US20010025526A1 - Device for measuring the mass of a flowing medium - Google Patents

Device for measuring the mass of a flowing medium Download PDF

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US20010025526A1
US20010025526A1 US09/866,721 US86672101A US2001025526A1 US 20010025526 A1 US20010025526 A1 US 20010025526A1 US 86672101 A US86672101 A US 86672101A US 2001025526 A1 US2001025526 A1 US 2001025526A1
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Prior art keywords
measuring
duct
inlet mouth
flowing medium
mass
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US09/866,721
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US6422070B2 (en
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Klaus Reymann
Dieter Tank
Uwe Konzelmann
Henning Marberg
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Priority claimed from DE4407209A external-priority patent/DE4407209C2/en
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01FMEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F5/00Measuring a proportion of the volume flow
    • 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

Definitions

  • the invention proceeds from a device for measuring the mass of a flowing medium according to the preamble of the main claim.
  • a device for measuring the mass of a flowing medium there is already a known device (EP 0,547,595 A2) which possesses a tubular inner housing and a tubular outer housing and in which a temperature-sensitive measuring element is accommodated in a central measuring duct of the inner housing, said measuring duct extending in the axial direction in the inner housing and being open on one side, in order to determine the mass of a flowing medium, in particular the intake air mass of an internal combustion engine.
  • the device is provided as a mountable intermediate piece, for example of an intake conduit through which the internal combustion engine can suck in air from the environment via an air filter.
  • the tubular inner housing connected to the outer housing by means of a plurality of ribs possesses, furthermore, a bypass duct which is cut out from the inner housing and is arranged concentrically to the measuring duct and which, taking the form of an annular gap, surrounds the measuring duct with a smaller axial extension.
  • a part stream of the medium flowing in the outer housing flows from an inlet mouth coaxial relative to the outer housing first into the measuring duct and flows round the temperature-sensitive measuring element arranged in the region of its downstream end, after which the flowing medium, reversing its direction of flow, flows from the measuring duct into the bypass duct.
  • the medium flowing upstream in the bypass duct leaves the latter through a slit-shaped outlet orifice cut out on the circumference of the inner housing relatively far downstream of the inlet mouth and is mixed again with the medium flowing past between the inner housing and the outer housing.
  • the design of the device as a mountable intermediate piece with an inner housing and with an outer housing necessitates a considerable overall size, so that the device is suitable to only a limited extent for confined conditions of installation, particularly in the engine region of a motor vehicle.
  • the advantage of the device according to the invention for measuring the mass of a flowing medium having the defining features of the main claim, is that a uniformly accurate measurement result can be achieved virtually independently of a fluctuating or pulsating flow.
  • the device is distinguished by a compact design and small overall size and therefore requires only a small installation space.
  • the device is therefore particularly suitable as a pluggable component especially for confined conditions of installation, for example in the engine region of a motor vehicle.
  • FIG. 1 shows a partial sectional representation of a side view of a device designed according to the invention
  • FIG. 2 shows a section along the line II-II in FIG. 1.
  • FIG. 1 shows a partial sectional representation of a side view of a device, designated by 1 , which serves for measuring the mass of a flowing medium, particularly the intake air mass of internal combustion engines.
  • the device 1 preferably has a slender cuboid shape extending elongately radially in the direction of a longitudinal axis 10 and is introduced, for example pluggably, into an orifice 6 of an intake conduit 7 , said orifice 6 being cut out from a wall 5 .
  • the device 1 is sealed off by means of a sealing ring 3 in the wall 5 and is fixedly connected to the latter, for example by means of a screw connection not represented in any more detail.
  • the wall 5 represented by hatching is part of the, for example, cylindrically designed intake conduit 7 , through which the internal combustion engine can suck in air from the environment via an air filter not shown in any more detail.
  • the wall 5 of the intake conduit 7 limits a flow cross section which, in the case of a cylindrical intake conduit 7 , has approximately a circular cross section, in the middle of which extends in the axial direction, parallel to the wall 5 , a mid-axis 11 oriented perpendicularly to the longitudinal axis 10 .
  • the device 1 projects into the flowing medium by means of a part designed below as a measuring part 17 , the measuring part 17 being divided symmetrically by the mid-axis 11 , for example approximately in the middle of the intake conduit 7 , so that the medium can flow against a temperature-sensitive measuring element 20 accommodated in the measuring part 17 , if possible without any disturbing marginal influences from the wall 5 .
  • the medium flows from right to left, the direction of flow being identified by corresponding arrows 30 .
  • the device 1 is composed, in one piece, of the measuring part 17 , of a carrier part 18 and of a holding part 19 and is produced, for example, from plastic by the plastic injection molding technique.
  • the measuring element 20 is designed, for example, in the form of a plate-shaped ceramic substrate and, as is to be taken from the prior art, for example from German Offenlegungsschrift 3,844,354, possesses one or more temperature-dependent resistors which are applied to the plate-shaped ceramic substrate in the form of resistive films, so-called hot-film resistors. It is also possible, as proposed, for example, in German Patent Application P 4,338,891, to design the measuring element 20 as a micromechanical component which has a dielectric membrane.
  • the individual resistive films of the measuring element 20 are electrically connected, by means of connecting leads 21 extending inside the device 1 , to an electronic evaluation circuit 22 which is represented by broken lines in FIG. 1 and which contains, for example, a bridge-like resistance measuring circuit.
  • the evaluation circuit 22 is accommodated, for example, in the carrier part 18 or in the holding part 19 of the device 1 .
  • electrical signals supplied by the evaluation circuit 22 can be fed for evaluation, for example, to a further electronic control unit which controls inter alia functions of the electronic idling control or engine power control of the internal combustion engine.
  • the measuring part 17 of the device 1 has a cuboid shape and has a measuring duct 33 extending in the axial direction in the measuring part 17 and an S-shaped deflecting duct 34 .
  • the measuring duct 33 extends axially in the measuring part 17 from an inlet mouth 36 having, for example, a rectangular cross section as far as a mouth 35 and is limited by an upper face 38 further from the mid-axis 11 and a lower face 37 nearer to the mid-axis 11 and by two side faces 39 , 40 , in the exemplary embodiment of FIG. 1 the measuring duct 33 being arranged eccentrically relative to the mid-axis 11 .
  • the plate-shaped measuring element 20 is oriented in the measuring duct 33 with its greatest extension radially in the direction of the longitudinal axis 10 and is divided symmetrically by the latter.
  • the measuring element 20 is held with its narrow end on one side in the carrier part 18 on the upper face 38 , so that the medium flows round said measuring element 20 together with its two side faces 23 in a manner approximately parallel to the mid-axis 11 . As represented in FIG.
  • the side faces 39 , 40 of the measuring duct 33 extend obliquely relative to a plane 14 spanned by the mid-axis 11 and the longitudinal axis 10 and form an acute angle with said plane 14 , so that the measuring duct 33 narrows axially in the direction of flow 30 , in order to open into the deflecting duct 34 with a minimum cross section at the mouth 35 .
  • the narrowing of the measuring duct 35 ensures that a uniform parallel flow as undisturbed as possible prevails in the region of the measuring element 20 .
  • the latter In order to avoid flow breakaways in the region of the inlet mouth 36 , the latter possesses rounded edge faces 41 .
  • the deflecting duct 34 has a rectangular cross section which corresponds approximately to the cross-sectional area of the inlet mouth 36 of the measuring duct 33 , so that the flow cross section increases abruptly at the mouth 35 between the measuring duct 33 and the deflecting duct 34 .
  • the axially flowing medium passes from the measuring duct 33 into the approximately S-shaped deflecting duct 34 and flows radially out of an outlet orifice 46 in the direction of an arrow 31 marked in FIG. 1, in order thereafter to mix again with the medium flowing past around the device 1 .
  • the outlet orifice 46 possesses, for example, a rectangular cross section and is provided on a lower outer face 45 of the measuring part 17 , said lower outer face being oriented parallel to the mid-axis 11 .
  • a front face 50 of the measuring part 17 is adjacent transversely to the lower outer face 45 on the right of the rectangular orifice 46 and leads in rounded form upstream of the inlet mouth 36 from the lower outer face 45 to the lower face 37 of the measuring duct 33 as far as the inlet mouth 36 .
  • the inlet mouth 36 of the measuring duct 33 and the outlet orifice 46 of the deflecting duct 34 are designed to be located radially one under the other, so that an axial distance, designated by a in FIGS. 1 and 2, is only extremely small or is absent.
  • the axial distance a is determined by an entry plane 55 , spanned by the inlet mouth 36 , to a centroid plane 56 passing through a centroid s of the outlet orifice 46 parallel to the entry plane 55 .
  • the centroid S is located at the intersection point of the median.
  • the temperature-sensitive measuring element 20 is heated to an excess temperature higher than that of the flowing medium and, mainly as a result of convection, transmits heat to the flowing medium, the heat quantity being dependent on the flow velocity occurring in the measuring duct 33 , so that the heating voltage or heating current necessary, for example, for maintaining the excess temperature is a measure of the flow velocity in the measuring duct 33 and of the intake air mass calculable from this in the intake conduit 7 .
  • the measuring element 20 has a non-linear characteristic, as a result of which, in the case of a pulsating flow and a pulsating heat transmission to the flowing medium, the measurement result does not correspond to the actual time-averaged flow velocity in the measuring duct 33 , but deviates considerably from this, depending on the intensity of the pulsations, as a consequence of a thermal inertia of the measuring element 20 .
  • the outlet orifice 46 is arranged radially underneath the inlet mouth 36 without or at only a short axial distance a, it is possible that the pressure changes both at the inlet mouth 36 and at the outlet orifice 46 , which are triggered during a pulsating flow, cancel one another out in terms of their effect on the deflecting duct 34 , so that a uniform velocity independent of these pressure changes prevails in the deflecting duct 34 .
  • the result of this effect of an air column flowing at virtually constant velocity in the deflecting duct 34 is that the medium also flows onto the measuring element 20 in the measuring duct 33 at a constant velocity in a manner uninfluenced by the pressure changes of the pulsations and their intensity and an exact measurement result can be established.
  • the outlet orifice 46 is designed radially underneath the inlet mouth 36 at a minimal axial distance a.
  • the distance a is itself dependent on the choice of the cross-sectional area of the inlet mouth 36 or on the cross-sectional area of the measuring duct 33 and should be at most approximately 50% of a minimum dimension b at the inlet mouth 36 .
  • the minimum dimension b of the inlet mouth 36 is marked accordingly in the exemplary embodiment in FIG. 1 and corresponds to the radial distance from the surface 38 of the carrier part 18 to the lower face 37 of the measuring duct 33 . If the measuring duct 33 is, for example, cylindrical with a circular cross section, the minimum dimension b corresponds to the diameter of the circular measuring duct 33 at the inlet mouth 36 .

Abstract

Known devices for measuring the mass of a flowing medium by means of a temperature-sensitive measuring element have the disadvantage that considerable measuring errors may occur in the event of a pulsating flow characterized by flow fluctuations.
In order to counteract these measuring errors, the device (1) possesses an axially extending measuring duct (33), in which a temperature-sensitive measuring element (20) is accommodated. The measuring duct (33) extends from the inlet mouth (36) to a deflecting duct (34), out of which the flowing medium flows out from an outlet orifice (46) without any axial distance from the inlet mouth (36) and radially underneath the latter.
The invention is provided for measuring the mass of a flowing medium, in particular for measuring the intake air mass of internal combustion engines.

Description

    PRIOR ART
  • The invention proceeds from a device for measuring the mass of a flowing medium according to the preamble of the main claim. There is already a known device (EP 0,547,595 A2) which possesses a tubular inner housing and a tubular outer housing and in which a temperature-sensitive measuring element is accommodated in a central measuring duct of the inner housing, said measuring duct extending in the axial direction in the inner housing and being open on one side, in order to determine the mass of a flowing medium, in particular the intake air mass of an internal combustion engine. The device is provided as a mountable intermediate piece, for example of an intake conduit through which the internal combustion engine can suck in air from the environment via an air filter. The tubular inner housing connected to the outer housing by means of a plurality of ribs possesses, furthermore, a bypass duct which is cut out from the inner housing and is arranged concentrically to the measuring duct and which, taking the form of an annular gap, surrounds the measuring duct with a smaller axial extension. A part stream of the medium flowing in the outer housing flows from an inlet mouth coaxial relative to the outer housing first into the measuring duct and flows round the temperature-sensitive measuring element arranged in the region of its downstream end, after which the flowing medium, reversing its direction of flow, flows from the measuring duct into the bypass duct. The medium flowing upstream in the bypass duct leaves the latter through a slit-shaped outlet orifice cut out on the circumference of the inner housing relatively far downstream of the inlet mouth and is mixed again with the medium flowing past between the inner housing and the outer housing. However, the design of the device as a mountable intermediate piece with an inner housing and with an outer housing necessitates a considerable overall size, so that the device is suitable to only a limited extent for confined conditions of installation, particularly in the engine region of a motor vehicle. [0001]
  • In the case of an internal combustion engine, as a result of the opening and closing of the inlet valves of the individual cylinders there occur considerable fluctuations or pulsations of the flow, the intensity of which depends on the intake frequency of individual pistons or on the rotational speed of the internal combustion engine. The pulsations of the flow are propagated from the inlet valves via the intake conduit as far as the measuring element in the inner housing and beyond this. The pulsations cause the measuring element, as a result of thermal inertia and directional insensitivity, depending on the intensity of the pulsations, to provide a measurement result which deviates considerably from the flow velocity prevailing on average in the measuring duct and from the intake air mass of the internal combustion engine which can be calculated from it. [0002]
  • ADVANTAGES OF THE INVENTION
  • In contrast to this, the advantage of the device according to the invention for measuring the mass of a flowing medium, having the defining features of the main claim, is that a uniformly accurate measurement result can be achieved virtually independently of a fluctuating or pulsating flow. [0003]
  • Advantageous developments and improvements of the device specified in the main claim are possible as a result of the measures listed in the subclaims. It is particularly advantageous that the device is distinguished by a compact design and small overall size and therefore requires only a small installation space. The device is therefore particularly suitable as a pluggable component especially for confined conditions of installation, for example in the engine region of a motor vehicle. [0004]
  • DRAWING
  • An exemplary embodiment of the invention is represented in simplified form in the drawing and is explained in more detail in the following description. [0005]
  • FIG. 1 shows a partial sectional representation of a side view of a device designed according to the invention and [0006]
  • FIG. 2 shows a section along the line II-II in FIG. 1.[0007]
  • DESCRIPTION OF THE EXEMPLARY EMBODIMENT
  • FIG. 1 shows a partial sectional representation of a side view of a device, designated by [0008] 1, which serves for measuring the mass of a flowing medium, particularly the intake air mass of internal combustion engines. The device 1 preferably has a slender cuboid shape extending elongately radially in the direction of a longitudinal axis 10 and is introduced, for example pluggably, into an orifice 6 of an intake conduit 7, said orifice 6 being cut out from a wall 5. The device 1 is sealed off by means of a sealing ring 3 in the wall 5 and is fixedly connected to the latter, for example by means of a screw connection not represented in any more detail. The wall 5 represented by hatching is part of the, for example, cylindrically designed intake conduit 7, through which the internal combustion engine can suck in air from the environment via an air filter not shown in any more detail. The wall 5 of the intake conduit 7 limits a flow cross section which, in the case of a cylindrical intake conduit 7, has approximately a circular cross section, in the middle of which extends in the axial direction, parallel to the wall 5, a mid-axis 11 oriented perpendicularly to the longitudinal axis 10. The device 1 projects into the flowing medium by means of a part designed below as a measuring part 17, the measuring part 17 being divided symmetrically by the mid-axis 11, for example approximately in the middle of the intake conduit 7, so that the medium can flow against a temperature-sensitive measuring element 20 accommodated in the measuring part 17, if possible without any disturbing marginal influences from the wall 5. In the exemplary embodiment shown in FIGS. 1 and 2, the medium flows from right to left, the direction of flow being identified by corresponding arrows 30.
  • The device [0009] 1 is composed, in one piece, of the measuring part 17, of a carrier part 18 and of a holding part 19 and is produced, for example, from plastic by the plastic injection molding technique. The measuring element 20 is designed, for example, in the form of a plate-shaped ceramic substrate and, as is to be taken from the prior art, for example from German Offenlegungsschrift 3,844,354, possesses one or more temperature-dependent resistors which are applied to the plate-shaped ceramic substrate in the form of resistive films, so-called hot-film resistors. It is also possible, as proposed, for example, in German Patent Application P 4,338,891, to design the measuring element 20 as a micromechanical component which has a dielectric membrane. The individual resistive films of the measuring element 20 are electrically connected, by means of connecting leads 21 extending inside the device 1, to an electronic evaluation circuit 22 which is represented by broken lines in FIG. 1 and which contains, for example, a bridge-like resistance measuring circuit. The evaluation circuit 22 is accommodated, for example, in the carrier part 18 or in the holding part 19 of the device 1. By means of a plug connection 24 provided on the holding part 19, electrical signals supplied by the evaluation circuit 22 can be fed for evaluation, for example, to a further electronic control unit which controls inter alia functions of the electronic idling control or engine power control of the internal combustion engine. A detailed description of the function and construction of temperature-dependent measuring elements is dispensed with, since the average person skilled in the art can take this from the prior art.
  • As represented in FIG. 2, which is a sectional representation along a line II-II in FIG. 1, the measuring [0010] part 17 of the device 1 has a cuboid shape and has a measuring duct 33 extending in the axial direction in the measuring part 17 and an S-shaped deflecting duct 34. The measuring duct 33 extends axially in the measuring part 17 from an inlet mouth 36 having, for example, a rectangular cross section as far as a mouth 35 and is limited by an upper face 38 further from the mid-axis 11 and a lower face 37 nearer to the mid-axis 11 and by two side faces 39, 40, in the exemplary embodiment of FIG. 1 the measuring duct 33 being arranged eccentrically relative to the mid-axis 11. It is also possible to arrange the measuring duct 33 centrically or in the region of the mid-axis 11 of the intake conduit 7. The plate-shaped measuring element 20 is oriented in the measuring duct 33 with its greatest extension radially in the direction of the longitudinal axis 10 and is divided symmetrically by the latter. The measuring element 20 is held with its narrow end on one side in the carrier part 18 on the upper face 38, so that the medium flows round said measuring element 20 together with its two side faces 23 in a manner approximately parallel to the mid-axis 11. As represented in FIG. 2, the side faces 39, 40 of the measuring duct 33 extend obliquely relative to a plane 14 spanned by the mid-axis 11 and the longitudinal axis 10 and form an acute angle with said plane 14, so that the measuring duct 33 narrows axially in the direction of flow 30, in order to open into the deflecting duct 34 with a minimum cross section at the mouth 35. The narrowing of the measuring duct 35 ensures that a uniform parallel flow as undisturbed as possible prevails in the region of the measuring element 20. In order to avoid flow breakaways in the region of the inlet mouth 36, the latter possesses rounded edge faces 41. The deflecting duct 34 has a rectangular cross section which corresponds approximately to the cross-sectional area of the inlet mouth 36 of the measuring duct 33, so that the flow cross section increases abruptly at the mouth 35 between the measuring duct 33 and the deflecting duct 34. The axially flowing medium passes from the measuring duct 33 into the approximately S-shaped deflecting duct 34 and flows radially out of an outlet orifice 46 in the direction of an arrow 31 marked in FIG. 1, in order thereafter to mix again with the medium flowing past around the device 1. Like the deflecting duct 34, the outlet orifice 46 possesses, for example, a rectangular cross section and is provided on a lower outer face 45 of the measuring part 17, said lower outer face being oriented parallel to the mid-axis 11. In FIG. 1, a front face 50 of the measuring part 17, said front face confronting the flow 30, is adjacent transversely to the lower outer face 45 on the right of the rectangular orifice 46 and leads in rounded form upstream of the inlet mouth 36 from the lower outer face 45 to the lower face 37 of the measuring duct 33 as far as the inlet mouth 36.
  • According to the invention, the [0011] inlet mouth 36 of the measuring duct 33 and the outlet orifice 46 of the deflecting duct 34 are designed to be located radially one under the other, so that an axial distance, designated by a in FIGS. 1 and 2, is only extremely small or is absent. The axial distance a is determined by an entry plane 55, spanned by the inlet mouth 36, to a centroid plane 56 passing through a centroid s of the outlet orifice 46 parallel to the entry plane 55. In the case, for example, of a rectangular cross-section area of the outlet orifice 46, the centroid S is located at the intersection point of the median. As is known, the temperature-sensitive measuring element 20 is heated to an excess temperature higher than that of the flowing medium and, mainly as a result of convection, transmits heat to the flowing medium, the heat quantity being dependent on the flow velocity occurring in the measuring duct 33, so that the heating voltage or heating current necessary, for example, for maintaining the excess temperature is a measure of the flow velocity in the measuring duct 33 and of the intake air mass calculable from this in the intake conduit 7. Because the convective heat transmission is based on non-linear physical laws, the measuring element 20 has a non-linear characteristic, as a result of which, in the case of a pulsating flow and a pulsating heat transmission to the flowing medium, the measurement result does not correspond to the actual time-averaged flow velocity in the measuring duct 33, but deviates considerably from this, depending on the intensity of the pulsations, as a consequence of a thermal inertia of the measuring element 20. Because the outlet orifice 46 is arranged radially underneath the inlet mouth 36 without or at only a short axial distance a, it is possible that the pressure changes both at the inlet mouth 36 and at the outlet orifice 46, which are triggered during a pulsating flow, cancel one another out in terms of their effect on the deflecting duct 34, so that a uniform velocity independent of these pressure changes prevails in the deflecting duct 34. The result of this effect of an air column flowing at virtually constant velocity in the deflecting duct 34 is that the medium also flows onto the measuring element 20 in the measuring duct 33 at a constant velocity in a manner uninfluenced by the pressure changes of the pulsations and their intensity and an exact measurement result can be established. However, this effect occurs only if the outlet orifice 46 is designed radially underneath the inlet mouth 36 at a minimal axial distance a. The distance a is itself dependent on the choice of the cross-sectional area of the inlet mouth 36 or on the cross-sectional area of the measuring duct 33 and should be at most approximately 50% of a minimum dimension b at the inlet mouth 36. The minimum dimension b of the inlet mouth 36 is marked accordingly in the exemplary embodiment in FIG. 1 and corresponds to the radial distance from the surface 38 of the carrier part 18 to the lower face 37 of the measuring duct 33. If the measuring duct 33 is, for example, cylindrical with a circular cross section, the minimum dimension b corresponds to the diameter of the circular measuring duct 33 at the inlet mouth 36.

Claims (9)

1. A device for measuring the mass of a flowing medium, in particular the intake air mass of internal combustion engines, with a temperature-sensitive measuring element, round which the flowing medium flows and which is arranged in a measuring duct running in the device and extending in the axial direction from an inlet mouth of the measuring duct to a deflecting duct, into which the medium flowing out of the measuring duct flows and flows out of an outlet orifice of the deflecting duct, wherein there is a short axial distance (a) or no axial distance at all between an entry plane (55) of the inlet mouth (36) of the measuring duct (33) and a centroid (S) of the outlet orifice (46) of the deflecting duct (34).
2. The device as claimed in
claim 1
, wherein the axial distance (a) from the entry plane (55) of the inlet mouth (36) to the centroid plane (56) limited by the centroid (S) of the outlet orifice (46) is at most approximately 50 percent of a minimum dimension (b) of the cross section of the inlet mouth (36).
3. The device as claimed in
claim 1
, wherein there is a measuring part (17) of cuboid shape.
4. The device as claimed in
claim 1
, wherein the inlet mouth (36) of the measuring duct (33) has a rectangular cross section.
5. The device as claimed in
claim 4
, wherein the measuring duct (33) has a rectangular cross section and narrows in the axial direction.
6. The device as claimed in
claim 1
, wherein the outlet orifice (46) of the deflecting duct (34) has a rectangular cross section.
7. The device as claimed in
claim 1
, wherein the inlet mouth (36) of the measuring duct (33) has rounded edge faces (41).
8. The device as claimed in
claim 1
, wherein the measuring element (20) is designed in the form of a micromechanical component.
9. The device as claimed in
claim 1
, said device (1) being designed as a pluggable component.
US09/866,721 1994-03-04 2001-05-30 Device for measuring the mass of a flowing medium Expired - Lifetime US6422070B2 (en)

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Applications Claiming Priority (5)

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DEP4407209.0 1994-03-04
DE4407209A DE4407209C2 (en) 1994-03-04 1994-03-04 Device for measuring the mass of a medium flowing in a line
DE4407209 1994-03-04
US54558395A 1995-11-03 1995-11-03
US09/866,721 US6422070B2 (en) 1994-03-04 2001-05-30 Device for measuring the mass of a flowing medium

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030159501A1 (en) * 2001-04-20 2003-08-28 Erhard Renninger Device for determining at least one parameter of a medium flowing in a conduit
US20040074291A1 (en) * 2002-07-05 2004-04-22 Thomas Lenzing Device for determining at least one parameter of a medium flowing in a line
US20050153293A1 (en) * 2002-02-04 2005-07-14 Oultram John D. Nucleic acid analysis
US7162374B2 (en) 2002-10-07 2007-01-09 Wagner Alarm-Und Sicherungssysteme Gmbh Device for the determination of flow parameters for a fluid and method for operating such a device

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19741031A1 (en) * 1997-09-18 1999-03-25 Bosch Gmbh Robert Device to measure mass of flowing medium, e.g. intake air of IC engine
JP4106224B2 (en) * 2002-03-14 2008-06-25 株式会社デンソー Flow measuring device
US6786089B2 (en) * 2002-03-28 2004-09-07 Denso Corporation Airflow meter
DE10217884B4 (en) * 2002-04-22 2004-08-05 Siemens Ag Device for measuring the air mass flowing in a line
US7047805B2 (en) 2004-04-09 2006-05-23 Visteon Global Technologies, Inc. Fluid flow meter having an auxiliary flow passage
US7302843B2 (en) * 2005-07-19 2007-12-04 C & L Performance, Inc. Mass air flow housing for mass air flow sensor
DE102006045656A1 (en) * 2006-09-27 2008-04-03 Robert Bosch Gmbh Flow dynamics improved plug-in sensor
JP2010101704A (en) * 2008-10-22 2010-05-06 Mitsubishi Electric Corp Flow measuring apparatus
JP5799682B2 (en) * 2011-09-05 2015-10-28 株式会社デンソー Air flow measurement device
DE102012224049A1 (en) * 2012-12-20 2014-06-26 Robert Bosch Gmbh Sensor device for detecting at least one flow characteristic of a fluid medium

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5627876A (en) * 1994-06-10 1997-05-06 Uniden America Corporation Call priority override in a land mobile radio system
US5790527A (en) * 1994-12-20 1998-08-04 Research Triangle Park Trunked radio frequency communication system for accommodating both frequency and time division based RF communications
US5881060A (en) * 1996-05-30 1999-03-09 Northern Telecom Limited Integrated cellular voice and digital packet data telecommunications systems and methods for their operation
US5960344A (en) * 1993-12-20 1999-09-28 Norand Corporation Local area network having multiple channel wireless access
US6173189B1 (en) * 1998-12-18 2001-01-09 Motorola, Inc. Method and apparatus for multi-protocol reverse channel infrastructure sharing
US6381461B1 (en) * 1997-10-23 2002-04-30 Siemens Aktiengesellschaft Method and radio communications system for transmitting data in a mobile radio network
US6381230B1 (en) * 1998-07-28 2002-04-30 Qualcomm Incorporated Method and system for providing personal base station communications
US6405048B1 (en) * 1996-08-28 2002-06-11 Telefonaktiebolaget L M Ericsson Method and system for autonomously allocating frequencies to a radio system sharing frequencies with an overlapping macro radio system
US6424633B1 (en) * 1996-02-09 2002-07-23 Siemens Ag Radio relay arrangement for extending the range on the radio link of a telecommunication system
US6452940B1 (en) * 1999-03-31 2002-09-17 Telefonaktiebolaget L M Ericsson (Publ) Mobile station migration from D-AMPS packet system to edge/GPRS packet system in an integrated wireless network
US6708028B1 (en) * 1993-12-22 2004-03-16 Nokia Mobile Phones, Ltd. Multi-mode radio telephone

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6165053A (en) 1984-09-07 1986-04-03 Hitachi Ltd Air-flowmeter
US4914947A (en) 1988-09-30 1990-04-10 Honeywell Inc. Sampling probe flow sensor
DE4441874A1 (en) * 1994-11-24 1996-05-30 Bosch Gmbh Robert Device for measuring the mass of a flowing medium
US5563340A (en) * 1995-03-28 1996-10-08 Ford Motor Company Mass air flow sensor housing
DE19623334A1 (en) * 1996-06-12 1997-12-18 Bosch Gmbh Robert Device for measuring the mass of a flowing medium
DE19643996A1 (en) * 1996-10-31 1998-05-07 Bosch Gmbh Robert Appliance for measuring mass of flowing medium for measuring air intake of IC engines
DE19735891A1 (en) * 1997-08-19 1999-02-25 Bosch Gmbh Robert Device for measuring mass of medium flowing in pipe, especially air in IC engine induction system
DE19815658A1 (en) * 1998-04-08 1999-10-14 Bosch Gmbh Robert Device for measuring the mass of a flowing medium

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5960344A (en) * 1993-12-20 1999-09-28 Norand Corporation Local area network having multiple channel wireless access
US6708028B1 (en) * 1993-12-22 2004-03-16 Nokia Mobile Phones, Ltd. Multi-mode radio telephone
US5627876A (en) * 1994-06-10 1997-05-06 Uniden America Corporation Call priority override in a land mobile radio system
US5790527A (en) * 1994-12-20 1998-08-04 Research Triangle Park Trunked radio frequency communication system for accommodating both frequency and time division based RF communications
US6424633B1 (en) * 1996-02-09 2002-07-23 Siemens Ag Radio relay arrangement for extending the range on the radio link of a telecommunication system
US5881060A (en) * 1996-05-30 1999-03-09 Northern Telecom Limited Integrated cellular voice and digital packet data telecommunications systems and methods for their operation
US6405048B1 (en) * 1996-08-28 2002-06-11 Telefonaktiebolaget L M Ericsson Method and system for autonomously allocating frequencies to a radio system sharing frequencies with an overlapping macro radio system
US6381461B1 (en) * 1997-10-23 2002-04-30 Siemens Aktiengesellschaft Method and radio communications system for transmitting data in a mobile radio network
US6381230B1 (en) * 1998-07-28 2002-04-30 Qualcomm Incorporated Method and system for providing personal base station communications
US6173189B1 (en) * 1998-12-18 2001-01-09 Motorola, Inc. Method and apparatus for multi-protocol reverse channel infrastructure sharing
US6452940B1 (en) * 1999-03-31 2002-09-17 Telefonaktiebolaget L M Ericsson (Publ) Mobile station migration from D-AMPS packet system to edge/GPRS packet system in an integrated wireless network

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030159501A1 (en) * 2001-04-20 2003-08-28 Erhard Renninger Device for determining at least one parameter of a medium flowing in a conduit
US6915682B2 (en) * 2001-04-20 2005-07-12 Robert Bosch Gmbh Device for determining at least one parameter of a medium flowing in a conduit
US20050153293A1 (en) * 2002-02-04 2005-07-14 Oultram John D. Nucleic acid analysis
US20040074291A1 (en) * 2002-07-05 2004-04-22 Thomas Lenzing Device for determining at least one parameter of a medium flowing in a line
US6973823B2 (en) 2002-07-05 2005-12-13 Robert Bosch Gmbh Device for determining at least one parameter of a medium flowing in a line
US7162374B2 (en) 2002-10-07 2007-01-09 Wagner Alarm-Und Sicherungssysteme Gmbh Device for the determination of flow parameters for a fluid and method for operating such a device

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