CN108150278A - A kind of internal-combustion engine system - Google Patents

A kind of internal-combustion engine system Download PDF

Info

Publication number
CN108150278A
CN108150278A CN201711275722.8A CN201711275722A CN108150278A CN 108150278 A CN108150278 A CN 108150278A CN 201711275722 A CN201711275722 A CN 201711275722A CN 108150278 A CN108150278 A CN 108150278A
Authority
CN
China
Prior art keywords
turbine
compressor
outlet
entrance
combustion engine
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.)
Pending
Application number
CN201711275722.8A
Other languages
Chinese (zh)
Inventor
郑新前
朱登渟
曾翰轩
王钧莹
王奥林
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tsinghua University
Original Assignee
Tsinghua University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Tsinghua University filed Critical Tsinghua University
Priority to CN201711275722.8A priority Critical patent/CN108150278A/en
Publication of CN108150278A publication Critical patent/CN108150278A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K25/00Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
    • F01K25/08Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for using special vapours
    • F01K25/10Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for using special vapours the vapours being cold, e.g. ammonia, carbon dioxide, ether
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/02Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
    • F01N3/0205Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust using heat exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N5/00Exhaust or silencing apparatus combined or associated with devices profiting from exhaust energy
    • F01N5/02Exhaust or silencing apparatus combined or associated with devices profiting from exhaust energy the devices using heat
    • F01N5/025Exhaust or silencing apparatus combined or associated with devices profiting from exhaust energy the devices using heat the device being thermoelectric generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B41/00Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02Engines with prolonged expansion
    • F02B41/10Engines with prolonged expansion in exhaust turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G5/00Profiting from waste heat of combustion engines, not otherwise provided for
    • F02G5/02Profiting from waste heat of exhaust gases
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The invention discloses a kind of internal-combustion engine systems, belong to technical field of internal combustion engines, including:Internal combustion engine (1) sets air inlet and exhaust outlet thereon;Turbine (2), entrance are communicated to the exhaust outlet of internal combustion engine (1);First compressor (3), entrance connection air, the air inlet of outlet to internal combustion engine (1);Second compressor (4), entrance are communicated to the outlet of turbine (2), outlet to air;Turbine (2) is by the first shafting (5) connection coaxial with the first compressor (3) and the second compressor (4), for first compressor (3) and the second compressor (4) to be driven to rotate and carry out compressed action.The present invention drives two compressor rotations using single turbine, while taking into account the plenum of internal combustion engine and exhaust energy comprehensive reutilization so that whole system structure is simpler and compact, installation space smaller, cost are lower.

Description

A kind of internal-combustion engine system
Technical field
The present invention relates to technical field of internal combustion engines more particularly to a kind of internal-combustion engine systems.
Background technology
Internal combustion engine has highly important effect in national product and life.At present, it is most automobile-used and peculiar to vessel Power is all internal combustion engine.Internal combustion engine consumes a large amount of fossil fuel, but the energy for averagely there was only 30%-40% is converted into machine Tool energy, the energy for having nearly 60%-70% are dispersed into the form of a variety of heat transfers in air in internal combustion engine working process.Its In, the exhaust energy of engine exhaust accounts for about the 30% of gross energy.That is, the energy that really utilizes of internal combustion engine and discharge Exhaust energy ratio is suitable, this causes the energy great waste.Internal combustion engine waste gas energy is recycled, is constantly carried The utilization ratio of high-energy source is the important means for realizing energy-saving and emission-reduction, has important meaning to the sustainable development of global economy Justice.
To solve the above problems, it is highly effective to recycle internal combustion engine waste gas energy using turbocharging in the prior art Technological means, at present using very extensive.Existing overwhelming majority diesel engine and 40% or so gasoline engine all employ whirlpool Take turns supercharging technology.The technical solution of the prior art mainly has following several:
1. scheme one:It is the structural representation for the turbocharged internal engine system being widely used in the prior art such as Fig. 1 Figure.Its operation principle is:The exhaust gas that internal combustion engine 1 discharges enters 2 expansion work of turbine, and turbine 2 is calmed the anger by 5 output work of shafting Machine 3,3 compressed air of compressor, increases admission pressure and density, compressed gas enter heat exchanger 6 and cool down, reduces into temperature Degree further increases density of the induced air, improves the dynamic property of internal combustion engine 1.It is discharged to later using post processing by the exhaust gas of turbine 2 In air.But the exhaust gas in this scenario, discharged after turbine 2 also has higher temperature, some energy can not recycle, To internal combustion engine waste gas energy underutilization.
2. scheme two:For the exhaust energy that turbine 2 is discharged in further Utilization plan one, the technical solution of the prior art It is to increase a turbo charge system after turbine 2 on the basis of scheme one, using two turbocharging technology, the two-stage whirlpool Wheel is used to plenum, but this scheme is not suitable for the little situation of power of IC engine demand, and two-step supercharging system It is matched with internal combustion engine more complicated.
3. scheme three:When single-stage turbocharging can meet power of IC engine demand, to avoid system matches complicated, Two turbocharging technology will not generally be used.But on the basis of scheme one, using the increase power turbine after turbine 2 Technology further recycles the exhaust energy of internal combustion engine, but the requirement of this scheme enters the gas pressure superatmospheric of power turbine Power, therefore, when entering the exhaust gas pressure of power turbine close to atmospheric pressure, the acting ability of power turbine is limited, Wu Fajin One step recycles the exhaust energy of internal combustion engine.
Invention content
(1) goal of the invention
The object of the present invention is to provide a kind of internal-combustion engine systems.Two pressures are driven simultaneously by a shafting using single turbine Mechanism of qi rotates, and one of compressor improves the dynamic property of internal combustion engine, another compressor for forming turbo charge system For forming the inverse Bo Leideng circulatory systems, the exhaust energy of internal combustion engine has further been recycled.The inverse Bo Leideng circulatory systems are will be useless Gas is passed through turbine, is followed by a cooling device and a compressor in turbine, blower outlet is air.Exhaust gas is swollen by turbine Enter cooling device after swollen acting to cool down, then be compressed to atmospheric pressure through compressor and be discharged into air, this process is known as inverse Bo Leideng Cycle.It solves the problems, such as that the exhaust energy of internal combustion engine in the prior art is under-utilized, at the same solve in the prior art by Limited, the problem of can not further recycling the exhaust energy of internal combustion engine in power turbine acting ability;Pass through single turbine drives Two compressor rotations carry out compressed action, solve in the prior art due to leading to whole system knot using two turbocharging Structure is more complicated, and the matching between two turbines is also very complicated, and cost is higher, is not suitable for the little feelings of power of IC engine demand The problem of condition.
(2) technical solution
To solve the above problems, the present invention provides a kind of internal-combustion engine system, including:Internal combustion engine sets air inlet thereon And exhaust outlet;Turbine, entrance are communicated to the exhaust outlet of the internal combustion engine;First compressor, entrance connection air, outlet connects Lead to the air inlet of the internal combustion engine;Second compressor, entrance are communicated to the outlet of the turbine, outlet to air; The turbine is by the connection coaxial with first compressor and the second compressor of the first shafting, for driving first compressor It is rotated with the second compressor and carries out compressed action.
Further, the turbine exports power to power plant by first shafting.
Further, the power plant is generator or the bent axle of the internal combustion engine.
Further, the internal-combustion engine system further includes:Charge air cooler, entrance are communicated to the outlet of first compressor, Outlet for cooling down the gas of the first compressor discharge, and increases the internal combustion to the air inlet of the internal combustion engine The density of the induced air of machine.
Further, the charge air cooler is air-cooled or water cooling heat exchanger.
Further, the internal-combustion engine system further includes:Cooling device, be arranged on the turbine and the second compressor it Between, for cooling down the gas of the turbine discharge.
Further, the cooling device is the first heat exchanger components, thermoelectric conversion member, Rankine cycle system and organic Rankine At least one of circulatory system.
Further, the entrance of first heat exchanger components is communicated to the outlet of the turbine, outlet to described second The entrance of compressor, for cooling down the gas of the turbine discharge.
Further, the entrance of the thermoelectric conversion member is communicated to the outlet of the turbine, outlet to described second The thermal energy of absorption for cooling down the gas of the turbine discharge, and is converted into electric energy output by the entrance of compressor.
Further, the Rankine cycle system or organic rankine cycle system include:Second heat exchanger components, first entrance The outlet of the turbine is communicated to, first outlet is communicated to the entrance of second compressor;Steam turbine, entrance are communicated to institute State the second outlet of the second heat exchanger components;Third heat exchanger components, entrance are communicated to the outlet of the steam turbine;Pump, entrance It is communicated to the outlet of the third heat exchanger components, outlet to the second entrance of second heat exchanger components;The steam turbine Power is exported by the second shafting;The Rankine cycle system or organic rankine cycle system are used to cool down the turbine discharge Gas, while the heat of absorption is converted into power output.
(3) advantageous effect
The above-mentioned technical proposal of the present invention has following beneficial technique effect:
A kind of internal-combustion engine system provided by the invention drives two compressors to turn simultaneously using single turbine by a shafting Dynamic, one of compressor improves the dynamic property of internal combustion engine, another compressor is used for group for forming turbo charge system Into the inverse Bo Leideng circulatory systems, the exhaust energy of internal combustion engine is further recycled, the exhaust gas for solving internal combustion engine in the prior art The problem of energy utilization is insufficient, while solve in the prior art since power turbine acting ability is limited, it can not further return The problem of receiving the exhaust energy of internal combustion engine;Compressed action is carried out by single two compressor rotations of turbine drives, is solved existing Have due to causing whole system structure more complicated using two turbocharging in technology, the matching between two turbines is also very multiple Miscellaneous, cost is higher, the problem of not being suitable for power of IC engine demand little situation.The internal-combustion engine system of the present invention, using list Two compressor rotations of turbine drives, while taking into account the plenum of internal combustion engine and exhaust energy comprehensive reutilization so that Whole system structure is simpler and compact, installation space smaller, cost are lower.
The internal-combustion engine system of the present invention can also utilize thermoelectric material to replace the heat exchanger in the inverse Bo Leideng circulatory systems, The thermal energy of exhaust gas is absorbed by thermoelectric material, reduces the temperature of gas, while the thermal energy of absorption is also converted by thermoelectric material Electric energy further improves the recovery utilization rate of the exhaust energy of internal combustion engine.
The internal-combustion engine system of the present invention can also utilize Rankine cycle system and organic rankine cycle system will inverse Bo Leideng The heat that heat exchanger in the circulatory system absorbs is recycled, and further improves the recycling profit of the exhaust energy of internal combustion engine With rate.
Description of the drawings
Fig. 1 is the structure diagram of turbocharged internal engine system in the prior art;
Fig. 2 is the internal-combustion engine system composition schematic diagram that the embodiment of the present invention one provides;
Fig. 3 is the internal-combustion engine system structure diagram that the embodiment of the present invention one provides;
Fig. 4 is internal-combustion engine system structure diagram provided by Embodiment 2 of the present invention;
Fig. 5 is the internal-combustion engine system structure diagram that the embodiment of the present invention three provides;
Fig. 6 is the internal-combustion engine system structure diagram that the embodiment of the present invention five provides;
Fig. 7 is the internal-combustion engine system structure diagram that the embodiment of the present invention six provides;
Fig. 8 is the internal-combustion engine system structure diagram that the embodiment of the present invention seven provides;
Fig. 9 is the internal-combustion engine system structure diagram that the embodiment of the present invention eight provides.
Reference numeral:
1st, internal combustion engine, 2, turbine, the 3, first compressor, the 4, second compressor, the 5, first shafting, 6, charge air cooler, 7, cooling Device, the 71, first heat exchanger components, 72, thermoelectric conversion member, the 73, second heat exchanger components, 74, steam turbine, 75, third heat exchanging part Part, 76, pump, the 77, second shafting.
Specific embodiment
Understand to make the object, technical solutions and advantages of the present invention clearer, With reference to embodiment and join According to attached drawing, the present invention is described in more detail.It should be understood that these descriptions are merely illustrative, and it is not intended to limit this hair Bright range.In addition, in the following description, the description to known features and technology is omitted, to avoid this is unnecessarily obscured The concept of invention.
Embodiment one
Fig. 2 is the internal-combustion engine system composition schematic diagram that the embodiment of the present invention one provides.
Fig. 3 is the internal-combustion engine system structure diagram that the embodiment of the present invention one provides.
Fig. 2, Fig. 3 are please referred to, the present invention provides a kind of internal-combustion engine system, including:Internal combustion engine 1, turbine 2, the first compressor 3rd, the second compressor 4 and the first shafting 5.
Internal combustion engine 1 sets air inlet and exhaust outlet thereon.Internal combustion engine 1 is a kind of dynamic power machine, by making fuel in inside Burning, and the thermal energy that fuel combustion is released is converted directly into the Thermal Motor of power.
Turbine 2, entrance are communicated to the exhaust outlet of internal combustion engine 1, outlet to the second compressor 4.
First compressor 3, entrance connection air, the air inlet of outlet to internal combustion engine 1, after will be atmospheric compressed It is sent into 1 inside of internal combustion engine and participates in work by combustion, improve the dynamic property of internal combustion engine 1.
Second compressor 4, entrance are communicated to the outlet of turbine 2, outlet to air, for discharge turbine 2 It is discharged in air after gas compression.
Turbine 2 is by the first shafting 5 and the 4 coaxial connection of the first compressor 3 and the second compressor, for driving first pressure The rotation of 3 and second compressor 4 of mechanism of qi carries out compressed action.Turbine 2 exports power to power plant by the first shafting 5, is used for Power output is carried out outward.
Optionally, power plant is generator or the bent axle of internal combustion engine 1, but the present invention is not limited system, power plant It can also be other equipment.
Fig. 2 is please referred to, in the present embodiment, internal-combustion engine system further includes charge air cooler 6, and entrance is communicated to the first compressor 3 outlet, the air inlet of outlet to internal combustion engine 1 for cooling down the gas of the first compressor 3 discharge, and increase internal combustion engine 1 Density of the induced air.
Fig. 3 is please referred to, optionally, charge air cooler 6 is air-cooled or water cooling heat exchanger, but the present invention is not limited system.
Fig. 2 is please referred to, in the present embodiment, internal-combustion engine system further includes cooling device 7, is arranged on turbine 2 and second Between compressor 4, for cooling down the gas of the discharge of turbine 2.
Please refer to Fig. 3, in the present embodiment, cooling device 7 be the first heat exchanger components 71, the entrance of the first heat exchanger components 71 It is communicated to the outlet of turbine 2, the entrance of outlet to the second compressor 4, for cooling down the gas of the discharge of turbine 2.
Optionally, the first heat exchanger components 71 are air-cooled or water cooling heat exchanger, but the present invention is not limited system.
Preferably, the first heat exchanger components 71 are the heat exchanger of water cooling, and the heat exchanger cooling effect of water cooling is more preferable so that second 4 wasted work smaller of compressor, energy regenerating utilization rate higher.
Fig. 3 is please referred to, specifically, turbine 2, the first compressor 3 and the second compressor 4 are coaxial, it is coaxial by the first shafting 5 Connection, turbine 2 drive the first compressor 3 and the second compressor 4 to work, while also by 5 connecting power device of the first shafting, to Outer carry out power output.According to the direction that gas flows, the arrangement of component is followed successively by the first compressor 3, charge air cooler 6, interior Combustion engine 1, turbine 2, the first heat exchanger components 71 and the second compressor 4.Wherein, turbine 2, the first compressor 3 and charge air cooler 6 form Turbo charge system;Turbine 2, the second compressor 4 and the first heat exchanger components 71 form the inverse Bo Leideng circulatory systems, 1 work of internal combustion engine The high temperature and high pressure gas discharged after work passes through 2 expansion work of turbine, and the second pressure is entered after being cooled down using the first heat exchanger components 71 The process that mechanism of qi 4 is compressed to atmospheric pressure is known as inverse Bo Leideng cycles.The internal-combustion engine system of the present invention, using the inverse vigorous thunder of single turbine The circulatory system is stepped on, takes into account the comprehensive reutilization of plenum and exhaust energy so that structure is simpler and compact, installation space Smaller, cost are lower.
The operation principle of the internal-combustion engine system of the present invention is described below:
Please refer to Fig. 2, the exhaust gas that the work of internal combustion engine 1 generates enters 2 expansion work of turbine, turbine 2 by the first shafting 5 with First compressor 3 is connected with the second compressor 4.
Turbine 2 by the first shafting 5 drive the first compressor 3 rotate, compressed air, make internal combustion engine 1 admission pressure and Density increases, and after being cooled down using charge air cooler 6, the density of the induced air of internal combustion engine 1 is made further to increase, and is conducive to improve internal combustion engine 1 dynamic property.Enter internal combustion engine 1 and mixed with fuel by being pressurized air after cooling and burn.
Meanwhile turbine 2 also drives the second compressor 4 to rotate by the first shafting 5.The outlet of second compressor 4 is air Environment, vacuum environment can be formed in its input end by being rotated by the second compressor 4.The outlet of turbine 2 and the second compressor 4 The pressure of import is almost equal, the pressure loss only generated through piping and the first heat exchanger components 71, this partial loss very little, Therefore, the outlet pressures subatmospheric of turbine 2.The exhaust gas pressure that the work of internal combustion engine 1 generates is higher, is expanded into turbine 2 To atmospheric pressure hereinafter, expansion is bigger, acting is more, that is, has recycled more exhaust energies.Exhaust gas by turbine 2 leads to It crosses heat exchanger 71 to be cooled down, gas temperature reduces.The engine exhaust gas of identical mass flow is by the expansion of turbine 2 and the second pressure Mechanism of qi 4 compresses, since the gas temperature and pressure that enter the second compressor 4 are far below the temperature and pressure into 2 gas of turbine, Therefore the wasted work of compressed gas can be smaller.By the first shafting 5, the remaining mechanical energy that turbine 2 generates is exported, the One shafting 5 can connect a generator and battery, this portion of energy be stored in the form of electric energy, the first shafting 5 can also The bent axle of internal combustion engine 1 is connected, power is provided for internal combustion engine 1.
Embodiment two
Fig. 4 is please referred to, the difference lies in cooling device 7 uses thermoelectric conversion member to the present embodiment with embodiment one 72 replace the first heat exchanger components 71.
The entrance of thermoelectric conversion member 72 is communicated to the outlet of turbine 2, and the entrance of outlet to the second compressor 4 is used Electric energy output is converted into the gas that cooling turbine 2 is discharged, and by the thermal energy of absorption.
Optionally, the material of thermoelectric conversion member 72 is thermoelectric material, and thermoelectric material is that one kind can convert heat into The material of electric energy.
Specifically, after the exhaust gas discharged of internal combustion engine 1 is by 2 expansion work of turbine, still also have higher temperature, also into The space of row heat recovery.The exhaust gas that turbine 2 is discharged absorbs the thermal energy of exhaust gas by thermoelectric conversion member 72 so that thermoelectricity 72 one side of converting member reduces the temperature of gas, has achieved the purpose that cooling, has on the other hand been converted into the thermal energy of absorption Electric energy further improves the recovery utilization rate of the exhaust energy of internal combustion engine 1.
The structure and connection relation of other parts in the present embodiment are identical in embodiment one, and details are not described herein.
Embodiment three
Since in the technical solution of embodiment one, the first heat exchanger components 71 absorb the heat of exhaust gas, it is useless that reduction can be reached The purpose of temperature degree, but whether the first heat exchanger components 71 are using air-cooled or water cooling heat exchanger, this part of absorption Heat is not recycled, but is dispersed into air.Therefore, in the present embodiment first is replaced using Rankine cycle system Heat exchanger components 71 are further recycled this partial heat that the second heat exchanger components 73 absorb, to improve energy Utilization rate.
Please refer to Fig. 5, in the present embodiment, Rankine cycle system includes the second heat exchanger components 73, steam turbine 74, third heat exchange Component 75,76 and second shafting 77 of pump.
The first entrance of second heat exchanger components 73 is communicated to the outlet of turbine 2, and first outlet is communicated to the second compressor 4 Entrance.
The entrance of steam turbine 74 is communicated to the second outlet of the second heat exchanger components 73.
The entrance of third heat exchanger components 75 is communicated to the outlet of steam turbine 74.
Optionally, third heat exchanger components 75 are air-cooled or water cooling heat exchanger, but the present invention is not limited system.
The entrance of pump 76 is communicated to the outlet of third heat exchanger components 75, and outlet enters to the second of the second heat exchanger components 73 Mouthful.
Steam turbine 74 exports power by the second shafting 77.Specifically, one end of the second shafting 77 is connect with steam turbine 74, The other end exports power to external power plant.
Rankine cycle system is used to cool down the gas of the discharge of turbine 2, while the heat of absorption is converted into power output, into One step recycles the exhaust energy of internal combustion engine 1, improves the utilization rate of energy.
Specifically, pump 76 provides power for the flowing of the working medium of Rankine cycle system, working medium passes through the second heat exchanger components 73, Heat exchange is carried out with the exhaust gas discharged from turbine 2.The working medium of Rankine cycle system is heated, and exhaust gas is cooled.After heating Working medium enters steam turbine 74, the expansion work in steam turbine 74, and the mechanical energy for generation of doing work is exported by the second shafting 77.Expansion Working medium afterwards enters third heat exchanger components 75 and cools down, and enters back into pump 76 and is recycled.This method can be further by internal combustion engine 1 Exhaust energy is recycled, and improves capacity usage ratio.
The structure and connection relation of other parts in the present embodiment are identical in embodiment one, and details are not described herein.
Example IV
The difference lies in replace Rankine cycle system to the present embodiment using organic rankine cycle system with embodiment three System.
The structure of organic rankine cycle system and Rankine cycle system, composition and operation principle all same, difference only exist It is water in, cycle fluid in Rankine cycle system, the cycle fluid in organic rankine cycle system is organic matter.
The structure and connection relation of other parts in the present embodiment are identical in embodiment three, and details are not described herein.
Embodiment five
Please refer to Fig. 6, the difference lies in the coolings in the present embodiment for the present embodiment and embodiment one and embodiment two Device 7 is to be combined the thermoelectric conversion member 72 in the first heat exchanger components 71 and embodiment two in embodiment one, i.e., together The gas that the first heat exchanger components of Shi Caiyong 71 and thermoelectric conversion member 72 discharge turbine 2 cools down, and is increasing cooling effect While, the thermal energy that thermoelectric conversion member 72 absorbs can also be converted into electric energy output.
Fig. 6 is please referred to, specifically, the gas that turbine 2 is discharged, first passes through the first heat exchanger components 71, using heat to electricity conversion Component 72 is communicated to the entrance of the second compressor 4, i.e. the entrance of the first heat exchanger components 71 is communicated to the outlet of turbine 2, and outlet connects Lead to the entrance of thermoelectric conversion member 72, the entrance of the outlet of thermoelectric conversion member 72 to the second compressor 4.
The present invention is not limited system, and the gas that turbine 2 is discharged can also first pass through thermoelectric conversion member 72, using First heat exchanger components 71 are communicated to the entrance of the second compressor 4, i.e. the entrance of thermoelectric conversion member 72 is communicated to going out for turbine 2 Mouthful, the entrance of outlet to the first heat exchanger components 71, outlet the entering to the second compressor 4 of the first heat exchanger components 71 Mouthful.
The structure and connection relation of other parts in the present embodiment are identical in embodiment one, and details are not described herein.
Embodiment six
Please refer to Fig. 7, the difference lies in the coolings in the present embodiment for the present embodiment and embodiment one and embodiment three Device 7 is to be combined the Rankine cycle system in the first heat exchanger components 71 and embodiment three in embodiment one, i.e., simultaneously The gas discharged using the first heat exchanger components 71 and Rankine cycle system to turbine 2 is cooled down, and is increasing the same of cooling effect When, the heat that the second heat exchanger components 73 absorb further is recycled, to improve the utilization rate of energy.
Fig. 7 is please referred to, specifically, the gas that turbine 2 is discharged, first passes through the first heat exchanger components 71, using Rankine cycle The second heat exchanger components 73 in system are communicated to the entrance of the second compressor 4, i.e. the entrance of the first heat exchanger components 71 is communicated to whirlpool The outlet of wheel 2, the first entrance of the second heat exchanger components 73 in outlet to Rankine cycle system, the of the second heat exchanger components 73 One outlet is to the entrance of the second compressor 4.
The present invention is not limited system, the gas that turbine 2 is discharged, and can also first pass through in Rankine cycle system second is changed Thermal part 73 is communicated to the entrance of the second compressor 4 using the first heat exchanger components 71, i.e., the second heat exchange in Rankine cycle system The first entrance of component 73 is communicated to the outlet of turbine 2, and first outlet is communicated to the entrance of the first heat exchanger components 71, the first heat exchange The outlet of component 71 is to the entrance of the second compressor 4.
The structure and connection relation of other parts in the present embodiment are identical in embodiment one, and details are not described herein.
Embodiment seven
Please refer to Fig. 8, the difference lies in the coolings in the present embodiment for the present embodiment and embodiment two and embodiment three Device 7 is to be combined the Rankine cycle system in the thermoelectric conversion member 72 and embodiment three in embodiment two, i.e., simultaneously The gas discharged using thermoelectric conversion member 72 and Rankine cycle system to turbine 2 is cooled down, and is increasing the same of cooling effect When, the thermal energy that thermoelectric conversion member 72 absorbs can also be converted into electric energy output, the second heat exchanger components 73 can also be absorbed Heat further recycled, to improve the utilization rate of energy.
Fig. 8 is please referred to, specifically, the gas that turbine 2 is discharged, first passes through thermoelectric conversion member 72, using Rankine cycle The second heat exchanger components 73 in system are communicated to the entrance of the second compressor 4, i.e. the entrance of thermoelectric conversion member 72 is communicated to whirlpool The outlet of wheel 2, the first entrance of the second heat exchanger components 73 in outlet to Rankine cycle system, the second heat exchanger components 73 First outlet is communicated to the entrance of the second compressor 4.
The present invention is not limited system, the gas that turbine 2 is discharged, and can also first pass through in Rankine cycle system second is changed Thermal part 73 is communicated to the entrance of the second compressor 4 using thermoelectric conversion member 72, i.e., the second heat exchange in Rankine cycle system The first entrance of component 73 is communicated to the outlet of turbine 2, and first outlet is communicated to the entrance of thermoelectric conversion member 72, heat to electricity conversion The outlet of component 72 is to the entrance of the second compressor 4.
The structure and connection relation of other parts in the present embodiment are identical in embodiment one, and details are not described herein.
Embodiment eight
Fig. 9 is please referred to, the difference lies in the coolings in the present embodiment to embodiment seven with embodiment one for the present embodiment Device 7 is will be in the first heat exchanger components 71 in embodiment one, the thermoelectric conversion member 72 and embodiment three in embodiment two Rankine cycle system is combined, i.e., simultaneously using the first heat exchanger components 71, thermoelectric conversion member 72 and Rankine cycle system pair The gas that turbine 2 is discharged is cooled down, while cooling effect is increased, the thermal energy that thermoelectric conversion member 72 can also be absorbed Electric energy output is converted into, the heat that the second heat exchanger components 73 absorb can also further be recycled, to improve energy The utilization rate of amount.
Fig. 9 is please referred to, specifically, the gas that turbine 2 is discharged, first passes through the first heat exchanger components 71, using heat to electricity conversion Component 72 is finally communicated to the entrance of the second compressor 4 by the second heat exchanger components 73 in Rankine cycle system, i.e., first changes The entrance of thermal part 71 is communicated to the outlet of turbine 2, the entrance of outlet to thermoelectric conversion member 72, thermoelectric conversion member 72 Outlet to Rankine cycle system in the second heat exchanger components 73 first entrance, the first outlets of the second heat exchanger components 73 connects Lead to the entrance of the second compressor 4.
The present invention is not limited system, and the gas that turbine 2 is discharged can also first pass through thermoelectric conversion member 72, using First heat exchanger components 71 are finally communicated to the entrance of the second compressor 4 by the second heat exchanger components 73 in Rankine cycle system. Alternatively, the gas that turbine 2 is discharged, first passes through the second heat exchanger components 73 in Rankine cycle system, using the first heat exchanger components 71, the entrance of the second compressor 4 is finally communicated to by thermoelectric conversion member 72.
In the present embodiment, the distributing order packet of the first heat exchanger components 71, thermoelectric conversion member 72 and Rankine cycle system It includes but is not limited to above-mentioned several sequences, the first heat exchanger components 71, thermoelectric conversion member 72 and Rankine cycle system can also be with them He sequentially arranges, and specific distributing order can suitably be adjusted according to actual needs.
The structure and connection relation of other parts in the present embodiment are identical in embodiment one, and details are not described herein.
Embodiment nine
The present embodiment and embodiment one to embodiment seven the difference lies in, the cooling device 7 in the present embodiment be by The first heat exchanger components 71 in embodiment one, the thermoelectric conversion member 72 in embodiment two, the Rankine cycle system in embodiment three Organic rankine cycle system in system and example IV is combined, i.e., simultaneously using the first heat exchanger components 71, heat to electricity conversion portion The gas that part 72, Rankine cycle system and organic rankine cycle system discharge turbine 2 cools down, and is increasing cooling effect Thermal energy at the same time it can also which thermoelectric conversion member 72 is absorbed is converted into electric energy output, can also inhale the second heat exchanger components 73 The heat of receipts is further recycled, to improve the utilization rate of energy.
Specifically, the gas that turbine 2 is discharged, first passes through the first heat exchanger components 71, using thermoelectric conversion member 72, then By Rankine cycle system, the entrance of the second compressor 4 is finally communicated to by organic rankine cycle system.
The present invention is not limited system, and the gas that turbine 2 is discharged can also first pass through thermoelectric conversion member 72, using First heat exchanger components 71 then by Rankine cycle system, are finally communicated to the second compressor 4 by organic rankine cycle system Entrance.
In the present embodiment, the first heat exchanger components 71, thermoelectric conversion member 72, Rankine cycle system and Organic Rankine Cycle The distributing order of system includes but not limited to above-mentioned several sequences, the first heat exchanger components 71, thermoelectric conversion member 72, Rankine cycle System and organic rankine cycle system can also sequentially be arranged with other, specific distributing order can according to be actually needed into The appropriate adjustment of row.
The structure and connection relation of other parts in the present embodiment are identical in embodiment one, and details are not described herein.
In above-described embodiment six, embodiment seven and embodiment eight, the Rankine cycle system in cooling device 7 can also be used Organic rankine cycle system replaces.
The present invention is directed to protect a kind of internal-combustion engine system, two compressors are driven by a shafting simultaneously using single turbine Rotation, one of compressor improve the dynamic property of internal combustion engine, another compressor is used for for forming turbo charge system The inverse Bo Leideng circulatory systems of composition, have further recycled the exhaust energy of internal combustion engine, solve the useless of internal combustion engine in the prior art The problem of gas energy utilization is insufficient, while solve in the prior art since power turbine acting ability is limited, it can not be further The problem of recycling the exhaust energy of internal combustion engine;Compressed action is carried out by single two compressor rotations of turbine drives, is solved In the prior art due to causing whole system structure more complicated using two turbocharging, the matching between two turbines is also very Complexity, cost is higher, the problem of not being suitable for power of IC engine demand little situation.The internal-combustion engine system of the present invention uses Single turbine drives two compressor rotations, while taking into account the plenum of internal combustion engine and exhaust energy comprehensive reutilization, makes Whole system structure is simpler and compact, installation space smaller, cost are lower.The internal-combustion engine system of the present invention, can be with profit Heat exchanger is replaced with thermoelectric material, the thermal energy of exhaust gas is absorbed by thermoelectric material, reduces the temperature of gas, while thermoelectric material The thermal energy of absorption is also converted into electric energy, further improves the recovery utilization rate of the exhaust energy of internal combustion engine.The present invention's is interior Combustion engine system can also be recycled the heat that the heat exchanger in the inverse Bo Leideng circulatory systems absorbs using Rankine cycle system It utilizes, further improves the recovery utilization rate of the exhaust energy of internal combustion engine.
In the description of the present invention, it should be noted that term " first ", " second ", " third ", " the 4th " are only used for retouching Purpose is stated, and it is not intended that instruction or hint relative importance.
It should be understood that the above-mentioned specific embodiment of the present invention is used only for exemplary illustration or explains the present invention's Principle, without being construed as limiting the invention.Therefore, that is done without departing from the spirit and scope of the present invention is any Modification, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.In addition, appended claims purport of the present invention Covering the whole variations fallen into scope and boundary or this range and the equivalent form on boundary and repairing Change example.

Claims (10)

1. a kind of internal-combustion engine system, which is characterized in that including:
Internal combustion engine (1) sets air inlet and exhaust outlet thereon;
Turbine (2), entrance are communicated to the exhaust outlet of the internal combustion engine (1);
First compressor (3), entrance connection air, the outlet of first compressor (3) to the internal combustion engine (1) Air inlet;
Second compressor (4), entrance are communicated to the outlet of the turbine (2), and the outlet of second compressor (4) arrives Air;
The turbine (2) is used for by the first shafting (5) connection coaxial with first compressor (3) and the second compressor (4) First compressor (3) and the second compressor (4) is driven to rotate and carry out compressed action.
2. system according to claim 1, which is characterized in that
The turbine (2) exports power to power plant by first shafting (5).
3. system according to claim 2, which is characterized in that
The power plant is generator or the bent axle of the internal combustion engine (1).
4. system according to claim 1, which is characterized in that further include:
Charge air cooler (6), entrance are communicated to the outlet of first compressor (3), the outlet of the charge air cooler (6) to institute The air inlet of internal combustion engine (1) is stated, for cooling down the gas of the first compressor (3) discharge, and increases the internal combustion engine (1) Density of the induced air.
5. system according to claim 4, which is characterized in that
The charge air cooler (6) is air-cooled or water cooling heat exchanger.
6. system according to claim 1, which is characterized in that further include:
Cooling device (7) is arranged between the turbine (2) and the second compressor (4), for cooling down the turbine (2) row The gas gone out.
7. system according to claim 6, which is characterized in that
The cooling device (7) is the first heat exchanger components (71), thermoelectric conversion member (72), Rankine cycle system and organic Rankine At least one of circulatory system.
8. system according to claim 7, which is characterized in that
The entrance of first heat exchanger components (71) is communicated to the outlet of the turbine (2), first heat exchanger components (71) Outlet to second compressor (4) entrance, for cool down the turbine (2) discharge gas.
9. system according to claim 7, which is characterized in that
The entrance of the thermoelectric conversion member (72) is communicated to the outlet of the turbine (2), and the thermoelectric conversion member (72) goes out Mouth is communicated to the entrance of second compressor (4), for cooling down the gas of the turbine (2) discharge, and by the thermal energy of absorption It is converted into electric energy output.
10. system according to claim 7, which is characterized in that the Rankine cycle system or organic rankine cycle system Including:
Second heat exchanger components (73), first entrance are communicated to the outlet of the turbine (2), second heat exchanger components (73) First outlet is communicated to the entrance of second compressor (4);
Steam turbine (74), entrance are communicated to the second outlet of second heat exchanger components (73);
Third heat exchanger components (75), entrance are communicated to the outlet of the steam turbine (74);
It pumps (76), entrance is communicated to the outlet of the third heat exchanger components (75), and the outlet of the pump (76) is described in The second entrance of second heat exchanger components (73);
The steam turbine (74) exports power by the second shafting (77);
The Rankine cycle system or organic rankine cycle system are used to cool down the gas of the turbine (2) discharge, while will inhale The heat of receipts is converted into power output.
CN201711275722.8A 2017-12-06 2017-12-06 A kind of internal-combustion engine system Pending CN108150278A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711275722.8A CN108150278A (en) 2017-12-06 2017-12-06 A kind of internal-combustion engine system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711275722.8A CN108150278A (en) 2017-12-06 2017-12-06 A kind of internal-combustion engine system

Publications (1)

Publication Number Publication Date
CN108150278A true CN108150278A (en) 2018-06-12

Family

ID=62465977

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711275722.8A Pending CN108150278A (en) 2017-12-06 2017-12-06 A kind of internal-combustion engine system

Country Status (1)

Country Link
CN (1) CN108150278A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101169067A (en) * 2006-10-24 2008-04-30 依维柯发动机研究公司 Engine apparatus with heat recovery system and relative heat recovery method
CN102165158A (en) * 2008-09-26 2011-08-24 雷诺卡车公司 Power assembly, especially for an automotive vehicle
CN104632357A (en) * 2014-12-30 2015-05-20 清华大学 Two-stage supercharging system of internal combustion engine
DE102015215518A1 (en) * 2015-08-14 2017-02-16 Bayerische Motoren Werke Aktiengesellschaft System for recovering energy from the exhaust gas of an internal combustion engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101169067A (en) * 2006-10-24 2008-04-30 依维柯发动机研究公司 Engine apparatus with heat recovery system and relative heat recovery method
CN102165158A (en) * 2008-09-26 2011-08-24 雷诺卡车公司 Power assembly, especially for an automotive vehicle
CN104632357A (en) * 2014-12-30 2015-05-20 清华大学 Two-stage supercharging system of internal combustion engine
DE102015215518A1 (en) * 2015-08-14 2017-02-16 Bayerische Motoren Werke Aktiengesellschaft System for recovering energy from the exhaust gas of an internal combustion engine

Similar Documents

Publication Publication Date Title
CN108868930B (en) Supercritical/transcritical carbon dioxide combined cycle power generation system utilizing waste heat of internal combustion engine
CN103233820B (en) Caes and the integrated power generation system of combined cycle
CN104265502A (en) Combined-type diesel engine waste heat energy recycling system
CN203374333U (en) Power generation system capable of stabilizing electricity peak-valley fluctuation
WO2015096414A1 (en) High-pressure reheating gas-steam combined cycle power generation system and power generation method
CN108374714A (en) A kind of Organic Rankine Cycle plenum internal-combustion engine system and method
CN110173347B (en) Waste heat recycling system of coal mine in-use equipment and operation method
CN103670558A (en) Internal combustion engine waste heat recovery system adopting double-pressure multistage expansion reheating
CN104265500A (en) High-temperature waste heat recovery system for diesel engine
CN106048118B (en) blast furnace gas recycling system
CN103397933B (en) Extreme heat machine and method of work thereof
CN108457744A (en) A kind of engine exhaust heat recovery system of equipment mechanical-electric coupling booster
CN108087103A (en) A kind of internal-combustion engine system
CN104929805A (en) Vehicle engine waste heat recycling device using reheat type organic Rankine cycle technology
CN108167053A (en) A kind of internal-combustion engine system
CN213807777U (en) Coupling system of thermal power generation system and compressed air energy storage system
CN207420711U (en) The energy-recuperation system of asymmetric double runner turbocharged engine
CN211777669U (en) Engine exhaust gas energy circulation structure
CN111734549A (en) Circulating system and method for waste heat recovery of EGR diesel engine
CN208380648U (en) A kind of association circulating power generation system of the double pressure supercritical carbon dioxide waste heat boilers of band
CN108087102A (en) A kind of internal-combustion engine system
CN110107384A (en) A kind of energy recovery utilizing system being classified separation output based on low speed machine exhaust energy
CN107605618B (en) Cogeneration unit with heat energy recovery system
CN108150278A (en) A kind of internal-combustion engine system
CN108716435A (en) A kind of pressurization system of internal combustion engine of integrated waste heat recovery

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20180612