static pressure. This voltage would indicate a static pressure of one hundred (100) psi or greater, whatever the case may be. 
     While the output of transducer  20  is also responsive to the dynamic pressure (P d ), the dynamic pressure (P d ) is an extremely small percentage of the total static pressure (P s ) and may, as indicated, be on the order of five (5) psi or less. The thin diaphragm associated with the transducer  21  will respond only to the dynamic pressure (P d ), as will be explained. As seen in the FIG., transducer  21  has the static plus the dynamic pressure applied to the top surface and is indicated again by P s +P d . Coupled to the bottom surface of the diaphragm is a tube or reference tube of an exceedingly long length, designated by reference numeral  18 . The tube  18  is coupled to the bottom surface of the diaphragm. Essentially, the tube  18  receives at an inlet both the static and dynamic pressure, which is P s +P d . 
     The tube, as shown, is in helical form. It is well known that the resonant frequency f of such a tube, as, for example, an organ pipe, is given by f=c/(4l), where c is the speed of sound, and l is the length of the tube. For instance, in air, where the speed of sound is approximately 1,200 feet per second, a tube length of two and a half (2½) feet will give a resonant frequency of one hundred and twenty (120) Hz. Thus, tube  18  acts as a low pass filter and will only pass frequencies which are below one hundred and twenty (120) Hz. In this manner, the dynamic frequency, which is five thousand hertz (5,000 Hz) or greater, will not pass through the tube  18 . Therefore, the underside of the diaphragm associated with transducer  21  only receives the status pressure (P s ). The static pressure (P s ) subtracted from the static pressure plus the dynamic pressure (P s +P d ) supplied to the top surface of the diaphragm such that the output of the differential unit  21  provides a pressure equal to the differential pressure (P d ). As seen, there is a stop member associated with diaphragm  21 . The stop member  25  assures that the diaphragm  21  will not deflect in a downward direction for pressures in excess of 25 psi, or some number higher than the desired dynamic pressure. The reference tube is fabricated by taking a tubular structure, which may be metal or some other material, and wrapping it such that it looks like a coil or a spring where one end is inserted into the transducer, as shown, and the other end is exposed to the static and dynamic pressure. Reference is made to U.S. Pat. No. 6,642,594, entitled “SINGLE CHIP MULTIPLE RANGE PRESSURE TRANSDUCER DEVICE,” issued on Nov. 4, 2003 to A. D. Kurtz, the inventor herein and assigned to the assignee herein, the entire disclosure of which is hereby incorporated by reference herein as well. 
     Therefore, the diaphragm associated with sensor  20  is intended for accurately measuring static pressure. The sensor unit  21  will measure dynamic pressure because of the differential operation of the sensor  21  and because of the tube. These dynamic pressures have relatively high frequencies measured primarily by the first assembly  21 , with the second assembly  20  measuring the steady state pressure, which is a large pressure. The fabrication of stops, such as  25  for transducers, is well known in the art. See, for example, U.S. Pat. No. 4,040,172, entitled “METHOD OF MANUFACTURING INTEGRAL TRANSDUCER ASSEMBLIES EMPLOYING BUILT-IN PRESSURE LIMITING,” issued on Aug. 9, 1997 to A. D. Kurtz et al. and is assigned to the assignee herein. See also U.S. Pat. No. 4,063,209, entitled “INTEGRAL TRANSDUCER ASSEMBLIES EMPLOYING BUILT-IN PRESSURE LIMITING,” issued on Dec. 13, 1997 to A. D. Kurtz et al. and assigned to the assignee herein. The entire disclosures of U.S. Pat. Nos. 4,040,172 and 4,063,209 are also incorporated by reference herein. 
     See also U.S. Pat. No. 6,595,066 (the “&#39;066 patent”), issued on Jul. 22, 2003 to A. D. Kurtz et al. and is assigned to the assignee herein and entitled “STOPPED LEADLESS DIFFERENTIAL SENSOR.” This patent describes a leadless device which is similar to the devices utilized in  FIG. 1  which has a stop apparatus associated therewith. The sensor depicted in the &#39;066 patent also operates as a differential sensor with a Wheatstone bridge sensor array. The output provides a difference between a pressure applied to the top side of the sensor with respect to the force applied to the bottom side of the sensor. This sensor acts as the sensor  21  associated and seen in  FIG. 1 . U.S. Pat. No. 6,595,066 is incorporated by reference herein. 
     See also U.S. Pat. No. 6,588,281, issued on Jul. 8, 2003, entitled “DOUBLE STOP STRUCTURE FOR A PRESSURE TRANSDUCER,” issued to A. D. Kurtz et al. and assigned to the assignee herein. That patent shows a stop device in both first and second directions. As one can ascertain from  FIG. 1 , a stop  25  is only required in the down direction. This is so, as the large pressure P s +P d , as applied to the top surface, could rupture the thin diaphragm if the pressure applied to the bottom surface momentarily is interrupted. In this manner, the diaphragm of the sensor  21  will impinge upon the stop  25  to prevent the fracture of the diaphragm. The interruption of the pressure applied to the bottom surface of the diaphragm could occur during pressure build-up or when the pressure source is first turned on or off. U.S. Pat. No. 6,588,281 is also incorporated by reference herein. 
     Referring now to  FIG. 2 , there is shown a transducer structure in which the helical tube  18  of  FIG. 1  is eliminated. As the tube or organ pipe illustrated in  FIG. 1  may be expensive and/or difficult to fabricate and incorporate, the semiconductor structure of  FIG. 2  operates to emulate the characteristics of the helical tube, including for example, frequency response, without providing such a helical tube. 
       FIG. 2  utilizes the same reference numerals as  FIG. 1  for corresponding parts. It is seen that there are again two sensor diaphragms  20  and  21 , each having piezoresistors located thereon and each receiving a pressure at a top surface, which is the static plus dynamic pressure designated as P s +P d . 
     A reference tube  25  is shown which receives the pressure P s +P d  at the inlet. Disposed between the back surface of transducer  21  and the input of the reference tube  25  is a silicon wafer  26 . 
     The wafer  26  has a plurality of holes or through channels, each having a diameter of less than about 0.001 inches and formed by etching or micromachining, for example. In this case, as indicated in  FIG. 2 , the small diameter holes or apertures serve to attenuate any high frequency components of the pressure caused by viscosity of the gas flowing through the apertures. The pressure and attenuation provided is determined by the diameter of the holes, the number of holes, as well as by the cavity volume on the underside of the sensing diaphragm. 
     The hole diameter, number of holes on the silicon wafer  26 , and the cavity size are selected such that a desired filtering frequency can be obtained utilizing the formula: 
     
       
         
           
             
               τ 
               = 
               
                 
                   32 
                   ⁢ 
                   
                       
                   
                   ⁢ 
                   γ 
                   ⁢ 
                   
                       
                   
                   ⁢ 
                   vVL 
                 
                 
                   
                     AD 
                     2 
                   
                   ⁢ 
                   
                     c 
                     2 
                   
                 
               
             
             , 
           
         
       
     
     wherein τ=attenuation,
         γ represents the ratio of specific heats, for air γ=1.4,   ν represents the kinematic viscosity, for air ν=14.5 m 2 /s or 0.0225 in 2 /s,   V represents the volume of the cavity or wafer,   L represents length of the pipe,   A represents the total area of feeding pipes or apertures,   D represents the diameter of feeding pipe or apertures, and   c represents the speed of sound, which is about 1,120 ft/s at room temperatures.       

     For example; to achieve a cut-off frequency of one hundred (100) Hz, or a time constant of ten (10) milliseconds, the following parameters can be selected:
         D=0.0002 inch   A=0.000625 inch 2  assuming 25% pososity and a 0.050″ chip   c=1,120 ft/s=13,400 inch/s   L=0.005   V=0.001 in 3 .       

     As one can see, attenuation is determined by the diameter of the hole as well as the number of holes. The wafer having the silicon holes acts as a single hole of considerably longer length. The fabrication of holes in silicon is well understood and can be accurately controlled. See for example, an article entitled “POROUS SILICON/A NEW MATERIAL FOR MEMS” published in the IEEE 1996 by V. Lehmann of Siemens Ag Munchen, Germany, which describes a technique for the formation of pores or holes in silicon with high aspect ratios utilizing electrochemical etching of n-type silicon wafers in hydrofluoric acid. 
     The wafer as shown in  FIG. 2  is an n-type silicon wafer. As the article indicates, porous silicon has been used for many years and may be formed on a silicon substrate during anodization in a hydrofluoric acid electrolyte. Pore formation is present for anodic densities below a critical current density. The pore geometry can be controlled, as can the pore cross section. The pore cross section can vary between a circle and a forearm star depending on the formation conditions. Subsequent to the electrochemical pore formation, the cross section of the pores can be made more circular by oxidation steps or can be made more square shaped by anisotropic chemical etching for example using aqueous HF. 
     Referring to  FIG. 3 , there is shown a series of pore cross sections, all of which shapes can be formed during the etching process, and which shapes have been described in the above-identified article. While circular shapes may be preferred, the pores can be of a square or any other suitable configuration represented by shapes designated A through E in  FIG. 3 . 
     While the above-identified article describes process steps which are standard techniques in microelectronic manufacturing, such techniques may be used to develop pore configurations in a silicon substrate, which enable communication between the bottom surface of the substrate to the top surface of the substrate. 
     Based on the diameter of the pores and based on the width of the silicon wafer, one can therefore obtain the same frequency characteristics as are available by a helical tube. The bottom surface of wafer diaphragm  21  thus receives only the static pressure (P s ), whereby the higher frequency dynamic pressure is completely suppressed by the semiconductor wafer  26  having pores of configurations A-E as shown in  FIG. 3 . 
     The pore configurations A to E have various cross sections and will extend from the top surface of the wafer to the bottom surface of the wafer. 
     Referring now to  FIG. 4  there is shown an alternate embodiment of a semiconductor arrangement that emulates the helical tube illustrated in  FIG. 1  and that functions in a manner similar to the apertured wafer structure  26  illustrated in  FIG. 2 .  FIG. 4  illustrates transducer diaphragms  20  and  21  arranged in a housing whereby the static plus dynamic pressure (P s +P d ) is applied to the top surface. The reference tube  25  again receives the static and dynamic pressure, which now is applied to the bottom surface of a semiconductor wafer  28 . The semiconductor wafer  28  has an input aperture  30 , which is directed into a coiled hollow helical structure fabricated on the surface of the semiconductor substrate. The helical structure has an output aperture  31  communicating with the underside of the diaphragm  21 . 
     Thus, the underside of the diaphragm  21  receives the static and dynamic pressure and because of the helical structure fabricated on the semiconductor wafer  28 , the dynamic pressure frequencies are again suppressed. 
     Referring to  FIG. 5 , there is shown a top view of the wafer  28 . The wafer  28  as shown in a cross sectional view of  FIG. 5 b    has a bottom silicon wafer  33  with a glass cover wafer  32 . The silicon wafer is first processed to provide a helical structure  40  on a top surface. The helical structure  40  is fabricated at a given depth. The helical structure communicates with an aperture  30  as shown in  FIG. 4  to enable the static plus the dynamic pressure to be applied to aperture  30 . 
     The pressure is then circulated within the helical structure as covered by the glass cover member  32  and at the output aperture  31  the pressure P s  which is the static pressure now applied to the underside of the diaphragm. 
     It is understood that there are numerous ways of fabricating helical structures in semiconductor material. These can be fabricated by utilizing stacking layers whereby a spiral coil is fabricated between these layers and effectively constitutes a helical semiconductor structure which manifests itself in having the same diameter and length as the helical tube shown in  FIG. 1 . In this case, the length of the spiral determines the frequency of operation according to the following formula: 
     
       
         
           
             
               f 
               = 
               
                 
                   c 
                   
                     4 
                     ⁢ 
                     
                         
                     
                     ⁢ 
                     L 
                   
                 
                 ⁢ 
                 
                   
                     1 
                     - 
                     
                       
                         ( 
                         
                           
                             
                               4 
                               ⁢ 
                               
                                   
                               
                               ⁢ 
                               v 
                             
                             
                               D 
                               2 
                             
                           
                           
                             c 
                             
                               4 
                               ⁢ 
                               
                                   
                               
                               ⁢ 
                               L 
                             
                           
                         
                         ) 
                       
                       2 
                     
                   
                 
               
             
             , 
           
         
       
     
     wherein c=speed of sound, about 1,120 ft/s;
         L=length of pipe or spiral;   D=diameter of pipe or spiral; and   ν=kinematic viscosity: for air, ν is about 14.5 m 2 /s or 0.0225 in 2 /s.       

     In an exemplary configuration, a spiral of 0.005 inch diameter and one (1) inch in length achieves a filtering frequency f of one hundred (100) Hz. 
     By varying lengths and diameters of the holes, as for example concerning the embodiment depicted in  FIG. 2 , one can tailor the frequency attenuation to desired value. According to an aspect of the present invention, such frequency attenuation can be attained in an exceedingly small space. The structures as described herein can be mounted directly behind a deflecting diagram and beyond the header, as shown in  FIG. 2  and  FIG. 4 , for example. 
     It should be noted that after using standard micromachining techniques, a significant number of these structures could be made simultaneously within a relatively small size (of silicon, for example). The processing techniques, as indicated above, will enable such structures to be produced, and hence produce reliable semiconductor attenuators or semiconductor filters for use in static and dynamic pressure measurements. 
     While it is understood that the figures and descriptions herein illustrate a dual transducer structure, it is understood that a single transducer can be utilized, whereby static and dynamic pressure applied to one surface and static and dynamic pressure are applied to the bottom surface or the opposing surface via a semiconductor attenuator such as a semiconductor wafer having through pores from the top to the bottom surface. Alternately, a semiconductor helical arrangement having a hollow passageway from an input port which receives the static and dynamic pressure to an output port which will only allow the static pressure to pass due to the length and diameter of the helix can be employed. 
     It is therefore understood that the above-noted semiconductor structures may replace the mechanical helical design in a more efficient and compact structure while enabling a great number of applications to be provided. While the above noted exemplary embodiments are preferred, it is also understood that alternative embodiments can be employed according to the teachings of this invention. 
     For example, a single transducer such as that depicted by reference numeral  21  can be utilized to produce an output indicative of dynamic pressure and whereby the static pressure would be cancelled. These and alternate embodiments can be ascertained by one skilled in the art and are deemed to be encompassed with the spirit and scope of the claims appended hereto.