[go: up one dir, main page]

CN1563681A - Igniting combustion system of engine preburning chamber - Google Patents

Igniting combustion system of engine preburning chamber Download PDF

Info

Publication number
CN1563681A
CN1563681A CNA2004100214327A CN200410021432A CN1563681A CN 1563681 A CN1563681 A CN 1563681A CN A2004100214327 A CNA2004100214327 A CN A2004100214327A CN 200410021432 A CN200410021432 A CN 200410021432A CN 1563681 A CN1563681 A CN 1563681A
Authority
CN
China
Prior art keywords
combustion chamber
chamber
combustion
main
fuel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CNA2004100214327A
Other languages
Chinese (zh)
Other versions
CN1316154C (en
Inventor
隆武强
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.)
Dalian University of Technology
Original Assignee
Dalian University of Technology
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 Dalian University of Technology filed Critical Dalian University of Technology
Priority to CNB2004100214327A priority Critical patent/CN1316154C/en
Publication of CN1563681A publication Critical patent/CN1563681A/en
Application granted granted Critical
Publication of CN1316154C publication Critical patent/CN1316154C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • 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

Landscapes

  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

一种可采用高压缩比和高空燃比的点燃式发动机预燃室燃烧系统,其属于发动机混合气形成和燃烧领域。由于安装在预燃室内的多孔喷嘴喷出的辅燃料束只在预燃室内形成过浓混合气,而主燃料束只在主燃烧室内形成稀混合气,尽管采用了较高的压缩比,但总的空燃比很大,在保证点燃的情况下,改善了发动机的经济性和排气污染。

Figure 200410021432

An ignition type engine pre-combustion chamber combustion system capable of adopting high compression ratio and high air-fuel ratio belongs to the field of engine mixture gas formation and combustion. Since the auxiliary fuel beam injected by the porous nozzle installed in the pre-combustion chamber only forms a rich mixture in the pre-combustion chamber, while the main fuel beam only forms a lean mixture in the main combustion chamber, although a higher compression ratio is adopted, the The total air-fuel ratio is very large, and the economy and exhaust pollution of the engine are improved under the condition of ensuring ignition.

Figure 200410021432

Description

点燃式发动机预燃室燃烧系统Ignition Engine Pre-chamber Combustion System

技术领域technical field

本发明涉及一种可采用高压缩比和高空燃比的点燃式发动机预燃室燃烧系统,其属于发动机混合气形成和燃烧领域。The invention relates to an ignition type engine pre-combustion chamber combustion system capable of adopting high compression ratio and high air-fuel ratio, which belongs to the field of engine mixture gas formation and combustion.

背景技术Background technique

众所周知,汽油或LPG等气体燃料较难自燃,故这类燃料发动机一直采用均质混合气并用外源点燃的燃烧方式。这样就存在两个问题:一是工作时混合气范围窄,α=0.6~1.2(A/F=9~18),并且常在α<1的浓混合气下工作,必然使发动机经济性差,并生成大量CO;二是理论和实践都已证明,提高压缩比是提高这类发动机热效率最有效的方法,但受到爆燃等不正常燃烧和排气污染的限制。目前点燃式发动机的有效热效率远不如压燃式的柴油机。为了解决点燃式发动机经济性和排气污染的问题,研究点燃式发动机采用新的燃烧方式是十分重要的。As we all know, gaseous fuels such as gasoline or LPG are difficult to spontaneously ignite, so this type of fuel engine has always used a combustion method of homogeneous mixture and ignited by an external source. In this way, there are two problems: one is that the mixture gas range is narrow during operation, α=0.6~1.2 (A/F=9~18), and it often works under the rich mixture gas of α<1, which will inevitably make the engine economical. And generate a large amount of CO; Second, both theory and practice have proved that increasing the compression ratio is the most effective way to improve the thermal efficiency of this type of engine, but it is limited by abnormal combustion such as deflagration and exhaust pollution. The effective thermal efficiency of current ignition engines is far inferior to that of compression ignition diesel engines. In order to solve the problems of ignition engine economy and exhaust pollution, it is very important to study new combustion methods for ignition engines.

发明内容Contents of the invention

为了解决上述点燃式发动机混合气浓度范围窄和不能采用较高压缩比的问题,本发明提供一种点燃式发动机预燃室燃烧系统,该燃烧系统采用高压缩比和高空燃比,采用质调节,利用局部瞬时的低空燃比,确保正常点燃和迅速燃烧,以达到提高点燃式发动机的热效率和降低排气污染的目的。In order to solve the above-mentioned problems of narrow concentration range of the ignition-type engine mixture and the inability to adopt a higher compression ratio, the present invention provides a pre-combustion chamber combustion system of the ignition-type engine, which adopts a high compression ratio and a high air-fuel ratio, and adopts mass regulation, The local instantaneous low air-fuel ratio is used to ensure normal ignition and rapid combustion, so as to achieve the purpose of improving the thermal efficiency of the ignition engine and reducing exhaust pollution.

本发明解决其技术问题所采用的技术方案是:一种点燃式发动机预燃室燃烧系统,它主要由一个气缸盖、活塞和气缸套组成的主燃烧室和一个设在气缸盖内的预燃室组成。一个多孔喷嘴伸入预燃室中,喷嘴喷出的燃料由辅燃料束和主燃料束组成,主燃料束直接从预燃室的出口进入主燃烧室,装在预燃室中的火花塞极易点燃由辅燃料束在预燃室内形成的过浓混合气,燃烧着的高温高压燃气经预燃室出口冲入主燃烧室,点燃由主燃料束在主燃烧室内形成的稀混合气,实现高压缩比和高空燃比的混合气迅速完全燃烧。这种燃烧系统的压缩比为9-20,,空燃比为16-40。The technical solution adopted by the present invention to solve the technical problems is: a kind of ignition type engine pre-combustion chamber combustion system, which mainly consists of a main combustion chamber composed of a cylinder head, a piston and a cylinder liner, and a pre-combustion chamber located in the cylinder head. room composition. A porous nozzle protrudes into the pre-chamber, and the fuel ejected from the nozzle is composed of auxiliary fuel beam and main fuel beam. The main fuel beam directly enters the main combustion chamber from the outlet of the pre-chamber, and the spark plug installed in the pre-chamber is very easy Ignite the over-rich mixture formed by the auxiliary fuel beam in the pre-combustion chamber, the burning high-temperature and high-pressure gas rushes into the main combustion chamber through the outlet of the pre-combustion chamber, and ignite the lean mixture formed by the main fuel beam in the main combustion chamber to achieve high The mixture with high compression ratio and high air-fuel ratio burns quickly and completely. The compression ratio of this combustion system is 9-20, and the air-fuel ratio is 16-40.

上述技术方案的指导思想是:辅燃料束在火花塞周围形成极易点燃的浓混合气,在预燃室内形成一次混合和燃烧,燃烧产生的高温高压燃气冲入主燃烧室,形成二次混合和燃烧,由于此时活塞已越过上止点开始下行,有效地控制了最高燃烧压力。The guiding ideology of the above-mentioned technical solution is: the auxiliary fuel bundle forms a highly ignitable rich mixture around the spark plug, forms primary mixing and combustion in the pre-combustion chamber, and the high-temperature and high-pressure gas generated by combustion rushes into the main combustion chamber to form secondary mixing and combustion. Combustion, since the piston has crossed the top dead center and started to descend, the maximum combustion pressure is effectively controlled.

本发明的有益效果是:由于安装在预燃室内的多孔喷嘴喷出的辅燃料束只在预燃室内形成过浓混合气,而主燃料束只在主燃烧室内形成稀混合气,尽管采用了较高的压缩比,但总的空燃比很大,在保证点燃的情况下,改善了发动机的经济性和排气污染。试验证明:压缩比为14,总空燃比为21时,燃油消耗率有明显下降,甚至比分隔式燃烧室的柴油机还好,污染可达欧洲III标准。The beneficial effect of the present invention is: because the secondary fuel jet sprayed by the multi-hole nozzle installed in the pre-combustion chamber only forms a rich mixture in the pre-combustion chamber, and the main fuel jet only forms a lean mixture in the main combustion chamber. Higher compression ratio, but the total air-fuel ratio is large, which improves the engine's economy and exhaust pollution under the condition of ensuring ignition. The test proves that: when the compression ratio is 14 and the total air-fuel ratio is 21, the fuel consumption rate is significantly reduced, even better than that of a diesel engine with a separate combustion chamber, and the pollution can reach the European III standard.

附图说明Description of drawings

下面结合附图和实施例对本发明作进一步说明。The present invention will be further described below in conjunction with drawings and embodiments.

图1是点燃式发动机预燃室燃烧系统一个实施例的纵剖面构造图。Fig. 1 is a longitudinal sectional view of an embodiment of an ignition engine pre-chamber combustion system.

图2是预燃室部分的放大视图。Figure 2 is an enlarged view of the pre-chamber section.

图中:1、气缸盖,2、活塞,3、气缸套,4、主燃烧室,5、预燃室,6、火花塞,7、镶体,8、喷嘴,9、预燃室镶块,10、辅燃料束,11、预燃室出口,12、主燃料束。In the figure: 1. Cylinder head, 2. Piston, 3. Cylinder liner, 4. Main combustion chamber, 5. Precombustion chamber, 6. Spark plug, 7. Inlay, 8. Nozzle, 9. Precombustion chamber insert, 10, auxiliary fuel bundle, 11, pre-chamber outlet, 12, main fuel bundle.

具体实施方式Detailed ways

在图1、2所示的实施例中,由气缸盖1、活塞2和气缸套3组成一个主燃烧室4,在气缸盖1内设有一个预燃室5,预燃室5由镶块9的内腔和预燃室镶体7的下部组合而成,镶块9下部设有预燃室出口11。火花塞6和喷嘴8安装在镶体7上,但头部都伸入预燃室5内,喷嘴8喷出的辅燃料束只在预燃室5内形成浓混合气,以利于火花塞6点燃,而主燃料束直接射向预燃室出口11并进入主燃烧室4形成稀薄混合气。该实施例采用的压缩比为14,总空燃比为21。In the embodiment shown in Figures 1 and 2, a main combustion chamber 4 is formed by the cylinder head 1, the piston 2 and the cylinder liner 3, and a pre-combustion chamber 5 is arranged in the cylinder head 1, and the pre-combustion chamber 5 is composed of an insert The inner cavity of 9 is combined with the bottom of pre-chamber inlay 7, and the bottom of inlay 9 is provided with pre-chamber outlet 11. The spark plug 6 and the nozzle 8 are installed on the inlay 7, but the heads all extend into the pre-combustion chamber 5, and the auxiliary fuel beam sprayed by the nozzle 8 only forms a rich mixture in the pre-combustion chamber 5, so as to facilitate the ignition of the spark plug 6. And the main fuel beam directly shoots to the pre-chamber outlet 11 and enters the main combustion chamber 4 to form a lean mixture. This example uses a compression ratio of 14 and an overall air-fuel ratio of 21.

Claims (2)

1.一种点燃式发动机预燃室燃烧系统,它主要由一个气缸盖(1)、活塞(2)和气缸套(3)组成的主燃烧室(4)和一个设在气缸盖(1)内的预燃室(5)组成,其特征在于:一个多孔喷嘴(8)伸入预燃室(5)中,喷嘴(8)喷出的燃料束由辅燃料束(10)和主燃料束(12)组成,主燃料束(12)直接从预燃室出口(11)进入主燃烧室(4),装在预燃室(5)中的火花塞(6)极易点燃由辅燃料束(10)在预燃室(5)中形成的过浓混合气,燃烧着的高温高压燃气经预燃室出口(11)冲入主燃烧室(4),点燃由主燃料束(12)在主燃烧室(4)形成的稀混合气,实现高压缩比和高空燃比的混合气迅速完全燃烧。1. A kind of ignition type engine pre-combustion chamber combustion system, it is mainly composed of a cylinder head (1), piston (2) and cylinder liner (3) main combustion chamber (4) and a cylinder head (1) The inner pre-chamber (5) is composed of, and it is characterized in that: a porous nozzle (8) stretches in the pre-chamber (5), and the fuel bundle ejected from the nozzle (8) is composed of auxiliary fuel bundle (10) and main fuel bundle (12) form, main fuel beam (12) directly enters main combustion chamber (4) from pre-chamber outlet (11), and the spark plug (6) that is contained in the pre-chamber (5) is very easy to ignite by auxiliary fuel beam ( 10) The over-rich mixture formed in the pre-combustion chamber (5), the burning high-temperature and high-pressure gas rushes into the main combustion chamber (4) through the pre-combustion chamber outlet (11), and is ignited by the main fuel beam (12) in the main combustion chamber. The lean mixture formed in the combustion chamber (4) realizes rapid and complete combustion of the mixture with high compression ratio and high air-fuel ratio. 2.据权利要求1所述的点燃式发动机预燃室燃烧系统,其特征在于:压缩比为9-20,,空燃比为16-40。2. The ignition type engine pre-combustion chamber combustion system according to claim 1, characterized in that: the compression ratio is 9-20, and the air-fuel ratio is 16-40.
CNB2004100214327A 2004-03-18 2004-03-18 Igniting combustion system of engine preburning chamber Expired - Fee Related CN1316154C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2004100214327A CN1316154C (en) 2004-03-18 2004-03-18 Igniting combustion system of engine preburning chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2004100214327A CN1316154C (en) 2004-03-18 2004-03-18 Igniting combustion system of engine preburning chamber

Publications (2)

Publication Number Publication Date
CN1563681A true CN1563681A (en) 2005-01-12
CN1316154C CN1316154C (en) 2007-05-16

Family

ID=34479819

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2004100214327A Expired - Fee Related CN1316154C (en) 2004-03-18 2004-03-18 Igniting combustion system of engine preburning chamber

Country Status (1)

Country Link
CN (1) CN1316154C (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101858245A (en) * 2010-04-28 2010-10-13 大连理工大学 Large Gas Fuel Engine Combustion System
CN102953800A (en) * 2012-11-07 2013-03-06 镇江恒驰科技有限公司 Ignition method of pre-combustion chamber of diesel-dual-fuel engine
CN103422970A (en) * 2013-07-17 2013-12-04 广州柴油机厂股份有限公司 Ignition device of gas engine utilizing precombustion chamber
CN106103933A (en) * 2014-03-13 2016-11-09 瓦锡兰芬兰有限公司 Pre-chamber arrangement, cylinder head and piston engine
CN107091145A (en) * 2017-06-07 2017-08-25 哈尔滨工程大学 A kind of precombustion chamber of marine large-diameter gas engine
CN110486142A (en) * 2018-05-15 2019-11-22 通用汽车环球科技运作有限责任公司 Variable volume pre-chambers for internal combustion engines
CN112211714A (en) * 2020-11-27 2021-01-12 山东交通学院 A gas engine shock-assisted pre-combustion chamber structure

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4204484A (en) * 1975-06-24 1980-05-27 Toyota Jidosha Kogyo Kabushiki Kaisha Auxiliary combustion chamber of internal combustion engine
JPS61182416A (en) * 1985-02-07 1986-08-15 Mitsubishi Motors Corp Subchamber type combustion chamber
DE10217996A1 (en) * 2002-04-23 2003-11-13 Man B & W Diesel Ag Self-igniting mixture-compressing internal combustion engine and method for its operation
CN2570482Y (en) * 2002-09-29 2003-09-03 天津大学 Natural gas engine pre-ignition chamber built-in type gas supply apparatus

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101858245A (en) * 2010-04-28 2010-10-13 大连理工大学 Large Gas Fuel Engine Combustion System
CN102953800A (en) * 2012-11-07 2013-03-06 镇江恒驰科技有限公司 Ignition method of pre-combustion chamber of diesel-dual-fuel engine
CN103422970A (en) * 2013-07-17 2013-12-04 广州柴油机厂股份有限公司 Ignition device of gas engine utilizing precombustion chamber
CN103422970B (en) * 2013-07-17 2015-09-30 广州柴油机厂股份有限公司 A kind of ignition mechanism adopting the gas engine of precombustion chamber
CN106103933A (en) * 2014-03-13 2016-11-09 瓦锡兰芬兰有限公司 Pre-chamber arrangement, cylinder head and piston engine
CN107091145A (en) * 2017-06-07 2017-08-25 哈尔滨工程大学 A kind of precombustion chamber of marine large-diameter gas engine
CN110486142A (en) * 2018-05-15 2019-11-22 通用汽车环球科技运作有限责任公司 Variable volume pre-chambers for internal combustion engines
CN112211714A (en) * 2020-11-27 2021-01-12 山东交通学院 A gas engine shock-assisted pre-combustion chamber structure

Also Published As

Publication number Publication date
CN1316154C (en) 2007-05-16

Similar Documents

Publication Publication Date Title
US20130104850A1 (en) Multi-fuel pre-mixed combustion system of internal combustion engine
CN101571069B (en) Internal Combustion Engine Dual Fuel Combustion System
CN114320572A (en) Multi-combustion mode ammonia fuel engine and control method thereof
CN106870186A (en) Dual fuel engine fuel injection method
US20080257304A1 (en) Internal combustion engine and combustion method of the same
US20230040984A1 (en) Air-assisted jet flame ignition device and ignition method thereof
CN217898006U (en) Combustion system and engine
CN107939517B (en) Jet ignition-based engine ultrahigh compression ratio combustion control device and method
CN116771486A (en) Pre-combustion chamber igniter, methanol engine and cold start control method thereof
CN1316154C (en) Igniting combustion system of engine preburning chamber
CN101858245A (en) Large Gas Fuel Engine Combustion System
US10393063B2 (en) Internal combustion engine piston with chamber
JP4073315B2 (en) Sub-chamber engine
CN2532249Y (en) Internal combustion chamber for gas storage and scavenging cavity
CN115045750A (en) Combustion system and engine
US12480453B2 (en) Ammonia-rich combustion coupled dual-mode prechamber ammonia-fueled engine control system
Lata et al. Experimental investigations on the performance of a dual fuel diesel engine with hydrogen and LPG as secondary fuels
CN100419231C (en) Gas internal combustion engine with premixed precombustion in-cylinder injection
Ogawa et al. Smokeless and low NOx combustion in a dual-fuel diesel engine with induced natural gas as the main fuel
CN207111228U (en) With symmetrical spherical precombustion chamber dual fuel engine combustion chamber peculiar to vessel
CN1265078C (en) Combustion system for igniting room of gasoline engine cylinder jacket
JP4145177B2 (en) Engine and operation method thereof
JP2005232987A (en) Subsidiary chamber type engine
CN1587661A (en) Top fire room combstion system for gasoline engine piston
JP3289133B2 (en) Method for improving fuel ignitability in intake pipe fuel injection compression ignition engine

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20070516

Termination date: 20100318