WO1999041735A1 - Resonant structures for transducers - Google Patents

Resonant structures for transducers Download PDF

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Publication number
WO1999041735A1
WO1999041735A1 PCT/GB1999/000421 GB9900421W WO9941735A1 WO 1999041735 A1 WO1999041735 A1 WO 1999041735A1 GB 9900421 W GB9900421 W GB 9900421W WO 9941735 A1 WO9941735 A1 WO 9941735A1
Authority
WO
WIPO (PCT)
Prior art keywords
mass
fluid
transducer
vibration
spring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/GB1999/000421
Other languages
English (en)
French (fr)
Inventor
John Gerrard Gallagher
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hydramotion Ltd
Original Assignee
Hydramotion Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hydramotion Ltd filed Critical Hydramotion Ltd
Priority to JP2000531837A priority Critical patent/JP4106181B2/ja
Priority to DE69907411T priority patent/DE69907411T2/de
Priority to EP99905010A priority patent/EP1053542B1/en
Priority to US09/622,311 priority patent/US6450013B1/en
Priority to AU25320/99A priority patent/AU2532099A/en
Publication of WO1999041735A1 publication Critical patent/WO1999041735A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/10Measuring characteristics of vibrations in solids by using direct conduction to the detector of torsional vibrations

Definitions

  • This invention relates to transducers and to resonant structures for transducers, particularly structures which comprise a first member, which may be driven into vibration, and a second member, which may carry a sensing element and is disposed in a medium of which a property is to be measured
  • the first and second members are intended to vibrate in antiphase, there being a vibrational node of normally zero displacement at a connection by means of which the vibrating structure is supported
  • a vibrational node of normally zero displacement at a connection by means of which the vibrating structure is supported
  • the nodal point is connected to a mechanical datum by a flexible means which is substantially more compliant than the first and second members
  • the amplitude and frequency of vibration which may be torsional or lateral or longitudinal of the first member are the same as those of the second member carrying the sensing element immersed in the medium, which may be gas, liquid or even solid
  • One important feature of the present invention is the use of a semi-rigid connecting member between the nexus of the first and second members and a support
  • the 'semi-rigid' member is intended to have a stiffness which significantly affects, and preferably controls, the relative motions of the first and second members It preferably provides a node which is more rigid than the first and second members
  • This kind of member can avoid the disadvantage of very compliant mounts, which are generally unable to withstand the high pressures and forces encountered in many industnal applications
  • the stiffness of the connecting member or means may be selected to control the sensitivity of the measuring instrument of which the transducer forms a part
  • a further feature of the invention is the use of a re-entrant member or resonator enclosed within a sensing element which preferably forms part of the second member but which may have utility independently of the connecting member mentioned above
  • a re-entrant element is intended to vibrate relative to the sensing element, being constituted preferably by a spring-mass structure, but unaffected by the medium in which the sensing element is immersed
  • Such a re-entrant element or additional resonator may enable the alteration of the -2- characteristics of the transducer in a simple and reliable manner
  • Figure 1 illustrates a resonator structure according to the invention, Figure 1 A illustrating the mechanical structure and Figure IB being a schematic model of the structure;
  • Figures 2 and 3 illustrate similar structures to that shown in Figure 1 , but operable in different vibrational modes, Figures 2A and 3A illustrating the structures and Figures 2B and 3B the schematic models,
  • Figure 4 is a graph illustrating variation of amplitude of vibration with frequency
  • Figure 5 is a graph of amplitude against frequency showing the effects of a connecting member.
  • Figures 1 , 2 and 3 each show a resonator structure forming part of a transducer for the measurement of properties of a medium, and including a first member 11, 21, composed of an inertial mass 11 and a shaft 21.
  • a second member of which the inertial mass is preferably constituted by a sensing element such as a paddle 12 includes a second shaft 22, the shafts 21 and 22 having a connection region, hereinafter called nexus 13
  • the nexus is itself supported by a connection member, in this example a tube 23, which is secured to a mounting base 10
  • the base and the connecting member define two distinct regions, one above and one below the mounting member so that for example the sensing element 12 may be disposed in a medium which is to be measured and the first member (which may be electromagnetically driven) can vibrate in air
  • the sensing element 12 may be disposed in a medium which is to be measured and the first member (which may be electromagnetically driven) can vibrate in air
  • the first member which may be electromagnetically driven
  • FIG. 1 The difference between Figures 1, 2 and 3 lies in the different modes of vibration experienced by the respective structures
  • the structure shown in Figure 1 is intended to vibrate torsionally, the first member twisting as shown by the arrow 1 and the lower member twisting in the opposite direction as shown by the arrow 1A
  • the members are intended to vibrate longitudinally, as exemplified by the double headed arrow 2 above the member 1 1
  • the members are intended to vibrate laterally, as shown by the double headed arrow 3
  • the driven end can be stimulated and sensed by a variety of means, electromagnetic force and field, piezoelectric stress and stain, acoustic pressure, or electrostatic force and field.
  • the structures also include, as will be explained later, a re-entrant resonator.
  • the sensing element 12 is a hollow paddle or cylinder and within the sensing element, physically separated from the medium surrounding the sensing element, is a mass 14 connected to the sense element by a shaft 24.
  • a similar resonator which is intended to vibrate in essentially the same mode, torsional, longitudinal or lateral as the remainder of the respective system vibrates.
  • the transducer illustrated comprises three and preferably four independent torsional spring- mass systems connected as shown in Figure IB.
  • Equivalent systems for longitudinal vibration and lateral vibration are shown in Figure 2B and Figure 3.
  • the following description is mainly concerned with torsional vibration.
  • Jl and Kl are the inertial mass and stiffness of the first member (11,21), J2 and K2 are the inertial mass and stiffness of the second member and so on.
  • K4 ⁇ 4 y(( ⁇ 2 (Kl + K2) + K2 - 2 ⁇ K2)/( ⁇ 2 Jl + J2))
  • K4 ⁇ 4 > (( ⁇ 2 (Kl + K2) + K2 - 2 ⁇ K2)/(crMl + M2))
  • This member 23 is designed to accommodate some residual movement at the nodal region
  • the rigidity of the member 23 imparts high structural strength and stability of alignment of transducer components whilst under the rigours of industrial use It also, importantly, controls the amount of torsional torque imparted from one side of the fluidic divide, from the shaft 21 into the shaft 21 on the other side, and in so doing forms a means for controlling the relative motion of the two shafts This allows the selection of instrument sensitivity based on the value ofK3
  • a semi-rigid member 23 alters the main modal response of the sensor from a single resonant peak Fj ( Figure 5) to that of two resonant peaks F- . and F 2 .
  • One peak is formed essentially from the desirable interaction of Kl, K2 and K4 (and their respective masses) but the second peak is a result of the substantial stiffness of K3 also interacting with these systems.
  • This second resonant peak is undesirable and is easily removed by filtering; its elimination is further aided by increased damping at the sensor mounting, facilitated by attachment to process plant or some other fixing
  • a metallic connection rather than an elastomeric connection, is also preferred since metals can be selected to have a much lower damping capacity than elastomers and thus give higher Q resonators as a result.
  • the new design allows the Q-factor to be maintained regardless of viscosity and can deliver extremely high vibrational efficiencies (greater than 5000) at the very highest fluid viscosity (millions of centipoise)
  • the design uses the spring-mass resonator combination 14, 24 mounted within the sensing element This resonator is free from the damping effects of the surrounding fluid and maintains its torsional strain energy regardless of fluid conditions
  • sensors can be manufactured as a standard design and adjusted to suit any fluid viscosity range simply by minor alteration of the stiffness (i.e. diameter) of the sense element 12. This can take place with little effect on the balance condition (equal frequencies) at the node since in most cases the resonant frequencies will be determined by Jl, Kl and J4, K4, rather than K2 (so long as K2»K4).
  • the characterisation of performance of a transducer by simply adjusting one dimension results in improved manufacturing efficiency and is thus commercially beneficial.
  • the drive end 11 of the resonator shown in Figure 1 is stimulated into torsional vibration by applying a twisting moment using a ferrous bar fixed normally to the shaft.
  • An electromagnet positioned some distance from the centre of rotation applies an electromagnetic force to the ferrous bar, causing it to make angular displacements.
  • the current to the electromagnet is switched or modulated at the resonant frequency of the spring-mass system causing the arrangement to vibrate at a resonant frequency.
  • a regenerative drive in which for example an electromagnetic pickup senses the angular movement
  • a signal from the pick-up is amplified and phase adjusted and then fed back to constitute a drive signal for the electromagnet
  • connection 23 forms a substantial fluid barrier capable of withstanding high fluid pressure and temperature
  • the sense element may have a selection of different end masses, or no mass -7- whatsoever, attached to its end point
  • the driven end may be stimulated and sensed by a variety of means, electromagnetic force and field, piezoelectric stress and strain, acoustic pressure, or electrostatic force and field
  • the transducer body can be screwed or welded to a conventional process connection such as a screwed fitting or flange
  • a further configuration uses two drive electromagnets and two magnetic pick-ups to promote torsional vibration and to inhibit any lateral vibrations of the shaft
  • the dnve shaft 11 is preferably balanced to match the frequency of vibration of the sense shaft 22 using end weights secured to the end of the shaft 1 1 In this way the node point is well established at the desired position and the vibrational performance of the transducer is made independent of any external stresses applied to the assembly
  • the Q or sharpness of the resonant peak, is an indication of the amount of energy lost versus the input energy to the vibrating system for each cycle of vibration As the energy loss increases due to increasing viscosity the Q of the system decreases
  • the transducer can be selectively configured for optimum viscosity range
  • the sense end mass is geometrically configured so that fluid is displaced during vibrational excursions then there will be a mass loading effect on the sense element Since the resonant frequency of the system is a function of the mass moment of inertia of the end element, the -8- resonant frequency will be modulated by the density of the fluid. Thus the density of the fluid can be correlated with the frequency of the vibration of the system.
  • the fluid density is determined.
  • the resonant frequency of the transducer is decreased with the addition of mass to the end of shaft (so long as this does not increase stiffness).
  • the frequency further decreases as the added mass is displaced further away from the axis of rotation as this increases the polar mass moment of inertia.
  • the frequency of vibration becomes very sensitive to small changes of mass on the disk.
  • a second resonator is employed. Since both sensors experience the same temperature, but only one is used for the mass measurement, the division of the frequencies from each transducer will yield a quotient that changes only with mass and is independent of temperature.
  • Such an instrument is capable of detecting changes in mass due to the following activities of matter placed on the disk or the disk itself:
  • Such measurements can be made on matter in the gas, liquid or solid phase or any combination of these phases in the chemical or physical process. For example, it is possible to measure the -9- loss of mass of a liquid lacquer as it releases a gaseous solvent vapour in its drying process; this yields the mass of liquid lacquer, the mass of gaseous solvent, and the remaining solid resin.
  • the Q of the system is measured to determine the viscosity or rheological behaviour of the disk material on the disk. This gives further analytical data for understanding the dynamic behaviour of matter in a physical or chemical process - for example the changes from liquid to solid state.
  • the arrangement is also useful for determining the viscosity of a droplet of fluid rather than complete immersion of the sensor in fluid.
  • the mass balance technique determines the quantity of fluid present and this is combined with the viscous energy loss reading to determine the fluid viscosity.
  • the skin depth is the amount of fluid near a vibrating surface that contributes to the added mass of the system. It is a function of density, viscosity and frequency of vibration. As a fluid becomes more viscous (more solid) its skin depth increases; for example, if a resin is drying on the measurement surface its viscosity increases and consequently an apparent increase in mass is witnessed due to the increase in skin depth.
  • This provides a continuous on-line measurement of a chemical reaction, determined by the type of surface chemical used and its reaction with other chemicals.
  • the nature of a reaction, and unknown reactants can be determined. For instance, in accordance with Faraday's Electrolysis Law, that the mass of electrolytically deposited material is a function of time, electric current and atomic mass and valency. With -10- mass, time and current known, the deposited atoms can be determined from atomic weight/valency estimates.
  • the instrument can be used for the continuous on-line measurement of air and water contaminants.
  • the use of the second reference resonator which has not been sensitised with the chemical composition eliminates frequency changes due to temperature or fouling.
  • Mass changes due to radioactive decay can be measured in a similar way.
  • the instrument can be used with a disk coated with a biochemical substrate which could, say, promote the growth of bacterial culture, so that a sensitive determination of the rate of growth of the culture can be made. Changes in the mass or rheological behaviour of inorganic, organic or biological matter in the gas, liquid or solid phases can be measured over time.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
PCT/GB1999/000421 1998-02-12 1999-02-10 Resonant structures for transducers Ceased WO1999041735A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2000531837A JP4106181B2 (ja) 1998-02-12 1999-02-10 トランスデューサ用共振構造
DE69907411T DE69907411T2 (de) 1998-02-12 1999-02-10 Resonanzstruktur für akustische wandler
EP99905010A EP1053542B1 (en) 1998-02-12 1999-02-10 Resonant structures for transducers
US09/622,311 US6450013B1 (en) 1998-02-12 1999-02-10 Resonant structures for transducers
AU25320/99A AU2532099A (en) 1998-02-12 1999-02-10 Resonant structures for transducers

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9802907.7A GB9802907D0 (en) 1998-02-12 1998-02-12 Resonant structures for transducers
GB9802907.7 1998-02-12

Publications (1)

Publication Number Publication Date
WO1999041735A1 true WO1999041735A1 (en) 1999-08-19

Family

ID=10826820

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB1999/000421 Ceased WO1999041735A1 (en) 1998-02-12 1999-02-10 Resonant structures for transducers

Country Status (8)

Country Link
US (1) US6450013B1 (https=)
EP (1) EP1053542B1 (https=)
JP (1) JP4106181B2 (https=)
CN (1) CN1125429C (https=)
AU (1) AU2532099A (https=)
DE (1) DE69907411T2 (https=)
GB (1) GB9802907D0 (https=)
WO (1) WO1999041735A1 (https=)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1698882A3 (de) * 2005-03-01 2014-01-29 Robert Bosch Gmbh Vorrichtung und Verfahren zur Messung von Eigenschaften eines fluiden Mediums
CN110914663A (zh) * 2017-04-27 2020-03-24 海德拉运动有限公司 振动的屈服应力流体的性质的测量

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6964196B2 (en) * 2002-07-08 2005-11-15 Texas Instruments Incorporated Resonant pivoting surface with inertially coupled activation
KR100587822B1 (ko) * 2004-07-15 2006-06-12 한국항공우주연구원 무중력 환경에서의 관성력과 표준 질량을 이용한 질량측정 시스템 및 방법
US20080037363A1 (en) * 2006-08-14 2008-02-14 Michael Joe Brannon Agitation system and method for measuring settling rate of solids from a suspension
KR100931153B1 (ko) * 2006-10-18 2009-12-10 현대자동차주식회사 대칭형 점도 센서
US8347693B2 (en) * 2010-08-26 2013-01-08 Halliburton Energy Services, Inc. Apparatus and methods for continuous compatibility testing of subterranean fluids and their compositions under wellbore conditions
US9267872B2 (en) * 2010-09-07 2016-02-23 Rheonics Gmbh Fluid properties measurement device having a symmetric resonator
WO2016109451A1 (en) 2014-12-29 2016-07-07 Concentric Meter Corporation Electromagnetic transducer
US10126266B2 (en) 2014-12-29 2018-11-13 Concentric Meter Corporation Fluid parameter sensor and meter
EP3215812B1 (en) 2014-12-29 2020-10-07 Concentric Meter Corporation Fluid parameter sensor and meter
GB201518986D0 (en) * 2015-10-27 2015-12-09 Hydramotion Ltd Method and apparatus for the measurement of fluid properties
EP3214424A1 (en) 2016-03-04 2017-09-06 Buira Nunez, Ernest A detection device, a system and a method for measuring fluid properties including viscosity and/or density
WO2018118011A1 (en) * 2016-12-19 2018-06-28 Rheonics, Inc. Resonant sensors for measuring fluid properties capable of operating at high temperatures and pressures
US11709119B2 (en) * 2020-01-06 2023-07-25 Saudi Arabian Oil Company Determining the rheological properties of a fluid through a non-linear response
GB202307930D0 (en) * 2023-05-26 2023-07-12 Hydramotion Ltd Multi-oscillator viscoelastic sensing

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DE915792C (de) * 1942-03-07 1954-07-29 Atlas Werke Ag Vorrichtung zum Senden und Empfangen von Schallwellen im Wasser oder sonstigen fluessigen Medien, insbesondere auf Schiffen
US3712117A (en) * 1971-01-12 1973-01-23 Nat Metal & Refining Co High precision wide dynamic range viscous loss measuring apparatus
GB2281621A (en) * 1993-09-06 1995-03-08 Yamaichi Electronics Co Ltd Measurement of liquid parameters using resonant vibration
JPH08247917A (ja) * 1995-03-13 1996-09-27 Yamaichi Electron Co Ltd 振動形検液装置

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JPS63272300A (ja) 1987-04-30 1988-11-09 Yamaichi Electric Mfg Co Ltd 円方向振動子

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Publication number Priority date Publication date Assignee Title
DE915792C (de) * 1942-03-07 1954-07-29 Atlas Werke Ag Vorrichtung zum Senden und Empfangen von Schallwellen im Wasser oder sonstigen fluessigen Medien, insbesondere auf Schiffen
US3712117A (en) * 1971-01-12 1973-01-23 Nat Metal & Refining Co High precision wide dynamic range viscous loss measuring apparatus
GB2281621A (en) * 1993-09-06 1995-03-08 Yamaichi Electronics Co Ltd Measurement of liquid parameters using resonant vibration
JPH08247917A (ja) * 1995-03-13 1996-09-27 Yamaichi Electron Co Ltd 振動形検液装置
US5723771A (en) * 1995-03-13 1998-03-03 Yamaichi Electronics Co., Ltd. Vibratory liquid detector

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1698882A3 (de) * 2005-03-01 2014-01-29 Robert Bosch Gmbh Vorrichtung und Verfahren zur Messung von Eigenschaften eines fluiden Mediums
CN110914663A (zh) * 2017-04-27 2020-03-24 海德拉运动有限公司 振动的屈服应力流体的性质的测量
CN110914663B (zh) * 2017-04-27 2023-06-13 海德拉运动有限公司 振动的屈服应力流体的性质的测量

Also Published As

Publication number Publication date
GB9802907D0 (en) 1998-04-08
EP1053542A1 (en) 2000-11-22
CN1125429C (zh) 2003-10-22
US6450013B1 (en) 2002-09-17
DE69907411T2 (de) 2004-03-18
CN1292912A (zh) 2001-04-25
DE69907411D1 (de) 2003-06-05
JP2002503819A (ja) 2002-02-05
EP1053542B1 (en) 2003-05-02
JP4106181B2 (ja) 2008-06-25
AU2532099A (en) 1999-08-30

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