Advanced lean burn injector igniter system

Abstract

An internal combustion engine with a piston having a piston head with a resonance cavity opening onto the head, and where a fuel nozzle located in a cylinder head is positioned to inject a fuel such as natural gas into the combustion chamber where resonance formed within the resonance cavity will ignite the fuel without the need of a spark plug. Inlet and exhaust ports in the cylinder head allow for air and combustion gas enter or leave the combustion chamber.

Claims

1. A piston for an internal combustion engine in which the engine is without a spark plug, the piston comprising: a piston head; a resonance cavity opening onto the piston head; and, the resonance cavity having a shape to produce ignition of a fuel within the engine without a spark plug due to a resonance formed within the resonance cavity.

2. The piston of claim 1, and further comprising: the resonance cavity is rectangular in a cross sectional side view.

3. The piston of claim 1, and further comprising: the resonance cavity has a cavity length greater than the cavity width.

4. The internal combustion engine of claim 1, and further comprising: the fuel is natural gas.

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

(1) FIG. 1 shows a cross section view of a reciprocating piston within a cylinder with a resonance cavity and injection nozzle of the present invention for auto-ignition.

(2) FIG. 2 shows a second embodiment of the present invention in which the resonance cavity is located in the cylinder head as a static part of the cylinder.

DETAILED DESCRIPTION OF THE INVENTION

(3) The present invention is an internal combustion engine with self-ignition, where the fuel can be a liquid fuel or a gaseous fuel. Resonance tube ignition, where a specially designed cavity combined with high pressure gas injection is used to induce shock waves which in-turn raises the local fuel/air mixture temperature above ignition. This process is very reliable and does not require a spark plug.

(4) In order to ignite a mixture of fuel and air, the temperature must be raised and the air/fuel ratio must be such that the mixture ignites. In a spark-ignition engine, the temperature rise is provided with a localized electrical energy discharge, whereas in a compression ignition (such as diesel) engine the entire air/fuel mixture rises in temperature due to mechanical compression of the gas and the heat of the cylinder wall. Resonance tube ignition occurs because of a rapid localized increase in temperature caused by a sudden increase in pressure from compression waves emanating from the nozzle that is injecting gas into a resonance tube within the combustion chamber cavity at sonic velocities and resonating in the cavity.

(5) FIG. 1 shows a combustion chamber of the present invention with a piston 11 reciprocating within a cylinder 12. The piston includes a piston head with a resonance cavity 13 that creates shock waves. The resonance cavity has a cavity width (w) and a cavity length (I). The combustion chamber is formed between the piston head and a cylinder head that includes an inlet valve 14 and an exhaust valve 15 as well as a nozzle 16 that opens into the combustion chamber.

(6) Air can be drawn into the combustion chamber through the inlet valve 14 while the exhaust gas from combustion can be discharged through the exhaust valve 15. A fuel such as natural gas can be injected into the combustion chamber through the nozzle 16. The gaseous fuel (or even air) can be injected into the resonance cavity 13 that will bounce off of the cavity floor and flow back toward the injection nozzle 16 as a bow wave (represented by the concave curve in FIG. 1 above the resonance cavity). Shock waves are formed from the bow waves striking the oncoming waves from the injector nozzle 16 that produce patterns of high pressure that result in high temperature. An injection of gaseous oxygen and gaseous hydrogen at 70 degrees F. will produce a heated gas in excess of 1,000 degrees F. which would be high enough temperature to auto-ignite the gas mixture and produce combustion within the combustion chamber.

(7) As the piston 11 moves up and down within the cylinder 12, the spacing or distance between the nozzle 16 and the opening of the resonance cavity 13 (nozzle-cavity gap) will change. One desirable feature of the present invention is that combustion should occur at or near to the top-dead-center (TDC) of the piston within the chamber. Thus, the nozzle-cavity gap will be near to the minimum when the piston 11 is at or near to the top-dead-center when the auto ignition is desirable. With the auto-ignition device of the present invention, much leaner bulk mixtures and higher pressures can be achieved than in the spark ignited engines of the prior art. The cavity width and the cavity length can be designed such that the auto-ignition temperature will only occur at the desired location of the piston within the cylinder such as at TDC.

(8) The engine in FIG. 1 can inject a fuel and air into the combustion chamber through the inlet valve 14 as in a typical ICE and inject compressed air through the nozzle 16 that would create the shock waves that induce an auto-ignition of the compressed fuel and air mixture. Thus, vaporized gasoline could be combusted with compressed air using the resonance cavity 13 that creates the shock waves to ignite the fuel/air mixture within a spark plug. In a diesel engine, the diesel fuel and the air can be injected through the inlet valve 14 and then compressed by the piston 11 moving upward in the cylinder 12, and compressed air can be injected through the nozzle 16 into the resonance cavity 13 to create the shock waves that produce the ignition of the fuel/air mixture. In either of these embodiments, a gaseous fuel such as natural gas can also be injected through the nozzle 16 to produce shock waves in the resonance cavity 13 to produce the combustion without using a spark plug.

(9) In another embodiment of the present invention, a resonance cavity can be formed on the cylinder head that would face toward a side of the cylinder where an injector nozzle would be located that would inject the compressed air or gas into the resonance cavity to produce the shock waves. Because the resonance cavity in this embodiment would not move and thus the nozzle-cavity gap would not change, the compressed air or gas would only be injected when the auto-ignition should occur such as when the piston is at TDC or nearby. FIG. 2 shows a cylinder head having the resonance cavity formed within along with fuel and air supply for the combustion chamber. U.S. Pat. No. 6,272,845 issued to Kassaev et al. on Aug. 14, 2001 and entitled ACOUSTIC IGNITER AND IGNITION METHOD FOR PROPELLANT LIQUID ROCKET ENGINE shows a piece than can be formed within the cylinder head of the engine to produce a similar effect at that disclosed in FIG. 1 embodiment. The FIG. 2 embodiment includes piston 21 with a typical flat head, a combustion chamber 22, an outlet orifice 23, an injection nozzle 24, a fuel injector tube 25, an acoustic resonator 26, a housing 27, and a cylindrical wall 28 among other structure as described in the Kassaev et al. patent.

(10) In this embodiment, compressed air is provided from an external source to the combustion chamber at, or close to TDC via the injection nozzle 24. This compressed air travels across the combustion chamber 22, enters the acoustic resonator 26, which reflects back into the chamber creating a shock that increases the temperature in the combustion chamber 22. At the appropriate time in the cycle, fuel is introduced into the combustion chamber creating a combustible mixture which is then ignited by the shock created. This ignites the fuel/air mixture in the engine via orifice 23.