FLUIDIC VOLUMETRIC FLUID FLOW APPARATUS AND METHOD

Abstract: A fluidic device having an inlet (16) and a flow path extending from the inlet (16) to an outlet (18). A part of the flow path defines a power jet nozzle (74) upstream of and leading to an interaction chamber (76). The interaction chamber (76) leads to the outlet (18). A splitter (78) is spaced from the power nozzle (74) across the interaction chamber (76) and is in alignment therewith to separate a pair of feedback inlets (80,82) leading from the interaction chamber (76). A pair of feedback channels (26,28) extend from the pair of feedback inlets (80,82) to respective feedback outlets (84,86). The feedback outlets (84,86) are oppositely disposed perpendicularly to the power nozzle (74) and intermediate the latter and the interaction chamber (76). A branch passage (30,32) extends from each feedback channel (26,28) to a respective variable-­ volume chamber (34,36) which is bounded by a flexible diaphragm (54,56). The diaphragms (54,56) are movable in response to pressure variations within the respective variable-volume chamber (34,36) and are each associated with a transducer (58,60) for producing an output signal in response to such movement. Fluid flow restrictions (38,40) are provided in each branch passage (30,32) for resisting dynamic oscillation (ringing) of fluid flow in the feedback channels (26,28) with the variable volume of fluid in the variable-volume chambers (34,36).

Description: The present invention relates to an apparatus and methods for the measurement of the volumetric flow rate of a flowing fluid. More particularly, the invention relates to dynamic or inferential measurement devices, as opposed to positive displacement measuring devices, which former devices are additionally of fluidic operation. Conventional fluidic measuring devices in the field to which the present invention relates are disclosed in the following United States patents: These teachings establish that the possibility of measuring fluid flow rate, either on a volume or mass basis, has been recognised for a number of years. The first three teachings listed above are believed to apply wall-attachment type fluidic oscillators to, respectively, the measurement of volumetric flow rate as a function of oscillator frequency, to the measurement of mass flow rate as a function of oscillator amplitude and frequency, and to the measurement of mass flow rate as a function of oscillator frequency and total pressure drop across the oscillator. The Ringwall patent (4,107,990) recognises the deficiencies of wall-attachment fluidic oscillators in the application to flow rate measurement. Accordingly, the Ringwall patent teaches the use of a differential pressure proportional fluidic oscillator to provide a volumetric flow rate meter. However, to extend the measurement range of the Ringwall teaching beyond that obtainable with a single oscillator, multiple amplifier stages must be used. Additionally, it is believed that the signal quality which is obtained from an oscillator as taught by Ringwall may be less than optimum. This output signal is believed to be contaminated with dynamic oscillation, or ringing, noise which is internally self-generated by the oscillator as a result of internal fluid inductances and capacitances. More specifically the oscillator disclosed in the Ringwall patent comprises a power nozzle and a splitter pointing towards the nozzle with an interaction chamber defined between them. Located on opposed sides of the interaction chamber are two feedback channels having inlets adjacent the splitter on each side of the chamber and outlets on each side of the chamber adjacent the power jet. Transducers sense pressure fluctuations in the feedback channels. An alternative approach to fluid mass flow rate measurement is shown in the present Applicants' United States Patent 4,508,127. The disclosure of the '127 patent is specifically incorporated herein by reference to the extent necessary for a complete disclosure and understanding of the present invention. The '127 patent teaches the use of a dynamic volumetric flow rate meter, such as a turbine meter, to obtain a single indicative volumetric fluid flow rate meter. A fluidic oscillator having a regulated total pressure drop across it is employed to generate a second signal indicative of fluid density. The two signals are combined by multiplication to obtain an indication of fluid mass flow rate. The construction disclosed in the '127 patent is similar to that disclosed in the Ringwall patent in its major features, the primary difference being in the location of the transducers. Branch channels lead from each feedback channel to respective variable-volume chambers, one of whose walls is a flexible diaphragm. A piezoelectric transducer is bonded to the outside of each diaphragm which senses distortions in the diaphragm caused by pressure changes in the chambers. However, it is desirable to provide a volumetric fluid flow rate meter which avoids the use of movingpart type flow meters. The fluidic oscillator because of its rugged, no-moving-parts construction is recognised as offering considerably improved service life over all flow meters having moving parts, such as the turbine flow meter, for example. Furthermore, the limited flow measurement range and need for multiple oscillators of the Ringwall teaching should be avoided. Finally, it is highly desirable to provide such a volumetric flow rate meter with a "clean output signal substantially free of both self-generated noise or ringing, and noise of electrical origin. The Applicants have discovered that internally self-generated noise in a fluidic oscillator may result from dynamic interaction between moving fluid in the feedback channels of the oscillator and the output signal generating apparatus. In other words, the feedback channels provide a fluid inductance, and the output transducers a fluid capacitance which under the influence of the pulsating, time variant oscillations of the oscillator itself set up an internal self-generated noise or ringing. This ringing noise appears in the output signal of the flow meter and degrades its performance or measurement accuracy. According to one aspect of the invention there is provided fluidic apparatus for measuring liquid volume flow rate comprising a fluidic oscillator including a power nozzle for receiving a flow of liquid and forming the flow of liquid into a liquid jet, a channel for the liquid jet having a significant fluidic inductance, means including a splitter pointing into the flow from the power nozzle for creating a pulsating pressure signal in the liquid jet in the channel, the frequency of the pulsating signal being indicative of liquid volume flow rate through the power nozzle, a transducer having a significant fluidic capacitance and which communicates with the channel and the pulsating pressure signal therein, the transducer producing an output signal in response to the pulsating pressure signal, characterised by a flow restriction between the transducer and the channel for inhibiting undesirable dynamic interaction or ringing of the fluidic inductance of the channel with the fluidic capacitance of the transducer. Preferably, a further fluid flow restriction is located in the channel downstream with respect to the communication of the pulsating pressure signal with the fluid capacitor. There may also be a vent passage opening outwardly from the fluid capacitor for purging compressible fluid therefrom, the vent passage including a further fluid flow restriction. Preferably, the output signal producing means comprises a variable-volume chamber communicating with the channel, a flexible electrically conductive diaphragm member bounding the variable-volume chamber to flex in response to the pulsating pressure signal, a piezoceramic disc secured in electrical contact with the diaphragm member for flexure therewith, and electrical circuit means including the diaphragm member and the piezoceramic disc for conducting the output signal. There may be electrical insulation means isolating the diaphragm member and the piezoceramic disc from the remainder of the apparatus, which may comprise a dielectric film coating on an outer peripheral edge portion of the diaphragm member. The apparatus may define means for additionally shielding the diaphragm member and the piezoceramic disc from ambient electrical interference. Preferably, the apparatus includes bypass means in fluid flow parallel with the fluidic oscillator, the bypass means defining a plurality of bypass passages, and flow restriction means in association with each bypass passage for replicating the discharge coefficient of the power nozzle. Preferably, the fluidic oscillator comprises a housing exteriorly defining a prismatic body, the bypass means comprising another housing similarly exteriorly defining another prismatic body, the two housings being congruent, the apparatus also including means for removably coupling the housing in side-by-side congruence as a module. Conveniently, the output signal producing means is disposed on a side of the housing opposite the bypass means. The apparatus preferably includes a second fluidic oscillator and a second bypass means each having respective housings substantially similar to the first fluidic oscillator and bypass means and being removably coupled to provide a complete second module, the housing defining like-disposed fluid inlets and outlets on opposite edge surfaces thereof, and the modules confronting one another across a plane of symmetry so that their respective output signal producing means face towards the plane of symmetry, a spacing member being interposed between the two modules on the plane of symmetry, the spacing member defining a chamber between the modules for communicating with the outlets. Preferably, there is also provided base means defining a prismatic recess sealingly receiving the module and defining a flow path for communicating fluid therethrough. Preferably, the bypass means carries the fluidic oscillator. The invention may be carried into practice in various ways and some embodiments will now be described by way of example with reference to the accompanying drawings. The following detailed description includes description of embodiments of the invention which may be employed as principal components of a liquid fuel volume flow rate sensor, a part of an electronic fuel controller for a turbine engine. However, the invention is not limited to such use and is not intended to be so limited. In fact, in many respects, the invention has almost universal application to the art of flow measurement. This broad scope of the present invention will quickly appear to those skilled in the art of flow measurement in view of the following. In the drawings:- Figure 1 schematically shows a liquid volumetric flow rate meter embodying the invention; Figure 2 schematically shows a fluidic flow rate sensing device embodying the invention; Figure 3 graphically presents data of output signal level verses fluid volumetric flow rate obtained by testing an embodiment of the present invention; Figure 4 shows a sequentially arranged group of laminae which when stacked and interbonded in the alphabetic order presented cooperatively define a fluid flow rate sensing device according to one embodiment of the invention; Figure 5 is a fragmentary plan view and a fragmentary partially cross-sectional view of a portion of the fluid flow rate sensing device of one embodiment of the invention; Figure 6 is a section on the line 6-6 in Figure 5; Figure 7 shows two laminae at an intermediate stage of manufacture which when stacked and interbonded with other like lamina substantially define a fluid bypass component of a fluid flow meter according to the invention; Figure 8 is an exploded perspective view of a fluid flow rate module embodying the invention and including a fluidic flow rate sensing device and a bypass member; Figure 9 is an exploded perspective view similar to Figure 8 showing an alternative embodiment of the invention which provides a redundant output fluid flow rate sensing module; Figures 10 and 11, respectively show fragmentary cross-sectional views of a fluid flow meter employing a redundant module like that depicted in Figure 9 and a housing providing for fluid flow to and from the flow rate sensing module; Figure 12 is a partial cross-sectional view of an alternative embodiment of a fluid flow meter embodying the invention; and Figure 13 is a cross-sectional view taken along line 13-13 of Figure 12. Figure 1 shows a fluidic liquid volumetric flow meter 10. The flow meter 10 includes a flow sensing device 12 and a bypass unit 14. An inlet 16 to the flow meter communicates both with the flow sensing device 12 and with the bypass unit 14, while an outlet 18 from the flow meter similarly communicates with both 12 and 14. The flow sensing device 12 includes a fluidic oscillator 20 having an inlet 22 and outlet 24 and feedback channels 26,28. Connected with the feedback channels 26,28 via branch passages 30 and 32 are a pair of variable-volume sensing chambers 34,36. Each of the branch passages 30,32 includes a fluid flow restriction 38,40, respectively. Similarly, each of the feedback passages 26,28 includes a fluid flow restriction 42,44. Extending from each of the variable volume sensing chambers 36,38 is one of a pair of vent passages 46,48 each having its respective fluid flow restriction 50 and 52. Each of the variable-volume chambers 34 and 36 is bounded by a flexible and electrically conductive diaphragm 54 and 56, respectively upon which is mounted a sensing transducer 58 and 60. As will be described below, the diaphragms are responsive to pressure variations within the chambers 34 and 36 to flex, which results in the transducers 58 and 60 providing electrical output signals via conductors 62 and 64. Although not shown in Figure 1, it will be seen that the fluidic oscillator 20 includes a power jet nozzle which directs a stream of fluid from the inlet toward the outlet. The power jet nozzle of the fluidic oscillator 20 results in a measurable pressure drop between the inlet 22 and the outlet 24 of the oscillator 20. Turning now to the structure of the bypass unit 14, it will be seen that this unit provides a plurality of flow paths each referenced with the numeral 66. Each flow path 66 is in fluid flow parallel with the flow path through the fluidic oscillator 20 between the inlet 22 and the outlet 24. Each flow path 66 of the bypass unit 14 is provided with a fluid flow restriction 68 which replicates the coefficient of discharge characteristic of the power jet nozzle within the fluidic oscillator 20. As a result, because the pressure drop across the flow meter 10 between the inlet 16 and outlet 18 is the same for the fluidic oscillator 20 as it is for the bypass unit 14, each of the flow paths 66 within the bypass module 14 will flow substantially the same fraction of volume of fluid per unit time as that which flows through the fluidic oscillator 20. Turning now to Figure 2, it will be seen that the fluidic oscillator 20 includes a housing 70 defining the inlet 22, the outlet 24 and the other components of the fluidic oscillator. The housing 70 defines a flow path 72 extending between the inlet 22 and the outlet 24. The flow path 72 defines a power jet nozzle 74 opening into an interaction chamber 76. The interaction chamber 76 opens downwardly out of the plane of Figure 2 to the outlet 24. The housing 70 also defines a knife-edged splitter member 78 which is aligned with and opposite to the power jet nozzle 74, across interaction chamber 76. The splitter member 78 separates a pair of feedback inlets 80 and 82 which communicate respectively with the feedback channels 26 and 28. Each one of the feedback channels 26 and 28 communicates respectively with one of a pair of feedback outlets 84, 86 which are oppositely disposed perpendicularly to the power jet nozzle 74, between the latter and the interaction chamber 76. In order to reduce the effect of electrical interference upon the output signal produced by the transducers 58,60, an electrical insulation 55 is provided between the diaphragms 54,56 and the housing 70. As a result both the diaphragms 54,56 and transducers 58,60 are electrically isolated from the housing 70. As will be seen below, the housing 70 may act additionally to shield the transducers 58.60 and diaphragms 54,56 from electrical interference. Having observed the basic structure of the fluidic oscillator 20, it is well to now consider its method of operation. It will easily be understood that when fluid flows into the inlet 16 of the fluid flow meter, a portion of this fluid must flow through the fluidic oscillator 20 via the inlet 22, and the flow path 76 leading to the outlet 24 and the bent passages 46,48. Fluid entering the inlet 22 upon flowing through the power jet nozzle 74 forms a stream of fluid 88 which projects across the interaction chamber 76 towards the splitter member 78. Upon encountering the splitter member 78, the fluid stream 88 divides so that a portion is received by each of the feedback inlets 80 and 82. Inherently, a slightly greater portion of the fluid stream 88 will be received by one of the feedback inlets 80 and 82 than the other. The velocity of the fluid stream 88 is partially reconverted to pressure at the feedback inlets 80 and 82 in proportion to the degree of split of the fluid stream 88. Fluid received by the feedback inlets 80 and 82 is communicated by the respective feedback channels 26 and 28 to the respective feedback outlets 84 and 86. Because one of the feedback inlets will have received a slightly greater portion of the fluid stream 88, fluid issuing from the associated feedback outlet will exert a greater lateral pressure force upon the fluid stream issuing from the power jet nozzle 74 than does the fluid from the other feedback outlet. As a result of the differential pressure effective at the outlets 84,86, the fluid stream 88 will be urged towards the feedback inlet having received the lesser portion of the stream 88. The phenomenon results in oscillation of the fluid stream 88 between the two feedback inlets 80 and 82 on opposite sides of the splitter member 78. The period of oscillation is a function of the velocity of the fluid stream 88 and the effective transport and feedback distances of the oscillator 20. This transport distance in substance is the linear dimension from the area where the power jet nozzle 74 opens to the interaction region 76 adjacent the feedback outlets 84 and 86, across the interaction chamber 76 to the feedback inlets 80, 82. The feedback distance is the dimension around the feedback channels 26 and 28 to the feedback outlets 84 and 86. It will be understood that not all of the fluid stream 88 is received into the feedback inlets 80 and 82 and that the majority of the fluid is allowed to flow from the fluidic oscillator 20 via the outlet 24. Considering the fluid with the feedback channels 26 and 28, it will be seen that when the fluid stream 88 is received into either one of the feedback inlets 80 or 82, the associated channel receives a portion of fluid the kinetic energy of which is partially converted to a pressure which migrates through the fluid within the feedback channel at the acoustic velocity of the particular fluid. The pressure in the feedback channels communicates via the branch passages 30 and 32 into the variable-volume sensing chambers 34 and 36. As a result, the diaphragms 54 and 56 flex in response to the pressure variations experienced within the sensing chambers 34 and 36. Flexing of the diaphragms 54 and 56 results both in variation of the volume defined within chambers 34,36, and in flexing of the transducers 58 and 60. Flexing the transducers 58, 60 results in an electrical signal conducted by conductors 62 and 64. It will be seen that as the diaphragms 54 and 56 flex, the volumes of the chambers 34 and 36 increase and decrease so that the chambers 34 and 36 exhibit fluidically a capacitance. The channels 26, 28 may be considered to exhibit a fluidic inductance which arises from the liquid density and the dimensions of these channels. In order to prevent the capacitance of the sensing chambers 34 and 36 from dynamically interacting with the inductance of the feedback channels 26 and 28 to produce noise or ringing, the system in accordance with the invention provides fluid flow restrictions 38 and 40 in the branch passages 30 and 32. However the present Applicants believe that the restrictions 38 and 40 would have the effect of reducing the magnitude of the pressure variations experienced in the chambers 34 and 36 and available for sensing by flexing of the diaphragms 54 and 56. In order to offset this reduction in the pressure variations experienced in the sending chambers 34 and 36, the fluid flow restrictions 42 and 44 are provided downstream of the respective branch passages at each of the feedback channels 26 and 28. Further in order to insure that all air or compressible gas is purged from the sensing chambers 34 and 36 and therefore does not interfere with flexing of the diaphragms 54 and 56 by fluid pressure variations experienced therein, the vent passages 46 and 48 having fluid flow restrictions 50 and 52 have been incorporated. These vent passages allow a relatively small but significant flow of fluid from the feedback passages 26 and 28 through the respective sensing chambers 34 and 36 so that all compressible gasses are purged. Turning to Figure 3, it will be seen that an oscillator according to an actual reduction to practice of the present invention displayed a high degree of linearity of oscillation frequency verses liquid flow rate passing therethrough. Figure 3 shows that the plotting points resulting from testing of the oscillator at various known liquid flow rates fall, in effect, perfectly on a straight line. The actual reduction to practice of the inventive oscillator was effected by the use of stacked fluidic laminae as shown in Figure 4. These laminae are alphabetically designated "a" to "j" in Figure 4 in stacking order. Features of the laminae which are analogous in structure or function to those depicted schematically in Figures 1 and 2 are referenced with the same numeral, perhaps with one or more primes added to distinguish portions of structure. Viewing Figure 4 in greater detail it will be seen that lamina "h" defines an inlet 22 in conjuction with laminae "g" and "i" having notches 22′ aligning with the inlet passage 22 in lamina "h" to define a convergent inlet opening. Lamina "h" likewise defines a pair of feedback passage portions 26′ and 28′. These feedback passage portions communicate with openings 26″,28″ defined in laminae "g" and "f", as well as with restrictive orifices 42 and 44, the latter of which are defined only in lamina "f". Viewing laminae "e" and "d" it will be seen that the feedback channels are completed by a air of aligning elongate openings 26‴ and 28‴ communicating the openings 26″ and 28″ of lamina "f" with the restrictive orifices 42 and 44. Lamina "c" defines a pair of restrictive orifices 38 and 40 respectively communicating with the elongate openings 26‴ and 28‴ of laminae "d and "e". The restrictive orifices 38 and 40 of lamina "c" align with holes 30 and 32 defined by lamina "b" to define the branch passages opening to the sensing chambers 34 and 36, recalling the description of Figures 1 and 2. Viewing Figure 4 once again, it will be seen that lamina "a" defines a pair or large openings 34′36′ communicating with the holes 30 and 32 of lamina "b", the function of which will be further described below. Lamina "a" also defines a pair of elongate notches 34″, 36″ extending radially outwardly from the openings 34′,36′ respectively. Lamina "b" defines a pair of holes 46′,48′ communicating also with the openings 50 and 52 of lamina "c". The vent passages are substantially defined by lamina "d" which provides a pair of elongate slots 46 and 48 communicating with the restrictive openings 50 and 52 and extending to the edge of the laminae. In order to complete the description of the laminae stack shown in Figure 4, it must be noted that lamina "i" defines four rather winged-shaped openings 76′ in alignment with the interaction chamber 76 defined by lamina "h". The openings 76 of lamina "i" align with a collection chamber portion 24′ of the outlet 24 defined by lamina "j" and communicating with an outlet slot 24 extending to the edge of the lamina. It will be understood that while lamina "a" is the top lamina of a fluidic laminae stack embodying the features of the present invention, the stack would ordinarily be bounded at its opposite side by a plain lamina having no fluidic openings and bounding the outlet chamber 24′ and outlet 24 below lamina "j" and the plane of Figure 4. Figures 5 and 6 in conjunction depict a fragment of the structure of the laminae stack shown in Figure 4. From Figure 5 in particular it will be seen that the laminae "a", "b" and "c" in conjunction substantially define the sensing chamber 34, the branch and vent passages 30 and 46′ respectively, and the flow restrictive orifices 38 and 50. The structure defining the sensing chamber 36 is substantially similar, and so will not be further described. Recalling the description of Figure 4, it will be seen that the restrictive opening 38 communicates with the opening 26‴ in lamina "d" while the flow restrictive orifice 50 communicates with vent passage slot 46 in lamina "d". Received within the opening 34′ of lamina "a" is an annular spacing and sealing member 92. The member sealingly engages the surface of lamina "b". The flexible diaphragm 54 is received into the opening 34′ of lamina "a" and sealingly engages the sealing and spacing member 92. Because of the sealing and spacing member 92, the diaphragm 54 is spaced slightly away from lamina "b" to define the sensing chamber 34. An annular capture member 94 is also received in the opening 34′ in engagement with the outer surface of the diaphragm 54. The capture member 94 has a chamfer 96 on ins outer diameter. Viewing Figures 5 and 6 in conjunction, it will be seen that the material of lamina "a" is swaged radially inwardly at 98 towards the centre of the opening 34′ and against the shoulder 96 presented by the ring 94 to capture the ring, the diaphragm 54 and the spacing member 92 within the opening 34A. Figure 6 shows that the swaging of lamina "a" is performed as a substantially circumferentially continuous groove 98. Because of the swaging 98 of the material of lamina "a" into engagement with shoulder 96 of the capture ring 94, the ring 94 is held into tight engagement with the diaphragm 54, and the latter is likewise held in sealing engagement with the sealing ring 92. The groove resulting from swaging lamina "a" at 98 is interrupted by a notch 34″, which extends radially outwardly from the opening 34′ of lamina"a". The diaphragm 54 defines a radially outwardly extending portion 57 extending into the notch 34″ outwardly of the ring 94. The portion 57 is bent upwardly out of the plane of the diaphragm 54 to displace its outer end towards the outer surface of lamina "a". One wire 62 is connected to the portion 58 adjacent the outer end. Mounted upon the diaphragm 54 by use of an electrically conductive adhesive is a piezoceramic disc which has previously been identified in the schematic representations of the invention as a transducer member. The piezoceramic disc conventionally responds to flexure of the diaphragm 54 by producing an electrical output conducted to a point of utilisation via the other conductor 62. In order to isolate electrically the diaphragm 54, and the piezoceramic disc 58 mounted thereon, from the housing cooperatively defined by laminae "a" - "j", the radially outer peripheral portion of the diaphragm is provided with a relatively thin coating of dielectric polymer. This polymer coating may be tetrafluoroethylene, for example. While this insulative coating on the diaphragm 54 is too thin to be effectively depicted in Figures 5 and 6, it is depicted schematically as insulation 55 on Figure 2. The insulative coating 55 on the diaphragm 54 is of sufficient thickness to isolate the diaphragm effectively from electrical contact with lamina "a" or "b" via the spacing ring 92, as well as from lamina "a" via the capture ring 94, as seen in Figure 6. Turning once again to Figure 1, it will be recalled that the bypass unit 14 defines a plurality of bypass passages 66, each provided with its own restriction 68 replicating the coefficient of discharge characteristic of the power jet within the fluidic oscillator 20. Figure 7 shows a pair of laminae 100, 102 at an intermediate stage of manufacture for the bypass unit 14. It will be noted that each of the laminae 100,102 similarly to the laminae "a" to "j" conventionally includes four unreferenced alignment holes which are used during the manufacture of a laminae stack, as will be readily understood by those skilled in the fluidic art. Viewing the laminae 100 and 102, it will be immediately noted that these laminae are substantially identical with one being reversed top to bottom with respect to the other. Each lamina includes a plurality of elongate openings 66 extending from near one edge to near the other edge. Intermediate of the ends of the opening 66 the laminae define a pair of confronting protrusions 68′ which cooperate to define a fluid flow restriction 68. Each of the elongate openings 66 has a width dimension which is referenced on lamina 100 with the character W. Also, the elongate openings 676 are spaced apart by a dimension referenced on lamina 102 with the reference character of I. It will be seen that when the laminae 100 and 102 are stacked one upon the other as depicted by the arrow 104, an interbonding region is provided on each side of each elongate opening 66, which in width is equal to dimension I. Therefore, a plurality of laminae 100, 102 each being substantially identical, may be stacked, with each one being reversed respective to its immediately adjacent neighbours, and interbonded. the interbonded stack of laminae 100, 102 is then trimmed at each side along a cutting line 106,108 to open the ends of the elongate openings 66. Those skilled in the fluidic art will recognise that a laminae stack for making a bypass unit 14 will also include at each end thereof for bounding the outermost bypass passages a plain lamina having no openings other than the unreferenced alignment holes. Viewing Figure 8, it will be seen that the resulting bypass unit 14 is essentially a prismatic solid having openings 66 extending therethrough from one face of the prism to the opposite face. Because of the way in which the laminae 100,102 were reversed or alternated in the stacking of the bypass unit 14, the plurality of bypass passages 66 are arranged within the bypass unit in a regular grid-like pattern. Also, viewing Figure 8 it will be noted that the previously unreferenced alignment holes which were conventionally used during manufacturing for staking the laminae preparatory to the interbonding process may advantageously be used for intersecuring a bypass unit 14 to a fluid flow rate sensing module 20. Each of the alignment holes which are referenced on Figure 8 with the numeral 110 may, when a bypass unit 14 is stacked with an oscillator module 20, align with one another and removably receive a rolled spring steel pin 112. The spring steel pin 112 is removably force-fitted into the aligned holes 110 of the bypass module 14 and oscillator module 20 to hold these two modules securely together while allowing optional disassembly. Figure 9 depicts a portion of a redundant fluid flow meter according to the invention. The redundant fluid flow meter of Figure 9 includes a first meter 10 having a bypass unit 14 and fluidic oscillator device 20, and a second fluid flow meter 10′ having an associated bypass unit 14′ and fluidic oscillator device 20′. The first and second fluid flow meters 10 and 10′ are substantially identical and are arranged with their inlets and outlets similarly disposed. Interposed between the two fluid flow metes 10 and 10′ is a spacing member 114 defining four through holes 116 which have the same spacing as the alignment holes 110 in the bypass units 14,14′ and the fluidic oscillator devices 20,20′. The spacing member 114 also defines a C-shaped through passage 118 opening outwardly in a downstream direction. When the fluid flow meters 10 and 10′ are assembled with the spacing member 114 the through passage 118 provides liquid communication to the outer face of the flexible diaphragms 54 an 56 of each of the fluid flow meters 10 and 10′. The through passage 118 within the spacing member 114 also provides a chamber 120 within which the conductor 62,64 from the piezoceramic discs and diaphragms on each of the oscillator devices 20 and 200′ are received. The conductors 62 and 64 may advantageously be led outwardly from the piezoceramic discs 58, 60 and chamber 120 through an opening 122 extending from the latter to open outwardly on the spacing member 114. Viewing Figure 9 and considering the arrangement of the modules 10 and 10′ when sandwiching the spacing member 114 therebetween, it will be seen that the alignment holes 110 of each of the fluid flow meters align with one another and with the through holes 116 of the spacing member 114. Consequently, relatively long spring steel roll pins 124 may be forcibly inserted into the aligned holes 110 of the fluid flow meters 10 and 10′ and into the through holes 116 of spacing member 114 to secure these elements together. Figures 10 and 11 illustrate that a fluidic flow meter like that illustrated in Figure 9 may advantageously housed within a housing 126 providing a rectangular recess 128 therein for receiving the fluidic flow meters 10 and 10′ along with the spacing member 114. The housing 126 provides an inflow passage 130 extending to the recess 128 and the flow meter 10, 10′ therein. Within the recess 128, the flow meter 10, 10′ is sealingly received upon a resilient gasket 132 disposed upon a shoulder 134 defined by the cooperation of the recess 128 and inflow passage 130. In order to urge the flow meter 10,10′ into sealing engagement with the gasket 132, a spacing member 136 and outlet cover plate 138 are provided. The spacing member 136 is rectangular in plan view to be received slidably within the recess 128 above the flow sensor 10. The spacing member 136 defines a through passage 140 leading from the outlets of the flow sensors 10,10′ and of the bypass units 14. The outlet cover plate 138 is removably secured to the housing 126, as by fasteners 142 passing therethrough and threadably engaging the housing 126. The outlet coverplate 138 defines an outlet port 144 opening from a chamber 146 defined by the cooperation of the spacer member 136, the through passage 140, the fluid flow sensors 10,10′ and the outlet coverplate 138. The housing 126 also defines a passage 148 aligned with the passage 122 (Figure 9) of the spacer member 114 and providing for passage of the conductors 62,64 outwardly of the housing 126. Recalling the description of Figures 2, 5 and 6, particularly with reference to the electrically insulative coating 55 upon the diaphragms 54,56 and their purpose, it will be noted that as installed in the cavity 128, the fluid flow meters 10,10′ are electrically in contact with the housing 126. On the other hand, the diaphragms 54,56 and piezoceramic discs 58,60 thereon are electrically isolated from and surrounded by the housing 126 and the remainder of the fluid flow meter. Additionally, it will be seen from Figure 9 that the remainder of the fluid flow meters 10,10′ along with the spacer member 114 virtually completely surround the diaphragms 54,56 and piezoceramic discs 58,60. Consequently, the applicants believe the remainder of the fluid flow meters 10,10′ may electrically shield the electrical output portions of the invention from electrical interference. Figures 12 and 13 show an alternative embodiment of the invention in which the fluidic oscillator module 20 is received between a bypass plate 150 and a bar-like retaining member 152. The bypass plate 150 provides a central inlet passage 154 leading to the inlet of the fluidic oscillator module 20. Also, the bypass plate provides a plurality of bypass passages extending therethrough, each replicating the coefficient of discharge of the power jet nozzle within the fluidic oscillator module 20. The bypass plate 150, oscillator module 20, and retainer 152 are received within a three-part housing generally referenced with the numeral 158. The housing 158 includes a central portion 160 defining a through bore 162. Each of the bypass plate 150 and retainer member 152 define a reduced diameter portion cooperating with the remainder of each to define respective shoulders 164,166. The reduced diameter portion of each of the bypass member 150 and retainer member 152 are received into the through bore 162 of the central portion 160 so that the shoulder 164 sealingly engages the central portion 160. A pair of fasteners 168 extend between the bypass plate 150 and retainer 152 to urge the latter into engagement with the central portion 160 of housing 158. The spacing between the bypass plate 150 and retainer member 152 is selected to receive captively the fluidic oscillator module 20 therebetween. A sealing member 170 is provided between the bypass plate 150 and the fluidic oscillator module 20. The central portion 160 of the housing 158 defines a radially extending boss 172 which defines a mounting surface 174 upon which is sealingly secured an electrical connector 176. The connector 176 provides for conduction outwardly of the housing 158 of the electrical signals originating with the piezoceramic transducers of the fluidic oscillator module 20. The housing 158 also includes a pair of end portions 178 and 180 which are substantially identical. The end portions 178 and 180 each define a threaded part 182 which is configured to mate sealingly with a standard tube fitting (not shown). The end portions 178 and 180 provide an inlet for fluid flow to the fluidic oscillator member 20 and bypass plate 150, and flow therefrom, as is indicated by the arrow 184. Each of the end portions 178 and 180 are sealingly secured to the centre portion 160 of the housing 158 by a plurality of fasteners 186 passing therethrough via aligned holes in each. The embodiment of the invention shown by Figures 12 and 13 has been found by the Applicants to be particularly useful for in-line applications in which it is desirable to determine the volumetric fluid flow rate through a pipeline or conduit, for example.

Claims: Fluidic apparatus for measuring liquid volume flow rate comprising a fluidic oscillator (20) including a power nozzle (74) for receiving a flow of liquid and forming the flow of liquid into a liquid jet (88), a channel (26) for the liquid jet (88) having a significant fluidic inductance, means including a splitter (78) pointing into the flow from the power nozzle (74) for creating a pulsating pressure signal in the liquid jet in the channel, the frequency of the pulsating signal being indicative of liquid volume flow rate through the power nozzle, a transducer (34, 54, 58) having a significant fluidic capacitance and which communicates with the channel and the pulsating pressure signal therein, the transducer producing an output signal in response to the pulsating pressure signal, characterised by a flow restriction (38) between the transducer and the channel for inhibiting undesirable dynamic interaction or ringing of the fluidic inductance of the channel with the fluidic capacitance of the transducer. Apparatus as claimed in Claim 1, characterised in that a further fluid flow restriction (42, 44) is located in the channel (26, 28) downstream with respect to the communication of the pulsating pressure signal with the fluid capacitors (34, 36). Apparatus as claimed in Claim 1 or Claim 2, characterised by a vent passage (46, 48) opening outwardly from each fluid capacitor (34, 36) for purging compressible fluid therefrom, the vent passage including a further fluid flow restriction (50,52). Apparatus as claimed in any preceding claim characterised in that the output signal producing means comprises a variable-volume chamber (34,36) communicating with the channel, a flexible electrically conductive diaphragm member (54,56) bounding the variable-volume chamber to flex in response to the pulsating pressure signal, a piezoceramic disc (58,60) secured in electrical contact with the diaphragm member for flexure therewith, and electrical circuit means (62,64) including the diaphragm member and the piezoceramic disc for conducting the output signal. Apparatus as claimed in Claim 4 characterised by electrical insulation means isolating the diaphragm member and the piezoceramic disc from the remainder of the apparatus. Apparatus as claimed in any preceding claim characterised by bypass means (14) in fluid flow parallel with the fluidic oscillator (20), the bypass means defining a plurality of bypass passages (66), and flow restriction means (68) in association with each bypass passage for replicating the discharge coefficient of the power nozzle (74). Apparatus as claimed in Claim 6 characterised in that the fluidic oscillator (20) comprises a housing exteriorly defining a prismatic body, the bypass means comprising another housing similarly exteriorly defining another prismatic body, the two housings being congruent, the apparatus also including means (112) for removably coupling the housings in side-by-side congruence as a module. Apparatus as claimed in Claim 7 characterised by a second fluidic oscillator (20') and a second bypass means (14') each having respective housings substantially similar to the first fluidic oscillator (20) and bypass means (14) and being removably coupled to provide a complete second module, the housing defining like-disposed fluid inlets and outlets on opposite edge surfaces thereof, and the modules confronting one another across a plane of symmetry so that their respective output signal producing means face towards the plane of symmetry, a spacing member (114) being interposed between the two modules on the plane of symmetry, the spacing member defining a chamber (120) between the modules for communicating with the outlets.

Inventors: GOLEMBIEWSKI, ALAN L., THURSTON, JOHN F.
Applicants: ALLIED-SIGNAL INC. (A DELAWARE CORPORATION)
Application year: 1987
Main classification: G01F1
IPC codes: G01F1