EP0632864A1 - Arrangement for determining the parameters of an internal combustion engine. - Google Patents
Arrangement for determining the parameters of an internal combustion engine.Info
- Publication number
- EP0632864A1 EP0632864A1 EP94900001A EP94900001A EP0632864A1 EP 0632864 A1 EP0632864 A1 EP 0632864A1 EP 94900001 A EP94900001 A EP 94900001A EP 94900001 A EP94900001 A EP 94900001A EP 0632864 A1 EP0632864 A1 EP 0632864A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- engine
- internal combustion
- light emission
- combustion engine
- combustion
- 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
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 78
- 238000011156 evaluation Methods 0.000 claims abstract description 35
- 230000003287 optical effect Effects 0.000 claims abstract description 33
- 230000001105 regulatory effect Effects 0.000 claims abstract description 8
- 239000000446 fuel Substances 0.000 claims abstract description 5
- 239000011521 glass Substances 0.000 claims description 9
- 239000013307 optical fiber Substances 0.000 claims description 9
- 230000001419 dependent effect Effects 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 238000012935 Averaging Methods 0.000 claims description 4
- 230000001276 controlling effect Effects 0.000 claims description 3
- 238000001514 detection method Methods 0.000 claims description 3
- 238000001914 filtration Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 claims description 2
- 230000035945 sensitivity Effects 0.000 claims description 2
- 238000011144 upstream manufacturing Methods 0.000 claims description 2
- 230000001427 coherent effect Effects 0.000 claims 1
- 239000000523 sample Substances 0.000 description 6
- 230000003595 spectral effect Effects 0.000 description 6
- 239000000567 combustion gas Substances 0.000 description 5
- 239000007789 gas Substances 0.000 description 3
- 238000011109 contamination Methods 0.000 description 2
- 238000012937 correction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000009499 grossing Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000007787 solid Substances 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
- 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
- F02D35/022—Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions using an optical sensor, e.g. in-cylinder light probe
-
- 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
- F02D41/1497—With detection of the mechanical response of the engine
Definitions
- the invention relates to a device for detecting engine parameters of an internal combustion engine, in particular a gasoline engine operated with gaseous fuels, with at least one optical sensor for observing the light emission caused by the combustion in a combustion chamber of the internal combustion engine and with at least one photodetector Conversion of the light emission into electrical signals, which are processed in an evaluation device.
- a control signal for controlling the ignition timing has mainly been obtained from the position of the light emission over time.
- the object of the invention is to create a device of the type mentioned at the outset with which it is possible to precisely control at least one engine parameter.
- Evaluation device comprises a device for determining the intensity maximum of the light emission of each combustion cycle in the corresponding electrical signal and the evaluation device further comprises a control unit which controls at least one engine parameter as a function of the intensity maxima.
- intensity maximums of the light emission in order to record an engine parameter and preferably to control engine parameters via a control unit.
- an engine parameter is, in particular, the fuel-air ratio (lambda).
- other engine parameters such as the ignition timing, the boost pressure, the engine temperature etc. can in principle be regulated depending on the intensity maximum or the integral value of the intensity of the light emission of each combustion cycle.
- the maximum of the light emission, which is reflected in the electrical signal of the photodetector can easily be determined by an electronic evaluation device and fed to the actual value input of a control device which then adjusts or controls at least one motor parameter as a function thereof.
- the device for determining the intensity maximum In order to smooth fluctuations in the light emission in individual successive combustion cycles, it is expedient for the device for determining the intensity maximum to be followed by an averager which emits a signal corresponding to the mean value from the intensity max a of a predeterminable number of combustion cycles, and that the output of the mean value generator is connected to the actual value input of the control unit.
- the maximum intensity can be averaged over 20 to 100 cycles, for example.
- a further preferred embodiment is characterized in that the evaluation device has a device for detecting misfires, which on the one hand receives signals related to the light emission and on the other hand receives signals dependent on a sensor from the crankshaft angle or the piston position of the engine and which provides an output signal at its output for an electrical signal below a threshold value at a point in time or time window dependent on the crankshaft angle or on the piston position in which the ignition normally takes place.
- the signals emitted by the device for detecting misfires can, for example, be counted and can cause an emergency shutdown of the engine if there are a certain number or frequency of misfires.
- the radicals formed during the ignition emit light in a certain frequency range, particularly in the ultraviolet range (approx. 200 nm to 350 nm).
- an optical bandpass filter which is preferably connected upstream of the photodetector, one can now specifically evaluate a specific spectral range, a so-called spectral window, and use the maximum light emission occurring in this spectral window to regulate motor parameters.
- the intensity of the radiation in the UV region is strongly dependent on the combustion gas / air ratio, a higher intensity occurring with smaller lambda values. This can be used to achieve lambda control on the basis of the light intensity of the UV emission.
- a bandpass filter preferably a colored glass filter
- the optical pickup for example by using specially doped
- the material which does not conduct outward from the combustion chamber itself has bandpass filtering properties and can therefore form a bandpass filter per combustion chamber if this is desired.
- a further advantageous embodiment of the invention consists in that in a multi-cylinder internal combustion engine for cylinder-selective control of the engine parameters, an optical pickup is arranged on the combustion chamber of each cylinder, each with its own photodetector and its own evaluation device belongs to a control unit which controls the engine parameters of the respective cylinder as a function of the electrical signals and adjustable setpoints corresponding to the light emission of the respective cylinder.
- the cylinder-selective control of engine parameters for example the fuel-air ratio for each cylinder individually, permits more precise control and operation of the engine.
- FIG. 1 shows a schematic cross section through the cylinder head area of a cylinder with an optical pick-up inserted
- FIG. 2 shows in a block diagram the evaluation device for an exemplary embodiment of the invention
- FIG. 3 schematically shows a multi-cylinder internal combustion engine with a cylinder-selective combustion gas Air-mixture control as a function of the light emission from the individual combustion chambers.
- Fig. 4 shows a self-calibration device in one
- the optical sensor (probe), designated overall by 1, is inserted in the cylinder head 7 of a cylinder of an internal combustion engine and held by means of a union nut 3.
- the optical pickup 1 comprises a light-conducting glass rod 2, which extends into the combustion chamber 9 above the bulb 8.
- the optical pickup comprises an optical waveguide plug adapter 4, which makes it possible to detachably connect an optical waveguide to the outer end of the glass rod 2, in particular in the form of a flexible optical fiber 6, via an optical waveguide plug 5.
- only the optical fiber connector 5 must be inserted into the optical fiber connector adapter 4 in the direction of the arrow 10. So it is possible that
- Light that is generated during combustion in the combustion chamber 9 is first fed to an evaluation device via the glass rod 2 and then via the flexible optical fiber 6.
- the flexible optical fiber allows the electronic evaluation device to be installed remotely and can be easily replaced in the event of damage.
- the light detected by an optical pick-up 1 from a combustion chamber is supplied to the electronic evaluation device 11 via an optical fiber 6 (for example, which is particularly transparent to the UV range).
- the optical fiber 6 can also be detachably connected to the evaluation device.
- a photodetector 12 for example a UV photodiode with a spectral sensitivity range from 185 to 1150 nm converts the light into electrical signals, which are then amplified in an amplifier 13 and in one
- High pass or band pass filter 14 are filtered.
- the electrical signals corresponding to the light emission are then passed by a device 15 for determining the intensity maximum of the light emission of each combustion cycle.
- the output signal present on line 16 thus reflects the maximum intensity of the light Emission of each combustion cycle again, it being possible, for example, for a high-pass filter or band-pass filter to be integrated in the optical pickup in order to observe only one spectral window.
- the filter can be formed by the glass rod 2, which consists of special glass. However, it is also possible to use a special filter element. Measurements have shown, among other things, that the radicals which arise during the ignition emit light in the ultraviolet range (approx. 200 nm to 350 nm). The intensity of this
- an optical high-pass filter is sufficient for this, which is only permeable to wavelengths smaller than 600 nm.
- the signal present on line 16 could be fed to the control unit 17, which then controls an engine parameter (for example the fuel / air ratio) via an output amplifier 18 and a motor parameter adjustment device (for example a mixture adjustment device 19).
- an engine parameter for example the fuel / air ratio
- a motor parameter adjustment device for example a mixture adjustment device 19
- the output signals on line 16 are averaged over a number of, for example, 10 to 100 cycles, for example 30 cycles, that is to say the mean value of the intensity maxima is determined over a predeterminable number of combustion cycles. This takes place in the mean value generator 18, the output 19 of which is connected to the actual value input 20 of the control unit 17.
- the integral value of the light intensity can be used for the averaging during the burning period.
- the probe drift (eg due to contamination of the combustion chamber probe) can be compensated for by a self-calibration device which acts, for example, on an additional input 36 of the amplifier 14 for the drift correction.
- a self-calibration device which acts, for example, on an additional input 36 of the amplifier 14 for the drift correction.
- the contamination can be determined during engine operation and a respective correction signal can be generated (FIG. 4).
- a light pulse is fed into the optical waveguide from the self-calibration device 37 at an arc-controlled angle. This light pulse continues via the optical waveguide 6 and the combustion chamber window 6 into the combustion chamber, from where it is reflected. The reflected pulse then returns to the self-calibration device 37.
- the intensity of the reflected pulse is a measure of the pollution of the combustion chamber window. With this size can then For example, the evaluation device is tracked (input 36).
- the self-calibration process is started by the self-calibration trigger device 38 whenever no combustion is taking place (e.g. change TDC or during compression). This is the same combustion chamber window and the same optical waveguide as in the evaluation unit described above.
- the evaluation device and the self-calibration device are decoupled via optics.
- a device 21 for detecting misfires is provided in FIG. 2, which signals are related to the light emission via the line 16 and signals dependent on the crankshaft angle or the piston bearing of the engine via a sensor 22 receives.
- Transducers for detecting the crankshaft angle or the piston bearings of the engine are well known to the person skilled in the art and need not be described in more detail here. They generally emit a certain trigger signal at a certain motor position.
- the device 21 for the detection of misfires now checks whether light emission occurs in a certain time window, which is determined by the trigger signal from the sensor 22. This should normally be the case if the ignition is successful. If this is not the case, it outputs a corresponding signal at its output 23, which indicates a misfire.
- This signal can be supplied to a logic block "inhibit" in the mean value generator 18, which causes those combustion cycles in which combustion misfires occur to be disregarded when averaging. This means that there is no falsification of the mean value for individual misfires. Misfires can also be communicated via line 34 to the emergency shutdown device 35, which, however, switches off the engine at a certain frequency of misfires.
- the part of the evaluation device essentially comprising parts 1, 6, 12, 13, 14, 15 (and possibly 18) represents an "optical lambda probe M , which is a function of the absolute value of the fuel-air ratio provides a corresponding analog signal at output 19.
- an "optical lambda probe M which is a function of the absolute value of the fuel-air ratio provides a corresponding analog signal at output 19.
- Such a lambda probe can also be marketed and used independently of the following control unit, but it is of course also possible to implement the electrical components of the lambda probe and control unit 17 together.
- the control unit 17 comprises a setpoint generator 25 via which the desired setpoint of the motor parameter can be set.
- a control difference xd results from the comparison of the set value w with the actual value x (intensity maximum averaged over several cycles in a spectral window). This is fed to stage 26, which then emits an actuating signal for regulating an engine parameter at its output. The control loop is thus closed.
- control differences xd of several optical sensors 1 can be connected. This level then takes, for example, the greatest value of all connected control differences for the calculation of the manipulated variable y.
- the combustion gas / air ratio can be regulated as a function of the light emission in all cylinders.
- cylinder-selective control is also conceivable and inexpensive, as is shown, for example, in FIG. 3.
- a five-cylinder internal combustion engine 29 is shown there as an example.
- the optical pickups 1, which are each connected to the electronic evaluation device 11 'via flexible optical fibers 6, extend into the combustion chamber of each cylinder.
- This electronic evaluation device 11 essentially comprises five evaluation devices 11, as shown in FIG. 2. Each of these evaluation devices 11 receives, via a line 30, a signal determined by a transducer 31, which indicates the crankshaft angle. A cylinder-selective control of engine parameters takes place via the evaluation devices 11, in the embodiment of the combustion gas shown in FIG. Air ratio of each individual cylinder. For this purpose, a control line 32 leads from each evaluation device 11 to the individual adjusting devices 33 for the combustion gas / air ratio. With this device it is therefore possible to regulate specific engine parameters in a cylinder-selective manner as a function of the light emission of each combustion cycle.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Investigating Or Analysing Materials By Optical Means (AREA)
Abstract
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT141/93 | 1993-01-28 | ||
AT14193 | 1993-01-28 | ||
PCT/AT1993/000164 WO1994017297A1 (en) | 1993-01-28 | 1993-10-27 | Arrangement for determining the parameters of an internal combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0632864A1 true EP0632864A1 (en) | 1995-01-11 |
EP0632864B1 EP0632864B1 (en) | 1997-07-23 |
Family
ID=3482617
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP94900001A Expired - Lifetime EP0632864B1 (en) | 1993-01-28 | 1993-10-27 | Arrangement for determining the parameters of an internal combustion engine |
Country Status (8)
Country | Link |
---|---|
US (2) | US5505177A (en) |
EP (1) | EP0632864B1 (en) |
JP (1) | JPH07505694A (en) |
AT (2) | ATE155850T1 (en) |
DE (1) | DE59306980D1 (en) |
DK (1) | DK0632864T3 (en) |
ES (1) | ES2105595T3 (en) |
WO (1) | WO1994017297A1 (en) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1994017297A1 (en) * | 1993-01-28 | 1994-08-04 | Jenbacher Energiesysteme Aktiengesellschaft | Arrangement for determining the parameters of an internal combustion engine |
AT403323B (en) * | 1995-08-24 | 1998-01-26 | Jenbacher Energiesysteme Ag | METHOD AND DEVICE FOR DETERMINING A KNOCKING INTENSITY SIGNAL OF AN INTERNAL COMBUSTION ENGINE |
US5904131A (en) | 1995-12-28 | 1999-05-18 | Cummins Engine Company, Inc. | Internal combustion engine with air/fuel ratio control |
US5949146A (en) * | 1997-07-02 | 1999-09-07 | Cummins Engine Company, Inc. | Control technique for a lean burning engine system |
US5923809A (en) * | 1998-02-02 | 1999-07-13 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Optical power source derived from engine combustion chambers |
DE10066074B4 (en) * | 2000-09-04 | 2006-09-07 | Iav Gmbh Ingenieurgesellschaft Auto Und Verkehr | Method for evaluating stratified charge combustion for direct injection gasoline engines |
US6732709B1 (en) | 2002-12-06 | 2004-05-11 | Caterpillar Inc | Dynamic engine timing control |
DE102004060893B4 (en) * | 2004-12-17 | 2006-07-27 | Mde Dezentrale Energiesysteme Gmbh | Method and device for controlling an ignition point in an Otto gas engine |
US8006677B2 (en) * | 2006-02-02 | 2011-08-30 | Immixt, LLC | Fuel control system and associated method |
US7721720B2 (en) * | 2006-04-10 | 2010-05-25 | Payne Edward A | Fuel control system and associated method |
US8256401B2 (en) * | 2006-05-21 | 2012-09-04 | Immixt, LLC | Alternate fuel storage system and method |
US7841317B2 (en) * | 2007-04-18 | 2010-11-30 | Williams Rodger K | Alternate fuel blending system and associated method |
WO2013032083A1 (en) * | 2011-08-30 | 2013-03-07 | 한국에너지기술연구원 | Parallel structured integrated linear engine generator |
US9527498B2 (en) * | 2012-08-29 | 2016-12-27 | Ford Global Technologies, Llc | Method to limit temperature increase in a catalyst and detect a restricted exhaust path in a vehicle |
KR20150034035A (en) * | 2013-09-25 | 2015-04-02 | 한국생산기술연구원 | An air fuel ratio instrumentation system including optical sensor |
US9964054B2 (en) | 2014-10-08 | 2018-05-08 | Immixt, LLC | Alternate fuel blending systems and associated methods |
US11204271B2 (en) | 2015-12-08 | 2021-12-21 | Gilbarco Inc. | Systems and methods for alternative fuel life-cycle tracking and validation |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2905506A1 (en) * | 1979-02-14 | 1980-09-04 | Bosch Gmbh Robert | IGNITION SENSOR, ESPECIALLY IN COMBUSTION ENGINES |
US4358952A (en) * | 1980-03-26 | 1982-11-16 | Robert Bosch Gmbh | Optical engine knock sensor |
DE3111135A1 (en) * | 1980-06-20 | 1982-03-11 | Robert Bosch Gmbh, 7000 Stuttgart | METHOD FOR CONTROLLING THE COMBUSTION IN THE COMBUSTION ROOMS OF AN INTERNAL COMBUSTION ENGINE |
JPS5773646A (en) * | 1980-10-27 | 1982-05-08 | Nippon Soken Inc | Knocking detector for internal combustion engine |
DE3108460A1 (en) * | 1981-02-13 | 1982-11-04 | Pischinger, Franz, Prof. Dipl.-Ing. Dr.Techn., 5100 Aachen | METHOD FOR DETECTING KNOCKING COMBUSTION AND DEVICE FOR IMPLEMENTING THE METHOD |
US4425788A (en) * | 1981-02-25 | 1984-01-17 | Robert Bosch Gmbh | Combustion monitoring system for multi-cylinder internal combustion engine |
US4446723A (en) * | 1981-03-20 | 1984-05-08 | Robert Bosch Gmbh | Optical combustion event sensor structure particularly knock sensor for an internal combustion engine |
JPS57186040A (en) * | 1981-05-13 | 1982-11-16 | Hitachi Ltd | Air-fuel ratio feedback controller |
JPS5882039A (en) * | 1981-11-11 | 1983-05-17 | Hitachi Ltd | Controller for air-fuel ratio for internal-combustion engine |
JPS59215952A (en) * | 1983-05-23 | 1984-12-05 | Toyota Motor Corp | Exhaust recirculation controlling method in diesel engine |
JPS59215928A (en) * | 1983-05-24 | 1984-12-05 | Toyota Motor Corp | Control of fuel injection amount of diesel engine |
DE3410067C2 (en) * | 1984-03-20 | 1996-07-18 | Bosch Gmbh Robert | Method for controlling an internal combustion engine with detection of the course of the light intensity |
DE3505063A1 (en) * | 1985-02-14 | 1986-08-14 | Bosch Gmbh Robert | METHOD AND DEVICE FOR CONTROLLING THE BURNS IN THE COMBUSTION ROOMS OF AN INTERNAL COMBUSTION ENGINE |
US4887574A (en) * | 1987-04-21 | 1989-12-19 | Hitachi, Ltd. | Control apparatus for internal combustion engines |
US4940033A (en) * | 1988-05-13 | 1990-07-10 | Barrack Technology Limited | Method of operating an engine and measuring certain operating parameters |
US5052214A (en) * | 1989-01-03 | 1991-10-01 | Luxtron Corporation | Knock detector using optical fiber thermometer |
GB9002935D0 (en) * | 1990-02-09 | 1990-04-04 | Lucas Ind Plc | Misfire detection |
US5113828A (en) * | 1990-02-26 | 1992-05-19 | Barrack Technology Limited | Method and apparatus for determining combustion conditions and for operating an engine |
US5103789A (en) * | 1990-04-11 | 1992-04-14 | Barrack Technology Limited | Method and apparatus for measuring and controlling combustion phasing in an internal combustion engine |
JPH04224260A (en) * | 1990-12-26 | 1992-08-13 | Nippondenso Co Ltd | Combustion condition detecting device for internal combustion engine |
WO1994017297A1 (en) * | 1993-01-28 | 1994-08-04 | Jenbacher Energiesysteme Aktiengesellschaft | Arrangement for determining the parameters of an internal combustion engine |
-
1993
- 1993-10-27 WO PCT/AT1993/000164 patent/WO1994017297A1/en active IP Right Grant
- 1993-10-27 EP EP94900001A patent/EP0632864B1/en not_active Expired - Lifetime
- 1993-10-27 JP JP6516476A patent/JPH07505694A/en active Pending
- 1993-10-27 DE DE59306980T patent/DE59306980D1/en not_active Expired - Fee Related
- 1993-10-27 AT AT94900001T patent/ATE155850T1/en not_active IP Right Cessation
- 1993-10-27 ES ES94900001T patent/ES2105595T3/en not_active Expired - Lifetime
- 1993-10-27 DK DK94900001.2T patent/DK0632864T3/en active
- 1993-10-27 US US08/307,565 patent/US5505177A/en not_active Expired - Fee Related
-
1995
- 1995-01-23 AT AT0800895U patent/AT301U1/en unknown
- 1995-11-21 US US08/560,201 patent/US5560338A/en not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
---|
See references of WO9417297A1 * |
Also Published As
Publication number | Publication date |
---|---|
DE59306980D1 (en) | 1997-09-04 |
DK0632864T3 (en) | 1998-02-16 |
JPH07505694A (en) | 1995-06-22 |
US5560338A (en) | 1996-10-01 |
US5505177A (en) | 1996-04-09 |
ATE155850T1 (en) | 1997-08-15 |
ES2105595T3 (en) | 1997-10-16 |
WO1994017297A1 (en) | 1994-08-04 |
AT301U1 (en) | 1995-07-25 |
EP0632864B1 (en) | 1997-07-23 |
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