WO2011000474A1 - Verfahren zur regelung eines gasmotors - Google Patents
Verfahren zur regelung eines gasmotors Download PDFInfo
- Publication number
- WO2011000474A1 WO2011000474A1 PCT/EP2010/003608 EP2010003608W WO2011000474A1 WO 2011000474 A1 WO2011000474 A1 WO 2011000474A1 EP 2010003608 W EP2010003608 W EP 2010003608W WO 2011000474 A1 WO2011000474 A1 WO 2011000474A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- calculated
- corrected
- deviation
- mixture
- torque
- Prior art date
Links
Classifications
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- 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
- F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D41/0027—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures the fuel being gaseous
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D19/00—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D19/02—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with gaseous fuels
- F02D19/021—Control of components of the fuel supply system
- F02D19/023—Control of components of the fuel supply system to adjust the fuel mass or volume flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D29/00—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
- F02D29/06—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving electric generators
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2250/00—Engine control related to specific problems or objectives
- F02D2250/18—Control of the engine output torque
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2400/00—Control systems adapted for specific engine types; Special features of engine control systems not otherwise provided for; Power supply, connectors or cabling for engine control systems
- F02D2400/14—Power supply for engine control systems
-
- 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
- F02D41/0002—Controlling intake air
-
- 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
- F02D41/0205—Circuit arrangements for generating control signals using an auxiliary engine speed control
-
- 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
- F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
- F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
- F02M21/0203—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels characterised by the type of gaseous fuel
- F02M21/0215—Mixtures of gaseous fuels; Natural gas; Biogas; Mine gas; Landfill gas
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/30—Use of alternative fuels, e.g. biofuels
Definitions
- the invention relates to a method for controlling a gas engine, in which
- both a fuel volume as a proportion of a fuel-air mixture and a mixture pressure of the fuel-air mixture in the receiver tube are set before the inlet valves of the gas engine.
- Gas engines are often used as a drive for emergency generators, quick-start generators or combined heat and power plants (CHP).
- the gas engine at a combustion air ratio of, for example 1.7, ie in lean operation with excess air, operated.
- the gas engine includes a throttle valve for defining the gas fraction in the gas
- Fuel-air mixture a mixer for combining the combustible gas with the air, a compressor as a sub-unit of an exhaust gas turbocharger, a radiator and a mixture throttle. About the mixture throttle, the filling of the
- a control method for a stationary gas engine with generator is known in which from a speed control deviation via a speed controller, a regulator torque is determined as a manipulated variable. From the regulator moment again and the actual rotational speed, a desired volume flow is determined via an efficiency map, which represents both the input variable for controlling the gas throttle valve and the input variable for determining the mixture pressure in the receiver tube.
- the central element is the parallel control of the two Actuators depending on the same control variable, here the target volume flow.
- the setting of the mixture pressure in the receiver pipe takes place via a subordinate one
- Receiver pipe pressure control loop In this receiver pipe pressure control loop, the target receiver pipe pressure corresponds to the reference variable and the measured receiver pipe pressure corresponds to the controlled variable.
- the gas engine and the generator then correspond to the controlled system.
- the target receiver pipe pressure is calculated from the setpoint volume flow below
- Constant values include the combustion air ratio and a stoichiometric air requirement.
- the illustrated method has proven itself in practice. However, the influence of different gas qualities (volume fraction) within the same gas family on the emission values remains critical.
- the DE 699 26 036 T2 describes a method for controlling a gas engine, in which from the speed control deviation via a PID controller, a control signal for
- Control of the mixture throttle is calculated. Also, depending on the speed control deviation, a correction value is determined, via which then the control signal for the throttle valve is changed.
- the object of the method is to suppress over the correction of vibrations of the engine speed, which occur after a change in the target engine speed.
- the invention is based on the object to minimize the influence of a different gas quality on the control method.
- the influence of different gas quality is minimized by calculating a deviation of the controller torque, ie the manipulated variable of the speed controller, to the generator torque and correcting the setpoint receiver pipe pressure based on this deviation.
- the deviation is a measure of how much the energy content of the gas actually used, for example biogas, depends on the energy content of the gas
- the gas engine on a The test bench is calibrated using natural gas as the reference gas.
- the gas locally which occurs as mixed gas from gases of a known gas family, the fuel parameters must be known. These are the calorific value, the stoichiometric
- the fuel parameters are then stored as fixed variables in the system.
- the speed controller via which the controller torque is calculated, refers to the natural gas.
- the target receiver pipe pressure is corrected by calculating it from corrected input variables, namely a corrected nominal volume flow, a corrected combustion air ratio and a corrected air requirement.
- the corrected nominal volume flow is calculated by multiplying the set flow rate by the square of the deviation.
- the corrected combustion air ratio is calculated from a reference combustion air ratio and the deviation, wherein the reference combustion air ratio via a map depending on
- Regulator torque and the actual speed of the gas engine is calculated.
- the corrected air requirement is also determined via a recursion procedure as a function of the deviation.
- the output of the gas engine remains unchanged.
- a gas engine powered by biogas for example, therefore has the same power output as a gas engine powered by natural gas. If the volumetric fraction of the combustible gas varies, then the desired receiver pipe pressure is adapted via the method according to the invention, so that the power output remains unchanged even in this case. The volume fraction therefore need not be known. As a consequence, the same results
- FIG. 1 is an overall diagram
- FIG. 2 is a block diagram
- FIG. 3 shows the calculation of the setpoint receiver pipe pressure as a block diagram
- FIG. 4 shows the calculation of the corrected air requirement as a block diagram
- FIG. 5 is a program flowchart
- Figure 6 is a subroutine.
- the generator 1 shows an overall diagram of a gas engine 1 in V-arrangement with a generator 5.
- the generator 5 is driven by the gas engine 1 via a shaft 2, a clutch 3 and a shaft 4.
- the gas engine 1 the following mechanical components are assigned: a throttle valve 6 for setting a supplied fuel volume flow, for example, biogas, a mixer 7 to
- Actuators are used, for example, a Venturispaltmischer or a rotary valve.
- the electronic engine control unit 14 includes the usual components of a microcomputer system, such as a microprocessor, I / O devices, buffers and memory devices (EEPROM, RAM).
- a microcomputer system such as a microprocessor, I / O devices, buffers and memory devices (EEPROM, RAM).
- Memory modules are the relevant for the operation of the gas engine 1 operating data applied in maps / curves. About this calculates the electronic
- Engine control unit 14 from the input variables, the output variables.
- input variables the A-side receiver tube pressure pRRA, a
- Engine control unit 14 are shown: an adjusted target volume flow Va (SL) for controlling the throttle valve 6, an A-side mixture throttle angle DKWA for driving the A-side mixture throttle valve 10, a B-side
- the signal OFF is representative of the further signals for controlling and regulating the gas engine 1.
- the arrangement has the following general functionality: About the position of
- Gas throttle valve 6, a fuel flow rate, which is supplied to the mixer 7, set.
- the position of the A-side mixture throttle valve 10 defines an A-side mixture volume and thus the A-side receiver pipe pressure pRRA in the A-side receiver pipe 12 in front of the intake valves of the gas engine 1.
- the B-side receiver pipe pressure pRRB about the B-side mixture throttle valve 11, the B-side receiver pipe pressure pRRB before the
- Inlet valves of the gas engine 1 set.
- the reference numeral 14 denotes a reduced block diagram of the electronic engine control unit, wherein the
- the inputs of the electronic engine control unit 14 in this illustration are the raw values of the engine speed nMOT, the A-side
- Receiver pipe pressure pRRA, the B-side receiver pipe pressure pRRB, the setpoint speed nM (SL) and an electrical active power Pwel are provided by the system controller 15. in the
- the generator torque MGen is calculated from the effective electric power Pwel. From the raw values of the engine speed nMOT, the electronic engine control unit 14 calculates via an unillustrated engine
- Engine control unit 14 are in this illustration, the A-side mixture throttle angle DKWA for controlling the A-side mixture throttle valve 10, the B-side mixture throttle angle DKWB for controlling the B-side mixture throttle valve 11 and the adjusted target volume flow Va (SL)
- a speed control deviation dn is calculated from the setpoint speed nM (SL) and the actual speed nM (IST).
- a speed controller 16 calculates the controller torque MR as a manipulated variable from the speed control deviation dn.
- the speed controller 16 is designed as a PIDT1 controller.
- the regulator torque MR is the first input variable of a consumption map 17.
- the second input variable corresponds to the actual rotational speed nM (IST). Depending on the two input variables is over the
- Consumption map 17 determines a desired volume flow V (SL).
- the setpoint volume flow V (SL) is both the input variable for a mass adaptation 31 and for a mixture quantity 18.
- the mass flow rate adaptation V (SL) is adjusted at least as a function of the generator torque MGen.
- the output quantity of the quantity adaptation 31 is an adapted nominal volume flow Va (SL), which is the input variable of the gas throttle valve 6.
- In the throttle valve 6 is a
- Integrated processing electronics via which the value of the adjusted nominal volume flow Va (SL) is assigned a corresponding cross-sectional area and a corresponding angle.
- SL adjusted nominal volume flow Va
- a fuel flow rate is set as the gas content of the fuel-air mixture.
- both the calculation of the target receiver pipe pressure and a subordinate receiver pipe pressure control loop are combined.
- the conversion of the nominal volume flow V (SL) within the mixture quantity 18 is shown in FIG. 3 and will be described in connection therewith.
- the further input variables of the mixture quantity 18 are the generator torque MGen, the regulator torque MR, the actual rotational speed nM (IST) and the two receiver tube pressures pRRA and pRRB as controlled variables of the subordinate receiver tube pressure control loop.
- the A-side mixture throttle angle DKWA and the B-side mixture throttle angle DKWB are calculated.
- the A-side mixture throttle angle DKWA the A-side mixture throttle valve 10 is controlled, via which the A-side receiver pipe pressure pRRA is controlled.
- With the B-side mixture throttle angle DKWB becomes the B-side
- Mixture throttle valve 11 is controlled, via which the B-side receiver pipe pressure pRRB is controlled.
- a central element is the parallel control of the gas throttle valve and mixture throttle valves as a function of the same control variable, in this case the nominal volume flow V (SL).
- FIG. 3 shows a block diagram of a function block 19 for determining the desired receiver pipe pressure pRR (SL), which is a part of the mixture quantity 18.
- the input variables of the function block 19 are the regulator torque MR calculated by the speed controller (FIG. 2: 16), the actual rpm nM (IST), the generator torque MGen and the nominal volume flow V (SL).
- the output variable is the nominal receiver pipe pressure pRR (SL), which is then the reference variable for the downstream receiver pipe pressure control loop.
- a corresponding receiver pipe pressure control loop is shown for example in DE 10 2007 045 195 B3.
- About a calculation 20 is from the
- Regulator moment MR and the generator torque MGen determines a deviation yS by calculating the quotient MR / MGen.
- the deviation yS is a measure of how much the energy content of the fuel actually used by the
- Energy content of the reference fuel deviates.
- the unit of energy content is given in kilowatt-hours per standard cubic meter of gas (kWh / nm 3 ). From the manufacturer of the gas engine, the system is set to natural gas as reference fuel. If natural gas is used, then the quotient MR / MGen equals one. If, however, a gas with lower energy content is used, for example biogas, then depending on
- Inertgasanteil the quotient in the range between 1, 4 to 1, 5 are.
- a characteristic map 21 is used to assign a reference combustion air ratio LAMr to the regulator torque MR and the actual rotational speed nM (IST).
- the reference combustion air ratio LAMr is the first input of a correction 22.
- the second input is a reference air demand LMINr, which is constant here.
- the reference air demand LMINr corresponds to the stoichiometric air requirement to completely burn one cubic meter of the reference gas.
- the third input is the deviation yS.
- the corrected combustion air ratio LAMk is calculated according to the following relationship:
- LAMk LAMr + [(1-yS 2 ) / LMINr] (1)
- the output of the correction 22, that is, the corrected combustion air ratio LAMk, is the first corrected input of a calculation 25 for determining the target receiver pipe pressure pRR (SL).
- About a correction 23 is dependent on the Deviation yS calculates a corrected air requirement LMINk.
- the correction 23 is shown in FIG. 4 and will be described in connection therewith.
- Air demand LMINk is the second corrected input of the calculation 25.
- the third corrected input of the calculation 25 is a corrected target volumetric flow Vk (SL). Calculated this is by the desired volume flow V (SL) is multiplied by the square of the deviation yS, calculation 24.
- yS mean the deviation, T1 the temperature measured in the receiver tube, p ⁇ the standard air pressure to normal zero (1013 hpa), LAMk corrected
- FIG. 4 shows the calculation of the corrected air requirement as a block diagram.
- the input variables are the deviation yS and the ignition timing ZZP.
- the output quantities are the corrected air requirement LMINk and a mixing parameter xSF.
- the corrected air requirement LMINk is calculated by means of a recursion loop 26. On the basis of the deviation yS and an efficiency ratio ETA is over a
- Calculation 27 calculated a mixing parameter xS.
- xS is the mixing parameter.
- the constant HUO corresponds to the highest assumed calorific value of the actually used fuel, for example biogas.
- the constant HUU corresponds to the lowest assumed calorific value of the fuel actually used.
- the constant HUr corresponds to the calorific value of the
- Reference fuel here: natural gas.
- HUO and HUU the provenance and the gas family from which the fuels originate must be known. During operation of the gas engine these are not changed.
- the mixing parameter xS is then passed to an efficiency map 28, via which a new.
- the mixing parameter xS and the ignition ZZP are then passed to an efficiency map 28, via which a new.
- Efficiency ratio ETA is determined.
- the efficiency ratio ETA can be embodied as the ratio of an actual efficiency to a reference efficiency determined on the test bench when using the reference fuel (natural gas).
- the new efficiency ratio ETA is then fed back to the calculation 27.
- a mixing parameter x S is then calculated again from the new efficiency ratio ETA according to the formula (3).
- the recursion loop is run through until an abort criterion is detected.
- An abort criterion is when the recursion loop has been iterated 26 times. Alternatively, an abort criterion is present if the difference of two recursively calculated mixing parameters is less than a limit value.
- the last computed mixture parameter is set as valid.
- Downstream of the recursion loop 26 is a filter 29, typically a PT1 filter, via which then the mixture parameters set as valid are filtered. From the filtered mixture parameter xSF and constant values K is over a
- LMINu means the minimum air requirement of the actually used
- the mixing parameter xSF is further processed internally, for example to adjust the fuel density and the ignition timing.
- the inventive method is shown in a program flowchart.
- the actual rotational speed nM (IST) and the target rotational speed nM (SL) are read in and then from S2 the rotational speed control deviation dn is calculated therefrom.
- the speed control deviation dn determines the speed controller, for example via a PIDT1 algorithm, as a manipulated variable, the regulator torque MR, S3.
- the consumption characteristic field (FIG. 2: 17) is used to calculate the desired volume flow V (SL) at S4 as a function of the regulator torque MR and the actual rotational speed nM (IST).
- the deviation yS is determined from the regulator torque MR and the generator torque MGen by calculating the quotient MR / MGen.
- a reference combustion air ratio LAMr is assigned to the regulator torque MR and the actual rotational speed nM (IST) via a characteristic map (FIG. 3: 21).
- the corrected combustion air ratio LAMk is then determined by the formula (1).
- a subroutine UP1 for calculating the corrected air requirement LMINk is branched at S8. The subroutine UP1 is shown in FIG. 6 and will be described in connection therewith.
- the corrected nominal volumetric flow Vk (SL) is calculated from the nominal volumetric flow V (SL) and the deviation yS at S9.
- the SoII receiver pipe pressure pRR (SL) is then calculated according to the corrected target volume flow Vk (SL), the corrected air requirement LMINk and the corrected combustion air ratio LAMk according to the formula (2). This completes the program.
- FIG. 6 shows the subroutine UP1 for calculating the corrected air requirement LMINk by means of the recursion method.
- a running variable i and the efficiency ratio ETA are set to the starting value one.
- the mixing parameter xS is then calculated by means of the formula (3).
- the constant HUO corresponds to the highest assumed calorific value of the actually used
- the constant HUU corresponds to the lowest assumed calorific value of the fuel actually used.
- the constant HUr corresponds to the calorific value of the reference fuel, here: natural gas.
- the provenance and the gas family from which the fuels originate must be known. During operation of the gas engine these are not changed.
- the mixing parameter is the
- the efficiency ratio ETA can as Ratio of an actual efficiency to be executed to the reference efficiency.
- a new mixture parameter is then determined with the previously calculated new efficiency ratio ETA and set as the new mixture parameter.
- the new mixing parameter is xS (2).
- the run variable i is incremented by one, S5, and its value is interrogated at S6. If the run variable i is less than four, query result S6: yes, then the program sequence is continued again at S3. If the query result at S6 is negative, the last calculated mixing parameter is set as valid.
- the valid mixing parameters calculated in such a way over a period of time are filtered at S7, for example via a PT1 filter. The result corresponds to the filtered mixing parameter xSF.
- S8 will be in
- the filtered mixture parameter xSF is further processed internally, for example to adjust the fuel density BD and the ignition timing ZZP. Thereafter, the main routine of Fig. 5 is returned to S8.
- the invention has been described with reference to a gas engine which drives a generator.
- a rapid-fire unit or a combined heat and power plant (CHP) can also be used.
- the generator torque MGen then corresponds to the torque which is output by the quick-response unit, for example.
- GECU electronic engine control unit
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201080031062.9A CN102575599B (zh) | 2009-07-03 | 2010-06-16 | 用于调节燃气发动机的方法 |
PL10724326T PL2449234T3 (pl) | 2009-07-03 | 2010-06-16 | Sposób regulacji silnika gazowego |
ES10724326T ES2432670T3 (es) | 2009-07-03 | 2010-06-16 | Procedimiento para la regulación de un motor de gas |
US13/382,100 US9273620B2 (en) | 2009-07-03 | 2010-06-16 | Method for regulating a gas engine |
AU2010268459A AU2010268459B2 (en) | 2009-07-03 | 2010-06-16 | Method for regulating a gas engine |
EP10724326.3A EP2449234B1 (de) | 2009-07-03 | 2010-06-16 | Verfahren zur regelung eines gasmotors |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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DE102009033082.8 | 2009-07-03 | ||
DE102009033082A DE102009033082B3 (de) | 2009-07-03 | 2009-07-03 | Verfahren zur Regelung eines Gasmotors |
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WO2011000474A1 true WO2011000474A1 (de) | 2011-01-06 |
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ID=42342723
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Application Number | Title | Priority Date | Filing Date |
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PCT/EP2010/003608 WO2011000474A1 (de) | 2009-07-03 | 2010-06-16 | Verfahren zur regelung eines gasmotors |
Country Status (8)
Country | Link |
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US (1) | US9273620B2 (de) |
EP (1) | EP2449234B1 (de) |
CN (1) | CN102575599B (de) |
AU (1) | AU2010268459B2 (de) |
DE (1) | DE102009033082B3 (de) |
ES (1) | ES2432670T3 (de) |
PL (1) | PL2449234T3 (de) |
WO (1) | WO2011000474A1 (de) |
Cited By (4)
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WO2014154314A1 (de) * | 2013-03-28 | 2014-10-02 | Mtu Friedrichshafen Gmbh | Verfahren und vorrichtung zum betrieb einer gas-brennkraftmaschine |
WO2015086141A1 (de) * | 2013-12-13 | 2015-06-18 | Mtu Friedrichshafen Gmbh | Verfahren zur drehzahlregelung einer brennkraftmaschine |
EP3597888A1 (de) * | 2018-07-18 | 2020-01-22 | Kohler Co. | Motorgeneratorsteuerung für motor mit festgelegter kraftstoffquelle |
CN112523882A (zh) * | 2020-11-09 | 2021-03-19 | 广西玉柴机器股份有限公司 | 燃气发动机进气压力闭环的燃料控制装置及燃料控制方法 |
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DE102009033082B3 (de) * | 2009-07-03 | 2011-01-13 | Mtu Friedrichshafen Gmbh | Verfahren zur Regelung eines Gasmotors |
JP5314719B2 (ja) * | 2011-02-28 | 2013-10-16 | 三菱重工業株式会社 | ガスエンジンの給気装置 |
CN102493884A (zh) * | 2011-12-23 | 2012-06-13 | 重庆潍柴发动机厂 | 一种大功率气体发动机进气控制方法 |
WO2014020231A1 (en) * | 2012-07-31 | 2014-02-06 | Wärtsilä Finland Oy | Method of and a control system for controlling the operation of an internal combustion piston engine |
CN104755842B (zh) * | 2012-09-10 | 2016-11-16 | 克利尔赛恩燃烧公司 | 使用限流电气元件的电动燃烧控制 |
EP2738373A1 (de) | 2012-12-03 | 2014-06-04 | Siemens Aktiengesellschaft | Gasturbinen-Brennstoffzufuhrverfahren und -anordnung |
KR101829042B1 (ko) * | 2013-10-28 | 2018-02-13 | 얀마 가부시키가이샤 | 부실식 가스 엔진 |
US9719445B2 (en) | 2015-08-11 | 2017-08-01 | General Electric Company | Lambda virtual sensor systems and methods for a combustion engine |
JP6586334B2 (ja) * | 2015-09-24 | 2019-10-02 | 川崎重工業株式会社 | 乗物の製造方法 |
US10378457B2 (en) * | 2017-11-07 | 2019-08-13 | Caterpillar Inc. | Engine speed control strategy with feedback and feedforward throttle control |
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Also Published As
Publication number | Publication date |
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PL2449234T3 (pl) | 2013-12-31 |
US20120109499A1 (en) | 2012-05-03 |
AU2010268459B2 (en) | 2015-09-03 |
DE102009033082B3 (de) | 2011-01-13 |
CN102575599A (zh) | 2012-07-11 |
ES2432670T3 (es) | 2013-12-04 |
CN102575599B (zh) | 2014-11-26 |
EP2449234A1 (de) | 2012-05-09 |
EP2449234B1 (de) | 2013-07-31 |
US9273620B2 (en) | 2016-03-01 |
AU2010268459A1 (en) | 2012-01-19 |
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