EP3705708A1 - Gas engine generator system - Google Patents
Gas engine generator system Download PDFInfo
- Publication number
- EP3705708A1 EP3705708A1 EP20160608.4A EP20160608A EP3705708A1 EP 3705708 A1 EP3705708 A1 EP 3705708A1 EP 20160608 A EP20160608 A EP 20160608A EP 3705708 A1 EP3705708 A1 EP 3705708A1
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- EP
- European Patent Office
- Prior art keywords
- gas
- engine
- gas engines
- engines
- cooling water
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- 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.)
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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
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/0004—Oilsumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P3/00—Liquid cooling
- F01P3/20—Cooling circuits not specific to a single part of engine or machine
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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
- F02D25/00—Controlling two or more co-operating engines
- F02D25/04—Controlling two or more co-operating engines by cutting-out engines
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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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N19/00—Starting aids for combustion engines, not otherwise provided for
- F02N19/02—Aiding engine start by thermal means, e.g. using lighted wicks
- F02N19/04—Aiding engine start by thermal means, e.g. using lighted wicks by heating of fluids used in engines
- F02N19/10—Aiding engine start by thermal means, e.g. using lighted wicks by heating of fluids used in engines by heating of engine coolants
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M5/00—Heating, cooling, or controlling temperature of lubricant; Lubrication means facilitating engine starting
- F01M2005/008—Lubrication means facilitating engine starting
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P11/00—Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
- F01P11/04—Arrangements of liquid pipes or hoses
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P5/00—Pumping cooling-air or liquid coolants
- F01P5/10—Pumping liquid coolant; Arrangements of coolant pumps
- F01P5/12—Pump-driving arrangements
- F01P2005/125—Driving auxiliary pumps electrically
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2031/00—Fail safe
- F01P2031/30—Cooling after the engine is stopped
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2037/00—Controlling
- F01P2037/02—Controlling starting
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P7/00—Controlling of coolant flow
- F01P7/02—Controlling of coolant flow the coolant being cooling-air
- F01P7/08—Controlling of coolant flow the coolant being cooling-air by cutting in or out of pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B43/00—Engines characterised by operating on gaseous fuels; Plants including such engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B63/00—Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices
- F02B63/04—Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices for electric generators
Definitions
- the volume of one cylinder of a spark-ignited engine is limited because of the constraint posed by flame propagation. Compression-ignited diesel engines are less limited in this respect, and a single diesel engine for ships can generate power as high as several tens of thousands of kilowatts. Gas engines on the other hand generate several hundred kilowatts. The electrical load of an individual generator ranges from zero to about 500 kilowatts. Sometimes a maximum power demand cannot be supplied by one engine. In this case, a number of engine generators made up of pairs of engines and generators have to be provided in parallel arrangement to produce power.
- each of the gas engines has an oil pan in which a minimum amount of oil necessary at start-up remains, while the system includes an independent oil tank capable of supplying oil to all of the gas engines.
- a fifth aspect of the present invention made to solve the problems described above is that, in the gas engine generator according to the first or second aspect, the system includes three or more gas engines.
- gas engine generator system includes three gas engines 1 in this embodiment, some systems may include four or more gas engines, or just two gas engines.
- a generator 2 is mounted to each of the plurality of gas engines 1. The gas engine 1 and generator 2 make up a single gas engine generator A.
- a plurality of gas engine generators A, A, ... are arranged in parallel, which, with necessary equipment added thereto, make up the gas engine generator system (see FIGS. 1 and 2 ).
- the air necessary for the combustion in the cylinders of the plurality of gas engines 1, 1, ... is filtered through an element 31b in an air cleaner 31a provided to the intake duct 31 shared by the plurality of gas engines 1, 1, ... and supplied to each gas engine 1, via the intake duct 31 and intake branch pipes 11a of the intake manifolds 11 (see FIG. 1 ) .
- the gas engine 1 of each gas engine generator A is equipped with an engine water pump 15 and an engine oil pump 16.
- the engine water pump 15 and the engine oil pump 16 are discretely provided to each gas engine 1 (see FIG. 1 ).
- the engine water pumps 15 of all the gas engines 1 are each connected to the cooling water supply passage 51 in parallel with each other.
- the engine oil pumps 16 of all the gas engines 1 are each connected to the oil supply passage 52 in parallel with each other.
- FIGS. 7A to 7C illustrate the running status of each gas engine generator A in the gas engine generator system, as the power demand increases from low to medium and from medium to high.
- the power demand increases from low to medium and from medium to high.
- the power demand is low, one of the gas engines 1 is operated.
- the power demand rises to a medium level, the second gas engine is operated.
- the power demand is high, all the gas engines 1 are operated.
- the total control unit 72 manages the operation and start/stop of the plurality of gas engines 1, 1, ... such that all the gas engines 1, 1, ... are equally chosen so that none of the gas engines 1 is disproportionately used i.e., that none of the gas engines 1 is used intensively. This prevents a specific one of the plurality of gas engines 1, 1, ... from being driven intensively for long hours, so that the service life of the gas engine generator system itself can be significantly prolonged.
- all the gas engines, generators, and engine control units are accommodated in a single housing as a package, with one air cleaner to filter air to be supplied for combustion to all the gas engines, and one muffler to reduce noise emitted by exhausts from all the gas engines.
- the generator system can be configured compactly in this way. Namely, the generator system can be designed as a unit. This will make installation of the generator system during construction work of a building even easier.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
Description
- The present invention relates to a gas engine generator system having a plurality of gas engines and capable of running accordingly to the increase and decrease in the amount of power demand.
- Small engine generators that combine a small engine and a generator coupled together have come in various types so far. Among these, a spark-ignited gas engine that runs on liquefied petroleum gas (LPG) or compressed natural gas (CNG) is advantageous in terms of simplicity and environmental friendliness as the power source of an independent, discrete generator.
- Since gas engines are reciprocating piston engines, when driven at a constant rpm and an air-fuel ratio, the smaller the load, the lower the thermal efficiency. When idling, the thermal efficiency is zero, which means the engine only consumes fuel while doing no work externally.
- The volume of one cylinder of a spark-ignited engine is limited because of the constraint posed by flame propagation. Compression-ignited diesel engines are less limited in this respect, and a single diesel engine for ships can generate power as high as several tens of thousands of kilowatts. Gas engines on the other hand generate several hundred kilowatts. The electrical load of an individual generator ranges from zero to about 500 kilowatts. Sometimes a maximum power demand cannot be supplied by one engine. In this case, a number of engine generators made up of pairs of engines and generators have to be provided in parallel arrangement to produce power.
- When the power demand is low, the large engine is driven to output a low power. The degree of opening of the throttle is reduced in this case, which deteriorates thermal efficiency. It is therefore preferable to use fewer engines when the power demand is low so that one engine outputs a larger power, and to increase the number of engines correspondingly as the power demand increases. This means that when there is a sudden surge in electrical load demand, another engine needs to be started up quickly. Engines, however, require a warm-up time. A cold engine cannot produce high power due to the poor quality of combustion in the cylinder and a large friction loss. The gap between the piston and the cylinder becomes larger because of which oil may penetrate into the combustion chamber, resulting in a plume of white smoke or increased oil consumption.
- Japanese Patent Application Laid-open Nos.
H 02-262846 H 09-195811 - Through intensive research, the inventors of the present application came up with the present invention to solve the problems described above, a first aspect thereof being a gas engine generator system including: a plurality of gas engines, generators connected to the gas engines, a cooling water supply passage for supplying cooling water to each of the gas engines, a system cooling water pump that circulates the cooling water, and engine water pumps each provided to each of the gas engines, the plurality of gas engines and the plurality of engine water pumps being arranged in parallel to the cooling water supply passage, the system cooling water pump being kept running when even one of the gas engines is running, so as to keep other engines that are stopped warmed up by the cooling water circulating in the cooling water supply passage, at least one of the gas engines being operated at first, with remaining gas engines being run successively in accordance with an increase in power demand, the system further including a total control unit (TCU), the total control unit (TCU) sending signals to select, run, and stop the plurality of gas engines to run the gas engines proportionately such that all of the gas engines have a constant rpm.
- A second aspect of the present invention made to solve the problems described above is that, in the gas engine generator system according to the first aspect, each of the gas engines has an oil pan in which a minimum amount of oil necessary at start-up remains, while the system includes an independent oil tank capable of supplying oil to all of the gas engines.
- A third aspect of the present invention made to solve the problems described above is that, in the gas engine generator system according to first or second aspect, all the gas engines, the generators, and engine control units are accommodated in a single housing as a package, the system being configured with one air cleaner to filter air to be supplied for combustion to all the gas engines, and one muffler to reduce noise emitted by exhausts from all the gas engines.
- A fourth aspect of the present invention made to solve the problems described above is that, in the gas engine generator system according to the third aspect, each of the plurality of gas engines in the package is equipped with an electric engine water pump, an electric engine oil pump, an oil filter, and a system oil tank.
- A fifth aspect of the present invention made to solve the problems described above is that, in the gas engine generator according to the first or second aspect, the system includes three or more gas engines.
- According to the present invention, when the generator system is running, the cooling water is kept circulating in the cooling water supply passage so that all the gas engines, whether running or stopped, are kept warmed up. When the power demand is low, at least one gas engine is operated (run), while the remaining gas engines are run successively in accordance with an increase in the amount of power demand.
- Since the plurality of gas engines including those that are stopped are kept warmed up by the cooling water circulated by the system cooling water pump in the cooling water supply passage when the generator system is running as described above, when the gas engines that are stopped are required to start up in response to an increase in power demand, they can start up immediately and start running in a stable and favorable condition shortly. The plurality of gas engines can thus run cost-effectively, as each of them can be driven with an optimal operation efficiency.
- Moreover, according to the present invention, the generator system includes a total control unit (TCU), which sends signals to serve the function of selecting, running, and stopping the plurality of gas engines to run the gas engines proportionately. Therefore, when the generator system is running, the gas engine that is started up first among the plurality of gas engines, and the gas engines that are started up second and onwards successively with an increase in power demand, can be differed each time. Thus the gas engine that is started up first is chosen equally so that intensive start-up of a specific gas engine is prevented in the operation of the generator system, which leads to a prolonged service life of the generator system itself.
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FIG. 1 is an entire view illustrating the configuration of a generator system; -
FIG. 2 is a schematic perspective view of mechanical parts of the generator system; -
FIG. 3 is a diagram showing the relationship between the degree of throttle opening and thermal efficiency of an engine; -
FIG. 4 is a diagram showing the number of engines driven in accordance with an increase in electrical load demand; -
FIG. 5 is a diagram showing the influence of the temperature of cooling water on the thermal efficiency of an engine; -
FIG. 6 is a diagram illustrating a simple method of storing a preset amount of oil in an oil pan of each engine; and -
FIGS. 7A to 7C are diagrams illustrating how more and more gas engines are started up with an increase in power demand in the generator system of the present invention. - One embodiment of the present invention will be described with reference to the drawings. A gas engine generator system of the present invention is generally made up of
gas engines 1,generators 2, a coolingwater supply passage 51, a systemcooling water pump 51a, anoil supply passage 52, asystem oil pump 52a, and so on. First of all, thegas engines 1 in the gas engine generator system are small to medium size gas engines. More particularly, they are gas engines that run on liquefied petroleum gas (LPG), compressed natural gas (CNG), or liquefied natural gas (LNG). These gas engines can also run on the propane-butane gas mixture commonly used for domestic purposes as well as utility gas. The system includes a plurality of such gas engines 1 (seeFIGS. 1 and2 ). - While the gas engine generator system includes three
gas engines 1 in this embodiment, some systems may include four or more gas engines, or just two gas engines. Agenerator 2 is mounted to each of the plurality ofgas engines 1. Thegas engine 1 andgenerator 2 make up a single gas engine generator A. A plurality of gas engine generators A, A, ... are arranged in parallel, which, with necessary equipment added thereto, make up the gas engine generator system (seeFIGS. 1 and2 ). - The gas engine generators A, A, ... arranged in parallel in the gas engine generator system share an
intake duct 31 and anexhaust duct 32. Eachgas engine 1 has anintake manifold 11 for taking in the air, and anexhaust manifold 12 for exhausting gases. Theintake manifold 11 includes anintake branch pipe 11a, and is connected to theintake duct 11 through thisintake branch pipe 11a. Theexhaust manifold 12 includes anexhaust branch pipe 12a, and is connected to theexhaust duct 32 through thisexhaust branch pipe 12a. Theexhaust branch pipes 12a of theexhaust manifolds 12 of the plurality ofgas engines 1 are connected to an exhaust port of theexhaust duct 32 shared by the plurality ofgas engines muffler 32a that reduces the noise. - The air necessary for the combustion in the cylinders of the plurality of
gas engines element 31b in anair cleaner 31a provided to theintake duct 31 shared by the plurality ofgas engines gas engine 1, via theintake duct 31 andintake branch pipes 11a of the intake manifolds 11 (seeFIG. 1 ) . - The exhaust travels from the exhaust manifolds 12 through the
exhaust branch pipes 12a andexhaust duct 32, and is released to the outside via themuffler 32a that reduces the noise. Fuel is supplied from a tank (not shown) via an electromagnetic shut-offvalve 41, and supplied to themixer 13 of eachgas engine 1 through afuel line 4 drawn as a thick solid line, after the pressure is adjusted by a low-pressure adjusting valve 42 to substantially the same level as the atmospheric pressure (seeFIG. 1 ). - The parallel arranged plurality of gas engine generators A, A, ... are equipped with the cooling
water supply passage 51 that is the circulating flow passage of cooling water, and theoil supply passage 52 that is the circulating flow passage of oil, in their surroundings. The coolingwater supply passage 51 includes an electric systemcooling water pump 51a for circulating cooling water in the coolingwater supply passage 51, and theoil supply passage 52 includes asystem oil pump 52a for circulating oil in the oil supply passage 52 (seeFIG. 1 ). - The
gas engine 1 of each gas engine generator A is equipped with anengine water pump 15 and anengine oil pump 16. Theengine water pump 15 and theengine oil pump 16 are discretely provided to each gas engine 1 (seeFIG. 1 ). Theengine water pumps 15 of all thegas engines 1 are each connected to the coolingwater supply passage 51 in parallel with each other. Theengine oil pumps 16 of all thegas engines 1 are each connected to theoil supply passage 52 in parallel with each other. - Cooling water to be supplied to each
gas engine 1 of each of the plurality of parallel gas engine generators A, A, ... is pumped through the coolingwater supply passage 51 by the system coolingwater pump 51a and supplied to theengine water pump 15 of eachgas engine 1. As the cooling water passes through and cools thegas engine 1, the temperature of the cooling water itself rises. The water then travels throughreturn lines 51r of the coolingwater supply passage 51, and releases heat in aradiator 51b before returning to the system coolingwater pump 51a. The cooling water thus circulates in the cooling water supply passage 51 (seeFIG. 1 ) . - When some of the gas engine generators A in the running gas engine generator system are stopped, the engine water pumps 15 of the
gas engines gas engines 1, and exits to returnlines 51r of the coolingwater supply passage 51 via cooling water discharge passages. - The engine oil that lubricates various parts of the
gas engines 1 is pumped up from asystem oil tank 52b by the electricsystem oil pump 52a, filtered by anoil filter 52c, and supplied to eachgas engine 1 through the oil supply passage 52 (seeFIG. 1 ). When the engines are running, the oil is pressurized by theengine oil pump 16 commonly provided to eachgas engine 1 and lubricates various parts of thegas engine 1. When somegas engines 1 are stopped in the running gas engine generator system, the oil that circulates in theoil supply passage 52 joins with the oil that came out into thereturn lines 52r unused, and flows back to thesystem oil tank 52b, as with the cooling water. - Next, a total control unit (TCU) 72 will be described. The total control unit (TCU) 72 opens the fuel shut-off
valve 41 when a signal S indicates the necessity of stopping electricity or generating electricity. The low-pressure adjusting valve 42 adjusts the pressure of the fuel to the atmospheric pressure or substantially to the atmospheric pressure so that it is ready to be supplied to eachgas engine 1. The TCU supplies power to the system coolingwater pump 51a and thesystem oil pump 52a to circulate the cooling water and oil. - The total control unit (TCU) 72 determines which one or ones of the plurality of
gas engines 1 should be driven, selects somegas engines 1 as required, and sends a signal to engine control units (ECU) 71 for starting up the engines. Based on this signal, the engine control unit (ECU) 71 activates a starter (not shown) to start up thegas engine 1. - The cooling water is pumped from the cooling
water supply passage 51 to the water jacket in thegas engine 1 by theengine water pump 15 provided to thegas engine 1. Similarly, the oil from theoil supply passage 52 is pressurized and pumped to the parts in thegas engine 1 that need lubrication such as bearings by theengine oil pump 16 provided to thegas engine 1. - An
oil overflow pipe 18a is provided to thegas engine 1 such as to protrude into theoil pan 18 inside thegas engine 1. Theoil overflow pipe 18a keeps a necessary level of oil, while allowing the oil to flow out from theoil pan 18 of thegas engine 1 through theoil overflow pipe 18a into thereturn line 52r of theoil supply passage 52. The oil that has flowed into thereturn line 52r circulates again in theoil supply passage 52. - The oil level can be maintained more reliably with the oil overflow pipe rather than with a level sensor and an electromagnetic valve or an electric pump (not shown). Moreover, the configuration can be made simpler and inexpensive. The amount of oil in the
oil pan 18 should be as low as possible so that the oil is replaced with the circulating oil quickly. To introduce oil from theoil supply passage 52 into thegas engine 1 for lubrication, abranch passage 100b that branches out from theoil supply passage 52 and leads to eachgas engine 1 may be provided, so that oil is constantly introduced into theoil pan 18 of thegas engine 1 through thebranch passage 100b and circulated by theengine oil pump 16 from theoil pan 18 to various parts in thegas engine 1 for lubrication (seeFIG. 6 ). -
Branch passages 100b are illustrated with imaginary lines (two-dot chain lines) inFIG. 1 andFIG. 6 . Thebranch passages 100b are disposed such as to deliver oil into the oil pans 18 of thegas engines 1. Asuction pipe 100a is provided inside thegas engine 1. The suction port side on one end of thissuction pipe 100a is submerged in the oil accumulated in theoil pan 18, while the other end of thesuction pipe 100a is connected to theengine oil pump 16, so that the oil is circulated in thegas engine 1 for lubrication by the action of the engine oil pump 16 (seeFIG. 6 ). - Fuel is supplied to the
mixer 13 as indicated by thick solid lines, where it is mixed with the air from theintake branch pipe 11a, and this gas mixture is sucked into the cylinders of thegas engine 1 from theintake manifold 11. The exhaust, that is the gas after combustion, travels from theexhaust manifold 12 through theexhaust branch pipe 12a and is guided from theexhaust duct 32 into themuffler 32a, where the noise is reduced, before being released to the outside. - The power output of the
gas engine 1 is controlled by a throttle valve of themixer 13 that is driven by athrottle actuator 14. A plurality of lines make up a signal line for transmission and reception of signals such as ignition signals between the engines and engine control units (ECUs) 71, whereby an ignition signal is sent to discrete ECUs, or conversely, information to be used for control such as engine rpm is sent from the ECUs. - Based on the signal, the engine control unit (ECU) 71 controls the rpm of the
gas engine 1. At the moment of an increase in power demand or electrical load demand, the rpm of thegas engine 1 decreases due to a surge in torque demand for thegas engine 1. When this happens, the throttle is opened to increase the rpm to a required level to restore the rotation speed. The power demand is sometimes called electrical load demand. The electric power generated by thegenerator 2 run by the power of thegas engine 1 is converted to a direct current at a prescribed voltage bydiscrete inverters 6 and supplied to atotal power inverter 8. The powers are summed up, and output as an alternating current with a prescribed voltage and frequency, or as a direct current with a prescribed voltage. - How
gas engines 1 to be driven in response to a power demand are selected will be explained with reference toFIG. 4 . Assuming that the power generation capacity of one generator is 50 kW, for example, and that the product of the power generation efficiency and the inverter efficiency is 0.909, the engine has to generate a power of 55 kW (50 kW/0.909). While it is possible to run thegas engines 1 such that all the generators are equal in output, this would mean that eachgas engine 1 would be running with a low degree of throttle opening, which would result in poor thermal efficiency. -
FIG. 3 shows the thermal efficiency when the throttle is opened gradually under a condition where the engine rpm and air-fuel ratio are constant. The more the throttle is opened to increase the power output, the better the thermal efficiency, because of the following: With the rpm being constant, there is no difference in friction loss whether the load is low or high. The lower the load, the higher the pumping loss, due to the increase in negative pressure in the intake manifold. Namely, the ratio of the energy of fuel effectively converted into work is reduced when the engine is run in a low load condition. The thermal efficiency of thegas engine 1 is therefore better when the degree of throttle opening is higher. - While it is advantageous to open the throttle as much as possible in terms of thermal efficiency, there is hardly any change in thermal efficiency after the degree of throttle opening has exceeded 80%. In consideration of the engine durability, it is therefore desirable to run the engine with about 80% degree of throttle opening. Here, the degree of throttle opening being zero means that the engine is idling, while 100% means that the throttle is fully opened.
- Referring to
FIG. 4 , control of the power output by thegas engines 1 and the number ofgas engines 1 in response to changes in power demand will be described. The solid lines indicate the case where the numbers of engines are switched, with the degree of opening of the throttle at 80%. The broken lines indicate the case where each engine is used up to 100% degree of throttle opening. The maximum power output by the engine is 55 kW. The number of engines is normally increased before the power output exceeds 80%, i.e., 44 kW. - For example, one
gas engine 1 is driven until the power demand exceeds 40 kW, i.e., until the power output of thegas engine 1 reaches 44 kW. When the power demand rises to 70 kW, it cannot be generated by just onegas engine 1. To generate a power of 70 kW, thegas engine 1 needs to produce 70/0.909, i.e., 77 kW. - Accordingly, the
second gas engine 1 is started up. This decision is made by the total control unit (TCU) 72, which then sends the command to the engine control unit (ECU) 71. The engine control unit (ECU) 71 immediately starts up thegas engine 1. Here, since the cooling water and oil that have been heated through the process of cooling thegas engine 1 that has already been running has been supplied to the stoppedgas engine 1, thegas engine 1 that has been stopped can smoothly start up and produce a large power. - The gas engine that was started up first may be operated to generate 40 kW, while the gas engine that was started up second may be operated to generate 37 kW. This selection is also made by the total control unit (TCU) 72, which then sends the command to the engine control unit (ECU) 71 of each engine. For generating a total of 155 kW by the
gas engines 1 together as shown inFIG. 4 , all fourgas engines 1 may be driven when all thegas engines 1 are to produce power of up to 80% degree of throttle opening, or threegas engines 1 may be driven if they are to be used up to 100%. Such operation should desirably be limited to a short period of time such as transient periods. - Therefore, with a set of four gas engine generators A, a power of up to 200 kW can be supplied, with a maximum power capacity of 220 kW. If the
gas engine 1 is a large engine capable of generating up to 220 kW by itself, the degree of throttle opening will be reduced when outputting 30 kW, for example, resulting in poor thermal efficiency. - A plurality of units of gas engine generators A independent from each other are arranged in parallel, and one or
more gas engines 1 are selected and driven in accordance with the power demand such that eachgas engine 1 is run with a degree of throttle opening not greater than 80% even when the load requires a larger degree of throttle opening, whereby the gas engine generator system can be operated with a good balance of thermal efficiency and durability. Generally, oil temperature shows the same tendency as that of cooling water. Namely, when the cooling water temperature rises, so does the oil temperature. - The temperature of the cooling water affects the thermal efficiency of the
gas engine 1 as shown inFIG. 5 . There is a temperature range where the thermal efficiency of thegas engine 1 is highest. Oil thickens when the temperature decreases, which increases friction loss and leads to poor combustion in the cylinder. On the other hand, too high a temperature causes knocking, which has an extremely negative effect on the thermal efficiency, and can damage the engine. For a gas engine, the suitable temperature range is from 80°C to 90°C. - Cooling water at a temperature of this range or lower than this range by 3°C to 5°C is supplied to each
gas engine 1, through heat dissipation using theradiator 51b. Heat dissipation is controlled by turning on and off anelectric fan 51c or by adjusting its rpm, according to the commands sent from the total control unit (TCU) 72. Since the oil is circulated as described above, theoil pan 18 needs to store only a minimum amount of oil required at the initial start-up. - Since the amount of oil stored inside the
gas engine 1 can be reduced to a minimum necessary, replacing the whole oil tank affects the entire oil to a lesser degree, which means maintenance work is made easier. This, of course, does not exclude the possibility of providing a drain plug to the bottom of eachoil pan 18 to remove the oil completely from each engine. - To respond to a power demand of a maximum of several hundred kilowatts, it is optimal that each engine has a maximum power capacity of less than 100 kilowatts, so that a single engine will run in a high load condition when the power demand is low, and as the power demand increases, the number of engines is increased. For this, it is necessary to keep the engines that are not driven yet in an instantly operable condition.
- Since generating power for the whole range of power demand by a single large engine entails poor thermal efficiency during low-load operations, it is beneficial to use a plurality of small-volume engines by design so as to make the engines run in a high-load condition even when the power demand is low. When responding to an increase in power demand that cannot be accommodated by one
gas engine 1, anothergas engine 1 is selected from the plurality ofother gas engines gas engine 1 is high. - A plurality of
gas engines FIGS. 7A to 7C illustrate the running status of each gas engine generator A in the gas engine generator system, as the power demand increases from low to medium and from medium to high. When the power demand is low, one of thegas engines 1 is operated. When the power demand rises to a medium level, the second gas engine is operated. When the power demand is high, all thegas engines 1 are operated. - According to the present invention, all the
gas engines 1,generators 2, and engine control units (ECUs) may be accommodated in onehousing 9 as a package (seeFIG. 2 ). Thehousing 9 may be equipped with theair cleaner 31a andmuffler 32a, so that the air for combustion to be supplied to all thegas engines muffler 32a reduces the noise emitted by the exhausts from all thegas engines 1. - In this embodiment, the plurality of
gas engines 1 accommodated in thehousing 9 and configured as a package may each be provided with an electricengine water pump 15, an electricengine oil pump 16, anoil filter 52c, and asystem oil tank 52b. As an alternative embodiment, cooling water may be supplied to all thegas engines 1 from the coolingwater supply passage 51 by means of the system coolingwater pump 51a alone, and oil may be supplied to all thegas engines 1 from theoil supply passage 52 by means of thesystem oil pump 52a alone. - The system has an integrated intake, exhaust, cooling, and lubricating system so as to improve maintenance, to reduce cost, and to facilitate packaging of a plurality of gas engine generators A, A, ... in a
single housing 9. Moreover, the gas engine generator system of the present invention is equipped with atotal control unit 72. - The
total control unit 72 manages the operation and start/stop of the plurality ofgas engines gas engines gas engines 1 is disproportionately used i.e., that none of thegas engines 1 is used intensively. This prevents a specific one of the plurality ofgas engines - According to the second aspect of the invention, each of the gas engines has an oil pan in which a minimum amount of oil necessary at start-up remains, while the system includes an independent oil tank capable of supplying oil to all of the gas engines. This improves the circularity of oil for the gas engines that are started up second and onwards with an increase in the amount of power demand during the operation of the generator system, and ensures an optimal condition for the gas engines when started up.
- According to the third aspect of the invention, all the gas engines, generators, and engine control units are accommodated in a single housing as a package, with one air cleaner to filter air to be supplied for combustion to all the gas engines, and one muffler to reduce noise emitted by exhausts from all the gas engines. The generator system can be configured compactly in this way. Namely, the generator system can be designed as a unit. This will make installation of the generator system during construction work of a building even easier.
- According to the fourth aspect of the invention, the plurality of sets of gas engines packaged in the housing are equipped with an electric engine water pump, an electric engine oil pump, an oil filter, and a system oil tank. The generator system can be made more compact and installable this way. According to the fifth aspect of the invention, the system includes three or more gas engines. This way, the load for each gas engine is reduced, which enables stable power generation.
- A
- Gas engine generator
- 1
- Gas engine
- 15
- Engine water pump
- 16
- Engine oil pump
- 18
- Oil pan
- 2
- Generator
- 31a
- Air cleaner
- 32a
- Muffler
- 51
- Cooling water supply passage
- 51a
- System cooling water pump
- 52
- Oil supply passage
- 52b
- System oil tank
- 52c
- Oil filter
- 71
- Engine control unit (ECU)
- 72
- Total control unit (TCU)
- 9
- Housing
Claims (5)
- A gas engine generator system comprising: a plurality of gas engines, generators connected to the gas engines, a cooling water supply passage for supplying cooling water to each of the gas engines, a system cooling water pump that circulates the cooling water, and engine water pumps respectively provided to the gas engines,
the plurality of gas engines and a plurality of the engine water pumps being arranged in parallel to the cooling water supply passage,
the system cooling water pump being kept running when even one of the gas engines is running, so as to keep other engines that are stopped warmed up by the cooling water circulating in the cooling water supply passage,
at least one of the gas engines being operated at first, with remaining gas engines being run successively in accordance with an increase in power demand,
the system further comprising a total control unit (TCU),
the total control unit (TCU) sending signals to select, run, and stop the plurality of gas engines so as to run the gas engines proportionately, and
all the gas engines are controlled so as to rotate at a constant revolution number. - The gas engine generator system according to claim 1, wherein each of the gas engines has an oil pan in which a minimum amount of oil necessary at start-up remains, while the system includes an independent oil tank capable of supplying oil to all of the gas engines.
- The gas engine generator system according to claim 1 or 2, wherein all the gas engines, the generators, and engine control units are accommodated in a single housing as a package, the system being configured with one air cleaner to filter air to be supplied for combustion to all the gas engines, and one muffler to reduce noise emitted by exhausts from all the gas engines.
- The gas engine generator system according to claim 3, wherein each of the plurality of gas engines in the package is equipped with an electric engine water pump, an electric engine oil pump, an oil filter, and a system oil tank.
- The gas engine generator system according to claim 1 or 2, wherein the system includes three or more gas engines.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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JP2019039962A JP6592212B1 (en) | 2019-03-05 | 2019-03-05 | Gas engine power generation system |
Publications (1)
Publication Number | Publication Date |
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EP3705708A1 true EP3705708A1 (en) | 2020-09-09 |
Family
ID=68234878
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP20160608.4A Pending EP3705708A1 (en) | 2019-03-05 | 2020-03-03 | Gas engine generator system |
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JP (1) | JP6592212B1 (en) |
Families Citing this family (1)
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JP6592212B1 (en) * | 2019-03-05 | 2019-10-16 | ライズピットカンパニー株式会社 | Gas engine power generation system |
Citations (5)
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JPH02262846A (en) | 1989-02-27 | 1990-10-25 | Fuji Electric Co Ltd | Operation controller for generator |
JPH09195811A (en) | 1996-01-19 | 1997-07-29 | Komatsu Ltd | Automatic load sharing device of generator and its control method |
JP2000073861A (en) * | 1998-08-26 | 2000-03-07 | Honda Motor Co Ltd | Cogeneration device |
JP6592212B1 (en) * | 2019-03-05 | 2019-10-16 | ライズピットカンパニー株式会社 | Gas engine power generation system |
GB2572986A (en) * | 2018-04-18 | 2019-10-23 | Caterpillar Inc | Combined engine systems |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5787731B2 (en) * | 2011-11-25 | 2015-09-30 | 株式会社東芝 | Gas engine system and power generator |
JP2017172341A (en) * | 2016-03-18 | 2017-09-28 | 大阪瓦斯株式会社 | Engine system and engine power generation system |
JP2018204594A (en) * | 2017-06-09 | 2018-12-27 | 株式会社ルネッサンス・エナジー・リサーチ | Engine type power generation device and its manufacturing method |
JP6923128B2 (en) * | 2017-06-09 | 2021-08-18 | 株式会社ルネッサンス・エナジー・リサーチ | A management system that manages the replacement of parts for engine-powered generators |
-
2019
- 2019-03-05 JP JP2019039962A patent/JP6592212B1/en active Active
-
2020
- 2020-03-03 EP EP20160608.4A patent/EP3705708A1/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02262846A (en) | 1989-02-27 | 1990-10-25 | Fuji Electric Co Ltd | Operation controller for generator |
JPH09195811A (en) | 1996-01-19 | 1997-07-29 | Komatsu Ltd | Automatic load sharing device of generator and its control method |
JP2000073861A (en) * | 1998-08-26 | 2000-03-07 | Honda Motor Co Ltd | Cogeneration device |
GB2572986A (en) * | 2018-04-18 | 2019-10-23 | Caterpillar Inc | Combined engine systems |
JP6592212B1 (en) * | 2019-03-05 | 2019-10-16 | ライズピットカンパニー株式会社 | Gas engine power generation system |
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JP6592212B1 (en) | 2019-10-16 |
JP2020143615A (en) | 2020-09-10 |
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