CN111485992A - Engine rapid combustion device suitable for low-evaporation characteristic fuel - Google Patents
Engine rapid combustion device suitable for low-evaporation characteristic fuel Download PDFInfo
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- CN111485992A CN111485992A CN202010520415.7A CN202010520415A CN111485992A CN 111485992 A CN111485992 A CN 111485992A CN 202010520415 A CN202010520415 A CN 202010520415A CN 111485992 A CN111485992 A CN 111485992A
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- 238000002485 combustion reaction Methods 0.000 title claims abstract description 172
- 239000000446 fuel Substances 0.000 title description 16
- 238000001704 evaporation Methods 0.000 title description 13
- 239000007921 spray Substances 0.000 claims abstract description 19
- 239000000203 mixture Substances 0.000 claims abstract description 10
- 230000005611 electricity Effects 0.000 claims abstract description 4
- 238000002347 injection Methods 0.000 claims description 5
- 239000007924 injection Substances 0.000 claims description 5
- 238000005474 detonation Methods 0.000 abstract description 5
- 230000001133 acceleration Effects 0.000 abstract description 2
- 238000004364 calculation method Methods 0.000 description 10
- 238000004088 simulation Methods 0.000 description 9
- 238000004458 analytical method Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 230000008020 evaporation Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 239000011148 porous material Substances 0.000 description 3
- 238000012795 verification Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 239000003350 kerosene Substances 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 229920006395 saturated elastomer Polymers 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005094 computer simulation Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 239000003502 gasoline Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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Classifications
-
- 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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/12—Engines characterised by precombustion chambers with positive ignition
-
- 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
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/16—Chamber shapes or constructions not specific to sub-groups F02B19/02 - F02B19/10
-
- 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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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
The utility model provides an engine combustion device, includes main combustion chamber, the spark plug, vice combustion chamber and flame jet hole, wherein, initial flame passes through the spark plug and discharges electricity in vice combustion chamber and produces, flame produces and develops rapidly in vice combustion chamber afterwards, and then produces stranded jet flow flame through connecting a plurality of flame jet holes of vice combustion chamber and main combustion chamber, and stranded jet flow flame sprays simultaneously and gets into main combustion chamber, is equivalent to main combustion chamber's high energy multinuclear ignition source, and the gas mixture in the main combustion chamber is lighted by many places large tracts of land flame simultaneously. The invention realizes the acceleration of the combustion speed of the mixed gas, improves the ignition stability and reliability and can effectively inhibit the detonation phenomenon.
Description
Technical Field
The invention relates to the technical field of energy utilization, in particular to a quick combustion device of an engine, which is suitable for low-evaporation-characteristic fuel.
Background
The low-evaporation characteristic fuel has the characteristics of low saturated vapor pressure, low evaporation speed and the like due to the physical and chemical characteristics of the low-evaporation characteristic fuel, and when the low-evaporation characteristic fuel is applied to a spark-ignition piston engine, the problems of poor quality of mixed gas formation, unstable combustion process, low flame propagation speed and the like are generally caused, so that the phenomena of difficult cold start, easy detonation, insufficient power output and the like of the engine can be caused. And the purpose that traditional spark plug ignition mode just relied on promotion ignition energy to reach promotion ignition reliability and stability then, but also can aggravate the wearing and tearing of spark plug electrode when the promotion of ignition energy, ignition coil self weight volume and cost electricity can increase, and simultaneously, traditional spark plug ignition is not obvious to big cylinder diameter engine combustion speed's promotion effect through promoting ignition energy, consequently, accelerate the combustion speed of low evaporation characteristic fuel engine, promote combustion stability, there is great technical barrier.
Disclosure of Invention
In view of the above, the main object of the present invention is to provide a fast combustion device for an engine with low evaporation characteristic fuel, so as to partially solve at least one of the above technical problems.
In order to achieve the above objects, as one aspect of the present invention, there is provided an engine combustion apparatus including a main combustion chamber, a spark plug, an auxiliary combustion chamber, and flame spray holes, wherein an initial flame is generated by discharging electricity in the auxiliary combustion chamber through the spark plug, and then the flame is generated and rapidly developed in the auxiliary combustion chamber, and further a plurality of jet flames are generated through the plurality of flame spray holes connecting the auxiliary combustion chamber and the main combustion chamber, and the plurality of jet flames are simultaneously sprayed into the main combustion chamber, corresponding to a high-energy multi-core ignition source of the main combustion chamber, and a mixture gas in the main combustion chamber is simultaneously ignited by a plurality of large area flames.
The number of the flame spray holes in the circumferential direction below the auxiliary combustion chamber structure body is five, and the five flame spray holes are asymmetrically arranged and matched with the main combustion chamber structure.
The engine combustion device is provided with a positioning bulge structure, so that five jet flame points generated by asymmetric arrangement of five flame spray holes are matched with a main combustion chamber.
Wherein each of the five flame spray holes is inclined at a different angle and is arranged at a different angle.
Wherein the diameter, the arrangement position and the angle of the flame spray holes are calculated by the optimization matching with the combustion chamber.
Wherein, the specific size parameter range of the flame spray holes is as follows:
range of diameter of the spray hole: 1.0-1.5 mm;
the inclination angle of the spray hole is as follows: 20-90 degrees relative to the central line of the device.
Based on the technical scheme, compared with the prior art, the engine combustion device disclosed by the invention at least has one of the following beneficial effects:
1. the combustion speed of the mixed gas is accelerated. The auxiliary combustion chamber enters into the multi-strand jet flame in the main combustion chamber through the jet flow of the flame jet hole, and is equivalent to a plurality of large-area high-energy ignition sources in the main combustion chamber, so that the ignition distribution surface in the main combustion chamber is more extensive, and compared with the single ignition source of the traditional spark plug, the ignition distribution surface can greatly accelerate the ignition of mixed gas and the propagation speed of flame, thereby effectively shortening the emergency combustion period and improving the efficiency of the engine.
2. And the ignition stability and reliability are improved. The space in the auxiliary combustion chamber is more difficult for receiving the influence of the great air current disturbance in the engine cylinder for main combustion chamber, also can prevent effectively simultaneously that the engine spark plug from being drenched by the fuel oil spraying, has promoted the reliability of igniteing, makes the gas mixture in the auxiliary combustion chamber change and fires, and then has guaranteed the gas mixture combustion stability in the main combustion chamber, reduces the combustion cycle fluctuation rate.
3. Effectively inhibit the detonation phenomenon. The extensive distribution of the jet flame of stranded efflux in the auxiliary combustion chamber efflux entering main combustion chamber is in each space range of main combustion chamber, can make the gas mixture in the main combustion chamber reach the multiple spot effect of igniteing simultaneously, the gas mixture combustion flame propagation speed in the main combustion chamber has greatly been accelerated, the possibility of the terminal gas mixture spontaneous combustion in the main combustion chamber has been reduced, and then effectively eliminate the detonation region, restrain the emergence of detonation phenomenon, and simultaneously, the acceleration of flame propagation speed, also the effectual combustion isochoricity that has improved, and then promote the engine and do work the ability.
Drawings
FIG. 1 is a schematic diagram of the basic structure of a rapid combustion device of an engine suitable for low evaporation characteristic fuel according to the present invention;
FIG. 2 is a detailed two-dimensional view of a secondary combustion chamber assembly in an embodiment of the present invention;
FIG. 3 is a schematic view of the mounting of the auxiliary chamber assembly to the engine cylinder head in an embodiment of the present invention;
FIG. 4 is a schematic view of a computational model of a fixed volume combustor in an embodiment of the invention;
FIG. 5 is a schematic view of the ignition position of the auxiliary chamber with/without scheme in the embodiment of the present invention, wherein FIG. 5(a) is the ignition position of the auxiliary chamber with scheme and FIG. 5(b) is the ignition position of the auxiliary chamber without scheme;
FIG. 6 is a comparison of the results of simulation analysis of combustion with/without a secondary combustion chamber in an embodiment of the present invention, wherein FIG. 6(a) is a heat release rate comparison and FIG. 6(b) is a pressure and pressure rise rate comparison;
FIG. 7 is a jet ignition scheme for the auxiliary chamber in an embodiment of the present invention, wherein FIG. 7(a) is a schematic ignition diagram for a first symmetrically arranged scheme and FIG. 7(b) is a schematic ignition diagram for a second asymmetrically arranged scheme;
FIG. 8 is a graph comparing the progress of the combustion reaction in two versions of a symmetric and asymmetric arrangement orifice precombustor in an embodiment of the present invention;
FIG. 9 is a graph comparing simulation results of flame spray velocity for different orifice diameters in an embodiment of the present invention;
FIG. 10 is a comparison of experimental cylinder pressures for an example of the present invention.
Detailed Description
In order to improve the combustion speed and the combustion stability of the low-evaporation characteristic fuel engine, promote the rapid combustion of the large-cylinder-diameter engine and further improve the working capacity of the engine, a scheme of a rapid combustion device of the engine suitable for the low-evaporation characteristic fuel is adopted, and the basic principle is as follows: an auxiliary combustion chamber is formed at an original spark plug, the auxiliary combustion chamber is positioned and connected with an engine through a positioning protrusion and a tabletting device, initial flame is generated by discharging in the auxiliary combustion chamber through the original spark plug, then the flame is generated and rapidly developed in the auxiliary combustion chamber, and then multi-strand jet flame is generated through a plurality of flame spray holes connecting the auxiliary combustion chamber and a main combustion chamber, the multi-strand jet flame is simultaneously sprayed into the main combustion chamber, which is equivalent to a high-energy multi-core ignition source of the main combustion chamber, and mixed gas in the main combustion chamber is simultaneously ignited by a plurality of large-area flames. Under this kind of ignition mode, the device's vice combustion chamber structure can ensure the steady development of initial flame kernel, and the stranded efflux flame that produces by the flame orifice provides a plurality of spatial distribution's large tracts of land ignition source for main combustion chamber, make the flame propagation distance shorten in the engine jar, the inside turbulent intensity of main combustion chamber has been strengthened simultaneously, flame propagation speed in the main combustion chamber has greatly been accelerated, engine ignition stability and reliability also obtain great promotion, consequently, the device has the combustion speed that accelerates low evaporation characteristic fuel engine, promote the potentiality that the engine does work the ability.
In order that the objects, technical solutions and advantages of the present invention will become more apparent, the present invention will be further described in detail with reference to the accompanying drawings in conjunction with the following specific embodiments.
Scheme device structure
1.1 apparatus details Structure
The specific structure of the device is shown in figure 1, the basic structure principle of the device is a hollow cylindrical structure external member, the internal cylindrical space is an auxiliary combustion chamber space, and the spark plug is connected with an auxiliary combustion chamber structure body through threads. A positioning convex structure is designed on the engine combustion device, so that five jet flame points generated by asymmetric arrangement of five flame jet holes are ensured to be matched with a main combustion chamber. Meanwhile, five small holes inclined at a certain angle are circumferentially distributed below the auxiliary combustion chamber structure, the inclination and the arrangement angle of the five asymmetrically-arranged small holes are different, the diameter, the arrangement position and the angle of the holes are calculated by optimizing and matching with the combustion chamber, and a specific structural dimension parameter schematic diagram is shown in fig. 2. Wherein the external diameter of the thread
22mm, minor diameter of thread
Is 10mm in diameter and has small holes
1.25mm, small hole inclination angle
Is 20 to 90 degrees.
1.2 schematic diagram of assembly structure of device and engine
The installation schematic diagram of the auxiliary combustion chamber device and the engine is shown in fig. 3, the auxiliary combustion chamber device is matched with the engine cylinder head in a positioning mode through the positioning protrusions, five jet flame points generated by asymmetric arrangement of five flame spray holes are ensured to be matched with the main combustion chamber, and the auxiliary combustion chamber is tightly pressed and fixed on the engine cylinder head through the tabletting device.
The flame in the auxiliary combustion chamber is jetted into the main combustion chamber through 5 asymmetrically-arranged flame jet holes which are distributed at the lower end in the circumferential direction and are inclined at a certain angle, and the low-evaporation-characteristic fuel mixed gas in the main combustion chamber is quickly ignited.
Simulation calculation analysis of quick combustion device of secondary combustion chamber and secondary combustion chamber
2.1 Combustion simulation analysis and comparison with Secondary Combustion Chamber
In order to verify the combustion optimization effect of the auxiliary combustion chamber rapid combustion device, a constant volume combustion chamber calculation model is constructed as shown in fig. 4. The calculation lasts 3ms, corresponding to 117 ℃ A at 6500 rpm. The ignition position of the scheme with or without the auxiliary combustion chamber is shown in fig. 5(a) and 5 (b).
As can be seen from fig. 6(a) and 6(b), of the two schemes, the scheme with the auxiliary combustion chamber device has the fastest combustion speed, and the heat release rate and the pressure rise rate reach the peak value firstly. The combustion speed of the combustion chamber without the auxiliary combustion chamber is slower, and particularly in the ignition process, the time consumed by 5% of reaction of the combustion chamber structure with the auxiliary combustion chamber is about 38% faster than that of the combustion chamber structure without the auxiliary combustion chamber. (the combustion time in the auxiliary combustion chamber is not counted, and the combustion time is compared with the combustion time from the main combustion chamber), therefore, the calculation result shows that the quick combustion device for the auxiliary combustion chamber can effectively accelerate the combustion speed of the engine.
2.2 Angle of Secondary Combustion Chamber hole optimally matches with Main Combustion Chamber
The quick combustion device of the auxiliary combustion chamber is a cylindrical structure sleeve, and the inner cylindrical space is the auxiliary combustion chamber. In order to optimize and match the flame injection angle of the small holes with the structural space of the main combustion chamber and enable the quick combustion device of the auxiliary combustion chamber to exert greater advantages, five small circular holes and five small circular holes which are asymmetrically arranged are uniformly and symmetrically arranged at the front end of the auxiliary combustion chamber in the circumferential direction, namely a scheme I and a scheme II are respectively designed, and the scheme I and the scheme II are shown in a symmetrical arrangement scheme of a graph 7(a) and an asymmetrical arrangement scheme of a graph 7 (b).
2.3 analysis of the calculation results of the optimal matching of the angle of the auxiliary combustion chamber hole and the main combustion chamber
As can be seen from FIG. 8, the burn rate progression is substantially the same for both schemes, with the reaction progression being faster for scheme two than for scheme one in the range of 1.2 to 2.0 ms. So the combustion effect of scheme two is better, and the burning rate is faster, has consequently also proved that five aperture schemes of asymmetric arrangement can make the flame distribution in the main combustion chamber more even, make the combustion that the gas mixture in the main combustion chamber is faster, have accelerated combustion reaction rate greatly.
2.4 simulation calculation analysis of the diameter of the secondary combustion chamber hole
The diameter of the small hole of the quick combustion device of the auxiliary combustion chamber has an important relation with the jet speed of the jet flame, so that the combustion speed of the engine mixture is also influenced. Fig. 9 shows the simulation calculation analysis of the small holes with different diameters on the secondary combustion chamber.
From the flame injection speeds of different pore diameters in fig. 9, the diameter of the pore with the diameter of 1.25mm has the fastest flame injection speed in the analog simulation calculation group, so that the pore with the diameter can be beneficial to igniting the mixed gas in the main combustion chamber more quickly, and the effect of the faster combustion speed of the mixed gas is achieved.
Third, test verification of quick combustion device of auxiliary combustion chamber
Based on the simulation calculation result, relevant test verification is carried out, and RP-3 aviation kerosene is adopted as the fuel of the test engine, the saturated vapor pressure of the aviation kerosene is lower and is about 1/10 of gasoline, and the evaporation characteristic is poor.
As can be seen from the test result cylinder pressure curve shown in FIG. 10, the scheme of the quick combustion device with the auxiliary combustion chamber has the advantages of higher combustion speed, higher pressure rise rate, pressure ratio reaching the peak value first and larger maximum explosion pressure, and further the power of the engine is improved.
In conclusion, through simulation, calculation and analysis and comprehensive verification of test results, the combustion speed of the engine with low-evaporation-characteristic fuel can be effectively increased to a certain extent by the aid of the quick combustion device with the auxiliary combustion chamber, so that the working efficiency of the engine is increased, and meanwhile, the feasibility of the quick combustion device for improving the combustion speed of the low-evaporation-characteristic fuel is fully proved.
The above-mentioned embodiments are intended to illustrate the objects, technical solutions and advantages of the present invention in further detail, and it should be understood that the above-mentioned embodiments are only exemplary embodiments of the present invention and are not intended to limit the present invention, and any modifications, equivalents, improvements and the like made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an engine combustion device, its characterized in that, including main combustion chamber, spark plug, vice combustion chamber and flame jet hole, wherein, initial flame passes through the spark plug and discharges electricity in vice combustion chamber and produces, flame produces and develops rapidly in vice combustion chamber afterwards, and then produces stranded jet flame through connecting a plurality of flame jet holes of vice combustion chamber and main combustion chamber, and stranded jet flame sprays simultaneously and gets into main combustion chamber, is equivalent to main combustion chamber's high-energy multinuclear ignition source, and the gas mixture in the main combustion chamber is lighted by many places large tracts of land flame simultaneously.
2. The engine combustion apparatus of claim 1, wherein the number of flame injection holes in the circumferential direction below the secondary combustion chamber structure is five, and the five flame injection holes are asymmetrically arranged to match the primary combustion chamber structure.
3. The engine combustion device of claim 2, wherein the engine combustion device is designed with a positioning protrusion structure to ensure that the five jet flame points generated by the asymmetric arrangement of the five flame spray holes are matched with the main combustion chamber.
4. The engine combustion device of claim 3, wherein each of the five flame spray holes is angled differently and are arranged at different angles.
5. The engine combustion device of claim 4, wherein the diameter, placement position and angle of the flame orifices are calculated from an optimized match to the combustion chamber.
6. The engine combustion device of claim 5, wherein the specific dimensional parameters of the flame orifices are as follows:
range of diameter of the spray hole: 1.0-1.5 mm;
the inclination angle of the spray hole is as follows: 20-90 degrees relative to the central line of the device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010520415.7A CN111485992A (en) | 2020-06-09 | 2020-06-09 | Engine rapid combustion device suitable for low-evaporation characteristic fuel |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010520415.7A CN111485992A (en) | 2020-06-09 | 2020-06-09 | Engine rapid combustion device suitable for low-evaporation characteristic fuel |
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| CN111485992A true CN111485992A (en) | 2020-08-04 |
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| CN202010520415.7A Pending CN111485992A (en) | 2020-06-09 | 2020-06-09 | Engine rapid combustion device suitable for low-evaporation characteristic fuel |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113803150A (en) * | 2021-08-24 | 2021-12-17 | 潍柴动力股份有限公司 | Speed response separation type combustion system and engine |
| CN115013143A (en) * | 2022-07-13 | 2022-09-06 | 天津大学 | Ignition type aviation kerosene engine combustion system and control method |
| CN115523070A (en) * | 2022-05-05 | 2022-12-27 | 湘潭大学 | Hydrogen jet ignition device |
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| DE2406805A1 (en) * | 1973-02-14 | 1974-08-22 | Honda Motor Co Ltd | COMBUSTION MACHINE WITH AT LEAST ONE CYLINDER |
| JP2000337150A (en) * | 1999-05-26 | 2000-12-05 | Yanmar Diesel Engine Co Ltd | Combustion method in sub-chamber type spark ignition engine |
| WO2008052246A1 (en) * | 2006-10-31 | 2008-05-08 | Turner, Geoffrey Russell | Internal combustion engine and method |
| CN107332109A (en) * | 2017-04-26 | 2017-11-07 | 周向进 | The spark plug and its internal combustion engine and automobile of a kind of flame |
| JP2018066369A (en) * | 2016-10-14 | 2018-04-26 | 本田技研工業株式会社 | Gas engine |
| WO2020048775A1 (en) * | 2018-09-07 | 2020-03-12 | Daimler Ag | Precombustion chamber spark plug for a combustion chamber of an internal combustion engine, in particular of a motor vehicle |
| CN213016533U (en) * | 2020-06-09 | 2021-04-20 | 天津内燃机研究所（天津摩托车技术中心） | Engine rapid combustion device suitable for low-evaporation characteristic fuel |
-
2020
- 2020-06-09 CN CN202010520415.7A patent/CN111485992A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2406805A1 (en) * | 1973-02-14 | 1974-08-22 | Honda Motor Co Ltd | COMBUSTION MACHINE WITH AT LEAST ONE CYLINDER |
| JP2000337150A (en) * | 1999-05-26 | 2000-12-05 | Yanmar Diesel Engine Co Ltd | Combustion method in sub-chamber type spark ignition engine |
| WO2008052246A1 (en) * | 2006-10-31 | 2008-05-08 | Turner, Geoffrey Russell | Internal combustion engine and method |
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| CN213016533U (en) * | 2020-06-09 | 2021-04-20 | 天津内燃机研究所（天津摩托车技术中心） | Engine rapid combustion device suitable for low-evaporation characteristic fuel |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113803150A (en) * | 2021-08-24 | 2021-12-17 | 潍柴动力股份有限公司 | Speed response separation type combustion system and engine |
| CN113803150B (en) * | 2021-08-24 | 2023-01-20 | 潍柴动力股份有限公司 | Speed response separation type combustion system and engine |
| CN115523070A (en) * | 2022-05-05 | 2022-12-27 | 湘潭大学 | Hydrogen jet ignition device |
| CN115013143A (en) * | 2022-07-13 | 2022-09-06 | 天津大学 | Ignition type aviation kerosene engine combustion system and control method |
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