CN211144677U

CN211144677U - Jet igniter of water-cooled engine

Info

Publication number: CN211144677U
Application number: CN201921111020.0U
Authority: CN
Inventors: 卫海桥; 华剑雄; 周磊; 高强; 冯钟辉; 舒歌群
Original assignee: Tianjin University
Current assignee: Tianjin University
Priority date: 2019-07-15
Filing date: 2019-07-15
Publication date: 2020-07-31
Anticipated expiration: 2029-07-15

Abstract

The utility model relates to a water-cooled engine jet igniter, which comprises an upper cavity and a lower cavity, wherein an oil injector and a spark plug are fixed on the upper cavity; the lower cavity comprises a cavity which is a precombustion chamber, and the tail end of the lower cavity is provided with a jet hole. The utility model has the advantages of lower oil consumption, good cooling effect and longer service life.

Description

Jet igniter of water-cooled engine

Technical Field

The utility model relates to an internal-combustion engine combustion technology field is a water-cooled engine jet igniter, can be used to the rarefied combustion of ignition engine and promote flame with higher speed, also can regard as the initial flame igniter that ignites of compression ignition engine.

Background

At present, how to further improve the thermal efficiency of internal combustion engines to reduce carbon dioxide emissions has long been a common concern worldwide. The traditional ignition engine ignites the chemical equivalent gas mixture uniformly mixed in the cylinder through the spark plug to form flame which is spread outwards, thereby pushing the piston to do work and generating power output. However, such spark ignition combustion has several problems that limit the improvement of the thermal efficiency: 1) the burning rate is limited by the flame propagation rate, and the burning is slow; 2) the combustion needs to be carried out at a stoichiometric ratio, and the lean state easily causes ignition failure of a spark plug and a slower combustion rate; 3) the tail end is easy to generate spontaneous combustion under the equivalent ratio combustion state, so that knocking is generated, the improvement of a compression ratio is limited, and the further improvement of the heat efficiency is limited.

Chinese patent CN106194395A discloses an engine turbulent jet ignition prechamber combustion system which can increase the combustion speed of the ignition engine and realize lean combustion, but the patent does not give a detailed igniter cooling structure and a detailed structure and installation manner of the prechamber.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing an oil consumption is lower, and the cooling effect is good, longer engine jet igniter of life-span.

The technical scheme is as follows:

a water-cooled engine jet igniter comprises an upper cavity and a lower cavity, wherein an oil injector and a spark plug are fixed on the upper cavity; the lower cavity comprises a cavity which is a precombustion chamber, and the tail end of the lower cavity is provided with a jet hole.

Preferably, the horizontal cross-section of the prechamber is circular arc rectangular, so that the prechamber has a smaller volume.

The contact surface of the lower cavity and the upper cavity is determined by a positioning pin so as to ensure that the installation angle of the lower cavity is matched with the positions of the oil injector and the spark plug, and the lower cavity and the upper cavity are fixed by a lower cavity fastening ring.

The oil injection direction of the oil injector fixed on the upper cavity faces the lower part of the spark plug.

The precombustion chamber is enclosed by the lower end surface of the upper cavity, the bottom surface of the oil sprayer, the bottom surface of the spark plug and the inner cavity of the lower cavity, and is communicated with the outside through the jet hole, so that jet acceleration of flame from the precombustion chamber to the outside is realized.

The interior of the upper cavity body is provided with a cooling water channel, and cooling liquid flows in and flows out through a cooling liquid inlet pipe and a cooling liquid outlet pipe which are arranged on the upper cavity body.

Drawings

FIG. 1 is an exploded view of the entire components of the jet igniter of the present invention

FIG. 2 is a vertical cross-sectional view of the fluidic igniter

FIG. 3 is a detailed structure of the lower end surface of the upper chamber 2 and the upper end surface of the lower chamber 4

FIG. 4 is a cooling water passage structure diagram of the jet igniter of the present invention

FIG. 5 shows a fuel supply structure

FIG. 6 is a structural diagram of all the parts of the present invention after being installed

Reference numerals:

1-spark plug, 2-upper cavity, 3-positioning pin a, 4-lower cavity, 5-lower cavity fastening ring, 6-positioning pin b, 7-water channel shell, 8-oil injector, 9-oil injector fastening bolt, 10-cooling liquid inlet pipe, 11-cooling liquid outlet pipe, 12-precombustion chamber, 13-jet hole, 14-oil beam, 15-positioning pin hole a, 16-positioning pin hole b, 17-cooling water channel, 18-fuel oil inlet, 19-high-pressure oil pipe connecting thread, 20-oil injector joint, 21-lower cavity mounting thread

Detailed Description

The utility model provides a water-cooled engine jet igniter, which consists of an upper cavity and a lower cavity, wherein the upper cavity is provided with an oil injector, a spark plug and an oil injector fastening bolt; the lower cavity comprises a cavity which is a precombustion chamber, the oil injector arranged in the upper cavity is a single-hole inclined oil injector, and the oil injection direction of the oil injector faces to the lower part of the spark plug. The horizontal cross section of the precombustion chamber is in a circular arc rectangle, so that the precombustion chamber has smaller volume. The upper cavity is provided with a cooling water channel, the downward depth of the cooling water channel is as close to the position of a fuel injector sealing ring as possible, and the cooling water channel surrounds the periphery of the fuel injector for a circle so as to ensure a better cooling effect.

The utility model provides a water-cooled engine jet point firearm contains 11 spare parts such as upper and lower cavities altogether, contains precombustion chamber structure, cooling water course structure and sprayer fuel feeding structure from the functional structure, and the following will combine the drawing to carry out detailed description to all spare parts and all structures.

Fig. 1 is an exploded view of all the parts of the fluidic igniter according to the present invention, showing a total of 11 parts constituting the fluidic igniter, which can be divided into an upper part and a lower part. The upper half part takes the cavity 2 as a core and comprises a spark plug 1, an upper cavity 2, an oil injector 8, an oil injector fastening bolt 9, cooling liquid inlet and

outlet pipes

10 and 11 and a water channel shell 7; the lower cavity 4 of the lower half part is a core and comprises the lower cavity 4,

positioning pins

3 and 6 and a lower cavity fastening ring 5.

The utility model provides a water-cooled engine jet igniter main part is cavity 2 and lower cavity 4, and the relative position of cavity is confirmed through locating

3 and 6 about going up to connect fixedly through cavity tighrening ring 5 down. The upper cavity is provided with a spark plug 1 and an oil sprayer 8, and the oil sprayer is fixedly pressed on the upper cavity 2 through an oil sprayer fastening bolt 9. The precombustion chamber 12 is enclosed by the lower end face of the upper cavity 2, the bottom face of the oil sprayer, the bottom face of the spark plug and the inner cavity of the lower cavity 4, the precombustion chamber 12 is communicated with the outside through the jet hole 13, and the jet acceleration of flame from the precombustion chamber to the outside is realized. The upper cavity 2 is internally provided with a cooling water channel 17, and cooling liquid flows in and flows out through a cooling liquid inlet pipe 10 and a cooling liquid outlet pipe 11 which are arranged on the upper cavity 2.

The fuel injector 8 and the spark plug 1 are installed at corresponding positions of the upper cavity 2, because the installation space is limited, the spark plug 1 needs to be installed firstly when the fuel injector 8 is installed, if the installation sequence is wrong (for example, the fuel injector is installed firstly, and then the spark plug is installed), the fuel injector can interfere with the installed fuel injector when the spark plug is installed, and the specific relative positions of the fuel injector and the spark plug are shown in the attached figure 2. Similarly, the fuel injector 8 should be removed first, and then the spark plug 1 should be removed. It should be noted that, because the sealing ring of the fuel injector 8 is in interference fit with the upper cavity 2, the times of assembling and disassembling the fuel injector should be reduced as much as possible to ensure the reliability of the sealing ring. The fuel injector 8 is fixed in the upper cavity 2 through a fuel injector fastening bolt 9. The cooling liquid inlet and

outlet pipes

10 and 11 are installed on the upper cavity 2, and the installation of the upper cavity part is completed after the water channel shell 7 is fixed on the upper cavity 2 through welding. The lower cavity 4 is positioned by the

positioning pins

3 and 6, and then is connected with the upper cavity by the lower cavity fastening ring 5.

Combustion chamber structure

Fig. 2 is a vertical cross-sectional view of the fluidic igniter, showing the relative positions of the spark plug 1 and the fuel injector 8, the shape of the combustion chamber 12, and the direction of the injected fuel jet 14. The oil injector 8 is a single-hole oil injector, and the oil injection flow coefficient of the oil injector is required to be as small as possible so as to reasonably control the oil injection pulse width. The number of the spray holes of the oil injector 8 is a single hole, and the spray holes are obliquely arranged, so that the spray direction of the spray holes faces to the lower part of the spark plug, and better oil-gas mixture is obtained.

Fig. 3 is a detailed structure of the lower end surface of the upper chamber 2 and the upper end surface of the lower chamber 4. The horizontal cross section of the cavity-the precombustion chamber-in the lower cavity is in the shape of an arc rectangle, and the structure can reduce the volume of the precombustion chamber and bring better oil consumption performance to the combustion of an engine. Since the pre-combustion chamber is of a non-circular structure, the long side direction of the arc rectangle must be consistent with the connecting line direction of the spark plug 1 and the fuel injector 8 during installation, so that the lower cavity 4 does not interfere with the spark plug 1 and the fuel injector 8 during installation. Locating

pins

3 and 6 are arranged between the upper cavity 2 and the lower cavity 4, so that the relative positions of the upper cavity and the lower cavity in the installation process can be kept unchanged, and the interference of parts in the installation process is avoided. A copper gasket can be arranged between the upper cavity and the lower cavity, and the upper cavity and the lower cavity are reliably sealed through slight deformation of the copper gasket after installation so as to bear high temperature and high pressure generated by combustion in the pre-combustion chamber. In addition, the end faces of the upper and lower cavities must ensure sufficient flatness to ensure sealing of the prechamber after installation. In this embodiment, the number of the jet holes at the end of the lower cavity is 7, the diameter of each jet hole is 1.5mm, the number of the jet holes can be 1-7, and the size of the jet holes can be 1.0-4.0mm, according to the application scenario, the optimal result is obtained in the specific implementation.

Cooling water channel structure

Fig. 4 is a specific cooling water passage structure diagram of the jet igniter of the present invention, which is also one of the features of the present invention, and specifically comprises a cooling liquid inlet pipe 10, a cooling liquid outlet pipe 11, an upper cavity 2 internal water passage 17, and a water passage housing 7. The water channel in the upper cavity 2 comprises two parts of completely bilaterally symmetrical structures, and each part of the structure consists of a vertical section and a horizontal section. The vertical section should be as deep as possible, as close to the depth of the injector seal ring as possible, in order to sufficiently cool the pre-combustion chamber and the injector; the horizontal section is positioned at the side of the oil sprayer, so that the oil sprayer can be better protected from being damaged by high temperature; the two horizontal sections are connected through a water channel shell 7, and in order to ensure the tightness of the water channel, the water channel shell 7 needs to be welded on the upper cavity 2. Mounting threads are arranged at the position, close to the upper end face, of the vertical section of the cooling water channel in the upper cavity 2, and the cooling liquid inlet pipe 10 and the cooling liquid outlet pipe 11 are mounted on the upper cavity 2 through the threads. Therefore, the cooling liquid can enter the cooling water channel 17 through the cooling liquid inlet pipe 10, and the cooling liquid flows out of the cooling liquid outlet pipe 11 after passing through the left vertical section, the left horizontal section, the water channel shell 7, the right horizontal section and the right vertical section in fig. 4. The coolant is not limited in kind, and may be a liquid medium such as water, engine coolant, or coolant.

Fuel supply structure

Fig. 5 shows a fuel supply structure, and a fuel injector fastening bolt 9 is installed in the upper cavity 2 through threads to realize compression of the fuel injector 8. The fuel injector fastening bolt 9 is of a hollow structure, and the middle through hole 18 is a fuel inlet and is communicated with an oil inlet on the fuel injector. The other end of the injector clamp bolt 9 is also threaded for connection to a fuel line. The middle part of the fuel injector fastening bolt 9 is of a hexagonal structure, so that the fuel injector fastening bolt can be conveniently installed and fastened by using a tool, if the tool and the cooling liquid inlet and

outlet pipes

10 and 11 are installed in the process of installing the fastening bolt 9, the fastening bolt can be installed firstly, and then the cooling liquid inlet and

outlet pipes

10 and 11 are installed.

Operating mode of igniter

Fig. 6 is the utility model discloses the structure picture after all spare parts installation, after all parts are all installed, this jet igniter installs on engine cylinder cover through cavity installation screw thread 21 down, advances with the coolant liquid pipeline that the size matches, goes out

pipe

10 and 11 and links to each other, passes through screw thread 19 with engine fuel pipe and sprayer fastening bolt 9 again and is connected, inserts fuel injection signal line sprayer joint 20 at last to overlap the ignition wire on the spark plug, this jet igniter can normally work.

For lean burn conditions of the engine, the injector 8 provides an appropriate additional fuel supply into the pre-chamber so that the fuel concentration in the pre-chamber is near stoichiometric when the engine combustion chamber fuel is in a lean condition. After passing through the jet hole, the flame combusted in the precombustion chamber generates a high-temperature high-activity jet substance, and the jet substance is used as a high-temperature high-activity heat source for multipoint ignition in an engine combustion chamber to ignite the lean gas in the combustion chamber, so that the stable combustion of the engine in a lean state is realized. The fuel injection by the fuel injector 8 should take place during the compression stroke of the engine in order to avoid fuel from the prechamber from spreading to the main combustion chamber, while the fuel injection from the prechamber cannot be delayed too much in order to avoid unstable combustion and excessive soot formation due to incomplete evaporation of the fuel. The control of said injectors 8 should be independent of the control of the main injectors of the engine to ensure the accuracy of the fuel quantity in the prechamber.

The utility model provides a water-cooled gasoline jet igniter, firstly, the jet igniter adopts turbulent jet flame to ignite the mixed gas in a combustion chamber, thereby solving the problem of slow combustion; secondly, during lean combustion, an additional oil supply device is arranged in the pre-combustion chamber, so that the mixed gas in the pre-combustion chamber is near the chemical equivalence ratio, and the problem of lean combustion fire is solved; moreover, lean combustion is realized, the heat efficiency is obviously improved, the knocking tendency of the engine is greatly reduced, and the compression ratio can be further improved, so that the heat efficiency is improved.

Compared with the Chinese patent CN106194395A, the water cooling system structure provided by the patent has the advantages that the water cooling system structure is detailed, the water cooling system structure is in the shape of a precombustion chamber with a circular arc rectangular horizontal section, and the volume of the precombustion chamber can be further reduced.

Claims

1. A water-cooled engine jet igniter comprises an upper cavity and a lower cavity, wherein an oil injector and a spark plug are fixed on the upper cavity; the lower cavity comprises a cavity which is a precombustion chamber, and the tail end of the lower cavity is provided with a jet hole.

2. The water-cooled engine jet igniter according to claim 1, wherein the horizontal cross section of the pre-combustion chamber is a circular arc rectangle, thereby enabling the pre-combustion chamber to have a smaller volume.

3. The water-cooled engine jet igniter according to claim 1, wherein the contact surface of the lower cavity and the upper cavity is determined by a positioning pin to ensure that the installation angle of the lower cavity is matched with the positions of the fuel injector and the spark plug, and the lower cavity and the upper cavity are fixed by a lower cavity fastening ring.

4. The water-cooled engine jet igniter according to claim 1, wherein the fuel injection direction of the fuel injector fixed to the upper cavity is directed below the ignition plug.

5. The water-cooled engine jet igniter according to claim 1, wherein the pre-combustion chamber is defined by a lower end surface of the upper cavity, a bottom surface of the injector, a bottom surface of the spark plug and an inner cavity of the lower cavity, and the pre-combustion chamber is communicated with the outside through a jet hole to realize jet acceleration of flame from the pre-combustion chamber to the outside.

6. The water-cooled engine jet igniter according to claim 1, wherein the upper chamber has a cooling water passage formed therein, and the coolant flows in and out through a coolant inlet pipe and a coolant outlet pipe installed in the upper chamber.