CN106014600A - Combustion system of gas engine - Google Patents

Combustion system of gas engine Download PDF

Info

Publication number
CN106014600A
CN106014600A CN201610445602.7A CN201610445602A CN106014600A CN 106014600 A CN106014600 A CN 106014600A CN 201610445602 A CN201610445602 A CN 201610445602A CN 106014600 A CN106014600 A CN 106014600A
Authority
CN
China
Prior art keywords
piston
combustion system
gas
gas engine
combustion
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
CN201610445602.7A
Other languages
Chinese (zh)
Inventor
王斌
李铁
葛琳琳
周昕毅
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.)
Shanghai Jiaotong University
Original Assignee
Shanghai Jiaotong 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 Shanghai Jiaotong University filed Critical Shanghai Jiaotong University
Priority to CN201610445602.7A priority Critical patent/CN106014600A/en
Publication of CN106014600A publication Critical patent/CN106014600A/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
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M25/00Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
    • 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 belongs to the technical field of engine mixed gas formation and combustion, and provides a combustion system of a gas engine. The combustion system of the gas engine comprises a cylinder liner, a cylinder cover, a piston, a combustion chamber and a diesel injector; according to the design scheme, the combustion chamber is w-shaped, an inlet of the piston is small while a basin bottom of the piston is deep, and the bottom surface of the piston is enveloped by two Bessel function curves. By the combustion system of the gas engine, the surface-to-volume ratio of the combustion chamber of the engine can be reduced effectively, so that heat transfer loss in a combustion process is reduced; emission of non-combusted hydrocarbon and carbon monoxide can be reduced effectively; and low oxynitride and high thermal efficiency are kept. The combustion system of the gas engine is reasonable in design and simple in structure, and is suitable for an engine in which natural gas used as main fuel is sprayed from a gas inlet channel and a small amount of diesel used as ignition fuel is directly sprayed from the inside of a cylinder.

Description

Gas engine combustion system
Technical field
The present invention relates to a kind of engine mixed gas that belongs to formed and the gas engine combustion system of combustion field, particularly A kind of combustion system using the diesel oil ignited gaseous mixture of trace.
Background technology
Natural gas, as the alternative energy source of great potential, is one of important means realizing traffic and transport field energy-saving and emission-reduction. Use natural gas as main fuel, trace diesel oil as the auxiliary fuel of the natural gas that ignites in compression ignition engine, can With the problem that effectively solution conventional diesel engine nitrogen oxide NOx and soot Soot discharge are high.But, conventional compression ignition formula is sent out Motivation is using diesel oil as main fuel, according to the spray burning characteristics design combustion system of diesel oil.If continuing to use this burning System carries out the pre-mixing combustion of natural gas/air, understands due to flow field intensity more weak in cylinder, bigger surface to volume ratio, and The problems such as flame propagation velocity is slow, heat transfer loss big, wall extinguishing is serious occur in combustion, and causes higher Unburned hydrocarbon UHC and carbon monoxide CO discharge, to such an extent as to have influence on the efficiency of combustion of electromotor.
Summary of the invention
Discharging to improve UHC and CO of gas engine combustion system, improve its efficiency of combustion, the present invention designs The combustion system that a kind of gas engine combustion system is special.This combustion system is keeping compression ignition engine higher compression On the premise of Bi, decrease the surface to volume ratio of combustor, thus improve the wall extinguishing of heat transfer loss and flame.By carrying Eddy flow around axial direction preferably promotes diesel pilot and being mutually mixed of pre-mixed gas in cylinder in high cylinder so that more The fuel activity of multizone is improved.Form stronger crowded stream and inverse squish near top dead center, be conducive to accelerating The spread speed of combustion process Flame.These factors all make in-cylinder combustion tissue be optimised, and efficiency of combustion is carried Height, thus reduce UHC and the CO discharge of electromotor.
The present invention is achieved through the following technical solutions, the present invention include cylinder jacket, cylinder head, piston, burning Room, diesel injector, cylinder head is arranged in the top of cylinder jacket, in piston arranges cylinder jacket, combustor by cylinder jacket (1), Cylinder head, piston are constituted, and diesel injector is arranged in the middle position of combustor, and natural gas is by intake port injection, in pressure Being that natural gas/air pre-mixing closes gas in combustor in compression process, diesel injector is many spray orifices, small-bore fuel injector, lives Two sections of Bessel function curves of underrun of plug give envelope.
Further, in the present invention, combustor have employed ω type design, and the entrance of piston is less, deeper at the bottom of basin.
Further, the combustion system of the present invention uses the diesel oil ignited natural gas of trace.
Further, in the present invention, draw combustion diesel fuel and can use single hop or multi-injection.
Further, in the present invention, combustion-chamber shape can be logical on the premise of keeping original high compression ratio constant The control node overregulating Bessel function curve is optimized
Piston bottom surface is formed by two sections of smooth curve envelopes, and every section of envelope curve is all used alone a three cubed Bezier Function is described by.Piston bottom shape can be changed by adjusting the setting of Bessel function multinomial coefficient, so as to Preferably adapt to the needs of Flow field flowing.Simultaneously, it is desirable to the region of Bessel function curve institute envelope is keeping volume On the premise of constant, (i.e. compression ratio is constant) reduces surface area as far as possible, to reduce heat transfer loss and the impact on burning thereof. Piston inlet port uses small-bore shrinkage type design, is conducive to producing strong crowded stream (piston near combustion top dead center Up) squeeze stream (descent of piston) with inverse.Combustor use dell formula ω type design, can produce at dell around The large scale eddy flow that the axial direction of motion of piston is stronger.
Compared with prior art, the advantage of the special combustion system of gas engine combustion system of the present invention includes: profit Build the curve shape of piston base with Bessel function, by rationally arranging Bessel function coefficient, face can be formed Smaller, meet In-Cylinder Flow demand and with diesel pilot spraying cooperate combustion-chamber shape design;Select ω type The combustor of design, reduces piston inlet port bore and uses dell type pelvic floor structure, being conducive to strengthening Flow field Intensity, thus flame when promoting the mixing of diesel pilot and environment gas and burn is propagated.Finally, this burning The heat transfer loss of system is minimized, efficiency of combustion is improved, UHC and CO discharge also decreases.
Accompanying drawing explanation
Fig. 1 is the structural representation of the gas engine combustion system described in the embodiment of the present invention;
Fig. 2 is based on the combustion-chamber shape described by Bessel function curve;
Label in accompanying drawing is respectively as follows: 1, cylinder jacket, and 2, cylinder head, 3, piston, 4, combustor, 5, diesel oil spray Oil device.
Detailed description of the invention
Below in conjunction with the accompanying drawings embodiments of the invention are elaborated, the present embodiment premised on technical solution of the present invention, Give detailed embodiment and concrete operating process, but protection scope of the present invention is not limited to following embodiment.
As it is shown in figure 1, the present invention includes cylinder jacket 1, cylinder head 2, piston 3, combustor 4, diesel injector 5, Cylinder head 2 is arranged in the top of cylinder jacket 1, and in piston 3 arranges cylinder jacket 1, combustor 4 is by cylinder jacket 1, cylinder Lid 2, piston 3 constitute, diesel injector 5 is arranged in the middle position of combustor 4, natural gas by intake port injection, Being that natural gas/air pre-mixing closes gas in combustor 4 in compression process, diesel injector 5 is many spray orifices, small-bore spray Oil device, two sections of Bessel function curves of the underrun of piston 3 give envelope;Combustor 4 have employed ω type design, The entrance of piston 3 is less, deeper at the bottom of basin;Combustion system uses the diesel oil ignited natural gas of trace;Draw combustion diesel fuel can use Single hop or multi-injection;Combustor 4 shape can be on the premise of keeping original high compression ratio constant, by regulation shellfish plug You are optimized by the control node of function curve.
Shown in Fig. 2 is to utilize the combustion-chamber shape described by Bessel function curve.Section A-B and B-C section are respectively two Individual three cubed Bessel function curve is constituted, and detailed expression formula is as follows:
Wherein t ∈ [0,1].
In the present embodiment, relative dimensions is provided that Cdep=24.37mm, Lcp3=16.08mm, Lcp4=4.68mm, R1=0.6975, R2=0.6949, R3=1.1, R4=0, Rbowl=35mm, Hpst=R1×Cdep=17.00mm, CP1=R3 ×Hpst=18.70mm, CP2=R4×Hpst=0mm, Lbt=R2×Rbowl=24.32mm.

Claims (5)

1. a gas engine combustion system, including cylinder jacket (1), cylinder head (2), piston (3), combustor (4), cylinder head (2) is arranged in the top of cylinder jacket (1), in piston (3) arranges cylinder jacket (1), and combustor (4) it is made up of cylinder jacket (1), cylinder head (2), piston (3), it is characterised in that also include diesel injector (5), Diesel injector (5) is arranged in the middle position of combustor (4), and natural gas is by intake port injection, in compression process Being that natural gas/air pre-mixing closes gas in combustor (4), diesel injector (5) is many spray orifices, small-bore fuel injector, Two sections of Bessel function curves of the underrun of piston (3) give envelope.
Gas engine combustion system the most according to claim 1, it is characterised in that described combustor (4) is adopted By ω type design, the entrance of piston (3) is less, deeper at the bottom of basin.
Gas engine combustion system the most according to claim 2, it is characterised in that combustion system uses trace bavin Oil ignites natural gas.
Gas engine combustion system the most according to claim 3, it is characterised in that draw combustion diesel fuel and can use list Section or multi-injection.
Gas engine combustion system the most according to claim 4, it is characterised in that combustion-chamber shape can protected Hold original high compression ratio constant on the premise of, by regulation Bessel function curve control node be optimized.
CN201610445602.7A 2016-06-20 2016-06-20 Combustion system of gas engine Pending CN106014600A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610445602.7A CN106014600A (en) 2016-06-20 2016-06-20 Combustion system of gas engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610445602.7A CN106014600A (en) 2016-06-20 2016-06-20 Combustion system of gas engine

Publications (1)

Publication Number Publication Date
CN106014600A true CN106014600A (en) 2016-10-12

Family

ID=57085541

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610445602.7A Pending CN106014600A (en) 2016-06-20 2016-06-20 Combustion system of gas engine

Country Status (1)

Country Link
CN (1) CN106014600A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114510799A (en) * 2022-01-26 2022-05-17 北京理工大学 Free piston engine thermal efficiency improving method based on driving process control
CN117028016A (en) * 2023-10-09 2023-11-10 潍柴动力股份有限公司 In-cylinder direct injection methanol engine and combustion chamber thereof and combustion chamber parameter determining method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62282113A (en) * 1986-05-30 1987-12-08 Isuzu Motors Ltd Direct injection type internal combustion engine
JPH01193019A (en) * 1988-01-29 1989-08-03 Toyota Motor Corp Combustion chamber of direct injection type diesel engine
US20040112323A1 (en) * 2002-12-13 2004-06-17 Zhengbai Liu Simplified combustion chamber
CN203146098U (en) * 2013-03-21 2013-08-21 中国第一汽车股份有限公司无锡油泵油嘴研究所 Combustion chamber suitable for low-temperature premixing combustion technology
CN204677337U (en) * 2015-06-16 2015-09-30 快马天然气动力科技(苏州)有限公司 A kind of universal Diesel Fuel-Natural Gas Dual fuel Electricity Spurt System

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62282113A (en) * 1986-05-30 1987-12-08 Isuzu Motors Ltd Direct injection type internal combustion engine
JPH01193019A (en) * 1988-01-29 1989-08-03 Toyota Motor Corp Combustion chamber of direct injection type diesel engine
US20040112323A1 (en) * 2002-12-13 2004-06-17 Zhengbai Liu Simplified combustion chamber
CN203146098U (en) * 2013-03-21 2013-08-21 中国第一汽车股份有限公司无锡油泵油嘴研究所 Combustion chamber suitable for low-temperature premixing combustion technology
CN204677337U (en) * 2015-06-16 2015-09-30 快马天然气动力科技(苏州)有限公司 A kind of universal Diesel Fuel-Natural Gas Dual fuel Electricity Spurt System

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
常思勤: "《车辆及其发动机CAD技术》", 31 July 1996, 北京理工大学出版社 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114510799A (en) * 2022-01-26 2022-05-17 北京理工大学 Free piston engine thermal efficiency improving method based on driving process control
CN117028016A (en) * 2023-10-09 2023-11-10 潍柴动力股份有限公司 In-cylinder direct injection methanol engine and combustion chamber thereof and combustion chamber parameter determining method
CN117028016B (en) * 2023-10-09 2024-01-12 潍柴动力股份有限公司 In-cylinder direct injection methanol engine and combustion chamber thereof and combustion chamber parameter determining method

Similar Documents

Publication Publication Date Title
US7213564B2 (en) Direct injection combustion chamber geometry
JPH05500252A (en) Methods and systems for controlled combustion engines
WO2017110516A1 (en) Auxiliary chamber type engine
US7011070B2 (en) Method of reducing particulates and enhancing burning rate within a combustion chamber
CN102322332A (en) Combustion chamber structure of CNG (Compressed Natural Gas) engine and fuel injection method thereof
JPH0340213B2 (en)
CN101440742A (en) Direct spraying composite flow guide laminating combustion system in spark ignition methanol cylinder
US20190017477A1 (en) Multi-Fuel Combustion Methods, Devices and Engines Using the Same
CN203146098U (en) Combustion chamber suitable for low-temperature premixing combustion technology
CN106014600A (en) Combustion system of gas engine
CN110953067B (en) Engine and double-jet combustion method thereof
CN107091145A (en) A kind of precombustion chamber of marine large-diameter gas engine
CN110714867B (en) Ignition device, combustion system and combustion method of internal combustion engine
CN208816234U (en) Engine
CN110821638B (en) Ignition chamber type engine with high-energy ignition fuel and control method thereof
CN106640360B (en) A kind of rotary engine vortex combustion cavity
CN104832949B (en) Airflow induction backward step standing vortex flame stabilization grading combustion chamber
JP2002266643A (en) Engine, its operating method and auxiliary combustion chamber mechanism
JP2005232987A (en) Subsidiary chamber type engine
JPH02153221A (en) Spark-ignition gas engine
JP4145177B2 (en) Engine and operation method thereof
CN110067638A (en) A kind of fuel jet ignition type premixed combustion of IC engine system
JP2001342860A (en) Fuel supply mechanism, engine having it, and fuel supply method
CN1811143A (en) Swirl chamber burning system for direct injection diesel engine
CN117588325A (en) Combustion system of large-cylinder-diameter precombustion chamber type ammonia fuel internal combustion engine for reducing flame propagation distance

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20161012

RJ01 Rejection of invention patent application after publication