Air-assisted jet flame ignition device and ignition method thereof
An air-assisted jet flame ignition device includes a housing, a fuel-air premixing unit, and a prechamber. The fuel-air premixing unit includes a fuel injector, an air injection valve, a premixing sleeve, a premixing sleeve inner core placed in the premixing sleeve, and a fuel injector fastening bolt. An inner wall surface of the premixing sleeve and an outer wall surface of the premixing sleeve inner core form a premixing sleeve inner cavity. An inner wall surface of the premixing sleeve inner core, a lower end surface of a nozzle of the fuel injector, and an upper end surface of an air inlet of the air injection valve form a premixing cavity. The premixing cavity coupled to the premixing sleeve inner cavity via a through hole on the sidewall of the premixing sleeve inner core. A prechamber nozzle is fixedly coupled to the lower part of the housing.
1. An air-assisted jet flame ignition device, comprising:
a housing comprising a lower part, wherein a circumference of the lower part comprises first external threads;
a fuel-air premixing unit comprising:
a fuel injector, comprising a nozzle, wherein the nozzle comprises a lower end surface;
an air injection valve comprising an air inlet, wherein the air inlet comprises an upper end surface;
a premixing sleeve comprising a first inner wall surface;
a premixing sleeve inner core placed in the premixing sleeve and comprising:
a sidewall;
a through hole located on the sidewall;
a second inner wall surface, wherein the second inner wall surface, the lower end surface, and the upper end surface are configured to form a premixing cavity; and
an outer wall surface, wherein the first inner wall surface and the outer wall surface are configured to form a premixing sleeve inner cavity, and wherein the premixing cavity is coupled to the premixing sleeve inner cavity via the through hole; and
a fuel injector fastening bolt,
a prechamber comprising:
a locating pin;
a prechamber nozzle fixedly coupled to the lower part using the locating pin, wherein a periphery of the prechamber nozzle comprises second external threads; and
a nozzle compression piece, wherein internal threads in fit with the first external threads are located inside the nozzle compression piece, and wherein the nozzle compression piece is configured to press the prechamber nozzle against the housing to form a prechamber cavity body.
2. The air-assisted jet flame ignition device of claim 1 , further comprising an air tube coupled to the premixing sleeve, wherein a high-pressure air is configured to enter, through the air tube, to the premixing sleeve inner cavity and is further injected into the premixing cavity via the through hole to be mixed with fuel to obtain a premixed fuel-air mixture, and wherein the air injection valve is configured to inject and the premixed fuel-air mixture into the prechamber cavity body.
3. The air-assisted jet flame ignition device of claim 2 , wherein the premixed fuel-air mixture has a scavenging capability and scavenges residual exhaust gas in the prechamber cavity body.
4. The air-assisted jet flame ignition device of claim 1 , wherein the air injection valve, the premixing sleeve inner core, the premixing sleeve, and the fuel injector are sequentially placed in and are jointly pressed against the housing by the fuel injector fastening bolt at a top.
5. An ignition method comprising:
defining a first turn-on time of a fuel injector of an ignition device as a fuel injection pulse width;
defining a second turn-on time of an air injection valve of the ignition device as an air injection pulse width;
turning on the fuel injector according to the fuel injection pulse width to inject fuel;
determining a delay time according to a fuel injection amount, wherein the delay time is called an air injection delay;
turning on, according to the air injection pulse width, the air injection valve after reaching the air injection delay to inject air to obtain a premixed fuel-air mixture;
injecting, by the air injection valve, the premixed fuel-air mixture into a prechamber cavity body of the ignition device; and
igniting, by a spark plug of the ignition device, the premixed fuel-air mixture to inject flame jets.
6. The ignition method of claim 5 , further comprising determining an excess air coefficient of a prechamber mixture by regulating the fuel injection pulse width and the air injection pulse width.
7. The ignition method of claim 5 , further comprising injecting an equivalent mixture with an excessive air coefficient less than 1 into the prechamber cavity body.
8. The ignition method of claim 6 , further comprising injecting an equivalent mixture with an excessive air coefficient less than 1 into the prechamber cavity body.
9. The ignition method of claim 6 , further comprising injecting a rich mixture with an excessive air coefficient less than 1 into the prechamber cavity body.
10. The ignition method of claim 5 , further comprising:
identifying that a rich mixture is needed in the prechamber cavity body; and
increasing, in response to the identifying, the fuel injection pulse width to obtain the rich mixture.
11. The ignition method of claim 5 , further comprising:
identifying that a lean mixture is needed in the prechamber cavity body; and
increasing, in response to the identifying, the air injection pulse width.
12. The ignition method of claim 5 , further comprising injecting a rich mixture with an excessive air coefficient less than 1 into the prechamber cavity body.
13. The ignition method of claim 5 , wherein a fuel injection pressure is 10 megapascals to 20 MPa.
14. The ignition method of claim 5 , wherein an air injection pressure is 0.4 megapascals to 1 MPa.
15. A fuel-air premixing component comprising:
a fuel injector comprising a nozzle, wherein the nozzle comprises a lower end surface;
an air injection valve comprising an air inlet, wherein the air inlet comprises an upper end surface;
a premixing sleeve comprising a first inner wall surface;
a premixing sleeve inner core placed in the premixing sleeve and comprising:
a sidewall;
a through hole located on the sidewall;
a second inner wall surface, wherein the second inner wall surface, the lower end surface, and the upper end surface are configured to form a premixing cavity, and wherein the premixing cavity coupled to the premixing sleeve inner cavity via the through hole; and
an outer wall surface, wherein the first inner wall surface and the outer wall surface are configured to form a premixing sleeve inner cavity; and
a fuel injector fastening bolt.
16. The fuel-air premixing component of claim 15 , further comprising an air tube coupled to the premixing sleeve, wherein a high-pressure air is configured to enter, through the air tube, to the premixing sleeve inner cavity and further injected into the premixing cavity via the through hole to be mixed with fuel to obtain a premixed fuel-air mixture, and wherein the air injection valve is configured to inject the premixed fuel-air mixture into a prechamber cavity body.
17. The fuel-air premixing component of claim 16 , wherein the premixed fuel-air mixture has a scavenging capability and scavenges residual exhaust gas in the prechamber cavity body.
18. The fuel-air premixing component of claim 16 , wherein a fuel injection pressure is 10 megapascals to 20 MPa.
19. The fuel-air premixing component of claim 16 , wherein an air injection pressure is 0.4 megapascals to 1 MPa.
20. The fuel-air premixing component of claim 15 , wherein the air injection valve, the premixing sleeve inner core, the premixing sleeve, and the fuel injector are sequentially placed in and are jointly pressed against a housing by the fuel injector fastening bolt at a top.