EP3394866A1 - Ankerhubbestimmung durch messung magnetischer hysteresekurven - Google Patents
Ankerhubbestimmung durch messung magnetischer hysteresekurvenInfo
- Publication number
- EP3394866A1 EP3394866A1 EP16801793.7A EP16801793A EP3394866A1 EP 3394866 A1 EP3394866 A1 EP 3394866A1 EP 16801793 A EP16801793 A EP 16801793A EP 3394866 A1 EP3394866 A1 EP 3394866A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- electromagnet
- valve
- rru
- slope
- armature
- 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.)
- Granted
Links
- 230000005291 magnetic effect Effects 0.000 title claims abstract description 57
- 238000000034 method Methods 0.000 claims abstract description 23
- 238000004519 manufacturing process Methods 0.000 claims abstract description 16
- 229920006395 saturated elastomer Polymers 0.000 claims description 18
- 238000003780 insertion Methods 0.000 claims description 4
- 230000037431 insertion Effects 0.000 claims description 4
- 230000002950 deficient Effects 0.000 claims 1
- 238000012360 testing method Methods 0.000 abstract description 19
- 230000004907 flux Effects 0.000 description 12
- 230000000875 corresponding effect Effects 0.000 description 6
- 230000005294 ferromagnetic effect Effects 0.000 description 6
- 238000005259 measurement Methods 0.000 description 6
- 238000009434 installation Methods 0.000 description 5
- 238000013459 approach Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 239000003302 ferromagnetic material Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000006247 magnetic powder Substances 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 241000024080 Hiera Species 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000003908 quality control method Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 238000012216 screening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/20—Output circuits, e.g. for controlling currents in command coils
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2432—Methods of calibration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2451—Methods of calibrating or learning characterised by what is learned or calibrated
- F02D41/2464—Characteristics of actuators
- F02D41/2467—Characteristics of actuators for injectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M65/00—Testing fuel-injection apparatus, e.g. testing injection timing ; Cleaning of fuel-injection apparatus
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/06—Electromagnets; Actuators including electromagnets
- H01F7/08—Electromagnets; Actuators including electromagnets with armatures
- H01F7/18—Circuit arrangements for obtaining desired operating characteristics, e.g. for slow operation, for sequential energisation of windings, for high-speed energisation of windings
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/06—Electromagnets; Actuators including electromagnets
- H01F7/08—Electromagnets; Actuators including electromagnets with armatures
- H01F7/18—Circuit arrangements for obtaining desired operating characteristics, e.g. for slow operation, for sequential energisation of windings, for high-speed energisation of windings
- H01F7/1844—Monitoring or fail-safe circuits
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/06—Electromagnets; Actuators including electromagnets
- H01F7/08—Electromagnets; Actuators including electromagnets with armatures
- H01F7/18—Circuit arrangements for obtaining desired operating characteristics, e.g. for slow operation, for sequential energisation of windings, for high-speed energisation of windings
- H01F7/1844—Monitoring or fail-safe circuits
- H01F2007/1855—Monitoring or fail-safe circuits using a stored table to deduce one variable from another
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/06—Electromagnets; Actuators including electromagnets
- H01F7/08—Electromagnets; Actuators including electromagnets with armatures
- H01F7/18—Circuit arrangements for obtaining desired operating characteristics, e.g. for slow operation, for sequential energisation of windings, for high-speed energisation of windings
- H01F7/1844—Monitoring or fail-safe circuits
- H01F2007/1861—Monitoring or fail-safe circuits using derivative of measured variable
Definitions
- the present invention relates to a method for determining the armature stroke on an electromagnetically actuated valve and a method for
- armature stroke should be between a lower threshold and an upper threshold. If the armature stroke is too small, the valve throttles. If the armature stroke is too big, can be amplified
- DE 10 2012 206 484 A1 and DE 10 2013 223 121 A1 disclose electromagnetic fuel injectors with measuring systems for the armature stroke. These measuring systems transmit the lifting movement of the armature in each case with additional transmission elements to a measuring device.
- valve body contains means for implementing a movement of the armature in a Opening or closing the valve.
- the electromagnet and the armature are inserted into the valve body.
- Valve body a magnetic hysteresis curve of a combination of
- Curve section of the hysteresis curve in the unsaturated state is determined.
- the test anchor preferably has the same dimensions and the same magnetic properties as the armature of the valve.
- the slope is rru from the slope determined rru * a corresponding to the first cam section curve portion of a hysteresis curve of the fully assembled valve having permanently touching the electromagnet armature.
- UK is the terminal voltage across the electromagnet
- I the current through the
- Electromagnet and R the ohmic resistance of the electromagnet.
- Electromagnet shows a typical ferromagnetic hysteresis loop, since at least in the ferromagnetic core of the electromagnet and in the likewise ferromagnetic armature each magnetic energy is stored. If an air gap between the armature and the electromagnet is formed by the drop of the armature from the electromagnet to a rest position, this also contains
- Air gap is a magnetic energy amount ⁇ , which depends on the width of the
- Hysteresis curve of the magnetic circuit with permanently attached to the electromagnet anchor more measured.
- the restoring force of the valve which may be, for example, a spring force, outweighs the magnetic force that drives the armature against the armature
- the inventors have recognized that the curve portion of the hysteresis curve with permanently attached to the electromagnet armature, which represents the unsaturated state of the electromagnet and in which the flow ⁇ im
- the pitch rru obtained prior to assembly of the valve is a very important reference value which, after installation of the valve, makes it possible to measure the armature stroke AH of the valve in a particularly simple and clear manner.
- n is the number of turns of the coil of the electromagnet.
- ⁇ 0 is the magnetic permeability of the vacuum.
- Ai and A2 are cross-sectional areas of the air gap, which are independent of its width, ie the armature stroke AH.
- Hysteresis curve of the magnetic circuit which is received in the fully assembled state of the valve, referred to as the "hysteresis curve of the valve".
- the slope rru * is determined via a predetermined first functional relationship from the slope rru.
- rr * is identical to rru. This approximation is already accurate enough for many applications.
- the valve body, and / or the means for implementing a movement of the armature in an opening or closing of the valve contain ferromagnetic materials, these materials influence the magnetic flux ⁇ of the magnetic circuit, and thus also rru * .
- the first functional relationship can be refined to the effect that this influence is taken into account. The more exactly rru * is determined, the more accurately can be determined from this the armature stroke AH.
- a particularly advantageous embodiment of the invention is to determine the first functional relationship to at least one fully assembled Valve the armature detected on the electromagnet and recorded in this state, the hysteresis curve.
- This valve is a special test specimen, which differs from the series-produced valves in that the armature stroke AH is always zero and the valve can not shift. Apart from this difference, the valve behaves magnetically just like the series-produced valves.
- the magnetic circuit of a valve receives and determines the first hysteresis curve before assembly, and after assembly of this magnetic circuit into the valve, the second hysteresis curve is established
- the slope rru * can also be obtained, for example, from the slope rru by calculating the influence of further ferromagnetic materials in the valve on the magnetic circuit formed by the electromagnet and the armature using numerical methods, for example the finite element method.
- rru * can also be refined by comparing reference values of further variables determined prior to assembly of the valve with values of these variables determined after assembly of the valve.
- the slope nri2 a second linear curve portion of the hysteresis curve, which is recorded on the combination of the electromagnet with the test anchor, determined in the saturated state.
- the current value lo is advantageously determined in addition, in which a linear continuation of the second curve section to the current axis I intersects the current axis I.
- Electromagnet attracted, so that the magnetic circuit is so far in the same state as in the reference measurement on the combination of the electromagnet and the test anchor.
- Comparative value to be obtained is advantageously added after mounting the valve, a further magnetic hysteresis curve of the valve.
- the slope nri3 of a second, substantially linear curve section of the further magnetic hysteresis curve, which represents the saturated state, is determined. This second curve section corresponds to the second
- Curve section of the magnetic hysteresis curve measured before assembly of the valve on the combination of solenoid and test anchor.
- the current value Ii in which a linear continuation of the second curve section to the current axis I intersects the current axis I, is advantageously additionally determined.
- the inventors have recognized that the comparison of the current value Ii with the current value Io offers an additional possibility of quality control for the magnetic properties of the components used in the valve. In particular, it can be monitored whether the armature, and / or between the armature and the electromagnet
- RLSS residual air gap disc
- the absolute value difference .DELTA. ⁇ between the current value Ii and the current value lo is determined and classified the valve as faulty when this difference in magnitude exceeds a predetermined threshold.
- the slopes nru and nri2 become a correlation and / or a second functional one
- the second functional relationship advantageously sets the ratio m2 / mi in a linear relationship to the current value lo.
- a parameterized approach of the form
- I 0 k l - + k 0 (3) be set up with two parameters ko and ki.
- the inventors have found in series studies of electromagnets that although rru, nri2 and lo taken by themselves subject to a sample scattering. However, within a charge of electromagnets of nominally identical geometry, made in nominally identical fashion, the correlation between rru, nri2 and lo is valid to a good approximation according to equation (3) with the same parameters ko and ki.
- the most important production parameters which have an influence on the parameters ko and ki are the magnetic powder used for the production of the magnet core of the electromagnet, the pressing density as well as a possible heat treatment of the magnetic core.
- Equations (1) and (2) do not directly use the reference value rru, but to determine rru * with the help of the second functional relationship between rru and nri2 and optionally also lo. If, for example, the approach according to equation (3) is made for this, the functional relationship is characterized by the parameters ko and ki.
- the parameters ko and ki obtained before the assembly of the valve can be utilized by determining the slope nri3 of a curve segment of the hysteresis curve representing the saturated state on the assembled valve and substituting it as nri2 in equation (3).
- Test anchor determined before mounting the valve Reference value rru.
- the slope is rru, the slope ⁇ 2, the slope rru * , and / or the first functional
- electromagnets can then be particularly easily decoupled from the mass production of electromagnetically actuated valves.
- a work may pre-produce electromagnets for several other works, the latter of which are different types of
- Information carrier may include, for example, a data matrix code, such as a QR code.
- decoupling of the production of electromagnets on the one hand and valves on the other hand can be simplified in a further particularly advantageous embodiment of the invention by a plurality of electromagnets according to the value of the slopes rru and / or ⁇ 2, and / or after the functional
- the functional relationship can be classified, for example, using the parameters ko and ki in equation (3).
- the classification discretizes the accuracy of the reference values for the electromagnet, but accelerates the mass production, since electromagnets from a class can each be further processed in identical form and no longer has to go to magnet-individual reference values. Furthermore, conspicuous electromagnets that can not be assigned to a class according to the specification can be rejected from the outset as scrap.
- the invention also relates to a method for determining the armature lift AH on an electromagnetically operable valve.
- This valve comprises an electromagnet, a movable armature by the electromagnet and preferably a valve body, within which the electromagnet, the armature and means for implementing a movement of the armature are arranged in an opening or closing of the valve.
- Curve section of the hysteresis curve of the valve in the unsaturated state determined. In this condition, the armature is effective through the valve
- the magnetic energy ⁇ in the air gap is calculated from the difference between the first slope m o and a second gradient rru * of the first curve section of FIG
- Hysteresis curve corresponding first, essentially linear
- Curve section of another magnetic hysteresis curve which would have the valve with anchored to the electromagnet anchor evaluated.
- at least one reference value rru determined before insertion of the electromagnet into the valve body can be used for this gradient rr * .
- the reference value rru may have been obtained in particular in the context of the production method described above.
- the methods disclosed in connection with the manufacturing method are available for determining rru * using the reference value rru.
- the second pitch rru from the slope nri3 a second linear curve portion of the magnetic hysteresis of the valve in the saturated state in
- Hysteresis curve determined.
- the correlation, or the functional relationship also be determined before the onset of the electromagnet in the valve body and preserved as a reference value.
- the functional relationship according to equation (3) may have been conserved in terms of the parameters ko and ki.
- the manufacturing process with which before the installation of the valve one or more reference values are obtained and conserved on the electromagnet, and the measuring method with which after mounting the valve advantageously using these reference values on the magnetic energy ⁇ in the air gap between the armature and electromagnet, the armature stroke AH is evaluated work synergistically hand in hand to allow in the end an accurate determination of the anchor stroke AH. Due to the advantageous gap-free measurement of hysteresis curves on all electromagnets used
- the armature stroke AH determined according to the invention can be used particularly advantageously as feedback in order to adjust the armature stroke at the factory in the manufacture of electromagnetically actuated valves for fuel injectors and to monitor them during operation.
- FIG 1 Schematic representation of an electromagnetically actuated valve 1 (Figure la) and a combination 6 of solenoid 2, 2a, 2b and test anchor 3a ( Figure lb);
- FIG. 2 shows a detail of the hysteresis curve 10 measured on the combination 6.
- Hysteresis curve 20 FIG. 4 Functional relationship 8 between the slope ratio determined in a series examination of electromagnets 2 and the current value lo.
- FIG. 5 Complete hysteresis curve 20 of the valve 1.
- FIG. 6 Exemplary influences of specimen scattering between
- Electromagnet 2 and test anchor 3a Electromagnet 2 and test anchor 3a.
- the valve 1 shown here by way of example as a 2/2-way valve comprises a valve body 5 with an inlet la and an outlet 1b.
- the valve 1 switches the flow of a medium between the inlet la and the outlet 1b.
- the valve body 5 a For this purpose, within the valve body 5 a
- Electromagnet 2 is arranged, which consists of a ferromagnetic magnetic core 2a and a coil 2b wound on the ferromagnetic magnetic core 2a. On the electromagnet 2 is a machine-readable
- Information carrier 7 attached, which contains a barcode with reference values. These reference values were measured on a combination 6 of the electromagnet 2 with a test anchor 3a before inserting the electromagnet 2 in the
- Valve body 5 measured.
- an armature 3 is arranged relative to the electromagnet 2 so that the electromagnet 2 can attract the armature 3.
- Coupling mechanism 4a is then the actuator 4c of the valve 1 against the force exerted by the valve spring 4b restoring force of the switching position shown in Figure la, in which the valve 1 is closed, in the switching position, not shown in Figure la, in which the valve 1 is opened , convicted.
- Coupling mechanism 4 a, the valve spring 4 b and the actuator 4 c together form the means 4, which convert the movement of the armature 3 in an opening or closing of the valve 1.
- the armature 3 In the closed switching position of the valve 1 shown in Figure la, there is an air gap between the armature 3 and the electromagnet 2 2. However, the armature 3 is attracted to the electromagnet 2, this air gap disappears 9.
- the width of the air gap 9 in the closed position, in which the armature 3 has dropped from the electromagnet 2 corresponds to the armature stroke AH of the valve. 1
- the electromagnet 2 and the armature 3 together form a magnetic circuit which is permeated by a magnetic flux ⁇ .
- a magnetic flux ⁇ Of this magnetic flux ⁇ , two flow lines are shown by way of example in FIG. 1a.
- FIG. 1b shows the combination 6 of the electromagnet 2 and the test anchor 3a, on which at least the pitch rru of a curve section 11 of FIG
- Hysteresis curve 10 is determined in the unsaturated state as a reference value.
- the test anchor 3a is also held in contact with the magnetic core 2a of the electromagnet 2 by means not shown in FIG. 1b, even if the coil 2b of the electromagnet 2 is not energized.
- Figure 2 shows a section of the hysteresis curve 10, which was recorded on the combination 6 of the electromagnet 2 and the test anchor 3a.
- the magnetic flux ⁇ is above the current I through the coil 2b of FIG.
- Electromagnet 2 applied.
- a first curve portion 11 which represents the unsaturated state of the electromagnet 2, the runs
- the hysteresis curve 10 also runs substantially linearly with a slope ⁇ 2, so that in this curve section 12 approximately ⁇ ( ⁇ ) with a constant C2.
- FIG. 3 shows a section of the hysteresis curve 20 which was received on the fully assembled valve 1.
- the magnetic flux ⁇ in the magnetic circuit of valve 1 formed by electromagnet 2 and armature 3 is applied via current I through coil 2 b of electromagnet 2.
- Electromagnet 2 went out and the current I successively reduced.
- the hysteresis curve 20 has a first in the unsaturated state
- Curve portion 21 in which it is substantially linear with a
- ⁇ ( ⁇ ) ⁇ ⁇ ⁇ + ⁇ with a constant c o .
- the hysteresis curve 20 also runs substantially linearly with a slope m3.
- approximately ⁇ ( ⁇ ) holds with a constant C3.
- the linear continuation 23 of the curve section 22 with the same slope nri3 to the current axis I intersects the current axis I at the current value Ii.
- Hysteresis curve 20 and the first curve section 31 of the hysteresis curve 30 From the energy ⁇ the sought anchor stroke AH can be determined.
- FIG. 4 shows the second functional relationship 8 between the
- Electromagnets 2 which are conspicuous in this way, are preferably sorted out as scrap.
- FIG. 5 shows, for a better understanding, a complete hysteresis curve 20 of the valve 1 with symmetrical modulation. Starting from the highest current value I in the saturated state, first the branch 28 is towards lower
- Solenoid 2 drops and the air gap 9 is formed between the armature 3 and the electromagnet 2. This is reflected in a discontinuous decrease in the magnetic flux ⁇ .
- the branch 28 of the hysteresis curve 20 then merges into the first curve section 21 in the unsaturated state.
- the magnetic flux ⁇ is substantially linear with the current I.
- the branch 28 of the hysteresis curve 20 merges into an attractive curve section.
- the armature 3 is attracted to the electromagnet 2, which shows in a small discontinuity in the curve.
- the branch 29 of the hysteresis curve 20 is passed through.
- the hysteresis curve 20 again merges into a sloping curve section 24 in which the armature 3 drops off the electromagnet 2 at the point 27b.
- the branch 29 of the hysteresis curve 29 passes into the upper right quadrant, the next attractive one begins Curve section 25.
- the armature 3 is again to the
- Electromagnet 2 tightened.
- FIG. 6 illustrates, on the basis of a few examples, how the specimen scattering between different electromagnets 2 can influence the course of the hysteresis curve 10 of a combination 6 from the respective electromagnet 2 with the test anchor 3a.
- Hysteresis curves 10 and 10a identical.
- the deviation in the composition of the magnetic cores 2a does not change the slope nri2 in the second curve section 12 nor the current value lo at which the linear
- FIG. 6b shows the opposite case, that within a series of five electromagnets 2, the hysteresis curves 10, 10a-10d respectively measured in the combination 6 with a test anchor 3a differ greatly only in the saturated state, while the hysteresis curves 10, 10a-10d in the unsaturated one Condition practically parallel to each other.
- the second curve sections 12 and 12a of the hysteresis curves 10 and 10a in the saturated state have different slopes ⁇ 2, and the linear ones
- FIG. 6c shows the case where, within a series of three electromagnets 2, the hysteresis curves 10, 10a, 10b measured in combination 6 with a test anchor 3a both in their slopes rru in the unsaturated region and in their slopes nri2 in the second
- the manufacturing method can be used in a simplified form. It can then be dispensed with to record a hysteresis curve 10 at each individual electromagnet 2. Instead, it is sufficient to measure a sample of a few electromagnets 2 of a batch of nominally identically dimensioned and manufactured electromagnets 2 and to determine therefrom the functional relationship 8 according to equation (3). For example, reference valves may be used for this sample, in which the armature 3 is fixed to the electromagnet 2 as a test anchor 3a. rru can then be evaluated for all other electromagnets 2 from the batch according to equation (4).
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Power Engineering (AREA)
- Magnetically Actuated Valves (AREA)
- Valve Device For Special Equipments (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102015226189.1A DE102015226189A1 (de) | 2015-12-21 | 2015-12-21 | Ankerhubbestimmung durch Messung magnetischer Hysteresekurven |
PCT/EP2016/079028 WO2017108342A1 (de) | 2015-12-21 | 2016-11-28 | Ankerhubbestimmung durch messung magnetischer hysteresekurven |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3394866A1 true EP3394866A1 (de) | 2018-10-31 |
EP3394866B1 EP3394866B1 (de) | 2020-10-21 |
Family
ID=57406252
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16801793.7A Active EP3394866B1 (de) | 2015-12-21 | 2016-11-28 | Ankerhubbestimmung durch messung magnetischer hysteresekurven |
Country Status (6)
Country | Link |
---|---|
US (1) | US10770212B2 (de) |
EP (1) | EP3394866B1 (de) |
KR (1) | KR102560239B1 (de) |
CN (1) | CN108431909B (de) |
DE (1) | DE102015226189A1 (de) |
WO (1) | WO2017108342A1 (de) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113586789B (zh) * | 2021-07-14 | 2024-03-29 | 杭州群科荟科技有限公司 | 一种气隙磁导式电磁阀的磁导计算方法及行程取值方法 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6208497B1 (en) * | 1997-06-26 | 2001-03-27 | Venture Scientifics, Llc | System and method for servo control of nonlinear electromagnetic actuators |
DE102010036941B4 (de) * | 2010-08-11 | 2012-09-13 | Sauer-Danfoss Gmbh & Co. Ohg | Verfahren und Vorrichtung zur Ermittlung des Zustands eines elektrisch angesteuerten Ventils |
DE102010063009B4 (de) * | 2010-12-14 | 2020-10-08 | Vitesco Technologies GmbH | Verfahren und Vorrichtung zur Charakterisierung einer Bewegung eines Kraftstoffinjektors mittels Erfassung und Auswertung einer magnetischen Hysteresekurve |
AT510600B1 (de) * | 2011-06-07 | 2012-05-15 | Ge Jenbacher Gmbh & Co Ohg | Endlageüberwachung eines gaseinblaseventils |
DE102012206484A1 (de) | 2012-04-19 | 2013-10-24 | Robert Bosch Gmbh | Kraftstoffinjektor mit einer Vorrichtung zur Messung eines Ankerhubs |
DE102013223121A1 (de) | 2013-11-13 | 2015-05-13 | Robert Bosch Gmbh | Kraftstoffinjektor |
DE102014224321A1 (de) * | 2014-11-27 | 2016-06-02 | Robert Bosch Gmbh | Verfahren zum Ermitteln des Ankerhubs eines Magnetaktors |
-
2015
- 2015-12-21 DE DE102015226189.1A patent/DE102015226189A1/de not_active Withdrawn
-
2016
- 2016-11-28 WO PCT/EP2016/079028 patent/WO2017108342A1/de active Application Filing
- 2016-11-28 US US16/065,001 patent/US10770212B2/en active Active
- 2016-11-28 EP EP16801793.7A patent/EP3394866B1/de active Active
- 2016-11-28 KR KR1020187020304A patent/KR102560239B1/ko active IP Right Grant
- 2016-11-28 CN CN201680075122.4A patent/CN108431909B/zh active Active
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Publication number | Publication date |
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US10770212B2 (en) | 2020-09-08 |
KR20180095630A (ko) | 2018-08-27 |
EP3394866B1 (de) | 2020-10-21 |
US20190006073A1 (en) | 2019-01-03 |
KR102560239B1 (ko) | 2023-07-28 |
CN108431909B (zh) | 2020-12-08 |
CN108431909A (zh) | 2018-08-21 |
WO2017108342A1 (de) | 2017-06-29 |
DE102015226189A1 (de) | 2017-06-22 |
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