CN102155290A - Auxiliary combustion-engine type pressurization system for restoring plateau power of internal-combustion engine - Google Patents
Auxiliary combustion-engine type pressurization system for restoring plateau power of internal-combustion engine Download PDFInfo
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- 238000002485 combustion reaction Methods 0.000 title claims abstract description 81
- 238000002347 injection Methods 0.000 claims abstract description 10
- 239000007924 injection Substances 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 3
- 239000007789 gas Substances 0.000 claims 11
- 238000010304 firing Methods 0.000 claims 7
- 239000000567 combustion gas Substances 0.000 claims 5
- 239000000295 fuel oil Substances 0.000 claims 4
- 230000008676 import Effects 0.000 claims 3
- 239000002912 waste gas Substances 0.000 claims 2
- 230000006835 compression Effects 0.000 claims 1
- 238000007906 compression Methods 0.000 claims 1
- 239000002737 fuel gas Substances 0.000 claims 1
- 239000010705 motor oil Substances 0.000 claims 1
- 230000001105 regulatory effect Effects 0.000 claims 1
- 230000002708 enhancing effect Effects 0.000 abstract 1
- 239000000446 fuel Substances 0.000 description 13
- 238000011084 recovery Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
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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
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/32—Engines with pumps other than of reciprocating-piston type
- F02B33/34—Engines with pumps other than of reciprocating-piston type with rotary pumps
- F02B33/40—Engines with pumps other than of reciprocating-piston type with rotary pumps of non-positive-displacement type
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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
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/44—Passages conducting the charge from the pump to the engine inlet, e.g. reservoirs
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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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
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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
- F02D2200/00—Input parameters for engine control
- F02D2200/70—Input parameters for engine control said parameters being related to the vehicle exterior
- F02D2200/703—Atmospheric pressure
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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
- F02D41/0002—Controlling intake air
- F02D41/0007—Controlling intake air for control of turbo-charged or super-charged engines
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Combustion & Propulsion (AREA)
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Abstract
Description
技术领域technical field
本发明涉及一种用于恢复内燃机高原动力的燃机型辅助增压系统,属于热力发动机技术领域。The invention relates to a gas-fired auxiliary supercharging system for recovering plateau power of an internal-combustion engine, which belongs to the technical field of heat engines.
背景技术Background technique
采用废气涡轮增压技术是目前恢复内燃机高原动力的最有效方法之一。普通单级涡轮增压系统可以在一定海拔范围内恢复内燃机的功率。这是因为,当海拔升高时,由于排气背压降低,涡轮膨胀比和涡轮前废气温度均增加,涡轮进口气体能量的增加导致涡轮输出功的增加,从而提高了涡轮增压器的转速,这样就会使压气机形成较高的增压压力,压比升高,补偿因海拔升高所产生的进气量减少,体现了涡轮增压的自动补偿能力。但是在更高海拔范围内,受增压器压比、转速和流量范围的限制,会出现内燃机进气量不足、功率下降、增压器转速升高、工作点进入非工作区等现象。若在更高海拔范围内恢复内燃机功率,则需要采用具有更高压比和流量范围的增压系统。The use of exhaust gas turbocharging technology is currently one of the most effective methods to restore the plateau power of the internal combustion engine. Ordinary single-stage turbocharging systems can restore the power of the internal combustion engine within a certain range of altitudes. This is because, when the altitude increases, due to the decrease of the exhaust back pressure, the expansion ratio of the turbine and the temperature of the exhaust gas before the turbine both increase, and the increase of the gas energy at the inlet of the turbine leads to an increase of the output work of the turbine, thereby increasing the speed of the turbocharger , so that the compressor will form a higher boost pressure, and the pressure ratio will increase, compensating for the reduction of intake air due to the increase in altitude, which reflects the automatic compensation ability of turbocharging. However, at a higher altitude range, limited by the pressure ratio, speed and flow range of the turbocharger, there will be insufficient air intake of the internal combustion engine, power reduction, increased turbocharger speed, and the operating point entering the non-working area. Restoring combustion engine power at higher altitudes requires a booster system with a higher pressure ratio and flow range.
二级增压系统作为优势明显的一种高增压系统,广泛地应用于军用及民用领域大功率柴油发动机。二级涡轮增压系统就是把两个涡轮增压器和柴油机在气路上串联起来。这种方法可保证整个系统具有较高的增压压力,而每一级增压器的增压比较低,压气机可以在宽流量范围、高效率区内稳定地工作。从而使涡轮增压器的可靠性提高,噪声降低,对环境温度和压力变化不敏感。但是这种增压系统在结构上需要布置两台增压器,以及它们之间的调节机构、连接管路等,这不仅需要对原有内燃机结构做出很大改动,同时也增加了有限空间内部件紧凑布置的难度;另外,对于采用二级增压系统的内燃机,在任何海拔高度下增压系统中的两级增压器都要同时投入工作,要有一定的实时调节策略控制每级增压器的运行,这对在低海拔地区或仅需要单级增压器就可以满足内燃机增压要求的情况来说,无疑增加了内燃机工作运行的复杂性。更重要的是,针对高海拔恢复功率的二级增压系统匹配和以平原工作性能提高为目的的增压系统匹配参数是完全不同的,难以兼顾。As a high-pressure supercharging system with obvious advantages, the two-stage supercharging system is widely used in high-power diesel engines in military and civilian fields. The two-stage turbocharging system is to connect two turbochargers and diesel engines in series on the air circuit. This method can ensure that the entire system has a high boost pressure, while the boost pressure of each stage of the supercharger is relatively low, and the compressor can work stably in a wide flow range and high efficiency area. As a result, the reliability of the turbocharger is improved, the noise is reduced, and it is insensitive to changes in ambient temperature and pressure. However, this supercharger system needs to arrange two superchargers in structure, as well as the adjustment mechanism and connecting pipelines between them, which not only requires great changes to the original internal combustion engine structure, but also increases the limited space. The difficulty of compact arrangement of internal components; in addition, for internal combustion engines using a two-stage supercharger system, the two-stage superchargers in the supercharger system must be put into operation at the same time at any altitude, and there must be a certain real-time adjustment strategy to control each stage. The operation of the supercharger undoubtedly increases the complexity of the operation of the internal combustion engine in low-altitude areas or when only a single-stage supercharger is required to meet the supercharging requirements of the internal combustion engine. More importantly, the matching parameters of the two-stage supercharging system for recovering power at high altitudes and the matching parameters of the supercharging system for the purpose of improving work performance on plains are completely different, and it is difficult to balance them.
发明内容Contents of the invention
本发明的目的是为了克服上述现有技术的不足,设计了一种带有辅助压气机和燃气动力装置的恢复内燃机高原动力的辅助增压系统。当内燃机在高海拔地区运行时,加装该辅助增压系统,通过主增压系统和辅助增压系统来恢复内燃机的功率;而内燃机在低海拔地区运行时,仅使用主增压系统与内燃机正常匹配工作。The purpose of the present invention is in order to overcome above-mentioned deficiencies in the prior art, has designed a kind of auxiliary pressurization system with the recovery internal combustion engine plateau power of auxiliary compressor and gas power plant. When the internal combustion engine operates at high altitudes, the auxiliary supercharging system is installed to recover the power of the internal combustion engine through the main supercharging system and the auxiliary supercharging system; when the internal combustion engine operates at low altitudes, only the main supercharging system and the internal combustion engine are used Normal matching works.
本发明的目的是通过下述技术方案实现的。The purpose of the present invention is achieved through the following technical solutions.
本发明用于恢复内燃机高原动力的燃机型辅助增压系统主要包括:辅助空滤器,辅助增压压气机,辅助燃烧压气机,辅助涡轮,电磁阀喷油装置,燃烧室,点火装置,起动与控制系统,切换阀;其中辅助增压压气机、辅助燃烧压气机和辅助涡轮同轴连接,辅助空滤器进口与大气相连通,辅助增压压气机进口、辅助燃烧压气机进口与辅助空滤器出口连通,电磁阀喷油装置为燃烧室提供燃油,燃烧室进口与辅助燃烧压气机出口连通,辅助涡轮进口与燃烧室出口连通,辅助涡轮出口与大气连通,两位三通切换阀分别与辅助增压压气机出口、大气和主增压系统进口连通;内燃机工作在高海拔地区时采用高压空气供给燃烧室直接起动辅助增压系统,新鲜空气首先通过辅助空滤器后,分别进入辅助增压压气机和辅助燃烧压气机压缩,燃油通过电磁阀喷油装置喷入到燃烧室中,经过雾化的燃油与来自辅助燃烧压气机的压缩空气混合,由燃烧室点火装置将油气混合物点燃,产生的高温燃气推动辅助涡轮膨胀做功,以驱动辅助增压压气机和辅助燃烧压气机,由辅助增压压气机流出的压缩空气流经切换阀和空滤器后,进入到压气机被进一步压缩,然后经过中冷器冷却降低空气的温度和体积流量,最后空气进入内燃机与燃油混合燃烧,燃烧产生的高温废气进入到主增压系统的涡轮膨胀做功,以驱动其压气机,经过涡轮膨胀后的废气排入大气。The gas-fired auxiliary supercharging system used to recover the plateau power of the internal combustion engine in the present invention mainly includes: auxiliary air filter, auxiliary booster compressor, auxiliary combustion compressor, auxiliary turbine, solenoid valve fuel injection device, combustion chamber, ignition device, starting It is connected with the control system and switching valve; the auxiliary booster compressor, auxiliary combustion compressor and auxiliary turbine are coaxially connected, the inlet of the auxiliary air filter is connected with the atmosphere, the inlet of the auxiliary booster compressor, the inlet of the auxiliary combustion compressor and the auxiliary air filter The outlet is connected, and the solenoid valve fuel injection device provides fuel for the combustion chamber. The outlet of the booster compressor is connected to the inlet of the main booster system; when the internal combustion engine is working at a high altitude, high-pressure air is used to supply the combustion chamber to directly start the auxiliary booster system. The fresh air first passes through the auxiliary air filter and then enters the auxiliary booster compressor respectively Compressed by the engine and the auxiliary combustion compressor, the fuel is sprayed into the combustion chamber through the solenoid valve fuel injection device, the atomized fuel is mixed with the compressed air from the auxiliary combustion compressor, and the fuel-air mixture is ignited by the combustion chamber ignition device to generate The high-temperature gas pushes the auxiliary turbine to expand and do work to drive the auxiliary booster compressor and the auxiliary combustion compressor. The compressed air flowing out of the auxiliary booster compressor flows through the switching valve and the air filter, enters the compressor to be further compressed, and then passes through the The intercooler cools down the temperature and volume flow of the air. Finally, the air enters the internal combustion engine and is mixed with fuel for combustion. The high-temperature exhaust gas generated by the combustion enters the turbine of the main supercharging system to expand and do work to drive its compressor. The exhaust gas after the expansion of the turbine is exhausted. into the atmosphere.
切换阀是两位三通阀,主增压系统进气口通过此阀的切换实现与大气或者辅助增压压气机相通。The switching valve is a two-position three-way valve, and the air inlet of the main booster system communicates with the atmosphere or the auxiliary booster compressor through the switching of this valve.
燃机型辅助增压系统作为标准配置直接安装在用于高原的专用车辆上,或作为辅助装置临时安装在进入高原地区工作的非专用车辆上。As a standard configuration, the gas-fired auxiliary booster system is directly installed on special vehicles used in plateaus, or temporarily installed as an auxiliary device on non-specialized vehicles working in plateau areas.
驱动辅助增压压气机的动力来源于与其同轴的燃气轮机。The power to drive the auxiliary booster compressor comes from the gas turbine coaxial with it.
燃机型辅助增压系统具有单独的控制器,根据增压压力调节系统的工作状况。The auxiliary boost system of the gas-fired type has a separate controller, which adjusts the working condition of the system according to the boost pressure.
燃机型辅助增压系统的起动采用高压空气供给燃烧室直接起动方式。The start-up of the auxiliary booster system of the gas-fired type adopts the direct start-up method of supplying high-pressure air to the combustion chamber.
本发明的有益效果是:车辆在平原地区工作时,完全不受高原恢复功率装置的影响;随着车辆行驶海拔高度的提高,主增压系统可以在一定范围内单独工作恢复内燃机的高原动力,也可以联合辅助增压系统共同工作,恢复内燃机的功率;辅助增压系统可以自由拆装,能够达到简化发动机机舱布置,增加运行可靠性,结构简单紧凑的目的。The beneficial effect of the present invention is that: when the vehicle is working in a plain area, it is not affected by the plateau recovery power device at all; as the altitude of the vehicle is increased, the main supercharging system can work independently within a certain range to recover the plateau power of the internal combustion engine, It can also work together with the auxiliary supercharging system to restore the power of the internal combustion engine; the auxiliary supercharging system can be disassembled freely, which can achieve the purpose of simplifying the layout of the engine room, increasing the reliability of operation, and having a simple and compact structure.
附图说明Description of drawings
图1是本发明实施方案的系统示意图。Figure 1 is a system schematic diagram of an embodiment of the present invention.
图中:1-辅助空滤器2-辅助增压压气机3-辅助燃烧压气机4-辅助涡轮5-电磁阀喷油装置6-燃烧室7-点火装置8-起动与控制系统9-切换阀10-空滤器11-压气机12-中冷器13-内燃机14-涡轮In the figure: 1-auxiliary air filter 2-auxiliary booster compressor 3-auxiliary combustion compressor 4-auxiliary turbine 5-solenoid valve fuel injection device 6-combustion chamber 7-ignition device 8-starting and control system 9-switching valve 10-air filter 11-compressor 12-intercooler 13-internal combustion engine 14-turbine
具体实施方式Detailed ways
为了更好地说明本发明的目的与优点,下面结合具体实施例对本发明内容作进一步说明。In order to better illustrate the purpose and advantages of the present invention, the content of the present invention will be further described below in conjunction with specific examples.
如图1所示,本发明的恢复内燃机高原动力的燃机型辅助增压系统主要包括辅助空滤器1,辅助增压压气机2,辅助燃烧压气机3,辅助涡轮4,电磁阀喷油装置5,燃烧室6,点火装置7,起动与控制系统8,切换阀9。主增压系统主要包括空滤器10,压气机11,中冷器12,内燃机13,涡轮14。As shown in Figure 1, the gas-fired auxiliary supercharging system for recovering the plateau power of the internal combustion engine of the present invention mainly includes an
内燃机工作在低海拔地区时,切换阀9仅使大气与空滤器10连通,依靠主增压系统(图1中虚线区域)与内燃机13正常匹配和工作,其工作原理与普通增压内燃机无异。When the internal combustion engine works at a low altitude, the switching valve 9 only connects the atmosphere with the
当内燃机工作在高海拔地区时,采用高压空气供给燃烧室6直接起动辅助增压系统,新鲜空气首先通过辅助空滤器1后,分别进入辅助增压压气机2和辅助燃烧压气机3,经过压缩后,空气温度和压力得到提高。燃油通过电磁阀喷油装置5喷入到燃烧室6中,经过雾化的燃油与来自辅助燃烧压气机3的压缩空气混合,由燃烧室点火装置7将油气混合物点燃,产生的高温燃气推动辅助涡轮4膨胀做功,以驱动辅助增压压气机2和辅助燃烧压气机3,控制系统8根据增压压力调节辅助增压系统的工作状况。由辅助增压压气机2流出的压缩空气流经切换阀9和空滤器10后,进入到压气机11被进一步压缩,温度和压力继续提高,然后经过中冷器12冷却,降低空气的温度和体积流量。经过这样的增压过程后,空气进入内燃机13与燃油混合燃烧,燃烧产生的高温废气进入到主增压系统的涡轮14膨胀做功,以驱动其压气机11,经过涡轮14膨胀后的废气排入大气。When the internal combustion engine is working in a high-altitude area, high-pressure air is used to supply the combustion chamber 6 to directly start the auxiliary supercharging system. After the fresh air first passes through the
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CN102434333A (en) * | 2011-11-25 | 2012-05-02 | 河南柴油机重工有限责任公司 | Auxiliary pressurization system for diesel engine bench test and its application method |
WO2015145083A1 (en) * | 2014-03-26 | 2015-10-01 | Societe De Motorisations Aeronautiques | Closed-cycle heat engine for an aircraft, and method for controlling the air supply thereof |
CN106285917A (en) * | 2016-08-05 | 2017-01-04 | 同济大学 | A kind of diesel engine starting aid system being applicable to high altitude localities and method |
US10774712B2 (en) | 2015-12-14 | 2020-09-15 | Volvo Truck Corporation | Internal combustion engine system and an exhaust treatment unit for such a system |
US10995657B2 (en) * | 2017-12-20 | 2021-05-04 | John Manley McDonald | Externally powered turbine for an internal combustion engine |
CN113790100A (en) * | 2021-08-20 | 2021-12-14 | 清华大学 | Diesel power generation unit and hybrid vehicle |
CN114087054A (en) * | 2021-12-25 | 2022-02-25 | 上海毅合捷汽车科技有限公司 | Combined circulating system of internal combustion engine and micro gas turbine |
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CN102434333A (en) * | 2011-11-25 | 2012-05-02 | 河南柴油机重工有限责任公司 | Auxiliary pressurization system for diesel engine bench test and its application method |
CN102434333B (en) * | 2011-11-25 | 2013-09-25 | 河南柴油机重工有限责任公司 | Auxiliary pressurization system for diesel engine bench test and using method of auxiliary pressurization system |
WO2015145083A1 (en) * | 2014-03-26 | 2015-10-01 | Societe De Motorisations Aeronautiques | Closed-cycle heat engine for an aircraft, and method for controlling the air supply thereof |
FR3019228A1 (en) * | 2014-03-26 | 2015-10-02 | Motorisations Aeronautiques | FIRM CYCLE THERMAL MOTOR FOR AIRCRAFT AND METHOD FOR CONTROLLING ITS AIR SUPPLY |
US10774712B2 (en) | 2015-12-14 | 2020-09-15 | Volvo Truck Corporation | Internal combustion engine system and an exhaust treatment unit for such a system |
CN106285917A (en) * | 2016-08-05 | 2017-01-04 | 同济大学 | A kind of diesel engine starting aid system being applicable to high altitude localities and method |
US10995657B2 (en) * | 2017-12-20 | 2021-05-04 | John Manley McDonald | Externally powered turbine for an internal combustion engine |
CN113790100A (en) * | 2021-08-20 | 2021-12-14 | 清华大学 | Diesel power generation unit and hybrid vehicle |
CN114087054A (en) * | 2021-12-25 | 2022-02-25 | 上海毅合捷汽车科技有限公司 | Combined circulating system of internal combustion engine and micro gas turbine |
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