CN214170667U

CN214170667U - Pre-combustion ignition device, combustion device and engine

Info

Publication number: CN214170667U
Application number: CN202022617032.XU
Authority: CN
Inventors: 陈策远; 韦静思; 许汉君; 武珊; 刘明嘉; 马桂香
Original assignee: Guangzhou Automobile Group Co Ltd
Current assignee: Guangzhou Automobile Group Co Ltd
Priority date: 2020-11-12
Filing date: 2020-11-12
Publication date: 2021-09-10
Anticipated expiration: 2030-11-12

Abstract

The utility model relates to a precombustion ignition device, combustion device and engine, including precombustion chamber, spark plug, sprayer, first pressure sensor, second pressure sensor and electrical control unit, spark plug and sprayer set up on the precombustion chamber, are provided with air inlet, oil inlet, jet and hold the chamber on the sprayer; the first pressure sensor is used for detecting the pressure of the precombustion chamber, and the second pressure sensor is used for detecting the pressure of the mixture of air and fuel in the accommodating cavity; the electronic control unit is used for controlling the injection opening to be opened so as to inject the mixed gas into the precombustion chamber through the injection opening. The flow velocity of the mixed gas is kept unchanged, and the total injection quantity of the mixed gas can be accurately controlled by controlling the injection pulse width, so that the equivalence ratio of the mixed gas in the injector can be controlled, and the combustion stability is improved.

Description

Pre-combustion ignition device, combustion device and engine

Technical Field

The utility model belongs to the technical field of the engine of car, especially, relate to a fire ignition, burner and engine precombuste.

Background

When the engine is started, the air-fuel mixture needs to be ignited by the ignition device. The ignition device not only affects the dynamic property, the economical efficiency and the emission performance of the engine, but also determines whether the engine can work normally.

In recent years, active prechamber ignition devices have been used in more and more engines, facing increasingly stringent fuel consumption and emission regulations. The ignition device is provided with the spark plug and the fuel injector on the precombustion chamber simultaneously, can ignite stably and quickly, realizes ultra-lean combustion with lambda >2.0, and has stable combustion, thereby obviously reducing the combustion loss. However, the ignition device also has some problems: 1) the ventilation effect in the pre-combustion chamber is poor, and the stability of the ultra-lean combustion working condition and the high EGR working condition is limited; 2) the problem of wall collision of oil bundles in the limited space of the precombustion chamber is obvious, and the wall wetting quantity is large (the wall wetting quantity of the traditional combustion chamber is usually less than 0.8 percent, and the wall wetting quantity in the precombustion chamber can be more than 20 percent by adopting a common fuel injector); 3) due to poor mixing of the fuel in the prechamber, the equivalence ratio distribution is not uniform, which deteriorates the emission performance. Due to the above technical deficiencies, the widespread use of active prechamber ignition devices presents major challenges.

An existing active pre-combustion chamber ignition system generally comprises a pre-combustion chamber, a spark plug, an oil supply pipeline, an air supply pipeline, an oil-air mixing chamber and an injection valve, wherein the spark plug and the injection valve are arranged on the pre-combustion chamber, the oil supply pipeline is connected with an oil inlet of the oil-air mixing chamber, the air supply pipeline is connected with an air inlet of the oil-air mixing chamber, and the oil-air mixing chamber is used for mixing fuel oil and air and then injecting the mixture into the pre-combustion chamber through an outlet of the injection valve. The scheme adopts the air auxiliary fuel injection of the precombustion chamber, namely the fuel is not directly injected in the precombustion chamber, but the mixed gas of the air and the fuel is injected, so that the wall wetting quantity caused by fuel injection in the narrow precombustion chamber can be reduced, and meanwhile, the waste gas in the precombustion chamber is discharged. However, the injection flow is usually affected by the difference between the working pressure of the injection valve and the pressure in the precombustion chamber, and the pressure in the precombustion chamber changes greatly, so that the air injection amount of the air-fuel mixture cannot be accurately controlled, and the ignition and combustion of the engine are unstable.

SUMMERY OF THE UTILITY MODEL

The utility model discloses the technical problem that will solve is: aiming at the problems that the pressure change in the precombustion chamber is large, so that the air injection quantity of mixed gas cannot be accurately controlled, and the ignition and combustion of an engine are unstable in the conventional active precombustion chamber ignition system, the precombustion ignition device, the combustion device and the engine are provided.

In order to solve the technical problem, an embodiment of the present invention provides a pre-combustion ignition device, including a pre-combustion chamber, a spark plug, an injector, a first pressure sensor, a second pressure sensor and an electronic control unit, wherein the spark plug, the injector, the first pressure sensor and the second pressure sensor are respectively electrically connected to the electronic control unit, the spark plug and the injector are disposed on the pre-combustion chamber, the injector is provided with an air inlet, an oil inlet and a jet orifice, and air entering from the air inlet and fuel entering from the oil inlet are mixed in an accommodating cavity disposed in the injector to form a mixture;

the first pressure sensor is used for detecting the pressure of the precombustion chamber, and the second pressure sensor is used for detecting the pressure of the mixed gas in the accommodating cavity; the electronic control unit is used for controlling the injection port to be opened so as to inject the mixed gas into the precombustion chamber through the injection port.

Optionally, the injector comprises a pre-combustion chamber injector, a mixing container and a nozzle, an inner cavity of the mixing container is vertically communicated, the accommodating cavity comprises a mixing cavity formed at one end, close to the nozzle, of the inner cavity of the mixing container, the air inlet is arranged on the mixing container and communicated with the mixing cavity, the nozzle is provided with the injection port, the injection port is communicated with the mixing cavity when opened, and the injection port is blocked from the mixing cavity when closed;

the oil inlet is arranged at the first end of the precombustion chamber oil sprayer, the second end of the precombustion chamber oil sprayer is inserted into the inner cavity of the mixing container, and the oil outlet of the precombustion chamber oil sprayer is communicated with the mixing cavity;

the nozzle comprises a nozzle body, a needle valve body and a control mechanism, the inner cavity of the nozzle body is communicated up and down, the jet orifice is formed at one end, close to the precombustion chamber, of the inner cavity of the nozzle body, and the needle valve body is movably arranged in the inner cavity of the nozzle body;

the control mechanism is electrically connected with the electric control unit and is used for controlling the needle valve body to move towards the direction close to or far away from the precombustion chamber so as to open or close the jet orifice.

Optionally, the accommodating chamber further comprises a storage chamber formed at one end of the inner cavity of the nozzle body close to the jet orifice, the mixing chamber, the storage chamber and the jet orifice are sequentially communicated when the jet orifice is opened, and the storage chamber is blocked from the mixing chamber when the jet orifice is closed;

the second pressure sensor is used for detecting the pressure of the mixed gas in the storage cavity and feeding the pressure back to the electronic control unit.

Optionally, an end of the injection port close to the prechamber forms a first tapered hole, an end of the injection port far from the prechamber forms a second tapered hole, a cross section of the first tapered hole gradually increases from the end far from the prechamber to the end close to the prechamber, a cross section of the second tapered hole gradually increases from the end far from the prechamber to the end close to the prechamber, an end of the second tapered hole far from the prechamber is connected with an end of the first tapered hole close to the prechamber, and an end of the second tapered hole close to the prechamber is radially outside an end of the second tapered hole far from the prechamber.

Optionally, one end of the needle valve body close to the pre-combustion chamber forms a needle valve head, and the cross section of the needle valve head is gradually increased from one end far away from the pre-combustion chamber to one end close to the pre-combustion chamber;

when the injection port is opened, a tapered flow passage is formed between the hole wall of the first tapered hole and the outer peripheral surface of the needle valve head, and the flow area of the tapered flow passage is gradually reduced from one end far away from the pre-combustion chamber to one end close to the pre-combustion chamber; and an equidistant flow passage is formed between the hole wall of the second tapered hole and the outer peripheral surface of the needle valve head, and the distance between the hole wall of the second tapered hole and the outer peripheral surface of the needle valve head is kept unchanged from one end far away from the precombustion chamber to one end close to the precombustion chamber.

Optionally, the accommodating chamber further includes a movable chamber formed in a middle section of the inner chamber of the nozzle body, the movable chamber communicating with the mixing chamber when the injection port is opened.

Optionally, the control mechanism includes armature, elastic component and solenoid, armature is fixed keeping away from of needle valve body the one end of precombustion chamber, armature holds in the activity chamber, the elastic component supports be in the armature is close to on one side of precombustion chamber and the axial one side chamber wall of activity chamber, the elastic component promotes along keeping away from the direction of precombustion chamber armature, solenoid is around establishing the outside of armature, solenoid with the electrical control unit electricity is connected, armature when solenoid circular telegram to being close to the direction of precombustion chamber removes in order to compress the elastic component.

Optionally, the second end of the pre-chamber fuel injector is in sealing connection with the inner cavity of the mixing container.

On the other hand, the utility model also provides a combustion apparatus, including main combustion chamber, main combustion chamber sprayer and aforementioned arbitrary technical scheme precombustion ignition, main combustion chamber sets up the below of precombustion chamber and with the precombustion chamber intercommunication, main combustion chamber sprayer sets up on the main combustion chamber.

On the other hand, the utility model also provides an engine, including aforementioned arbitrary technical scheme precombustion ignition.

The embodiment of the utility model provides a precombustion ignition, burner and engine, compared with the prior art, earlier with fuel and air leading-in hold the intracavity and carry out intensive mixing in order to form the gas mixture, then when reaching the predetermined injection moment of sprayer, and the electronic control unit judges the ratio of the pressure that holds the chamber that second pressure sensor detected and the pressure of the precombustion chamber that first pressure sensor detected when more than 2, open the jet, spout the gas mixture in the precombustion chamber with the sound velocity from the jet, then the gas mixture in the precombustion chamber is lighted to the spark plug, the flame of formation reentrants the gas mixture in the main combustion chamber in order to light the main combustion chamber. Because the flow velocity of the mixed gas at the injection port reaches the sound velocity, the choking effect is generated at the position, the flow velocity of the mixed gas is kept unchanged and cannot be changed along with the change of the pressure in the precombustion chamber, the total injection quantity of the mixed gas can be accurately controlled by controlling the injection pulse width, so that the oil injection quantity required in the injector can be accurately calculated, the equivalence ratio of the mixed gas in the injector can be further controlled, the quick and stable ignition process is realized, and the combustion stability under the lean-burn working condition and the high EGR rate working condition is improved.

Drawings

Fig. 1 is a schematic structural diagram of a combustion apparatus according to an embodiment of the present invention;

FIG. 2 is an exploded view of the pre-ignition device of FIG. 1;

FIG. 3 is a cross-sectional view of the mixing chamber of FIG. 2;

FIG. 4 is a cross-sectional view of the nozzle of FIG. 2 in a closed position;

FIG. 5 is a cross-sectional view of the nozzle of FIG. 2 in an open state;

FIG. 6 is a schematic view of the nozzle body of FIG. 4;

fig. 7 is a characteristic diagram of the change of the cumulative mass of the outflow injected into the precombustion chamber by the combustion apparatus according to the embodiment of the present invention at different fuel-on times.

The reference numerals in the specification are as follows:

10. a pre-combustion ignition device; 1. a precombustion chamber; 2. a spark plug; 3. an ejector; 31. a pre-combustion chamber fuel injector; 311. an oil inlet; 312. an oil outlet; 32. a mixing vessel; 321. an air inlet; 322. a mixing chamber; 323. An O-shaped groove; 324. a mating hole; 325. a second mounting hole; 33. a nozzle; 331. a nozzle body; 3311. a first tapered bore; 3312. a second tapered bore; 3313. a storage chamber; 3314. a first mounting hole; 3315. a communicating hole; 3316. a movable cavity; 332. a needle valve body; 3321. a needle valve head; 333. equidistant flow channels; 334. a tapered flow channel; 335. an armature; 336. an elastic member; 337. an electromagnetic coil; 338. a power plug; 339. an ejection port;

20. a main combustion chamber; 30. an air inlet; 40. an exhaust hole; 50. a main combustion chamber fuel injector;

60. a gas supply assembly; 61. an air cleaner; 62. a throttle valve; 63. a voltage stabilizing cavity; 64. a flow meter; 65. An air compressor; 66. an air tank; 67. a pressure regulating valve; 68. a one-way valve;

70. an oil supply assembly; 71. an oil tank; 72. a low pressure pump; 73. a fuel filter; 74. a high pressure pump; 75. An oil rail; 76. a fuel pressure sensor.

Detailed Description

In order to make the technical problem, technical solution and advantageous effects solved by the present invention more clearly understood, the following description is given in conjunction with the accompanying drawings and embodiments to illustrate the present invention in further detail. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.

As shown in fig. 1 and fig. 2, the embodiment of the present invention provides a precombustion ignition device 10, including precombustion chamber 1, spark plug 2, injector 3, first pressure sensor, second pressure sensor and electronic control unit, spark plug 2, injector 3, first pressure sensor and second pressure sensor are connected with electronic control unit electricity respectively, spark plug 2 and injector 3 set up on precombustion chamber 1, be provided with air inlet 321 on injector 3, oil inlet 311 and jet 339, the air that gets into by air inlet 321 mixes in the holding chamber that sets up in injector 3 with the fuel that gets into by oil inlet 311 in order to form the gas mixture.

The first pressure sensor is used for detecting the pressure of the precombustion chamber 1 and feeding back the pressure to the electronic control unit, and the second pressure sensor is used for detecting the pressure of the mixed gas in the accommodating cavity and feeding back the pressure to the electronic control unit.

When the preset injection time of the injector 3 is reached and the electronic control unit judges that the ratio of the pressure of the mixture in the accommodating chamber to the pressure of the precombustion chamber 1 is more than 2, the injection port 339 is controlled to be opened so as to inject the mixture into the precombustion chamber 1 through the injection port 339 at the sound velocity.

Firstly, fuel oil and air are introduced into an accommodating cavity and are fully mixed to form mixed gas, then when the preset injection time of an injector 3 is reached and an electric control unit judges that the ratio of the pressure of the accommodating cavity to the pressure of a precombustion chamber 1 is greater than or equal to 2, an injection port 339 is opened, the mixed gas is injected into the precombustion chamber 1 from the injection port 339 at the sound velocity, then a spark plug 2 ignites the mixed gas in the precombustion chamber 1, and the generated flame enters a main combustion chamber 20 to ignite the mixed gas in the main combustion chamber 20; then, when the electronic control unit judges that the ratio of the pressure of the accommodating cavity to the pressure of the precombustion chamber 1 is less than 2, the injection port 339 is closed.

The embodiment of the utility model provides a precombustion ignition device 10, compared with the prior art, because the gas mixture flow rate of jet 339 department reaches the sound velocity, this department produces "choked up" effect, the velocity of flow of gas mixture remains unchanged, can not change along with the change of 1 internal pressure in precombustion chamber, can spray the total amount of injection of the accurate control gas mixture of pulse width through control, thereby can accurate calculation obtain required fuel injection quantity in sprayer 3, and then can control the equivalence ratio of gas mixture in sprayer 3, realize quick and stable ignition process, improve the combustion stability under lean burn operating mode and high EGR rate operating mode.

Preferably, the first pressure sensor is integrated on the spark plug 2, so that the types of parts of the pre-combustion ignition device 10 are reduced, the overall structure of the pre-combustion ignition device 10 is more compact, and the occupied space of the pre-combustion ignition device 10 is reduced.

In one embodiment, as shown in fig. 1 to 5, the injector 3 includes a prechamber injector 31, a mixing container 32, and a nozzle 33, an inner cavity of the mixing container 32 penetrates up and down, an accommodating cavity includes a mixing cavity 322 formed at an end of the inner cavity of the mixing container 32 near the nozzle 33, an air inlet 321 is provided on the mixing container 32 and communicates with the mixing cavity 322, an injection port 339 is provided on the nozzle 33, the injection port 339 communicates with the mixing cavity 322 when opened, and the injection port 339 is blocked from the mixing cavity 322 when closed.

The oil inlet 311 is arranged at a first end of the pre-chamber oil sprayer 31, a second end of the pre-chamber oil sprayer 31 is inserted into the inner cavity of the mixing container 32, and the oil outlet 312 of the pre-chamber oil sprayer 31 is communicated with the mixing cavity 322.

The nozzle 33 includes a nozzle body 331, a needle valve body 332, and a control mechanism, wherein an inner cavity of the nozzle body 331 penetrates vertically, an injection port 339 is formed at an end of the inner cavity of the nozzle body 331 near the prechamber 1, and the needle valve body 332 is movably disposed in the inner cavity of the nozzle body 331.

The control mechanism is electrically connected with the electronic control unit and is used for controlling the needle valve body 332 to move towards the direction close to or away from the prechamber 1 so as to open or close the jet port 339.

The second pressure sensor is used for detecting the pressure of the mixture in the mixing cavity 322 and feeding the pressure back to the electronic control unit. When the preset injection time of the injector 3 is reached and the electronic control unit judges that the ratio of the pressure of the mixture in the mixing chamber 322 to the pressure of the prechamber 1 is 2 or more, the control mechanism controls the needle valve body 332 to move in a direction approaching the prechamber 1, thereby opening the injection port 339 to inject the mixture into the prechamber 1. The fuel and the air can be fully mixed in the mixing cavity 322 and then sprayed into the precombustion chamber 1 through the jet orifice 339, so that the wall collision problem caused by fuel injection in the precombustion chamber 1 is reduced, the wall wetting quantity is reduced, the waste gas in the precombustion chamber 1 is also favorably discharged, the equivalence ratio of the mixed gas in the injector 3 can be controlled, the full combustion of the mixed gas in the precombustion chamber 1 is facilitated, the generation of incomplete combustion products is reduced, and the combustion stability is improved.

Preferably, the prechamber injector 31, the mixing container 32 and the nozzle 33 are formed separately. The ejector 3 adopts a split structure, so that the processing difficulty is reduced, and the processing precision is favorably controlled.

Preferably, the pre-combustion chamber fuel injector 31 is a standard in-cylinder direct injection fuel injector of the engine, and has the advantages of simple structure, convenient operation and cost reduction. In addition, in order to further reduce the wall wetting amount, a pressure reducing device may be added to the pre-chamber injector 31 to reduce the injection pressure of the pre-chamber injector 31.

Preferably, the nozzle 33 is made of silicon nitride, which has high strength at high temperature, can resist cold and hot shock, and has low cost. In addition, the nozzle 33 may be made of heat resistant steel.

In one embodiment, as shown in fig. 4 and 5, the receiving chamber further includes a storage chamber 3313 formed at an end of an inner cavity of the nozzle body 331 near the injection port 339, the mixing chamber 322, the storage chamber 3313, and the injection port 339 are sequentially communicated when the injection port 339 is opened, and the storage chamber 3313 is blocked from the mixing chamber 322 when the injection port 339 is closed.

The second pressure sensor is used for detecting the pressure of the mixture in the storage chamber 3313 and feeding back to the electronic control unit. When the preset injection timing of the injector 3 is reached and the electronic control unit judges that the ratio of the pressure of the mixture in the storage chamber 3313 to the pressure of the precombustion chamber 1 is 2 or more, the control mechanism controls the needle valve body 332 to move in a direction approaching the precombustion chamber 1, thereby opening the injection port 339 to inject the mixture into the precombustion chamber 1. The mixed gas in the mixing chamber 322 is sprayed out from the spraying opening 339 after passing through the storage chamber 3313, the storage chamber 3313 is always communicated with the spraying opening 339, the spraying opening 339 is communicated with the mixing chamber 322 when being opened, and the spraying opening 339 is blocked from the mixing chamber 322 when being closed, so that the storage chamber 3313 is arranged to slow down the fluctuation of the flow rate of the mixed gas generated at the moment when the spraying opening 339 is opened or closed, the flow rate and the equivalence ratio of the mixed gas can be accurately controlled, and the combustion stability is improved.

In one embodiment, as shown in fig. 6, a first tapered hole 3311 is formed at an end of the jet port 339 close to the prechamber 1, a second tapered hole 3312 is formed at an end of the jet port 339 far from the prechamber 1, a cross section of the first tapered hole 3311 gradually increases from the end far from the prechamber 1 to the end close to the prechamber 1, a cross section of the second tapered hole 3312 gradually increases from the end far from the prechamber 1 to the end close to the prechamber 1, an end of the second tapered hole 3312 far from the prechamber 1 is connected to the end of the first tapered hole 3311 close to the prechamber 1, and an end of the second tapered hole 3312 close to the prechamber 1 is located radially outside of the end of the second tapered hole 3312 far from the prechamber 1. Facilitating smoother movement of the needle valve body 332 and more precise control of the switching of the jet 339 between open and closed by the control mechanism.

In an embodiment, as shown in fig. 5 and 6, an end of the needle valve body 332 close to the prechamber 1 forms a needle head 3321, and the cross section of the needle head 3321 is gradually increased from an end far from the prechamber 1 to an end close to the prechamber 1.

When the injection port 339 is opened, a tapered flow passage 334 is formed between the hole wall of the first tapered hole 3311 and the outer peripheral surface of the needle valve head 3321, and the flow area of the tapered flow passage 334 is gradually reduced from one end far away from the prechamber 1 to one end close to the prechamber 1; an equidistant flow passage 333 is formed between the hole wall of the second tapered hole 3312 and the outer peripheral surface of the needle head 3321, and the distance between the hole wall of the second tapered hole 3312 and the outer peripheral surface of the needle head 3321 is constant from the end distant from the prechamber 1 to the end close to the prechamber 1. The mixture is accelerated to sonic velocity through the convergent flow channel 334 and then injected into the prechamber 1 through the equidistant flow channel 333. The provision of the tapered flow passage 334 accelerates the flow velocity of the air-fuel mixture to the sonic velocity, enabling the air-fuel mixture to reach the sonic velocity in a shorter time. When the injection port 339 is opened, the distance between the hole wall of the second tapered hole 3312 and the outer peripheral surface of the needle valve head 3321 is kept constant from the end far from the prechamber 1 to the end near the prechamber 1, that is, the hole wall of the second tapered hole 3312 is parallel to the outer peripheral surface of the needle valve head 3321, so that fluctuation of the flow rate of the mixture gas at the moment when the injection port 339 is opened or closed can be alleviated, and when the injection port 339 is closed, the needle valve head 3321 can abut against the hole wall of the second tapered hole 3312 to close the injection port 339, so that the sealing performance of the injection port 339 closing is improved.

In one embodiment, as shown in fig. 4 and 5, the receiving chamber further includes a movable chamber 3316 formed at a middle section of the inner cavity of the nozzle body 331, the movable chamber 3316 communicating with the mixing chamber 322 when the jet port 339 is opened;

the control mechanism comprises an armature 335, an elastic member 336 and an electromagnetic coil 337, the armature 335 is fixed at one end of the needle valve body 332 far away from the prechamber 1, the armature 335 is accommodated in the movable cavity 3316, the elastic member 336 is supported on one side of the armature 335 close to the prechamber 1 and on one axial side cavity wall of the movable cavity 3316, the elastic member 336 pushes the armature 335 in the direction far away from the prechamber 1, the electromagnetic coil 337 is wound on the outer side of the armature 335, the electromagnetic coil 337 is electrically connected with the electronic control unit, and the armature 335 moves in the direction close to the prechamber 1 when the electromagnetic coil 337 is electrified to compress the elastic member 336. Initially, the armature 335 receives a force of the elastic member 336 in a direction away from the prechamber 1, so that the needle valve head 3321 abuts against a hole wall of the second tapered hole 3312, and then the injection port 339 is closed, and when the electronic control unit determines that the injection port 339 can be opened, the electromagnetic coil 337 is energized, so that the armature 335 compresses the elastic member 336 to drive the needle valve body 332 to move in a direction close to the prechamber 1, and then the injection port 339 is opened. The control mechanism has a simple structure and is convenient for controlling the opening and closing of the jet 339.

Preferably, as shown in fig. 4, the control mechanism further comprises a power plug 338 disposed on the nozzle body 331, the power plug being electrically connected to the electromagnetic coil 337.

In one embodiment, as shown in fig. 6, a first mounting hole 3314 is formed at an end of the inner cavity of the nozzle body 331 far from the prechamber 1, the accommodating chamber further includes a communication hole 3315 formed at a middle section of the inner cavity of the nozzle body 331, the first mounting hole 3314, the communication hole 3315 and the movable chamber 3316 are sequentially communicated, an end of the mixing vessel 32 near the prechamber 1 is fixed in the first mounting hole 3314, and the mixing chamber 322 is communicated with the communication hole 3315. The structure is simple, and the installation and positioning of the mixing container 32 and the nozzle body 331 are convenient.

Preferably, an end of the mixing vessel 32 near the prechamber 1 is interference fit with the first mounting holes 3314.

In one embodiment, the second end of the pre-chamber fuel injector 31 is sealingly connected to the interior cavity of the mixing vessel 32.

Preferably, as shown in fig. 3, a second mounting hole 325 and a matching hole 324 are formed at one end of the inner cavity of the mixing container 32, which is far away from the prechamber 1, an O-shaped groove is formed at the middle section of the inner cavity of the mixing container 32, an O-shaped ring is arranged in the O-shaped groove, the second mounting hole 325, the matching hole 324, the O-shaped groove 323 and the mixing cavity 322 are sequentially communicated, the second end of the prechamber fuel injector 31 is inserted into the inner cavity of the mixing container 32 through the second mounting hole 325 and the matching hole 324, the matching hole 324 is matched with the part of the prechamber fuel injector 31, which is abutted against the matching hole 324, and the inner cavities of the prechamber fuel injector 31 and the mixing cavity 322 are hermetically connected through interference fit of the O-shaped ring and the second end of the prechamber fuel injector 31. The positioning accuracy of the pre-chamber fuel injector 31 and the mixing container 32 is improved, so that the connection between the pre-chamber fuel injector 31 and the mixing container 32 is more stable, and the shaking is avoided.

In one embodiment, the preset injection timing is a timing at which a crank angle of the engine reaches a preset angle. When the crankshaft of the engine rotates to a preset angle and the electronic control unit judges that the ratio of the pressure of the mixture in the accommodating cavity to the pressure of the precombustion chamber 1 is more than 2, the injection port 339 is controlled to be opened. If the ratio of the pressure of the mixture in the accommodating chamber to the pressure of the precombustion chamber 1 is less than 2 when the crankshaft of the engine rotates to a preset angle, the injection port 339 is not opened, the preset angle of the crankshaft of the engine needs to be reset, and the new preset angle is smaller than the previous preset angle. The preset injection time of the injector 3 is based on the rotation angle of the crankshaft of the engine, which is beneficial for the electronic control unit to better control the opening and closing of the injection port 339 and can more accurately control the total injection amount of the mixed gas.

As shown in fig. 7, the flow rate of the mixture injected from the injector 3 into the precombustion chamber 1 at different preset injection timings is linearly related to the injection time, so that the total injection amount of the mixture can be obtained according to the injection time. Since the total amount of the mixture to be injected is known, the total amount of air to be introduced and the amount of fuel to be injected by the pre-chamber fuel injector 31 can be obtained by simple calculation (based on the total amount to be injected and the equivalence ratio of the mixture), thereby ensuring the stability of the pressure in the injector 3 and the equivalence ratio of the mixture. In fig. 7, the abscissa is the crank angle of the engine, and the ordinate is the cumulative mass flow of the mixture injected by the injector 3, and in fig. 7, the preset injection timings are set to be crank angles of 600 °, 620 °, and 640 °, respectively, for example.

On the other hand, as shown in fig. 1, the utility model also provides a combustion apparatus, including main combustion chamber 20, main combustion chamber 20 sprayer and the precombustion ignition device 10 that any preceding embodiment mentioned, main combustion chamber 20 sets up in precombustion chamber 1's below and communicates with precombustion chamber 1, and main combustion chamber 20 sprayer sets up on main combustion chamber 20.

The embodiment of the utility model provides a combustion apparatus, compared with the prior art, because the gas mixture flow velocity of jet 339 department reaches the sound velocity, this department produces "choked up" effect, the velocity of flow of gas mixture remains unchanged, can not change along with the change of 1 internal pressure in precombustion chamber, can spray the total amount of injection of the accurate control gas mixture of pulse width through control, thereby can accurate calculation obtain required fuel injection quantity in the sprayer 3, and then can control the equivalence ratio of gas mixture in the sprayer 3, realize quick and stable ignition process, improve the combustion stability under lean burn operating mode and high EGR rate operating mode.

In one embodiment, as shown in fig. 1, the combustion apparatus further includes an air supply assembly 60 and an oil supply assembly 70, and the main combustion chamber 20 is provided with an air intake hole 30 and an air exhaust hole 40.

The air supply assembly 60 comprises an air filter 61, a throttle valve 62, a pressure stabilizing cavity 63, a flow meter 64, an air compressor 65, an air tank 66, a pressure regulating valve 67 and a one-way valve 68, wherein the air compressor 65 and the pressure regulating valve 67 are respectively and electrically connected with the electronic control unit; air sequentially passes through the air filter 61 and the throttle valve 62 and enters the pressure stabilizing cavity 63, the air is divided into two paths from the pressure stabilizing cavity 63, and one path of the air enters the main combustion chamber 20 through the air inlet hole 30; the other flow passes through the flow meter 64 to reach the air compressor 65, and is compressed by the air compressor 65 to enter the air tank 66 for storage, and during operation, high-pressure air in the air tank 66 is regulated to the working pressure of the injector 3 by the pressure regulating valve 67, and then enters the mixing cavity 322 through the one-way valve 68 and the air inlet 321.

The fuel supply assembly 70 comprises a fuel tank 71, a low-pressure pump 72, a fuel filter 73, a high-pressure pump 74, a fuel rail 75 and a fuel pressure sensor 76, wherein the high-pressure pump 74 and the fuel pressure sensor 76 are respectively electrically connected with the electronic control unit; the fuel passes through the low-pressure pump 72 and the fuel filter 73 from the fuel tank 71 to reach the high-pressure pump 74, and after further pressurization, the fuel enters the fuel rail 75, the fuel rail 75 is respectively communicated with the main combustion chamber 20 fuel injector and the prechamber fuel injector 31, a part of the fuel in the fuel rail 75 is injected into the main combustion chamber 20 through the main combustion chamber 20 fuel injector, and the other part of the fuel is injected into the mixing cavity 322 through the prechamber fuel injector 31.

Preferably, the pressure regulating valve 67 is an integrated flow control pressure regulating valve.

On the other hand, the utility model discloses still provide an engine, including the precombustion ignition device 10 mentioned in any one of the preceding embodiments.

The embodiment of the utility model provides an engine, compared with the prior art, because the gas mixture flow velocity of jet 339 department reaches the sound velocity, this department produces "choked" effect, the velocity of flow of gas mixture remains unchanged, can not change along with the change of the 1 internal pressure in precombustion chamber, can be through the total amount of injection of the accurate control gas mixture of control injection pulse width, thereby can the accurate required fuel injection quantity that obtains in the sprayer 3 of calculation, and then can control the equivalence ratio of gas mixture in the sprayer 3, realize quick and stable ignition process, improve the combustion stability under lean burn operating mode and high EGR rate operating mode.

The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims

1. A pre-combustion ignition device is characterized by comprising a pre-combustion chamber, a spark plug, an injector, a first pressure sensor, a second pressure sensor and an electronic control unit, wherein the spark plug, the injector, the first pressure sensor and the second pressure sensor are respectively and electrically connected with the electronic control unit, the spark plug and the injector are arranged on the pre-combustion chamber, the injector is provided with an air inlet, an oil inlet and an injection port, and air entering from the air inlet and fuel entering from the oil inlet are mixed in an accommodating cavity arranged in the injector to form mixed gas;

2. The pre-ignition device according to claim 1, wherein the injector includes a pre-chamber injector, a mixing container, and a nozzle, an inner cavity of the mixing container is vertically penetrated, the accommodating chamber includes a mixing chamber formed at an end of the inner cavity of the mixing container near the nozzle, the intake port is provided on the mixing container and communicates with the mixing chamber, the nozzle is provided with the injection port, the injection port communicates with the mixing chamber when opened, and the injection port is blocked from the mixing chamber when closed;

3. The pre-ignition device as claimed in claim 2, wherein the receiving chamber further includes a storage chamber formed at an end of the inner chamber of the nozzle body near the injection port, the mixing chamber, the storage chamber and the injection port being sequentially communicated when the injection port is opened, the storage chamber being blocked from the mixing chamber when the injection port is closed;

4. The pre-combustion ignition device as claimed in claim 2, wherein an end of the injection port close to the pre-combustion chamber forms a first tapered hole, an end of the injection port far from the pre-combustion chamber forms a second tapered hole, a cross section of the first tapered hole gradually increases from the end far from the pre-combustion chamber to the end close to the pre-combustion chamber, a cross section of the second tapered hole gradually increases from the end far from the pre-combustion chamber to the end close to the pre-combustion chamber, an end of the second tapered hole far from the pre-combustion chamber meets an end of the first tapered hole close to the pre-combustion chamber, and an end of the second tapered hole close to the pre-combustion chamber is located radially outside an end of the second tapered hole far from the pre-combustion chamber.

5. The pre-combustion ignition device of claim 4, wherein an end of the needle valve body near the pre-combustion chamber forms a needle valve head, the needle valve head gradually increasing in cross-section from an end away from the pre-combustion chamber to an end near the pre-combustion chamber;

6. The pre-ignition device as claimed in claim 2, wherein the receiving chamber further includes a movable chamber formed in a middle section of the inner chamber of the nozzle body, the movable chamber communicating with the mixing chamber when the injection port is opened.

7. The pre-combustion ignition device of claim 6, wherein the control mechanism includes an armature fixed to an end of the needle valve body remote from the pre-combustion chamber, an elastic member accommodated in the movable chamber, and an electromagnetic coil, the elastic member being supported on a side of the armature close to the pre-combustion chamber and an axial side chamber wall of the movable chamber, the elastic member urging the armature in a direction away from the pre-combustion chamber, the electromagnetic coil being wound around an outer side of the armature, the electromagnetic coil being electrically connected to the electronic control unit, the armature moving in a direction close to the pre-combustion chamber when the electromagnetic coil is energized to compress the elastic member.

8. The pre-combustion ignition device of claim 2, wherein the second end of the pre-chamber fuel injector is in sealing connection with the inner cavity of the mixing vessel.

9. A combustion apparatus comprising a main combustion chamber, a main combustion chamber injector and a pre-combustion ignition device according to any one of claims 1 to 8, the main combustion chamber being disposed below the pre-combustion chamber and communicating with the pre-combustion chamber, the main combustion chamber injector being disposed on the main combustion chamber.

10. An engine comprising a pre-ignition device as claimed in any one of claims 1 to 8.