Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02D—CONTROLLING COMBUSTION ENGINES
  • F02D35/00—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
  • F02D35/02—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
  • F02D35/028—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions by determining the combustion timing or phasing
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
  • G01L23/00—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid
  • G01L23/22—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid for detecting or indicating knocks in internal-combustion engines; Units comprising pressure-sensitive members combined with ignitors for firing internal-combustion engines
  • G01L23/221—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid for detecting or indicating knocks in internal-combustion engines; Units comprising pressure-sensitive members combined with ignitors for firing internal-combustion engines for detecting or indicating knocks in internal combustion engines
  • G01L23/225—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid for detecting or indicating knocks in internal-combustion engines; Units comprising pressure-sensitive members combined with ignitors for firing internal-combustion engines for detecting or indicating knocks in internal combustion engines circuit arrangements therefor
  • G01L23/226—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid for detecting or indicating knocks in internal-combustion engines; Units comprising pressure-sensitive members combined with ignitors for firing internal-combustion engines for detecting or indicating knocks in internal combustion engines circuit arrangements therefor using specific filtering
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02D—CONTROLLING COMBUSTION ENGINES
  • F02D35/00—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
  • F02D35/02—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02D—CONTROLLING COMBUSTION ENGINES
  • F02D35/00—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
  • F02D35/02—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
  • F02D35/023—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions by determining the cylinder pressure
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02D—CONTROLLING COMBUSTION ENGINES
  • F02D35/00—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
  • F02D35/02—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
  • F02D35/025—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions by determining temperatures inside the cylinder, e.g. combustion temperatures
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02D—CONTROLLING COMBUSTION ENGINES
  • F02D35/00—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
  • F02D35/02—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
  • F02D35/027—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions using knock sensors
• • 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
  • F02D41/26—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using computer, e.g. microprocessor
  • F02D41/28—Interface circuits
• • 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
  • F02D41/02—Circuit arrangements for generating control signals
  • F02D41/14—Introducing closed-loop corrections
  • F02D41/1401—Introducing closed-loop corrections characterised by the control or regulation method
  • F02D2041/1413—Controller structures or design
  • F02D2041/1432—Controller structures or design the system including a filter, e.g. a low pass or high pass filter
• • 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
  • F02D41/26—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using computer, e.g. microprocessor
  • F02D41/28—Interface circuits
  • F02D2041/286—Interface circuits comprising means for signal processing
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
  • G01M15/00—Testing of engines
  • G01M15/04—Testing internal-combustion engines
  • G01M15/08—Testing internal-combustion engines by monitoring pressure in cylinders

Definitions

• the invention relates to a method according to the preamble of the independent claim.
• the pressure profiles in the interior of the cylinders are recorded via suitable pressure sensors, charge amplifiers and fast data acquisition systems. Due to the not always ideally possible installation of the pressure sensors as well as external influences such as structure-borne noise or structure-borne sound vibrations, caused e.g. By closing the valves, the measured pressure curve is subject to various disturbing influences, which affect the accuracy of the evaluations. For this reason, it is known to filter the cylinder pressure signal.
• the cylinder pressure signal is first digitized synchronously in time, then converted on an angle basis and then smoothed by a weighted averaging, whereby the weight function and the window width for this sliding averaging can be varied over the crank angle.
• crank angle-dependent filtering of the cylinder pressure curve adapted to specific disturbances is undertaken, wherein, however, the crank angle information is in turn derived from the cylinder pressure curve.
• the crank angle information is only approximately known at a certain point in time, and that the instantaneous speed changes caused by the individual cylinders remain completely unconsidered.
• the sampling frequency is generally much higher on a time base than on a crank angle basis, the detected combustion chamber signal loses information due to the angle-synchronous smoothing.
• the determination of the crankshaft position from a cylinder pressure curve analysis is severely limited in its accuracy and can not be used for high-quality data analysis.
• the object of the invention is now to provide an improved method for the at least partial suppression of a combustion chamber signal, by which the disadvantages of the prior art are overcome.
• the invention preferably relates to a method for producing an at least partially suppressed output data stream by detecting and selectively filtering a combustion chamber signal recorded on an internal combustion engine, comprising the following steps:
• Creating a first transformed combustion chamber signal data stream by transforming the first filtered combustion chamber signal data stream from time base to crank angle basis using the recorded crank angle signal data stream and creating a second transformed combustion chamber signal data stream by transforming the second optionally filtered combustion chamber signal data stream from time base to crank angle basis using the recorded crank angle signal data stream,
• the output data stream in a first crank angle range comprises the first transformed combustion chamber signal data stream and in a second crank angle range, the second transformed combustion chamber signal data stream.
• the first transformed combustion chamber signal data stream serves as a base signal and is replaced by certain or selectable crank angles by the second transformed combustion chamber signal data stream.
• crank angles, between which the first transformed combustion chamber signal data stream is replaced by the second transformed combustion chamber signal data stream are freely selectable, and / or that the first transformed combustion chamber signal data stream serves as the base signal and values from the second transformed combustion chamber signal data stream between freely selectable crank angles are adopted in the base signal.
• first combustion chamber signal data stream may be filtered and / or numerically smoothed in a first filter before the transformation on a crank angle basis and / or for the second combustion chamber signal data stream to be filtered and / or numerically smoothed in a second filter before the transformation on a crank angle basis.
• thermodynamic zero point correction is made.
• the second crank angle region comprises at least a part of the high-pressure part or the entire high-pressure part of the combustion process
• the second crank angle range 30 ° before the top dead center of the high pressure part to 120 ° after top dead center of the high-pressure part of the combustion process comprises.
• the output data stream in the transition region between the first crank angle range and the second crank angle range comprises a transitional data stream or is formed by the transition data stream, by which a continuous and / or smooth transition between the first transformed combustion chamber signal data stream and the second transformed combustion chamber signal data stream is formed, wherein the transition data stream is formed by a cross-fading function such as in particular a Gaussian integral curve or a linear function.
• the first filter and the second filter are independent of each other and freely parameterizable.
• the first filter is adapted to carry out a basic smoothing of the combustion chamber signal or the first combustion chamber signal data stream in the low-pressure part of the combustion process and / or that the first filter is adapted to filter relevant disturbances such as mechanical disturbances or structure-borne sound vibrations caused by the valve closure.
• the second filter is adapted to filter in the high pressure part of the combustion process, in particular disturbances caused by the sensor mounting, but to pass other vibrations such as knocking vibrations.
• the filter or filters are or are designed as low-pass filters, band-pass filters, band-stop filters or filters for numerical smoothing.
• the first filter is a low-pass filter, or that the first filter is a low-pass filter with a cut-off frequency of 1 kHz to 5 kHz.
• the second filter is a low-pass filter, or that the second filter is a low-pass filter with a cut-off frequency of 20 kHz to 100 kHz.
• the filter or filters are or are designed to filter the respective combustion chamber signal data stream in real time.
• the combustion chamber signal is a cylinder pressure signal of the combustion chamber, or a pressure signal of a combustion chamber pressure sensor of an indexed engine.
• the filter running times of the filtered combustion chamber signal data stream or the filtered combustion chamber signal data streams are compensated, and / or that the transformation based on the crankshaft angle and the compensation of the filter run times are performed in one step, in particular at the same time.
• crank angle signal corresponds to a crank angle course, which is recorded by means of a crank angle sensor.
• the time-synchronized digitization is in each case carried out by an A / D converter, wherein the A / D converter is in particular an 18-bit converter with a sampling rate of 2 MHz.
• the filter or filters are digital filter stages, in particular digital filter stages of the FIR type (Finite Impulse Response Filter).
• the creation of the output data stream takes place in real time, but in particular in real time, delayed by the filter runtime to be compensated.
• the creation of the output data stream takes place in real time, in particular delayed by the filter running time to be compensated, and that for the composition the transformed combustion chamber signal data streams to the output data stream a digital signal processor or a FPGA ("Free Programmable Gate Array") is used.
• the method comprises the following steps:
• Combustion chamber signal data signal streams such that the output data stream is formed in a first crank angle range by the first transformed combustion chamber signal data stream, in a second crank angle range by the second transformed combustion chamber signal data stream, and in a third or further crank angle range by the third or further transformed combustion chamber signal data stream.
• pr (phi) pn (phi) * (l-u (phi-phin)) + pl (phi) * (u (phi-phin))
• phi> phin + m: pr (phi) pl (phi) where phi is the crank angle, where phi l is the first freely adjustable crank angle, where phin is another freely adjustable crank angle, where pl (phi) is the crank angle first transformed combustion chamber signal data stream, where pn (phi) is another transformed combustion chamber signal data stream, where u is the transition data stream forming crossfade function, and z is a first freely adjustable crank angle window, and m is another freely adjustable crank angle window, and pr is the output data stream is.
• a filter in particular a digital filter, which is used only in a certain predefinable crank angle range.
• the disturbing vibrations due to valve closing occur approximately in a range of 120 ° before TDC (top dead center).
• a thermodynamic zero-point correction typically a range of 100 ° to 50 ° before TDC is used.
• the maximum pressure gradient and knocking vibrations occur only at the OT and after. It is therefore advantageous to let the low-pass filter act only up to about 30 ° before TDC and then turn off.
• the sudden deactivation of a filter typically leads to discontinuities in the waveform.
• a smooth or smooth transition between filtered and unfiltered signal is provided. This will be a so-called cross-fading function (eg a Gaussian integral curve) is used and defines a crank angle range for the transition:
• the high-frequency data stream (eg 18 bits with 2 MHz sampling rate) supplied by an A / D converter is passed into two independent digital filter stages (eg of the FIR type) whose types and cut-off frequencies are determined by the end user of the Measuring system can be freely defined.
• These may be, for example, low passes or band-stop filters. The latter are advantageous, for example, when narrow-band resonances dependent on the mounting of the sensor occur in the high-pressure part of the cylinder pressure curve. Following these filters, the data is transformed to crank angle using signals from a crank angle sensor.
• the base curve used is preferably that with the first filter, in particular the base filter, filtered curve. From a certain user-definable crank angle phil, the values of the second curve are taken over for the result signal and from another freely definable crank angle phi2 again on the first curve.
• a smooth transition is made between the curves filtered with the first filter and with the second filter.
• a cross-fading function for example a Gaussian integral curve
• a transition window (s) is defined for the transition:
• pr (phi) p2 (phi) * (l-u (phi-phi2)) + pl (phi) * (u (phi-phi2))
• Examples of a possible blending function u (phi) would be e.g. a linear function or a Gaussian integral curve.
• the method for generating the filtered curve of a cylinder pressure curve optionally comprises the steps of guiding the digitized pressure curve through two digital filter stages, which are freely parameterizable in terms of type and cutoff frequency, the Output curves are then reassembled into a resulting new pressure curve, wherein before a definable crank angle the values of the output curve of the first filter, then the values of the output curve of the second filter and then again the values of the output curve of the first filter are used. It is preferably provided that a sliding switching between the output curves of the digital filter is performed by means of a cross-fading function. In this case, the digital filtering, the conversion of the filtered data from time base to crank angle and the composition of the output curves to a resulting crank angle-dependent course are performed in real time in a digital signal processor or FPGA ("Free Programmable Gate Array").
• FIG. 1 shows a schematic representation of the sequence of a method for creating a suppressed or an at least partially suppressed combustion chamber signal data stream.
• combustion chamber signal 1 combustion chamber signal data stream 2, crank angle signal 3, crank angle signal data stream 4, first filter 5, second filter 6, third filter 7, transformation (of the first combustion chamber signal data stream) 8, transformation (of the second combustion chamber signal data stream) 9, transformation (of the third combustion chamber signal data stream) 10, parameter 11, composition of (the output data stream) 12, disturbed signal 13, high-frequency change of the combustion chamber signal data stream at ignition 14, purged output data stream 15, transition data stream 16, first crank angle region 17, transition region 18, second Crank angle range first transformed combustion chamber signal data stream second transformed combustion chamber signal data stream third transformed combustion chamber signal data stream 23, second optionally filtered combustion chamber signal data stream 24, third optionally filtered combustion chamber signal data stream 25, first combustion chamber signal data stream 26, second combustion chamber signal data stream 27, third combustion chamber signal data stream 28.
• a combustion chamber signal 1 is recorded in a first step.
• This combustion chamber signal 1 can be, for example, a pressure signal recorded via a pressure sensor or a different signal. Also possible would be the output of a knock sensor or the output of a temperature sensor.
• the invention is carried out by way of example on the basis of a pressure signal, in particular based on a pressure signal of the combustion chamber pressure sensor of an indexed engine.
• the recorded combustion chamber signal 1 is converted into a combustion chamber signal data stream 2. This conversion takes place in particular by digitizing, preferably by time-synchronized digitizing, for example in an A / D converter.
• crank angle signal 3 is recorded and subsequently digitized.
• This conversion of the crank angle signal 3 into a crank angle signal data stream 4 takes place, in particular, by high-frequency, time-synchronized digitizing, for example by scanning, counting and interpolating the pulses of an angle-mark transmitter. This digitization can be done for example in an A / D converter.
• this is split into a first combustion chamber signal data stream 26 and into a second combustion chamber signal data stream 27 and / or duplicated.
• the splitting into a first combustion chamber signal data stream 26 and into a second combustion chamber signal data stream 27 enables the independent processing of the combustion chamber signal data stream 2 in two different method steps.
• the first combustion chamber signal data stream 26 is filtered in a first filter 5, without influencing the second combustion chamber signal data stream 27.
• the first filter 5 may be, for example, a low-pass filter, a band-pass filter or a band-stop filter.
• the first filter 5 is designed as a low-pass filter, preferably as a low-pass filter with a cut-off frequency of 1 kHz to 5 kHz.
• the first filter 5 is used for basic suppression.
• it is the task of the first filter 5 to filter the disturbances 13 of the combustion chamber signal 1 caused by the valve closure of the valves of the internal combustion engine. These are relatively high-frequency disturbances which can be removed by the low-pass filter from the combustion chamber signal 1 or from the combustion chamber signal data stream 2.
• a transformation 8 of the first filtered combustion chamber signal data stream 23 takes place from time base to crank angle basis, wherein the crank angle signal data stream 4 used for this purpose is the data of the crank angle signal 3.
• the compensation of the filter running times takes place. These filter runtimes arise, in particular due to the real-time calculation of, in particular digital, filters. This compensation results in no signal shifts on the crank angle axis even at different speeds.
• the second combustion chamber signal data stream 27 can also be filtered and / or numerically smoothed in a second filter 6.
• This filtering or smoothing in the second filter 6 is preferably carried out in parallel and thus independently of the filtering of the first combustion chamber signal data stream 26 in the first filter 5. If appropriate, according to a further embodiment, the second combustion chamber signal data stream 27 can also be passed on unfiltered.
• the second filter 6 is designed as a low-pass filter, preferably as a low-pass filter with a cut-off frequency of 20 kHz to 100 kHz. Furthermore, the second filter 6 is a possibly additional suppression.
• a transformation 9 of the second optionally filtered combustion chamber signal data stream 24 is performed from time base to crank angle basis.
• the transformation 9 is also preferably the compensation of the filter run times.
• a third optionally filtered combustion chamber signal data stream 25 is provided, which is created by filtering a third combustion chamber signal data stream 28 in a third filter 7.
• This third optionally filtered combustion chamber signal data stream 25 is also transformed in a transformation 10 from time base to crank angle-based. In the transformation 10, the compensation of the filter run times preferably also takes place.
• an output data stream 15 is formed by assembling 12.
• This output data stream according to the present embodiment comprises parts of the first transformed combustion chamber signal data stream 20 and of the second one
• the output data stream 15 comprises at least a portion of the first transformed combustion chamber signal data stream 20 and at least a portion of the second transformed combustion chamber signal data stream 21.
• a first crank angle region 17 is provided in which the output data stream 15 corresponds to the first transformed combustion chamber signal data stream 20.
• a second crank angle range 19 is provided in which the output data stream 15 corresponds to the second transformed combustion chamber signal data stream 21.
• the first crank angle region 17 preferably comprises the region in which a disturbance to be filtered or eliminated occurs.
• the first crank angle region 17 includes the low-pressure part of the combustion process and the region in which the valves of the corresponding cylinder of the internal combustion engine are closed.
• the disturbed signal 13, for the sake of clarity only, is replaced by the first transformed combustion chamber signal stream 20 filtered in the first filter 5 according to the present method so that the perturbations are eliminated and the output data stream 15 is or is suppressed.
• the output data stream 15 is formed by the second transformed combustion chamber signal data stream 21, which also maps high-frequency combustion chamber signals such as high-frequency changes of the combustion chamber signal data stream by a knocking combustion 14 and / or possible disturbances caused by the sensor assembly.
• the second crank angle region 19 comprises the high-pressure part of the combustion process.
• a transition region 18 with a transitional data stream 16 is arranged.
• the transitional data stream 16 is suitable and / or adapted to effect a continuous course of the output data stream 15 between the two successive transformed combustion chamber signal data streams 20, 21.
• the transitional data stream 16 can be, for example, a Gaussian integral curve whose boundary conditions correspond to the boundary conditions of the joined combustion chamber signal data streams.
• the filters are set up to filter and / or numerically smooth the combustion chamber signal data streams before the transformation on a crank angle basis in a filter.
• the first transformed combustion chamber signal data stream corresponds to a first filtered and / or smoothed and transformed combustion chamber signal data stream.
• the second, third and further transformed combustion chamber signal data stream include a second, third and further optionally filtered and / or optionally smoothed and transformed
• Combustion room signal stream corresponds.
• the high-pressure part of the combustion process corresponds to the high-pressure region of the combustion process.
• the low-pressure part of the combustion process corresponds to the low-pressure region of the combustion process.
• the output data stream is formed in a first crank angle range by the first transformed combustion chamber signal data stream and in a second crank angle range by the second transformed combustion chamber signal data stream.
• the combustion chamber signal data stream is split or duplicated into two, three, four, five, six or more combustion chamber signal data streams.
• the first, second, third, fourth, fifth, sixth or further combustion chamber signal data streams split or duplicated from the combustion chamber signal data stream are filtered or smoothed in an associated first, second, third, fourth, fifth, sixth or further filter.
• the filtered or optionally filtered first, second, third, fourth, fifth, sixth or further combustion chamber signal data streams are transformed in a respective first, second, third, fourth, fifth, sixth or further transformation from time base to crank angle basis.
• the output data stream comprises or is formed by parts of a first, second, third, fourth, fifth, sixth or further transformed combustion chamber signal data stream.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Computer Hardware Design (AREA)
• Microelectronics & Electronic Packaging (AREA)
• Physics & Mathematics (AREA)
• General Physics & Mathematics (AREA)
• Combined Controls Of Internal Combustion Engines (AREA)

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• 2016
  • 2016-09-28 AT ATA50874/2016A patent/AT518869B1/de not_active IP Right Cessation
• 2017
  • 2017-09-28 CN CN201780059825.2A patent/CN109790793A/zh active Pending
  • 2017-09-28 JP JP2019537885A patent/JP6695510B2/ja not_active Expired - Fee Related
  • 2017-09-28 WO PCT/EP2017/074646 patent/WO2018060339A1/de unknown
  • 2017-09-28 EP EP17777039.3A patent/EP3519687A1/de not_active Withdrawn
  • 2017-09-28 US US16/336,474 patent/US10774758B2/en active Active

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