WO1997049997A1 - Flow transducer - Google Patents

Flow transducer Download PDF

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Publication number
WO1997049997A1
WO1997049997A1 PCT/GB1997/001719 GB9701719W WO9749997A1 WO 1997049997 A1 WO1997049997 A1 WO 1997049997A1 GB 9701719 W GB9701719 W GB 9701719W WO 9749997 A1 WO9749997 A1 WO 9749997A1
Authority
WO
WIPO (PCT)
Prior art keywords
flow
sensor according
inlet
outlet
sensor
Prior art date
Application number
PCT/GB1997/001719
Other languages
English (en)
French (fr)
Inventor
Amir Hassan Malek Mohamady Noori
Original Assignee
Specialised Laboratory Equipment 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 Specialised Laboratory Equipment Ltd. filed Critical Specialised Laboratory Equipment Ltd.
Publication of WO1997049997A1 publication Critical patent/WO1997049997A1/en

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Classifications

    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61BDIAGNOSIS; SURGERY; IDENTIFICATION
    • A61B5/00Measuring for diagnostic purposes; Identification of persons
    • A61B5/08Detecting, measuring or recording devices for evaluating the respiratory organs
    • A61B5/087Measuring breath flow
    • A61B5/0878Measuring breath flow using temperature sensing means
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01FMEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/68Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using thermal effects
    • G01F1/684Structural arrangements; Mounting of elements, e.g. in relation to fluid flow
    • G01F1/6842Structural arrangements; Mounting of elements, e.g. in relation to fluid flow with means for influencing the fluid flow
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00Indicating or recording presence, absence, or direction, of movement
    • G01P13/02Indicating direction only, e.g. by weather vane
    • G01P13/04Indicating positive or negative direction of a linear movement or clockwise or anti-clockwise direction of a rotational movement
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/10Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring thermal variables
    • G01P5/12Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring thermal variables using variation of resistance of a heated conductor

Definitions

  • the present invention relates to a flow transducer or hot wire sensor useful for measuring bi-directional flow of gas, for example during the ventilation of patients.
  • Flow and volume information coupled with a pressure transducer will provide useful information, such as the detection of a leak in the system, the compliance of the circuit, the effect of the drugs on compliance and the synchronisation of the patient with the ventilator. Such information is particularly critical in patients ventilated with high frequency ventilators, since in general they have the most severe respiratory problems.
  • the hot-wire principle is well known, and the technique of measuring fluid flow with a hot wire is used in many different applications, ranging from measuring wind speed in a wind tunnel to the quantity of air injected into a fuel injection carburettor.
  • the principle is that passage of a moving fluid over a hot surface tends to cool the surface, the rate of the heat loss from the hot surface being proportional to fluid velocity.
  • FIG. 1 shows a common arrangement for hot-wire flow measurement.
  • a sensing wire S commonly of platinum, inserted in one leg of a Wheatstone Bridge W is kept at a constant temperature by the action of a servo amplifier R the output of which provides the bridge supply (see, for example, "Evaluation of a Constant Temperature Hot Wire Sensor for Respiratory Gas Flow Measurement", J S Lundsgaard, Med. Biolog. Eng. Comput. , vol. 17, pages 211-215) .
  • a control T such as a variable resistor, in a second leg of the bridge, is adjusted to pre-set a required temperature. When the flow velocity increases the sensing wire becomes cooler and its resistance decreases, forcing the output of the amplifier to rise and bring the wire temperature back to the pre-set value. Because the output of the bridge is dependent on convected heat loss, the result is a true mass flow measurement.
  • a vane is used to enable the measurement of flow direction.
  • US Patent No. 4 363 238 discloses another arrangement in which two hot-wires A, C are used, with an interposed bar B to shield one of the wires in one direction, as illustrated schematically in Figure 2. It is necessary for wire A and bar B to be accurately positioned relative to each other for reliable results.
  • the present invention provides a hot-wire sensor comprising a flow conduit having an inlet portion and an outlet portion and arranged such that in use the majority of fluid flowing from the inlet to the outlet follows a first flow path and the majority of fluid flowing from the outlet to the inlet follows a second flow path, the first and second paths being spatially separate along at least a portion of their respective lengths, a first sensing wire placed in said portion of the first flow path and a second sensing wire placed in said portion of the second flow path.
  • spatial separation of the first and second flow path portions may be produced by making the inlet and the outlet of the sensor non-collinear.
  • the inlet portion and outlet portion are parallel, and they may be of generally uniform internal cross section, e.g. circular, square or rectangular.
  • the conduit may have an enlarged central portion where the spatially separate portions are located, and the inlet, outlet and central portion may have common (continuous) upper and lower wall portions.
  • the sensor could include other transducers, for example a pressure transducer.
  • An island may be located within the sensor, for example between the first and second wires, to provide the spatially separate flow path portions laterally either side thereof, by its position and/or shape.
  • This island could extend fully or partially between the upper and lower walls of the flow conduit, and could include the other transducer(s) .
  • a sensor according to the present invention used as a bidirectional flow sensor can have a fast response time and a high dynamic range enabling it to work with HFO (high frequency oscillation) ventilators which could produce a sinusoidal flow of 20 Hz.
  • HFO high frequency oscillation
  • Figure 1 shows a known circuit arrangement for a hot wire anemometer
  • Figure 2 shows a known hot wire anemometer employing two wires for distinguishing oppositely directed flows
  • Figure 3 shows a schematic view of a hot wire sensor arrangement incorporating a sensor according to the present invention
  • Figure 4 is the elevation of a first embodiment of sensor according to the invention.
  • Figure 5 is the cross-sectional plan view of the sensor of Figure 4.
  • Figure 6 is the outlet end view of the sensor of Figure 4.
  • Figure 7 is the inlet end view of the sensor of Figure 4.
  • Figure 8 is a cross-section view of the sensor of Figure 5 along the line A-A;
  • Figure 9 is a second embodiment of sensor including flow separation barrier.
  • FIG 10 is a third embodiment of sensor including pressure transducer;
  • a sensor 1 according to the present invention (for example, as described in more detail with respect to Figures 4 to 8, Figure 9, or Figure 10) comprises two hot wires 2, 3 which are connected, by way of terminals 2a, b and 3a, b respectively, to their respective circuits in a control module 100 acting to keep their respective temperatures at a constant level, well above the ambient temperature.
  • the momentum of the flow will tend to carry it in a path straight to the wire 2 so that wire 2 will experience considerably more fluid flow than wire 3.
  • the differential output from the wires is quite large. When the flow is smaller, it tends to be less focused, and therefore a relatively large fraction of the flow will also be experienced by wire 3, tending to reduce the differential output from the wires.
  • Wire 3 can now be regarded as the sensing wire and the information from wire 2 could be discarded.
  • the control module compares the information from wire 2 to that from wire 3. If the difference between the flow indicated by wire 2 and that indicated by wire 3 is less than a predetermined level (the level is dependent on the sensor application) the flow is displayed as being zero. Otherwise, if the comparison indicates the higher flow is experienced by wire 2, the flow is taken as having the direction 101 and its magnitude is taken as that indicated by wire 2; and if the comparison indicates the higher flow is experienced by wire 3, the flow is taken as having the direction opposite that of direction 101 and its magnitude is taken as that indicated by wire 3.
  • a predetermined level the level is dependent on the sensor application
  • the sensor 1 comprises a flow conduit having an enlarged central portion 6 between an inlet 4 intended to connect to a ventilator Wye piece and an outlet 5 intended to connect to a endotracheal tube connector (as should be clear, the terms inlet and outlet are used merely to distinguish the two ends of the sensor, and are not definitive of flow direction) .
  • Inlet 4 and outlet 5 are parallel but offset, such that a side wall portion 7 of inlet 4 and a side wall portion 9 of outlet 5 continue as opposed side wall portions 8, 10 respectively of the enlarged portion.
  • Wall portions 11, 12 serve to connect the wall portions 10 and 8 to the other (opposed) side walls 13, 14 respectively of the inlet and outlet.
  • the inlet and outlet are of circular internal cross section, so that their upper and lower wall portions of the inlet and outlet are curved, and merge smoothly and continuously with the planar upper and lower wall portions of the enlarged portion.
  • the upper and lower wall portions of the inlet and outlet could be of another shape (e.g. planar in the case of a rectangular or square cross section, thereby providing a better transition to the enlarged portion) .
  • the walls of the enlarged portion may be non-planar, and could be shaped to encourage separation of the two flow paths, such as by providing smooth ridges therebetween.
  • the overall consideration should be that the boundaries of the flow conduit are smooth and do not exhibit discontinuities capable of disturbing the smoothness of the flow paths.
  • the joins between the side wall portions (8, 12; 12, 14; 9, 11; 11, 13) are smooth, rather than angular.
  • Sensing wires 2 and 3 are located in lateral spaced relation and at the same height, e.g. mid-height, within the enlarged portion 6, wire 2 being in line with the inlet 4 and wire 3 being in line with the outlet 5.
  • both the flow conduit and the transducer as a whole have a two-fold rotational axis of symmetry at right angles to the plane of Figure 5. It may be necessary to provide some means of distinguishing the input and output in order that the outputs from the two hot wires can be correctly identified.
  • Figure 9 shows views similar to those of Figures 4 to 8 for a second embodiment of sensor la wherein like parts have like references.
  • a flow separation barrier 16 is arranged between the wires 2, 3 and extends fully between the upper and lower walls of the flow conduit. Its position and shape assist in flow separation and so enhance flow direction detection at low fluid flow rates by production of a higher differential output from the sensor wires 2, 3.
  • the flow separation barrier 16 could comprise a pressure transducer.
  • Figure 10 shows views similar to those of Figures 4 to 8 for a third embodiment of sensor lb in which like parts are given like references in which a pressure transducer 15 is disposed centrally between the two hot wires 2, 3 for measuring the pressure delivered to the patient. This will allow the control module to determine the compliance and the airway resistance of the respiratory circuit. To a certain extent it will also assist in lateral separation of the differently directed flows as in the embodiment of Figure 9.
  • the pressure transducer can be placed at other locations, such as in the inlet or outlet, which is more likely to give an accurate pressure measurement, or at another position within the enlarged portion 6, as desired.
  • the degree to which the transducer extends into the sensor may be altered, between extending fully to the opposed wall (cf Figure 9) to a position flush with the wall (or even recessed below the wall) in which it is mounted.
  • the sensor may be operated at constant temperature using a circuit of the type outlined in Figure 1.
PCT/GB1997/001719 1996-06-25 1997-06-24 Flow transducer WO1997049997A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9613310.3A GB9613310D0 (en) 1996-06-25 1996-06-25 Hot wire sensor
GB9613310.3 1996-06-25

Publications (1)

Publication Number Publication Date
WO1997049997A1 true WO1997049997A1 (en) 1997-12-31

Family

ID=10795861

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB1997/001719 WO1997049997A1 (en) 1996-06-25 1997-06-24 Flow transducer

Country Status (2)

Country Link
GB (1) GB9613310D0 (de)
WO (1) WO1997049997A1 (de)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2773610A1 (fr) * 1998-01-09 1999-07-16 Bosch Gmbh Robert Dispositif de mesure de la masse d'un milieu circulant dans une conduite
FR2802632A1 (fr) * 1999-12-15 2001-06-22 Drager Medizintechnik Gmbh Dispositif et procede de mesure de la vitesse d'ecoulement d'un gaz
EP1950535A1 (de) * 2006-08-07 2008-07-30 General Electric Company Verfahren und System zur dynamischen Kompensation eines bidirektionalen Durchflusssensors während der Atmungstherapie
DE102009045956A1 (de) * 2009-10-23 2011-04-28 Endress + Hauser Flowtec Ag Verfahren zur Erfassung des Durchflusses und thermisches Durchflussmessgerät
WO2011161060A1 (en) * 2010-06-22 2011-12-29 Heinen & Löwenstein Gmbh Ventilation aid, ventilator, system and method for the non-invasive ventilation of premature infants
DE102011051196A1 (de) * 2011-06-20 2012-12-20 BBT Automotive Components GmbH Luftmassenmesser

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3147618A (en) * 1961-06-08 1964-09-08 Hastings Raydist Inc Fluid flow measuring apparatus
DE2164180A1 (de) * 1970-12-26 1972-07-20 Yokogawa Electric Works Ltd Strömungsmesser
EP0267354A1 (de) * 1986-11-04 1988-05-18 VDO Adolf Schindling AG Vorrichtung zur Bestimmung der Durchflussrichtung
JPH07234143A (ja) * 1994-02-25 1995-09-05 Unisia Jecs Corp 内燃機関の吸入空気流量検出装置
JPH07280613A (ja) * 1994-04-13 1995-10-27 Unisia Jecs Corp 空気流量検出装置

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3147618A (en) * 1961-06-08 1964-09-08 Hastings Raydist Inc Fluid flow measuring apparatus
DE2164180A1 (de) * 1970-12-26 1972-07-20 Yokogawa Electric Works Ltd Strömungsmesser
EP0267354A1 (de) * 1986-11-04 1988-05-18 VDO Adolf Schindling AG Vorrichtung zur Bestimmung der Durchflussrichtung
JPH07234143A (ja) * 1994-02-25 1995-09-05 Unisia Jecs Corp 内燃機関の吸入空気流量検出装置
JPH07280613A (ja) * 1994-04-13 1995-10-27 Unisia Jecs Corp 空気流量検出装置

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 096, no. 001 31 January 1996 (1996-01-31) *
PATENT ABSTRACTS OF JAPAN vol. 096, no. 002 29 February 1996 (1996-02-29) *

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2773610A1 (fr) * 1998-01-09 1999-07-16 Bosch Gmbh Robert Dispositif de mesure de la masse d'un milieu circulant dans une conduite
FR2802632A1 (fr) * 1999-12-15 2001-06-22 Drager Medizintechnik Gmbh Dispositif et procede de mesure de la vitesse d'ecoulement d'un gaz
EP1950535A1 (de) * 2006-08-07 2008-07-30 General Electric Company Verfahren und System zur dynamischen Kompensation eines bidirektionalen Durchflusssensors während der Atmungstherapie
DE102009045956A1 (de) * 2009-10-23 2011-04-28 Endress + Hauser Flowtec Ag Verfahren zur Erfassung des Durchflusses und thermisches Durchflussmessgerät
US9046397B2 (en) 2009-10-23 2015-06-02 Enrdress + Hauser Flowtec AG Method for registering flow and a thermal, flow measuring device
WO2011161060A1 (en) * 2010-06-22 2011-12-29 Heinen & Löwenstein Gmbh Ventilation aid, ventilator, system and method for the non-invasive ventilation of premature infants
DE102011051196A1 (de) * 2011-06-20 2012-12-20 BBT Automotive Components GmbH Luftmassenmesser
DE102011051196B4 (de) * 2011-06-20 2015-08-13 BBT Automotive Components GmbH Luftmassenmesser

Also Published As

Publication number Publication date
GB9613310D0 (en) 1996-08-28

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