阅读说明：本技术 一种内燃机点火装置、燃烧系统及燃烧方法 (Ignition device, combustion system and combustion method of internal combustion engine ) 是由 王志 李富柏 赵自庆 范钦灏 刘伟 于 2019-11-21 设计创作，主要内容包括：本发明涉及内燃机领域,公开了一种内燃机点火装置、燃烧系统及燃烧方法,其中点火装置包括射流室和点火机构；射流室的内部设有点火机构,射流室的一端插入主燃烧室且通过射流喷孔与主燃烧室连通,射流喷孔包括第一喷孔和第二喷孔,第一喷孔的孔径大于第二喷孔的孔径,第一喷孔用于在点火后向主燃烧室喷射火焰射流,第二喷孔用于在点火后向主燃烧室喷射自由基射流。本发明实施例提供的一种内燃机点火装置、燃烧系统及燃烧方法,通过射流火焰和活性自由基快速稳定的点燃主燃烧室内的稀薄混合气；还可有利于控制主燃烧室内的燃烧温度,有利于实现氮氧化物的近零排放,提高热效率。(The invention relates to the field of internal combustion engines, and discloses an ignition device, a combustion system and a combustion method of an internal combustion engine, wherein the ignition device comprises a jet flow chamber and an ignition mechanism; the inside of efflux room is equipped with ignition mechanism, and the one end of efflux room inserts main combustion chamber and communicates with main combustion chamber through the efflux orifice, and the efflux orifice includes first orifice and second orifice, and the aperture of first orifice is greater than the aperture of second orifice, and first orifice is used for after igniteing to main combustion chamber jet flame jet, and the second orifice is used for after igniteing to main combustion chamber jet free radical jet. According to the ignition device, the combustion system and the combustion method of the internal combustion engine provided by the embodiment of the invention, the thin mixed gas in the main combustion chamber is quickly and stably ignited through jet flow flame and active free radicals; the method is also beneficial to controlling the combustion temperature in the main combustion chamber, realizing the near zero emission of nitrogen oxide and improving the thermal efficiency.)

1. An ignition device of an internal combustion engine, characterized by comprising a jet chamber and an ignition mechanism; the inside of efflux chamber is equipped with ignition mechanism, the one end of efflux chamber insert main combustion chamber and through the efflux orifice with main combustion chamber intercommunication, the efflux orifice includes first orifice and second orifice, the aperture of first orifice is greater than the aperture of second orifice, first orifice is used for after igniteing to main combustion chamber jet flame jet, the second orifice is used for after igniteing to main combustion chamber jet free radical jet.

2. The ignition device of an internal combustion engine according to claim 1, wherein a cavity is externally connected to the other end of the jet chamber, one end of the cavity communicates with a direct injection nozzle for injecting ignition fuel into the cavity, and the cavity is provided at the other end with a vaporization nozzle hole and communicates with the jet chamber through the vaporization nozzle hole.

3. The internal combustion engine ignition device according to claim 1, wherein the second nozzle hole is located at a middle portion of an end surface of the jet chamber, the first nozzle hole is located at a periphery of the second nozzle hole, and a jet direction of the first nozzle hole is inclined outward.

4. The internal combustion engine ignition device according to claim 3, characterized in that the first nozzle holes are evenly distributed in the circumferential direction of one end of the jet chamber; or the first spray holes are grouped into a group two by two, the plurality of groups of first spray holes are uniformly distributed along the circumferential direction of one end of the jet chamber, and the jet directions of the two first spray holes in any group are intersected.

5. The internal combustion engine ignition device according to any one of claims 1 to 4, characterized in that the aperture of the first nozzle hole is 1.5 to 2.5 mm; the aperture of the second spray hole is 0.5-1.0 mm; the ratio of the volume of the jet chamber to the volume of the main combustion chamber is less than or equal to 3%.

6. The internal combustion engine ignition device of claim 2, wherein said vaporization orifices are symmetrically distributed about said ignition mechanism; the ignition fuel comprises a gaseous fuel or a liquid fuel.

7. An internal combustion engine combustion system comprising the internal combustion engine ignition device of any one of claims 1 to 6, further comprising an air inlet nozzle in communication with the main combustion chamber, wherein the air inlet nozzle is configured to inject combustion fuel into the main combustion chamber, and the main combustion chamber is movably coupled to a piston.

8. A combustion method for an internal combustion engine based on the ignition device for an internal combustion engine according to any one of claims 1 to 6, comprising:

introducing combustion fuel into the main combustion chamber to form thin mixed gas in the main combustion chamber;

injecting ignition fuel into the jet chamber in gaseous or mist form;

igniting in the jet chamber;

the aperture of the jet flow spray hole on the jet flow chamber is controlled, so that two jet flows, namely flame jet flow and free radical jet flow, are sprayed from the jet flow chamber to the main combustion chamber.

9. The combustion method of an internal combustion engine according to claim 8, further comprising, after injecting the ignition fuel in a gaseous or mist state into the jet chamber, before ignition in the jet chamber:

the lean mixture inside the main combustion chamber is compressed.

10. The combustion method of an internal combustion engine according to claim 8, wherein an excess air ratio of the lean mixture is 1.5 or more.

Technical Field

The invention relates to the technical field of internal combustion engines, in particular to an ignition device, a combustion system and a combustion method of an internal combustion engine.

Background

The internal combustion engine is used as the most important power source in the transportation field, and plays an important role in the process of economic development and social progress. However, in recent years, with the increase in the amount of stored internal combustion engines, the consumption of fossil energy has been rapidly increased, and environmental problems such as air pollution and greenhouse effect have become increasingly serious. Therefore, the transformation and the upgrading of the energy-saving and emission-reducing technology of the internal combustion engine are more and more urgent due to the energy and environmental problems. For internal combustion engines, lean burn strategies with high excess air ratios are an effective path to improve thermal efficiency and reduce emissions.

However, under lean conditions with a high excess air ratio, the laminar flame speed of the combustible mixture is slow, the flame thickness increases, and it is difficult for the conventional spark plug with limited ignition energy to establish a minute flame kernel close to the flame thickness and maintain stable growth of the flame kernel, thereby easily causing misfire.

Disclosure of Invention

The embodiment of the invention provides an ignition device, a combustion system and a combustion method of an internal combustion engine, which are used for solving or partially solving the problem that a traditional spark plug is difficult to establish a tiny fire core close to the thickness of flame and is easy to cause fire under the existing lean-burn condition with a high excess air coefficient.

The embodiment of the invention provides an ignition device of an internal combustion engine, which comprises a jet flow chamber and an ignition mechanism; the inside of efflux chamber is equipped with ignition mechanism, the one end of efflux chamber insert main combustion chamber and through the efflux orifice with main combustion chamber intercommunication, the efflux orifice includes first orifice and second orifice, the aperture of first orifice is greater than the aperture of second orifice, first orifice is used for after igniteing to main combustion chamber jet flame jet, the second orifice is used for after igniteing to main combustion chamber jet free radical jet.

On the basis of above-mentioned scheme, the other end external connection of efflux room has the cavity, the one end and the direct injection nozzle of cavity are linked together, the direct injection nozzle be used for to spout into ignition fuel in the cavity, the cavity is equipped with the vaporization orifice and passes through at the other end the vaporization orifice with efflux room intercommunication.

On the basis of the scheme, the second spray hole is located in the middle of one end face of the jet chamber, the first spray hole is located on the periphery of the second spray hole, and the jet direction of the first spray hole is inclined outwards.

On the basis of the scheme, the first spray holes are uniformly distributed along the circumferential direction of one end of the jet flow chamber; or the first spray holes are grouped into a group two by two, the plurality of groups of first spray holes are uniformly distributed along the circumferential direction of one end of the jet chamber, and the jet directions of the two first spray holes in any group are intersected.

On the basis of the scheme, the aperture of the first spray hole is 1.5-2.5 mm; the aperture of the second spray hole is 0.5-1.0 mm; the ratio of the volume of the jet chamber to the volume of the main combustion chamber is less than or equal to 3%.

On the basis of the scheme, the vaporization spray holes are symmetrically distributed about the ignition mechanism; the ignition fuel comprises a gaseous fuel or a liquid fuel.

The embodiment of the invention provides a combustion system of an internal combustion engine, which comprises the ignition device of the internal combustion engine and an air inlet nozzle communicated with a main combustion chamber, wherein the air inlet nozzle is used for injecting combustion fuel into the main combustion chamber, and the main combustion chamber is movably connected with a piston.

The embodiment of the invention provides an internal combustion engine combustion method based on the internal combustion engine ignition device, which comprises the following steps: introducing combustion fuel into the main combustion chamber to form thin mixed gas in the main combustion chamber; injecting ignition fuel into the jet chamber in gaseous or mist form; igniting in the jet chamber; the aperture of the jet flow spray hole on the jet flow chamber is controlled, so that two jet flows, namely flame jet flow and free radical jet flow, are sprayed from the jet flow chamber to the main combustion chamber.

On the basis of the above scheme, after the ignition fuel is injected into the jet flow chamber in a gaseous or mist state, and before ignition is performed in the jet flow chamber, the method further comprises the following steps: the lean mixture inside the main combustion chamber is compressed.

On the basis of the scheme, the excess air coefficient of the lean mixture is more than or equal to 1.5.

The embodiment of the invention provides an ignition device, a combustion system and a combustion method of an internal combustion engine.A jet flow chamber is arranged, and the thin mixed gas in a main combustion chamber can be quickly and stably ignited by jet flow flame and active free radicals through jet flow ignition; through the arrangement of the first spray hole and the second spray hole, a plurality of flame surfaces and a plurality of active islands which are divergently distributed, namely high-temperature free radicals can be formed in the main combustion chamber, so that the thin mixed gas in the main combustion chamber releases heat in a distributed and staged manner, and the combustion which is rapid and stable and does not knock is realized; the method is also beneficial to controlling the combustion temperature in the main combustion chamber, realizing the near zero emission of nitrogen oxide and improving the thermal efficiency.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and those skilled in the art can also obtain other drawings according to the drawings without creative efforts.

FIG. 1 is a schematic diagram of a combustion system of an internal combustion engine according to an embodiment of the present invention;

FIG. 2 is a schematic top view of a first distribution of first nozzles according to an embodiment of the present invention;

FIG. 3 is a schematic top view illustrating a second distribution of first nozzles according to an embodiment of the present invention.

Description of reference numerals:

1-a direct injection nozzle; 2-an ignition mechanism; 3-vaporization spray hole;

4-main combustion chamber; 5, a piston; 6-flame jet flow;

7-radical jet; 8-active island; 9-a jet chamber;

10-an air inlet nozzle; 11-cavity body; 12 — a first orifice;

13-second nozzle hole.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

An ignition device of an internal combustion engine according to an embodiment of the present invention, referring to fig. 1, includes a jet chamber 9 and an ignition mechanism 2; ignition mechanism 2 is equipped with in the inside of efflux chamber 9, and the one end of efflux chamber 9 inserts main combustion chamber 4 and communicates with main combustion chamber 4 through the efflux orifice, and the efflux orifice includes first orifice 12 and second orifice 13, and the aperture of first orifice 12 is greater than the aperture of second orifice 13, and first orifice 12 is used for after igniteing to spray flame jet 6 in main combustion chamber 4, and second orifice 13 is used for after igniteing to spray free radical jet 7 in main combustion chamber 4.

The ignition device of the internal combustion engine provided by the embodiment adopts jet ignition, the jet chamber 9 is arranged, ignition fuel is sprayed into the main combustion chamber 4 through the jet chamber 9, the jet chamber 9 can play a role in uniform distribution of the ignition fuel, and the ignition fuel is favorably sprayed into the main combustion chamber 4 uniformly. Ignition fuel is uniformly distributed in the jet flow chamber 9, then the ignition fuel in the jet flow chamber 9 is ignited through the ignition mechanism 2, and the ignited ignition fuel is sprayed into the main combustion chamber 4 through a jet flow spray hole at one end of the jet flow chamber 9, so that stable combustion is formed in the main combustion chamber 4.

One end of the jet chamber 9 is provided with a jet orifice which can limit and control the part for jetting the ignition fuel. And the ignition device of the internal combustion engine can be provided with jet flow spray holes with different aperture sizes so as to control the specific form of ignition fuel sprayed into the main combustion chamber 4 and adjust and control the combustion process in the main combustion chamber 4.

The ignition device for the internal combustion engine is provided with a first jet hole 12 with a larger aperture at one end of a jet chamber 9, and the aperture of the jet hole is required to ensure that ignition fuel ignited in the jet chamber 9 enters a main combustion chamber 4 in a combustion state, namely, in a flame shape to form a flame jet 6. In addition, a second nozzle hole 13 with a smaller hole diameter is provided, and the hole diameter of the nozzle hole is smaller, so that ignition fuel ignited and combusted in the jet chamber 9 is quenched in flame when passing through the second nozzle hole 13 and enters the main combustion chamber 4 in the form of a high-temperature medium, namely, the free radical jet 7 is formed.

The jet ignition can quickly and stably ignite the lean mixture in the combustion chamber through jet flame and active free radicals, the ignition energy of the jet ignition can be improved by several orders of magnitude compared with that of a traditional spark plug, and the jet ignition is a novel ignition technology capable of effectively and stably realizing the lean combustion with high excess air coefficient. The jet ignition system integrates a conventional spark plug and an oil injector to form a small-volume jet chamber 9. The fuel injector can inject fuel into the jet flow chamber 9 to form homogeneous and stoichiometric mixed gas, and the spark plug ignites the mixed gas in the jet flow chamber 9 to generate flame jet flow 6 and free radical jet flow 7 so as to ignite the dilute mixed gas in the main combustion chamber 4.

Through the arrangement of the first jet hole 12 and the second jet hole 13, a plurality of flame surfaces and a plurality of active islands 8 which are distributed divergently, namely high-temperature free radicals, can be formed in the main combustion chamber 4 through the ignition device, and the active islands 8 form an autoignition ignition source, so that under the promotion action of the propagation, compression, heat radiation and active free radicals of the plurality of flame surfaces, the dilute mixed gas in the main combustion chamber 4 is subjected to distributed staged heat release, and combustion which is rapid, stable and free of knock is realized; the combustion temperature in the main combustion chamber 4 can be controlled not to be too high, the near zero emission of nitrogen oxides can be realized, and the heat efficiency is improved.

On the basis of the above embodiment, further, the other end of the jet chamber 9 is externally connected with a cavity 11, one end of the cavity 11 is communicated with the direct injection nozzle 1, the direct injection nozzle 1 is used for injecting ignition fuel into the cavity 11, and the cavity 11 is provided with the vaporization nozzle hole 3 at the other end and is communicated with the jet chamber 9 through the vaporization nozzle hole 3.

The cavity 11 is a hollow cavity and is disposed at the other end of the jet chamber 9. The other end of the cavity 11 can be connected to the inlet at the other end of the jet chamber 9. The cavity body at the other end of the cavity body 11 is provided with a vaporization spray hole 3, and the interior of the cavity body 11 is communicated with the jet chamber 9 through the vaporization spray hole 3.

The cavity 11 and the vaporization nozzle hole 3 are provided so that ignition fuel ejected from the direct injection nozzle 1 needs to be injected into the jet chamber 9 through the vaporization nozzle hole 3. The vaporization orifice 3 allows defined control of the distribution and particle size of the ignition fuel injected into the jet chamber 9, so that the ignition fuel is injected into the jet chamber 9 with a more uniform distribution orientation and smaller particle size.

The cavity 11 thus acts like a vaporization of the ignition fuel, in particular of the liquid fuel, so that the liquid fuel is sprayed uniformly into the jet chamber 9 in an approximately atomized form. The uniform distribution and ignition of the liquid fuel in the jet flow chamber 9 are facilitated, the formation of uniformly distributed ignition sources in the main combustion chamber 4 is further facilitated, and the difficulty in mixing the mixed gas in the main combustion chamber 4 is reduced. And the liquid fuel is uniformly sprayed through the cavity 11, compared with the direct injection into the jet flow chamber 9, the generation of carbon smoke can be reduced, and the combustion efficiency is favorably improved.

Further, the aperture of the vaporization orifice 3 is preferably 0.3 to 0.6 mm. Is favorable for forming better atomization effect on the liquid fuel.

In addition to the above embodiments, the second nozzle hole 13 is located in the middle of one end surface of the jet chamber 9, the first nozzle hole 12 is located on the periphery of the second nozzle hole 13, and the jet direction of the first nozzle hole 12 is inclined outward. I.e., the first nozzle hole 12 is located near the edge of the end of the jet chamber 9, and the second nozzle hole 13 is located near the center of the end surface of the jet chamber 9. The flame jet flow 6 and the free radical jet flow 7 are uniformly sprayed into the main combustion chamber 4. And the flame jet flow 6 is distributed at the periphery of the free radical jet flow 7, so that the temperature of the free radical jet flow 7 can be maintained, and stable combustion can be formed.

The second nozzle holes 13 may be circumferentially distributed in a circle, in an array, or in any other regular or irregular distribution in the middle of the end surface of one end of the jet chamber 9, so as to be suitable for the size of the end surface of the jet chamber 9, and are not limited.

The jet direction of the first jet hole 12 inclines outwards, namely the jet direction of the first jet hole 12 is not vertical downwards, and is inclined towards the periphery of the jet chamber with a certain inclination angle. The jet of the first nozzle hole 12 can be distributed more evenly in the main combustion chamber 4.

Further, the end of one end of the jet chamber 9 may be convex, and the first nozzle hole 12 may be disposed at the edge of the end face of one end of the jet chamber 9, so that the jet direction of the first nozzle hole 12 is inclined outward. The end of one end of the jet chamber 9 may be in a frustum shape, that is, the cross section is gradually reduced, and the first nozzle hole 12 may be disposed on a side wall of the frustum shape, so that the jet direction of the first nozzle hole 12 is inclined outward.

Further, referring to fig. 2, the first nozzle holes 12 are uniformly distributed along the circumferential direction of one end of the jet chamber 9; alternatively, referring to fig. 3, the first nozzle holes 12 are grouped into two groups, the multiple groups are uniformly distributed along the circumferential direction of one end of the jet chamber 9, and the jet directions of the two first nozzle holes 12 in any group are intersected. The two distribution modes of the first spray holes 12 can ensure that the jet flow is uniformly distributed in the main combustion chamber 4, thereby being beneficial to improving the combustion efficiency.

On the basis of the above embodiment, further, the aperture of the first nozzle hole 12 is 1.5-2.5 mm; the aperture of the second spray hole 13 is 0.5-1.0 mm. The first and second orifices 12, 13 of this size are effective to form respective flame jets 6 and radical jets 7.

In addition to the above embodiment, the ratio of the volume of the jet chamber 9 to the volume of the main combustion chamber 4 is 3% or less. Not only can be beneficial to the ignition fuel to be quickly and uniformly distributed in the jet flow chamber 9, but also can ensure the speed of the fuel injected into the main combustion chamber 4, and is beneficial to the smooth ignition and stable combustion in the main combustion chamber 4.

On the basis of the above embodiment, further, the vaporization nozzle holes 3 are symmetrically distributed about the ignition mechanism; the ignition fuel comprises a gaseous fuel or a liquid fuel. The ignition mechanism 2 may be mounted centrally on top of the jet chamber 9. The electrodes of the spark plug may be inserted into the incident flow chamber 9. Ignition fuel entering the jet chamber 9 through the vaporization jet holes 3 can be uniformly distributed around the ignition mechanism, facilitating uniform ignition.

Further, the ignition mechanism 2 may also adopt an ignition mode such as a glow plug, a corona, a microwave, or the like, specifically may be a spark plug, a glow plug, a laser igniter, a corona igniter, or a microwave igniter, and may also be other structures capable of realizing ignition, without limitation.

On the basis of the above embodiments, further, the present embodiment provides a combustion system of an internal combustion engine, the combustion system of an internal combustion engine includes the ignition device of an internal combustion engine according to any one of the above embodiments, and further includes an air intake nozzle 10 communicated with the main combustion chamber 4, wherein the air intake nozzle 10 is used for injecting combustion fuel into the main combustion chamber 4, and the main combustion chamber 4 is movably connected with a piston 5.

On the basis of the above embodiment, further, the present embodiment provides an internal combustion engine combustion method based on the internal combustion engine ignition device of any of the above embodiments, the internal combustion engine combustion method including: introducing combustion fuel into the main combustion chamber 4 to form thin mixed gas in the main combustion chamber 4; injecting ignition fuel into the jet chamber 9 in gaseous or mist form; ignition takes place in the jet chamber 9; by controlling the aperture of the jet nozzle hole on the jet chamber 9, two jets of flame jet 6 and radical jet 7 are jetted from the jet chamber 9 to the main combustion chamber 4.

The ignition fuel may be a gaseous fuel, where the ignition fuel is injected into the jet chamber 9 in gaseous form; the ignition fuel may also be a liquid fuel, in which case the ignition fuel is injected into the jet chamber 9 in the form of a mist. The two jet flows are jetted to the main combustion chamber 4, so that distributed staged combustion can be realized in the main combustion chamber 4, rapid and stable combustion without explosion is realized, the combustion temperature is favorably controlled, and the generation of nitrogen oxides is reduced.

On the basis of the above embodiment, further, after injecting the ignition fuel into the jet chamber 9 in a gaseous or mist state, before ignition in the jet chamber 9, the method further includes: the lean mixture inside the main combustion chamber 4 is compressed. The piston 5 can be pushed to compress the thin mixed gas in the main combustion chamber 4, the thin mixed gas in the main combustion chamber 4 is extruded into the jet flow chamber 9 from the jet flow nozzle hole at the bottom of the jet flow chamber 9 at a high speed under the compression action of the piston 5 to form strong turbulence, and the strong turbulence and ignition fuel sprayed in the jet flow chamber 9 quickly form combustible mixed gas with homogeneous equivalence ratio. Is favorable for smooth ignition and stable combustion.

In addition to the above embodiment, the excess air ratio of the lean mixture is 1.5 or more. The combustion method of the internal combustion engine is suitable for ignition combustion of the lean mixture with the excess air coefficient, and is beneficial to improving the heat efficiency and reducing the emission.

On the basis of the above embodiments, further, for lean combustion with high air excess coefficient, it is necessary to propose an ignition combustion organization method and an implementation device with faster and more stable combustion based on the combustion theory in order to obtain higher thermal efficiency and lower emissions.

The combustion organization method and the device thereof related to the embodiment comprise an engine, an air inlet nozzle 10, a gas phase jet igniter (DGI) integrating a spark plug, a direct injection nozzle 1 and a cavity 11, a jet chamber 9, a jet orifice special diameter design, a main combustion chamber 4 and the like. Engines using high Compression Ratios (CR)>15) The main combustion chamber 4 adopts lean combustion mixed gas (excess air coefficient lambda)>1.5), plus the engine's inherent Exhaust Gas Recirculation (EGR), the fuel rate injected in the jet chamber 9 is first vaporized in the cavity 11 and then in the gaseous or mist phaseThe mixed gas is jetted into a jet flow chamber 9 in a formula mode, two groups of jet holes with large aperture (1.5-2.5mm) and small aperture (0.5-1.0mm) are designed at the bottom of the jet flow chamber 9, flame jet flow 6 and free radical jet flow 7 are generated simultaneously, so that a plurality of flame surfaces and dispersed active islands 8 are formed in a main combustion chamber 4, the mixed combustion process that the whole lean mixture in the middle of the main combustion chamber 4 is spontaneously combusted and the lean mixture at the edge is consumed by turbulent premixed flame is realized, and high efficiency is obtained while NO smoke and near zero NO are generated_xAnd (5) discharging.

The intake nozzle 10 injects fuel in the intake passage to form a lean mixture (excess air ratio λ >1.5) and enters the main combustion chamber 4 through the intake stroke. The center of the top of an engine cylinder is provided with a jet chamber 9 with a small volume (< 3% of the volume of a combustion chamber), the bottom of the jet chamber 9 is provided with two groups of spray holes with different diameters (the number of holes in each group is 4-8), each group of spray holes are uniformly distributed along the circumferential direction, the diameter of an outer ring hole is set to be 1.5-2.5mm, and the diameter of an inner ring hole is set to be 0.5-1.0 mm.

The top of the jet chamber 9 is provided with a spark plug, small holes (the number of the holes is 3-6) are uniformly distributed around the electrode of the spark plug, the small holes are connected with the cavity 11, and the cavity 11 is communicated with the direct injection nozzle 1. In the intake stroke of the engine, the direct injection nozzle 1 injects gaseous or liquid fuel into the cavity 11, and the liquid fuel is vaporized into a gaseous phase in the cavity 11 or is injected into the jet chamber 9 from small holes uniformly distributed around the spark plug electrode.

Under the compression action of the piston 5, the thin mixed gas in the main combustion chamber 4 is extruded into the jet flow chamber 9 from the jet hole at the bottom of the jet flow chamber 9 at a high speed to form strong turbulence, and the strong turbulence and the gas-phase fuel injected in the jet flow chamber 9 quickly form combustible mixed gas with homogeneous equivalence ratio. When the spark plug is ignited near a compression top dead center, the mixed gas in the jet flow chamber 9 is ignited and combusted to form two different jet flows to be ejected from the jet holes, wherein the hole group with the larger diameter of the outer ring generates flame jet flow 6, the hole group with the smaller diameter of the inner ring quenches the flame to generate free radical jet flow 7, so that a plurality of flame surfaces and a plurality of scattered active small islands 8 (spontaneous combustion ignition sources) are formed in the main combustion chamber 4, and the dilute mixed gas in the main combustion chamber 4 is rapidly and stably combusted under the promotion action of the propagation, compression, heat radiation and active free radicals of the plurality of flame surfacesAnd the distributed type staged heat release is realized, and the combustion which is fast and stable and does not knock is realized. Meanwhile, Exhaust Gas Recirculation (EGR) is introduced on the basis to form a diluted combustion condition of a lean mixture, so that the combustion temperature in the cylinder is favorably controlled to be less than 1800K, and NO is realized_xNear zero emission and 45% thermal efficiency.

The embodiment aims to provide an organizing method and an implementing device thereof, which can realize the rapid and stable combustion of lean mixture with high excess air coefficient. The combustion organization method and the device thereof can simultaneously generate flame jet flow 6 and active jet flow, promote the main combustion chamber 4 to generate distributed staged heat release, achieve rapid and detonation-free combustion, further improve the thermal efficiency and reduce the emission.

The distributed gas phase jet ignition combustion organizing method and the device thereof disclosed by the embodiment comprise a DGI igniter (containing a fuel vaporization cavity, namely a cavity 11), a jet chamber 9 containing jet holes with different diameters and a combustion chamber, wherein the DGI igniter integrates the ignition and fuel injection functions. The central arrangement of the spark plug electrode of the igniter, the small hole is distributed around the electrode, in the intake stroke of the engine, the nozzle firstly sprays the fuel oil into the vaporization cavity to vaporize, the gaseous fuel enters the jet flow chamber 9 from the small hole and is rapidly mixed with the gas compressed and extruded by the piston 5 to form a homogeneous equivalence ratio mixed gas, the spark plug discharges to ignite the homogeneous mixed gas in the jet flow chamber 9 when the top dead center is nearby, the temperature and the pressure in the jet flow chamber 9 are increased, the flame jet flow 6 and the free radical jet flow 7 are formed through the jet hole at the bottom of the jet flow chamber 9, and the multiple points of the thin mixed gas in the combustion chamber are integrally self-ignited under the action of the propagation, compression, heat radiation and active free radicals of multiple flame surfaces, so that the fast and stable premixed low-temperature combustion without explosion is realized, thereby greatly improving the heat.

The fuel is vaporized in the cavity 11 and is injected into the jet flow chamber 9 in a gas phase form, so that the formation of homogeneous premixed combustible mixed gas is facilitated, and the problems of uneven mixing, carbon deposition and the like caused by the direct injection of liquid fuel into the jet flow chamber 9 can be avoided. The jet holes with different diameters are arranged at the bottom of the jet flow chamber 9 to form two forms of flame jet flow 6 and free radical jet flow 7, so that multiple flame surfaces and scattered active islands 8 (self-ignition sources) are generated in the main combustion chamber 4, and under the action of propagation, compression, heat radiation and free radicals of the multiple flame surfaces, the dilute mixed gas in the main combustion chamber 4 is rapidly and stably combusted (distributed staged heat release), and high efficiency and low emission are obtained.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.