Abstract:
Embodiments of an ultra miniature pressure probe are disclosed. The pressure probe can include a probe body, a plurality of transducer ports, and a plurality of transducers. The probe body can be a longitudinal tubular body having a front conical end. The transducer ports can be disposed about the front end of the body. The transducers can be leadless SOI transducers, each having an active deflection area associated with a semiconductor substrate. Each transducer can be in communication with a header for supporting the transducer. The header can have a thickness substantially less than the probe diameter and can comprise a flange about an edge of the header. Each of the plurality of transducer ports can define an aperture and a counter-bore, wherein each transducer is positionable in an associated transducer port with the flange of the header of the transducer being welded to the counter-bore of the transducer port.

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
     This application is a continuation application claiming priority to co-pending U.S. patent application Ser. No. 12/686,847, filed 13 Jan. 2010, which is a continuation-in-part of U.S. patent application Ser. No. 12/315,438, filed 3 Dec. 2008, which is a continuation of U.S. patent application Ser. No. 11/983,009, filed 6 Nov. 2007, now U.S. Pat. No. 7,484,418. The contents and substance of these applications are incorporated by reference as if fully set forth below. 
    
    
     TECHNICAL FIELD 
     This invention relates to multi-hole pressure probes and more particularly to a multi-hole pressure probe containing piezoresistive sensors fabricated utilizing silicon-on-insulator (SOI) techniques. 
     BACKGROUND 
     The so-called multi-hole pressure probe has been a standard technique for measuring mean flow angles, stagnation, and static pressures for over four decades. Generally, these probes make use of the known (through experiment or analysis) geometrical variation of all static pressure on fixed shapes (sphere, cylinder, wedge, etc.) which changes in a repeatable way as a function of that shape&#39;s orientation to the flow. Since the Mach number is a unique function of the ratio of stagnation to static pressure, it can also be derived from the pressures measured by such a probe. Up to two orthogonal flow angles as well as stagnation and static pressure can be deduced from pressures measured at four or five well chosen locations on the probe (using five rather than four measurement locations generally improves the accuracy but requires a larger probe). Fewer measurements yield fewer flow variables. For example, if the probe size is a concern, then two measurements can be used to find either one flow angle or stagnation and static pressures. The static pressure ports on these steady state probes are usually connected to remote pressure transducers via long lengths of small diameter tubing. This restricts their time response to several seconds or longer. 
     With the advent of miniature semiconductor pressure transducers in the late 1960&#39;s the pressure transducer could be moved much closer to the measurement location by mounting it in the probe body itself, thus enhancing the time response of the measurement. Such miniature semiconductor transducers were provided by Kulite Semiconductor Products, Inc., the assignee herein. Kulite Semiconductor Products, Inc. has many patents relating to miniature pressure transducers. The development of a miniature semiconductor pressure transducer led to the evolution of a class of so called high frequency response probes, with frequency responses in the kilohertz (KHz) range. Because of the relatively high drift rate of early semiconductor transducers, these probes were only used for unsteady measurements. Conventional remote transducers, fit through separate ports for use in high accuracy measurements of the steady state values. The new technology enabled the fabrication of probes that can survive harsh environmental characteristics as determined by the needs of industry and government, aero propulsion test facilities and the like. 
     High frequency response of these probes are set by three factors: (1) the frequency response of the transducer (generally much higher than other factors and so not limiting); (2) the resonant frequency of any cavity between the surface of the probe and a transducer diaphragm; and (3) the vortex shedding frequency of the probe body (which scales with the probe size and the fluid velocity). The latter two factors, 2 and 3 scale with the probe size so that smaller probes will yield higher usable frequency response. 
     Recent advances in semiconductor transducer technology have greatly improved the stability and accuracy, as well as increase the temperature range of the transducer. These advances combine to suggest that very small probes with wider dynamic range can measure the entire frequency range from steady state to over 10 KHz. Therefore, to improve the frequency response of such probes a smaller, flatter sensor with no cavities is required. In addition, the static responses of the transducers used in the probe are limited by the static properties of the sensors used in these probes. The sensing diaphragm made by solid state diffusion uses a P-N function to isolate the sensing network from the lower underlying bulk deflecting member. Since it is made using P-N junction isolation, of course static thermal properties are now limited in their upper temperature usefulness. Recent work has resulted in the manufacture of a new type of piezoresistive sensor using SOI techniques wherein the piezoresistive network is isolated from the deflecting material by an oxide layer, while being molecularly attached to it such is shown in FIG. 1 of U.S. Pat. No. 5,286,671 entitled, “Fusion Bonding Techniques for Use in Fabricating Semiconductor Devices,” by Dr. A. D. Kurtz and assigned to Kulite Semiconductor Products, Inc., the assignee herein. The process for fabricating the composite dielectrically isolated structure requires the use of two separate wafers. The first “pattern” wafer is specifically selected to optimize the piezoresistive performance characteristics of the sensor chip, while the second “substrate wafer” is specifically selected for optimizing the micromachined capabilities of the sensing diaphragm. A layer of the higher quality thermally grown oxide is then grown on the surface of the substrate, while the piezoresistive patterns are introduced onto the pattern wafer. The piezoresistive patterns are diffused to the highest possible concentration level, equal to solid solubility, in order to achieve the most stable, long term electrical performance characteristics of the sensing network. Once the pattern and the substrate wafers are appropriately processed, the two wafers are fusion bonded together in accordance with the above-noted U.S. Pat. No. 5,286,671. The resulting molecular bond between the two wafers is as strong as the silicon itself, and since both the sensing elements and the diaphragm are made from the same material, there is no thermal mismatch between the two, thus resulting in a very stable and accurate performance characteristic with temperature. The presence of dielectric isolation enables the sensor to function at very high temperatures without any leakage effects associated with the P-N junction isolation type devices. Since the device is capable of operating at high temperatures, a high temperature metallization scheme is introduced to enable the device to interface with the header at these high temperatures. 
     The transducer formed by the techniques depicted in U.S. Pat. No. 5,286,671 as indicated above, enables the use of a probe which has an improved high frequency operation while being extremely small. The probe is basically a longitudinal tubular member having a front probe surface which contains holes or apertures. Each hole or aperture is associated with a separate transducer where each transducer contains a separate housing, which housing fits into the hole in the transducer probe. When mounting each transducer in its own miniature header, multiple transducers can be used simultaneously in a probe while further enabling the probe to be very small (less than 100 thousands of an inch, i.e. 100 mils, in diameter). 
     SUMMARY 
     A miniature pressure probe is disclosed herein. The pressure probe comprises: a longitudinal tubular body symmetrically disposed about a central axis and having a given diameter, the body having a front conical end and a back end, a plurality of transducer accommodating ports disposed about the front end, a plurality of leadless SOI transducers each having an active deflection area associated with a semiconductor substrate, each transducer having a header for supporting the same, with the transducer header having a thickness substantially less than the probe diameter, with each header and transducer positioned in an associated transducer port of the probe and operative to respond to flow pressure. Additionally, the header can comprise a flange weldable to a counter-bore and its associated transducer port, so as to seal the transducer header to the probe body. 
    
    
     
       BRIEF DESCRIPTION OF THE FIGURES 
         FIG. 1  is a cross-sectional view of a transducer and header arrangement fabricated by SOI technology. 
         FIG. 2  is a perspective view of a transducer showing a glass contact wafer positioned above a silicon sensor wafer according to an embodiment of this invention. 
         FIG. 3  consists of  FIGS. 3A-3B , with  3 A being a front view of a probe, while  FIG. 3B  is a cross-sectional view taken of the same probe taken through line A-A of  FIG. 3A . 
         FIG. 4  consists of  FIGS. 4A-4B , with  FIG. 4A  being a top view of a transducer having a housing according to this invention.  FIG. 4B  is a cross-sectional view of the housing and sensor arrangement of  FIG. 4A . 
         FIG. 5  consists of  FIGS. 5A-5B , with  FIG. 5A  being a front view of a probe having a sensor assembly according to this invention.  FIG. 5B  shows a cross-sectional view of the sensor of  FIG. 5A  having an angled probe body. 
         FIG. 6  consists of  FIGS. 6A-6B  depicting an angle and static probe front view in  FIG. 6A  and depicting a cross-sectional view of the angle and static probe taken through line A-A of  FIG. 6A . 
         FIG. 7  consists of  FIGS. 7A-7B  illustrating a transducer structure in which a header of the transducer comprises a weldable flange.  FIG. 7A  illustrates a front view of the transducer structure, while  FIG. 7B  illustrates a cross-sectional side view. 
         FIG. 8  consists of  FIGS. 8A-8B  illustrating a receiving portion of the probe body having a counter-bore for receiving the flange of the transducer structure.  FIG. 8A  illustrates a front view of the transducer structure, while  FIG. 8B  illustrates a cross-sectional side view. 
         FIG. 9  consists of  FIGS. 9A-9B  illustrating an all-welded 5-sensor probe, with  FIG. 9A  being a front view and  FIG. 9B  being a cross-sectional side view of the probe. 
         FIG. 10  consists of  FIGS. 10A-10B  illustrating an all-welded 4-sensor probe, with  FIG. 10A  being a front view and  FIG. 10B  being a cross-sectional side view of the probe. 
     
    
    
     DETAILED DESCRIPTION 
     According to an embodiment of the invention, a multi-hole pressure probe has an internal hollow and has on the front end of the probe a plurality of apertures which communicate with the internal hollow. A pressure transducer has a first layer of semiconductor material bonded to a glass contact substrate, the semiconductor material having a central active area which deflects upon application of a force and a surface of the material is coated with an oxide layer. Positioned on the oxide layer are piezoresistive sensing elements. These sensing elements are positioned within a cavity on the glass substrate when the contact glass wafer is bonded to the semiconductor material. The glass substrate has apertures which are filled with a glass metal frit and contain header pins. The entire transducer is positioned within a separate header. A plurality of such transducers, are each positioned in its own header, and each is individually inserted into a respective aperture of the probe. This enables the measurement of flow angles, static pressures, within the structure. By mounting each sensor in its own miniature header, four or five such sensors can be used simultaneously in a probe while enabling the probe to be very small. 
     Referring to  FIG. 1  there is shown a transducer configuration using SOI techniques. In this technique, the piezoresistive network indicated by reference numerals  24  and  25  is configured in a Wheatstone bridge configuration and the piezoresistors as  24  and  25  which are four in number are isolated from the deflecting material by an oxide layer  12 . 
       FIG. 1  also shows a surrounding header  44  which header houses and encloses the transducer apparatus. The process for fabricating the composite dielectrically isolated structure as shown in  FIG. 1  requires the use of two separate wafers. The term substrate is used synonymously with the term wafer and is defined as being a small disc of material, either semiconductor or glass. The first pattern wafer is selected to optimize the piezoresistive performance characteristics of the sensor chip, while the second substrate wafer is specifically selected to optimize the micromachining capabilities of the sensing diaphragm. Once the wafers are bonded together, the non-doped side of the pattern wafer is selectively removed and the P+ network is left bonded to the oxide layer positioned on the substrate wafer. This forms a composite dielectrically isolated wafer. The deflection area is designated by reference numerals  40  and  41 , with center boss designated as  42 . Essentially, the regions  40  and  41  are thin regions, also called active areas, which deflect upon application of a force thereto. The piezoresistive sensors  24  and  25  are located within the active areas  40  and  41  and as indicated will vary their resistance upon application of a force thereto. The sensors  24  and  25  are also associated with contact areas which basically are metal and enable the device with the header to operate at desired temperatures. The metallization that is used for establishing high temperature contacts is PtSi/Ti/Pt. In this manner, the first layer of Pt silicide is used to create a high temperature ohmic contact to the device, the second (Ti) is used as both an adhesion layer and a barrier that prevents the top Pt layer from diffusing into the underlying PtSi ohmic contact layer at very high temperatures. Platinum (Pt) is used as a top layer because it is highly inert and is very suitable for high temperature operation. 
     Once the metallized contact barriers are defined, (e.g., using conventional photolithographic technology), the micromachining of the deflecting diaphragm takes place. The micromachining as for example, the machining of areas  40 ,  41  and  42  is performed using either a combination of different wet (isotropic and anisotropic) chemical processes or deep reactive ion etching (DRIE) can also be implemented. The shape and performance characteristics of the micromachined sensing or deflecting diaphragms are modeled using finite element analysis, and the SOI sensing chip is configured to be directly mounted into the probe body, thus eliminating redundancy and sensor packaging in probe installation which have historically increased the probe size. This also facilitates a better thermal match within the chip and its mount improving stability and accuracy. As indicated the piezoresistive patterns are isolated from the silicon substrate  11  by the silicon dioxide layer  12 . 
     The layer of silicon dioxide is preferably a high quality grown oxide which is then grown on the surface of the substrate, while the piezoresistive patterns are introduced into the pattern wafer. The piezoresistive patterns are preferably diffused in highest possible concentration level equal to solid solubility, in order to achieve the most stable long term electrical performance characteristics of the sensing network. Once the pattern and the substrate wafers are appropriately processed, the two are fusion bonded together using the techniques described in the above noted U.S. Pat. No. 5,286,671 which is incorporated herein in its entirety. The resulting molecular bond between the two wafers is as strong as silicon itself and since both the sensing elements and the diaphragm are made from the same material, there is no thermal mismatch between the two, thus resulting in a very stable and accurate performance characteristic with temperature. The presence of dielectric isolation in the composite wafer  11  enables the sensor to function at very high temperatures without any leakage effects associated with the P-N junction isolation type devices. 
     As seen, bonded to the composite sensor  11  is a glass wafer contact wafer  16 . The glass contact wafer  16  contains apertures  20 . The apertures  20  eventually receive a glass metal frit to make contact with the contacts  34  associated with the piezoresistive sensors  24  and  25 . The header contains a header glass layer  30  which layer is attached to the contact glass wafer by means of a glass frit bonding agent. As indicated the apertures  20  are filled with a glass metal frit and header pins  31  and  32  are inserted into each of the apertures before the glass metal frit hardens. When the glass metal frit hardens the header pins  31  and  32  are permanently retained within the glass metal frit filled apertures as  20 . 
     Referring to  FIG. 2  there is shown an exploded view of the semiconductor transducer depicted in  FIG. 1 . The transducer is shown without a header but basically shows the glass contact wafer  73  which is wafer  16  of  FIG. 1  together with the contact through holes  70  and  71 . Cavity  72  is formed in the contact glass wafer which cavity  72  enables diaphragm deflection. Bonded to the contact glass wafer  73  is a silicon composite sensor wafer  76  which is wafer  11  of  FIG. 1 . The wafer  76  has grown thereon a layer  77  of, for example, silicon dioxide  77 . The layer  77  is configured as a peripheral rim which surrounds the active regions of the wafer  76 . The wafer  76  contains piezoresistors as  81 ,  82 ,  83 , and  84 . These are analogous to piezoresistors  24  and  25  of  FIG. 1 . Thus as seen, there are four piezoresistors which are connected to form a Wheatstone bridge. The piezoresistors are P-type silicon piezoresistors protected by a silicon dioxide or other oxide coating. 
     Part of the connections, as indicated in  FIG. 2  are made on the composite sensor wafer by means of connective land areas  80  which are connected at one end to a piezoresistor and at another end to another piezoresistor thus forming one arm of the bridge. The conductive land areas are each associated with a contact, such as contact  70  for land area  80 . The configuration is well known and offers many advantages as indicated above. The leadless technology in accordance with U.S. Pat. No. 5,955,771, entitled “Sensor for Use in High Vibrational Applications and Methods for Fabricating the Same”, to A. D. Kurtz, and A. Ned and assigned to the assignee herein and U.S. Pat. No. 5,973,590, entitled “Ultra-Thin Surface Mount Wafer Sensor Structures and Methods for Fabricating the Same” by A. D. Kurtz, A. Ned and S. Goodman, issued in 1999 to Kulite Semiconductor Products, Inc., show this technology (described above), thus achieving substantial sensor size reduction. 
     This technology as employed in  FIGS. 1 and 2  is entirely capable of high frequency and high accuracy performance in high temperature, harsh environments. The leadless technology enables the mounting of the sensor chip “upside down” thus exposing only the backside of the sensor chip to the applied pressure. This is shown in  FIG. 1  where the force (F) is applied to the top side of the silicon composite wafer. Meanwhile, the piezoresistors are isolated by the cavity  72  between semiconductor composite sensor wafer  11  and the glass contact wafer  16 . The leadless technology also eliminates the use of gold wire bonds which can fail at high temperatures, under high vibration, or under dynamic pressure conditions. Thus, one uses a very high temperature glass/metal frit to connect between the leadless chip and a leadless header  44  on which the chip is mounted. The fabrication of the leadless chip requires processing of silicon on insulator (SOI) pattern wafer and the ceramic glass wafer. 
     The ceramic glass wafer which is designated as the contact glass wafer as  16  of  FIG. 1 and 73  of  FIG. 2  is micromachined to be molecularly bonded to the pattern side of the SOI composite sensor wafer  76  of  FIG. 2  or wafer  11  of  FIG. 1  using the Anodic Bond method. The molecular bond takes place between the ceramic glass and the dielectrically isolated P+ Si layer. The bond takes place around the active area, the contact regions and also over the entire extending rim  85  of  FIG. 2 . Once the bond is made the sensing area is hermetically sealed from the surrounding environment, while the contacts are left accessible for interconnections only through adjacent openings in the contact glass. The contact areas are then filled with a thermally matched glass/metal frit and the chip is mounted onto a header using a high temperature non conductive glass. This glass is designed to fire at the same temperature as the glass/metal frit. Such glasses in combination with metals are well known and many examples exist in the prior art. The connections between the filled contacts and the header pins are made at the same time. Once the chip is mounted onto the header, only the backside of the sensor chip is exposed to the pressure medium as shown in  FIG. 1 . It is of course understood that the piezoresistors of  24  and  25  are hermetically protected and the overall thickness of the header-chip combination can be made as small as 10-20 mils (1 mil is equal to one-thousandth of an inch, i.e. 0.001 inch). The typical chip as shown in  FIG. 1  and  FIG. 2  will have an overall dimension on the order of 20 to 30 mils in diameter with a membrane thickness of 0.01 to 0.02 mils and having a high sensitivity and high accuracy. By designing the chip to have optimized sensing membranes by using Finite Element analysis software to model the chip&#39;s mechanical performance sensors having: 1) overall dimension on the order of 20 to 30 mils in diameter, 2) membrane thickness of 0.01 to 0.02 mils, 3) high sensitivity and 4) high accuracy are obtained. The probe design will take the full benefit of all the descried sensor features and will implement the custom designed leadless packaging methods. Such a structure, when used as the sensor in a multiple-hole pressure probe gives rise to a number of advantages. By mounting each leadless sensor in its own miniature header four or five such sensors can be used simultaneously in a probe, while enabling the probe to be very small (less than 100 mils in diameter) as shown in  FIG. 4 . Since the leadless sensor is first affixed to its own header, the header sensor structure can have its leads attached before mounting in the probe as shown in  FIG. 5 . The small diameter and thickness of the mounted sensor/header combination makes it possible to pass the leads out of a central aperture in the probe body (shown in  FIG. 6 ) and then affix the sensor header structure to a prepared position on the probe. The small overall thickness of the header-chip combination also insures that when mounted on the probe, it will not protrude past the surface and thus avoid distortion of the airflow. The design of the probe body can be customized for any application with the sensor/header selection kept separate. The probes utilizing this type of construction will be truly robust and capable of withstanding harsh environments, while exhibiting excellent performance characteristics. The probe design makes use of the full benefit of all the described sensor features and can be utilized to design specifically high frequency and reliable probes. 
     Referring to  FIG. 3 , which consists of  FIGS. 3A and 3B , there is shown an angled probe according to this invention and employing the transducers as depicted  FIG. 1  and  FIG. 2 .  FIG. 3A  shows a front view of the probe. As seen, the probe  100  is circular in cross-section and has four probe holes or apertures, namely  120 ,  130 ,  121  and  135 . The probe  100  has a front conical surface as can be seen in  FIG. 3B  which shows a cross-sectional view taken through line  3 B- 3 B of  FIG. 3A . As seen, the probe  100  has an internal cavity  110  and is basically symmetrically disposed about the center line or axis  114 . Each aperture contains a separate transducer, such as  101  and  103 , and each transducer is associated with a separate sensor structures, such as  102  or  104 . The transducers  101  and  103  are the transducer structures shown in  FIGS. 1 and 2 . Thus the transducers have extending pins as pins  105   a ,  105   b  for transducer  101  and pins  106   a ,  106   b  for transducer  103 . As seen, each transducer has its own housing which housing is accommodated by a probe aperture or port. The front of the probe, as indicated, is generally conical in shape. Each pin associated with the transducers is connected to its own wire as indicated by wires  111   a  and  111   b  for transducer  101 , and  112   a  and  112   b  for transducer  102 . When used as a sensor in a multiple-hole pressure probe, such a structure as shown in  FIG. 3  gives rise to a number of great advantages. By mounting each leadless sensor in its own miniature header, four or five such sensors can be used simultaneously in a probe, while enabling the probe to be extremely small (less than 100 mils in diameter). Since the leadless sensor structure is first affixed to its own header, the header sensor structure can have its leads attached before mounting in the probe. This is clearly shown in  FIG. 4 . 
     Thus, in  FIG. 4 , which consists of  FIGS. 4A and 4B , there is shown a transducer header  141 , or housing, which accommodates the sensor configuration  140  as that of  FIGS. 1 and 2 . The transducer header  141  as indicated contains the sensor  140  and is associated with pins  142  and  143 , where each pin has a wire such as  144  and  145  emanating there. These are analogous to pins  105   a  and  105   b  of  FIG. 3 . 
       FIG. 5A  shows the front view of a probe  152 . The probe has four apertures designated as  151 ,  153 ,  154 , and  155 .  FIG. 5B  shows a cross-sectional view. It is seen that the probe  152  is again symmetrically disposed about axis  156  and has the apertures  154 ,  153  adapted to accommodate an associated transducer as shown in  FIG. 4 . Thus, as seen the aperture  154  has a top portion which is of a size adapted to enclose and contain the transducer header  141 . The bottom portion of the aperture  154  has an opening  155  which communicates with the internal hollow  157  of the probe  152 . Also aperture  153  has a top portion to accommodate the transducer and a smaller bottom portion  158  which also communicates with the hollow  157  of the probe. As one can see, the configuration depicted in  FIG. 4B  together with wires  141  and  145  can be inserted into aperture  154  with the wires as  144  and  145  directed through the bottom portion or aperture  155  into the internal hollow  157  of the probe. In this manner, the entire structure is extremely compact and utilizes for example in particular in regard to  FIG. 5  as well as  FIG. 3 , four separate transducers to measure four different flow values. 
     Referring to  FIG. 6 , there is shown  FIG. 6A  which depicts a front view of an angle and static probe  160 .  FIG. 6B  is a cross-sectional view taken through line  6 B- 6 B of  FIG. 6A . As seen, from  FIG. 6A  the probe  160  has a circular configuration and has port apertures  161 ,  162 ,  163 ,  166  and  167 . Apertures  163 ,  166  and  167  are located on the flat front surface  164  of the probe with aperture  163  located at the center of the probe on the flat surface  164  while apertures  161  and  162  are positioned on the angled front portion of the probe as depicted in  FIG. 6B . 
     As seen in  FIG. 6B , each aperture, such as  161 ,  162 , and  163  contains its own transducer structure. For example, transducer structure  169  is contained in aperture  161 ; transducer structure  173  is contained in aperture  162 , and transducer structure  171  is contained in aperture  163 . Aperture  163  communicates with an extended passage  168  where the end of passage  168  communicates with an aperture containing transducer structure  171 . Each of the transducers is also associated with respective pins, as pins  180   a ,  180   b  associated with transducer  169 ; pins  182   a ,  182   b  associated with transducer  173 ; and pins  184   a ,  184   b  associated with transducer  171 . The probe housing has openings surrounding each of the pins to enable the pins to be connected to wires such as  181   a ,  181   b  connected to pins  180   a ,  180   b  respectively, wires  185   a ,  185   b  connected to pins  184   a ,  184   b  respectively and wires  183   a ,  183   b  connected to pins  182   a ,  182   b  respectively. This enables connections to the piezoresistive sensor arrangements on each of the transducers. Thus, as one can ascertain, by mounting each leadless sensor in its own miniature header to provide probe design that enables a multiple number of transducers to be employed in a single probe. Since the leadless sensor is affixed to its own header the resultant transducer structure can have its leads attached before mounting in the probe as explained above. The small diameter and thickness of the mounted sensor/header combination makes it possible to pass the leads out of a central aperture in the probe body as shown for example in  FIG. 6  and then affix the sensor header structure to a prepared position on the probe. The design of the probe body can be customized for any application where the sensor/header selection kept separate. 
     The probes utilized in this type of construction are truly robust and capable of withstanding harsh environments while exhibiting excellent performance characteristics. Additionally, the new leadless assembly/packaging of the probes enables one to implement an additional center transducer as shown in  FIG. 6 . This does not increase the size of the overall miniature probe. The central transducer is used for static measurements by placing it in the probe body itself and allowing a narrow tube to extend out to the front of the transducer to measure pressure applied to the front. This is a very useful configuration and is simply implemented with the transducers and headers depicted above. 
       FIGS. 7A-10B  illustrate yet another novel construction of a pressure probe. The above-described pressure probes can utilize various methods for securing the leadless headers of the transducer structures into the probe apertures. For example, a header can be secured into an aperture through glassing or epoxing. These methods, however, can limit the overall performance of the probe.  FIGS. 7A-10B  illustrate various portions and components of an all-welded construction of the ultra miniature probe. 
     Specifically,  FIGS. 7A-7B  illustrate a transducer structure  740  in which a header of the transducer comprises a weldable flange  715 .  FIG. 7A  illustrates a front view of the transducer structure  740 , while  FIG. 7B  illustrates a cross-sectional side view. As shown in  FIG. 7 , in the welded construction approach, the headers  710  can be welded to the probe body  820  (see  FIGS. 8A-10B ) within transducer ports  830  (see  FIGS. 8A-10B ), or receivers, of the probe body  820 . A header  710  of a transducer structure  740  can be a specially designed leadless header  710  containing an additional ultra thin flange  715  at its front, as shown in  FIGS. 7A-7B . 
       FIGS. 8A-8B  illustrate a transducer port of the probe body having a counter-bore for receiving the flange  715  of the transducer structure  740 .  FIG. 8A  illustrates a front view of the transducer structure, while  FIG. 8B  illustrates a cross-sectional side view. As shown, the probe body  820  is designed to contain transducer ports  850  having specific recesses (counter-bores)  855  to accept the thin flanges  715  from the individual headers  710 . In other words, the probe body  820  can comprise a plurality of transducer ports  850  for receiving the transducer structures  740 . Each transducer port  850  defines an aperture  858  for receiving the transducer structure  740 , and further comprises a counter-bore  855  for receiving the flange portion  715  of the header  710  of the transducer structure  740 . 
       FIGS. 9A-9B  and  10 A- 10 B illustrate fully assembled all-welded pressure probes, with  FIGS. 9A and 10A  being front views and  FIGS. 9B and 10B  being cress-sectional side views. In the all-welded probe, the leadless sensors are mounted onto the header  710 , such as by utilizing the mounting process described in U.S. Pat. No. 5,955,771, entitled “Sensors for Use in High Vibrational Applications and Methods for Fabricating Same,” which is owned by Kulite Semiconductor Products, Inc. After the sensors are mounted, the headers  710  can be inserted into the probe body  820  and secured into place, to result in those probes depicted in  FIGS. 9A-9B  and  10 A- 10 B. In an exemplary embodiment, securing a header  710  in place can be accomplished by welding the header  710  to its associated transducer port  850  in the probe body. Welding can be performed about the flange  715 , to weld the flange  715  to the counter-bore  755  of the associated transducer port  850 , in a weldable area  910 , as shown in  FIGS. 9A and 10A . During welding, an overlapping spot weld process or other conventional welding methods can be used. 
     This novel approach eliminates all of the prior mounting difficulties by completely eliminating the use of glues and epoxies. The elimination of glues and epoxies, in combination with using only ultra high temperature materials, enables the construction of an ultra high temperature probe suitable for operation above 500° C. This method and construction also avoids the performance problems that epoxy use can cause, for instance hysteresis, non-linearity, and unusual temperature effects. This approach additionally eliminates leakage paths between the front of the probe (front of the sensors) and rear of the probe (back of the sensors). In contrast to prior designs relying on glassing or epoxing, the all-welded design can assure hermetic isolation. 
     A 5-hole probe  900  design of the all-welded construction is shown in  FIGS. 9A-9B , while a 4-hole design  1000  is shown in  FIGS. 10A-10B . While only 4 and 5-hole designs are depicted, an all-welded pressure probe can accommodate the use of four sensors (4-hole probe), five sensors (5-hole probe), or various other numbers of sensors. 
     It should be obvious to one skilled in the art that there are many additional configurations that can be employed and to fabricate probes of different sizes and construction. All of these alternate embodiments are deemed to be encompassed within the spirit and scope of the claims appended hereto.