DENSITY INSENSITIVE CORIOLIS MASS FLOW RATE METER

Abstract: Design criteria for Coriolis mass flow rate meters with flow conduits having two modes of oscillation where the ratio of the resonant frequencies for the two modes is held constant irrespective of changes in the density of the fluid passing through the flow conduits. The design criteria embodied in the requirement that the ratio of modal mass to modal inertia for a flow conduit equal the ratio of the mass of all attachments to the flow conduit divided by the inertia of attachments to the flow conduit.

Description: DESCRIPTION DENSITY INSENSITIVE CORIOLIS MASS FLOW RATE METER Technical Field The present invention relates to Coriolis mass flow rate meters that include oscillating flow conduits. The flow conduits used in these Coriolis mass flow rate meters are mounted so they can oscillate at resonance frequencies about at least two axes. One of the axes is associated with externally applied forces used to oscillate each flow conduit. The other axis is asεociateα with deflections of each flow conduit caused by Coriolis forces arising from the combination of the driven oscillation and flov; of fluids through the flow conduit. For the present invention the flov/ conduits are designed so as to have the ratio of both resonance frequencies remain constant even when the mass of the flow conduits change because the density of the fluid passing through the flow conduits changes. Background Art In the art of measuring mass flow rates of flowing substances it is known that flowing a fluid through a oscillating flow conduit induces Coriolis forces to act on the conduit. It is also known that the magnitudes of such Coriolis forces are related to both the mass flow rate of the fluid passing through the conduit and the angular velocity at which the conduit is vibrated. One of the major technical problems previously associated, with efforts to .design and utake Coriolis mass flow rate instruments was the necessity either to measure accurately or control precisely the angular velocity of an oscillated flow conduit so that the mass flow rate of the fluid flowing through the flow conduits could be calculated using measurements of effects caused by Coriolis forces. Even if the angular velocity of a flow conduit could be accurately determined or controlled, precise measurement of the magnitude of effects caused by Coriolis forces was another severe technical problem. This problem arises in part because the magnitude of generated Coriolis orces axe very small, therefore ^resulting Coriolis force induced effects are minute. Further, because of the small magnitude of the Coriolis forces, effects resulting from external sources such as invariably present vibrations induced, for -example, by neighboring machinery or pressure surges in fluid lines cause erroneous determinations of mass flow rates. Such error sources may even completely mask the effects caused by generated Coriolis taxc&s .rende i g a-flow meter useless. A mechanical structure and measurement technique which, among other advantages: (a) avoids the need to measure or control the magnitude of the angular velocity of a Coriolis mass flow rate instrument's oscillating flow conduit; (b) concurrently provides requisite,sensitivity andaccuracy fcr the measurement of effects caused by Coriolis forces; and, (c) is not susceptible to errors resulting from external vibration sources, is taught in United States Patent Nos. Re 31,450, entitled Method and Structure for Flow Measurement'and,issued " November 29., laSS; 4,422=,338 entitled Method and Apparatus for Mass Flow Measurement and issued December 27, 1983; and 4,491,025 entitled Parallel Path Coriolis Mass Flow Rate Meter and issued January 1, 1985. The mechanical arrangements disclosed in these patents incorporate flow conduits having no pressure sensitive joints or sections, such as bellows or other pressure deformable portions. These flow conduits are solidly mounted in a cantilever fashion from their inlet and outlet ports. For example, the flow conduits can be welded or brazed to a support, so they can be oscillated in spring-like fashion about axes which are located near the solidly mounted sections of the flow conduits. Additionally the mounted flow conduits are preferably designed so they have resonant frequencies about the axes located near the solid mountings which are lower than the resonant frequencies about the axes relative to which Coriolis forces act. By so designing the flow conduits a mechanical situation arises whereby the forces opposing generated Coriolis forces are predominantly linear spring forces. The Coriolis forces, opposed by substantially linear spring forces, deflect the flow conduit about axes located between the portions of the flow conduits in which Coriolis forces are generated. The magnitude of the deflections are a function of the magnitudes of the generated Coriolis forces and the linear spring forces opposing the generated Coriolis forces. As stated above the flow conduits in aαdition to being deflected by the Coriolis forces are also driven to oscillate. Accordingly, one portion of each flow conduit on which the Coriolis forces act will be deflected so as to move ahead, in the direction in which the flow conduit is moving, of the other portion of the flow conduit on which Coriolis forces are acting. The amount of time required after the first .portion of- the oscillating flow conduit deflected by Coriolis forces has passed a preselected point on the path of oscillation for the flov/ conduit to the instant when the second portion passes a preselected point is a linear function of the mass flow rate of the fluid passing through the flow conduit; i.e. the relationship between the measured time and the mass flow rate of the fluid passing through the flow conduit is only dependent on constants derived from the mechanics of the flow conduit and its solid mounting. This relationship is not dependent on variables other than time which must be measured or ^ controlled. Optical seaisørs-as described in United States Patent No. Re 31,450 and electromagnetic velocity sensors as described in United States Patent Nos. 4,422,338 and 4,491,025 have been used for making the required time measurements from which mass flow rates of fluids can be determined. A double flow conduit embodiment with sensors for making the necessary time measurements is described in United States Patent No. 4,491,025. The double flow conduit embodiment -described in United.States -Patent No. 4,491,025 provides a Coriolis mass flow rate meter structure which is operated in a tuning fork manner as is also described in United States Reissue Patent Re 31,450. The tuning fork operation contributes to minimizing effects of external vibration forces. Kiiiimizing .effects of .external vibration. ' forces is important because these forces can induce errors in the required time measurement. Disclosure of Invention The density of fluids passing through Coriolis mass flow rate meters is always subject to change. For example, variable mixtures of constituents in a fluid or changes in the temperature of a fluid can alter fluid density. Changes in fluid density cause the masses of the oscillating flow conduits to also change and the variation of flow conduit mass in turn causes the resonance frequencies of the oscillating flow conduit to change. It is an object of the present invention to provide Coriolis mass flow rate meters which have the ratio of two resonance frequencies for each oscillating flow conduit maintained at a constant value irrespective of fluid density changes. Flow conduits made from tubes having essentially uniform wall thickness of homogeneous material and mounted so they can be oscillated inherently have resonance frequencies for all modes of oscillation where the ratio of any two resonance frequencies remains constant irrespective of changes in the density of fluids passing through the flow conduit. Attaching weights to such flow conduits which do not have their masses altered by fluid density changes, such as sensor components and drive components for oscillating a flow conduit, does however change the ratio of resonance frequencies as fluid density changes unless the positions for the masses of the weights attached to the flow conduit are uniquely selected. It is an object of the present invention to determine the unique positions for mounting drive components and sensors components on flow conduits such that changes in fluid density do not alter the magnitude of the ratio of the resonance frequencies of the flow conduits about the axes relative to which the flow conduits are driven to oscillate and about the axes relative to which the flow conduits are deflected by Coriolis f,orces_. B rief Description of Drawin g s The various objects, advantages and novel features of the present invention will be more readily apprehended from the following detailed description when read in conjunction with the appended drawings, in which corresponding components are designated by the same reference numerals throughout the various figures. FIG. 1 is a perspective view of the flow conduit arrangement for a Coriolis mass flow rate meter which can be used -with...the .present invention; FIG. 2 is a graph showing the amplification factor for an oscillating structure versus the ratio of the frequency at which the structure is driven to oscillate over the resonance frequency for a mode of oscillation of the structure; and, FIG. 3 is a plan front view of a flow conduit with dimensions identified for specifying the locations for attaching sensors and driver components an the.flow conduit -which has the-ratio of th -resonance ^ frequency about the A-A axis to the resonance frequency about the B-B axis maintained at a constant value that is independent of fluid density changes. Best Mode for Carrying Out the Invention A.Coriolis.mass flew..rate meter as.-generally designated by numeral 10, for which the present invention can be used, is shown in Figure 1. The flow meter 10 incorporates twin flov/ conduits 12. Other arrangements utilizing a single flow conduit and a spring arm, or a single light weight flow conduit solidly mounted to a relatively massive support can also be used with the present invention. The flow meter 10 in addition to the flow conduits 12 includes a driver 14, such as a permanent magnet and wire coil combination as is known in the art, to vibrate the flow conduits 12 as the prongs of a tuning fork. The flow meter 10 further includes sensors 16 mounted on the flow conduits 12. The sensors 16 shown in Figure 1 are analog velocity sensors which provide signals linearly representative of the actual movement of the flow conduits 12 over their entire path of motion. When the flow conduits 12 are oscillating and fluid is flowing through them, the flow conduits 12 are deflected about axes A-A by Coriolis forces. The effects of these deflections are monitored by the sensor 16. A detailed description of the mechanical operation of flow meter 10 is set forth in the aforementioned United States Patents: Re 31,450; and, 4,491,025. The sensors 16 are electromagnetic velocity sensors. Each sensor, 16, consists of a permanent magnet and a coil, with the coil designed so as to always be moved within the essentially uniform magnetic field of the magnet. Descriptions of the operation of sensors 16 for single and twin conduit Coriolis mass flow rate meters are set forth in the aforementioned United States Patents: 4,422,338; and 4,491,025. If the driver 14 and sensors 16 were not mounted on the flow conduits 12 then changes in the density of fluid passing through the flow conduits 12 would not alter the ratio of any of the resonance frequencies for the various modes of oscillation of the flow 2477 8 conαuits 12. This situation results from the fact that without the attachment of the driver 14 and the sensors 16 all the.resonance frequencies for the flow conαuits 12 are functions of the various modal stiffnesses, k^ , and modal masses H^- of the flow conduits 12 when filleα with fluid. Specifically, the various resonance frequencies ι £, can be calculated from: uk- * ι (1) When the density of the fluid in the flow conduits 12 changes, all of the modal masses change by the same percentage. Therefore the ratio of any two resonance jfreqiiencles remains constant irrespective of fluid density changes. This universal situation is negated when constant masses, i.e. masses not altered by changes in tluiα density, are attached to the flow conduits 12 because then the modal masses for the various modes of oscillation of the structure must be written as a summation. In such a case the resonance frequencies are calculated from the following relationship-: i - r^i/(!*'.+ / ) (2) Where: K are the masses of the attachments to the flow conduits 12 which are not altereα by changes in fluid .density, It is S TΪ from equation 2 "that if the density of the fluid passing through the flow conduits 12 changes the resonance frequencies, )j, all change in different proportions because the denominators include the summation of both oenεity sensitive modal masses and 2477 density insensitive masses. Therefore, the ratio of any two resonance frequencies is expected to change as fluid density changes. The flow conduits 12 of a preferred embodiment of flow meter 10 are driven to oscillate at the resonance frequency, lόo , for the mode of oscillation about the axes, B-B, by the driver 14. When fluid passes through the oscillating flow conduits 12, Coriolis forces cause the flow conduits 12 to deflect about the axes A-A at the same frequency as the driver 14 forces the flow conduits 12 to oscillate about the axes B-B. It is known in the art of analyzing mechanical oscillations that for each mode of oscillation of a mechanical structure a function description of the oscillatory motion can be written and that from these functions plots can be made of the amplification factor versus the ratio of the frequency at which a mechanical structure is driven to oscillate divided by the resonance frequency for the Selected mode of oscillation of the structure. An exempliary discussion of relevant analysis of mechanical oscillations is set out in Greenwood, D. T. , Principles of Dynamics. Prentice-Hall, pp 97-104 (1965) . A plot is shown in Figure 2 for such a function. At the value of one for the ratio of drive frequency, tύ©, to resonance requency,l-ύ | , the amplification factor has its maximum value. This situation is true for structures having small damping forces, which is the case for the flow conduits 12 of the flow meter 10. The fluids which pass through the flow conαuits 12 however can increase the damping forces on the flow conduits 12 and thereby decrease the amplification factor. In most practical applications, the effect of damping caused by fluids 8/02477 10 on the amplification factor is assumed to be a very negligible one which does not adversly effect the .operation of .Cor olis mass flow rate meters 10. Since the amplification factor is related to the magnitude of deflection of the structure, a large amplification factor means that when an oscillating structure is driven to oscillate at a resonance frequency large deflections will occur. Because the shape of the curve in Figure 2 is very steep on both sides of the maximum amplification factor value any changes in the value of the ratio of the drive frequency to the resonance frequency causes a large change in the amplificiation factor. Applying these facts to the Jlow meter 10 and using^Figure.2, the response of the • flew conduits 12 to Coriolis forces can be understood. From figure 2 it is seen that for deflections about the A-A axes the ma irnu amplification factor will occur when the flow conduits 12 are driven to oscillate at the resonance frequency for oscillations about the A-A axes. In a preferred embodiment the flow conduits 12 are driven to oscillate resonantly about the B-B axes which has a lower frequency than the resonant frequency-about-the _ft-A axes, :_For the preferred embodiment this difference in frequencies results in the flow conduits 12 operating at an amplification factor of approximately 1.2 as shown in Figure 2 by the line labeled C which has a value of approximately 0.4. The range of acceptable - -amplificatio -factors can .be -£rom greater than one (1.0) to five (5.0) It is advantageous to maintain an essentially constant amplification factor because the amount of deflection for flov; conduits 12 about the A-A axes is determined by the magnitude of„ Coriolis orces and the 02477 ' ' 11 amplification factor. If the amplification factor is not maintained at an essentially constant value, errors will arise in the determination of the mass flow rate of fluid passing through the deflected flow conαuits 12. Previously, the control of the amplification factor for flow meters was addressed by operating the flow conduits 12 at ratios of the drive frequency to resonance frequency having values where the amplification factor was essentially one, i.e. to the left of the line C in Figure 2. By so designing the flow conduits 12 with its attachments results in the situation where changes in the ratio of drive frequency to resonance frequency posed a relatively small problem because the amplification factor was nearly constant. However, if increased sensitivity is desired the amplification factors must be above one. Here the prior design approach i^ no longer acceptable. As seen from Figure 2 it is necessary to keep the ratio of the frequency at which the flow conduits 12 are driven to oscillate to the resonance f equency about the A-A axes, i. e. W 0 /i \ , essentially constant in order to have an essentially constant amplification factor above one. For flow conduits 12 with driver 14 and sensors 16 attached to the flow conduits 12 it has been found with the present invention that it is possible to maintain the ratio of drive frequency to the resonance frequency constant independent of fluid density changes. /02477 12 The flow conduits 12 can be analyzed as a six degree, of reedom mechanical structure having the following equations of motion : M L X C + K* X- = 0 j^ θ; + K? θ t - = o Where M- are the modal masses for the structure; X* are the translational displacements of the modal masses along three perpendicular translation axes; J ( - are the modal inertias for the structure.; θ^ are the angular displacements of the modal masses about three perpendicular rotation axes; K^ are the translational modal stiffnesses of the structure along the three translation axes; and; K- are the rotational modal stiffnesses of the structure about the three rotation .axes. From these general equations, which have solutions for all modes of oscillation of the flow conduits 12 in all directions, the specific resonance frequency ,oJ ώ , about the B-B axes for the flow conduits 12 can be the A- flow conduits 12 with respect to the B-B axes; and. A K^ are the modal stiffnesses of the flow conduits 12 with respect to the A-A axes. Since the modal stiffnesses, K^ and K ύ , are constants and the ratio of uSo/nii , is to be held constant the following relationship has to be obtained for the flow conduits 12: 3 " i/v i - constant ( 3) This equation as written is only accurate for flow conduits 12 without attachments having masses that are independent of fluid density variations. When attachments, e.g. driver 14 and sensors 16, are fixed onto flow conduits 12 ; it has been found equation (3) must be rewritten as: " (f>) + T = constant ^ Where J c - ( z>) are modal inertias for the conduits 12 and the contained fluid which is dependent on density; hi I ( £> ) are the modal massec of the flow conduits 12 e ά the contained fluid which is dependent on density; J is the total rotational inertia about the A-A axes of the attachments to flow conduits 12 which are independent of fluid density; and M is the total mass of the attachments to flow conduits 12 which are independent of fluid density. It has been found for the present invention that to have the left side of equation (4) equal a constant irrespective of changes in fluid density the following relationship must be maintained: JUϋ£ - S ( 5 ) i < » 3 " In designing flow meters 10 to have constant ratios of the drive resonance frequency to the resonance frequency about the A-A axes the modal inertias and modal masses which are solutions of equation (5) for the.flow conduits 12 r ust be determined by either calculation or experiment. These modal masses and inertias must be determined with all of the attachments, e.g. driver 14 and sensors 16, mounted on the flow conduits 12 'th t are necessary for operation of flow meter 10. To determine the modal masses and inertias the following procedure is used: 1. The resonant frequency, OJ 0 , for ,,©scϋlaticn * o£.-£he flow conduits 12 ^without any attachments about the Έ-Έ axes is determined either experimentally or by using an analytical method such as a finite element computer program. 2. Next each of the attachments, i.e_. the driver 14 and sensor 16 components, are assigned locations on the flow conduits 12, and the resonant frequency, t 0 , for oscillation of the flow conduits 12 with the attachments having a total mass M about the B-B axes is determined either experimentally or by using an analytical method such as a finite element computer program. 3. The following relationships then are used to determine the modal masses for the oscillations about the B-B axes: i^ s K ^M -(p) ( 6 ) A 1*1 = κ i /(Mi <f>)+rvC) ( 7 ) Solving equati is ( 6) and ( 7) f or M 4. The steps 1 through 3 are now repeated for oscillations of the flow conduits 12 about the A-A axes to determine the modal inertias . J { - ( p ) . Unlike the calculations for modal masses, however, modal inertia calculations require a combination of the mass M of each attachment and the perpendicular distance, Y , of the attachment from the A-A axis in the form M r z . After the resonant frequency, U^', for oscillations of the flow conduits 12 about the A-A axes without any attachments, and the resonant frequency, \A) ( , for oscillations of the flow conduits 12 about the A-A axes with attachments are determined, the following relationships can be used : cu>; - «> Tι<^ (9) Solving equations (9) and (10) for the modal inertias J Λa) the following is obtained: (ID vo, J Now using the above procedures for a selected pair of flow conduits 12 and selected masses for the components of driver 14 and sensors 16, and for selected positions of the attachments on flow conduits 12 all of the necessary characteristics of the flow conduits 12 with their attachments are known. If the ratio of resonance frequencies about the A-A, and B-B, axes will be insensitive to fluid density changes equation (5> must oe satisfied, i..e-.s The positions for mounting sensors 16 and driver 14 components on the flow conduits 12 and the masses of- the-components are-varied -until^equation (5) is satisfied. Flow meters 10 of the type shown in Figure 1 have thi.ce locations for each flow conduit 12 where attachments are made. One location is for the components of the driver 1.4, an «.twovlocations are for 8/02477 ' the components of the sensors 16. It is required that the driver 14 components be mounted on the A-A axes of flow conduits 12. This fact arises from the requirement to drive the flow conduits 12 to oscillate about the B-B axes and not to impose oscillations of the flow conduits 12 about the A-A axes by the forces from the driver 14. In so mounting the driver 14 essentiallly on the A-A axes, the inertia J is essentially unaffected by the attachment of the driver 14 components to the flow conduits 12. Thus the critical attachments are the sensor 16 components. These sensor 16 components must be positioned essentially adjacent to the flow conduits 12 at the widest separation to sense the maximum signals and to have the shortest mounting distance from the flow conduits 12 so as to minimize extraneous harmonic motions of mounted sensor 16 components. Therefore, the preferable positions of the components for the driver 14 and the sensors 16 on the flow conduits 12 are localized and the determination of the unique combination of driver 14 and sensor 16 component masses and mounting locations on flow conduits 12 where equation (5) is satisfied can be determined using the procedure disclosed above. Using the procedure described above a pair of flow conduits 12 with driver 14 and sensors 16 components attached to the flow conduits 12 were designed and tested to verify that the combinations provided a ratio of resonance frequencies about the A-A and B-B axes which was independent of fluid density changes. The flow conduits 12 were made from seamless 316L stainless steel tubing, 18, (see Figure 3) per American Society for Testing Materials (ASTM) No. A- 632. The tubing 18 had an outside diameter of 1.110 centimeters and a wall thickness of 0.071 centimeters, and was bent so as to have the dimensions set out below in Table I: Table I (see Figure 3) Parameter Dimension (centimeters) L 19.050 R 5.080 W 20.320 For driver 14 and sensors 16 having components of equal mass and with the tubing 18 the procedure of this invention was .used to .calculate the locations, 20, for mounting the components of sensors 16 (see Figure 3) and the location 22, for mounting the components of driver 14 to provide an arrangement which has an essentially constant ratio of resonance frequencies about the A-A and B-B axes that is independent of fluid density changes. The dimensions for the calculated locations where the components of drivers 14 and sensors 16 are mounted with respect to the tubing 18 -is set. out below in.Table XX. Table II (see Figure 3) Parameter Dimension (centimeters) D .15.240 d 0.871 F 0.871 Using the arrangements set out in Table I and Table i: with driver 14 and sensor 16 components having 325 grain masses the operational parameters set out in Table III were calculated and experimentally measured as indicated for a tubing 18 filled with either air having a specific gravity of zero or water having a specific gravity of one. Table III Resonance Resonance Mode of Fr eαuency Freσuency Oscillation Measured Cal culated (Hertz) Fl ui d ( Hertz ) (He ) ai r 94.475 89.546 ai r 223 .500 224.639 water 84.500 83 .360 water 199.800 208.233 is for oscillations about the B-B axis and is for oscilations about the A-A axis. For the results set out in Table III the following ratio of resonance frequencies are obtained. Table IV Fl uid Measured Calculated ai r 0.423 0.399 water 0.423 0.400 These results show that for the experimentally measured resonance frequencies- there is no difference between the resonance frequency ratios for air and water. While for the calculated resonance frequencies there is a 0.25 percent difference in the ratios. This difference is neglible in actual meters as is demonstrated by the measured results also set out in Table IV. Other embodiments of the invention will be apparent to those of skill in the art from consideration of this specification or practice of this invention. The specification is intended as exemplary only with the true scope of the invention being indicated by the following claims.

Claims: Claims 1. A method for designing Coriolis mass flow rate meters having flow conduits with essentially uniformly thick walls made of a homogeneous material, each of said flow conduits driven to oscillate resonantly, comprising: a) determination of a first resonant frequency for said flow conduit, having no attachments, about the axis relative to which the flow conduit is driven to oscillate; b) determination of a second resonant frequency for said flow conduit, with all attachments to said flow conduit required for operation of said flow meter, about the axis relative to which said flow conduit is driven to oscillate; c) determination of the modal mass for said flow conduit as a function of the determined first and second resonant frequencies and of the masses of said attachments; d) determination of a third resonant frequency for said flow conduit, having no attachments, about the axis relative to which said flow conduit is deflected by Coriolis forces; e) determination of a fourth resonant frequency for said flow conduit, with all attachments to said flow conduit required for operation of said flow meter, about the axis relative to which said flow conduit is deflected by Coriolis forces; f) determination of the modal inertia for said flow conduit as a function of the determined third and fourth resonant frequencies and of the inertias of said attachments; and g) changing the masses and locations of mounting of said attachments to said flow conduit so that the ratio of the modal mass to modal inertia equals the ratio of the mass of said attachments to the inertia of said attachments, „_,.,., PCT/US87/02482 /02477 ' —22- thereby having the ratio of the second resonant frequency to the fourth resonant frequency equal a constant. 2. A method according to claim 1 wherein said attachments include drive means for forcing said flow conduit to oscillate and sensor means for sensing deflections of said flow conduit. 3. A method according to claim 1 wherein said Coriolis mass flow rate meter has an amplification factor in the range of greater than one (1.0) to about five (5.0). 4. A method for designing Coriolis mass flow rate meters having flow co uits-..with-essentially uniformly thick walls made of a homogeneous material, each of said flow conouits driven to oscillate resonantly, comprising: a) determination of a first resonant frequency for said flow conduit, having no attachments, about the axis relative to which the flow conduit is driven to oscillate; b) determination of a second, esonant frequency for said flow conduit, wi all attachments to said flow conduit required for operation of said flow meter, about the axis relative to which said flow conduit is driven to oscillate; c) determination of the modal inertia for said flow conduit as a function of the determined first and second xesonant-frequencies and of the inertias of said attachments; d) determination of a third resonant frequency for said flow conduit, having no attachments, about the axis relative to which said flow conduit is deflected byXoriolis forces; e) determination of a fourth resonant frequency for said flow conduit, with all attachments to said flow conduit required for operation of said flow -meter, aboutthe axis relative to which said flow conduit is deflected by Coriolis forces; f) determination of the modal mass for said flow conduit as a function of the determined third and fourth resonant frequencies and of the masses of said attachments; and g) changing the masses and locations of mounting of said attachments to said flow conduit so that the ratio of the modal mass to modal inertia equals the ratio of the mass of said attachments to the inertia of said attachments, thereby having the ratio of the second resonant frequency to the fourth resonant frequency equal a constant. 5. A method according to claim 4 wherein said attachments include drive means for forcing said flow conduit to oscillate and sensor j eans for sensing deflections of said flow conduit. 6. A method according to claim 4 wherein said Coriolis mass flow rate meter has an amplification factor in the range of greater than one (1.0) to about five (5.0).

Inventors: CAGE DONALD, GRAMMENS GERALD MARTIN, CAGE, DONALD, GRAMMENS, GERALD, MARTIN
Applicants: MICRO MOTION INC, MICRO MOTION, INC.
Application year: 1987
Main classification: G01F1
IPC codes: G01F1