Internal combustion engine with gas feeding system

Abstract

An engine is equipped with a gas feeding system, including main gas injectors each associated with an intake duct of a respective engine cylinder, a gas distribution manifold communicating with said main injectors, a gas tank, connected to the manifold, where pressurized gas is accumulated, a controlled pressure valve interposed between the tank and manifold, and a control unit for controlling the pressure valve to establish a gas pressure in the manifold. A spark plug of each cylinder is mounted within a support body that defines a combustion pre-chamber and a channel for auxiliary gas injection within the pre-chamber, communicating with a respective auxiliary gas injector. The auxiliary gas injectors are in communication with the manifold, downstream of the pressure valve. In the channel, a non-return valve and a restricted passage are provided in series, providing for passage of gas flow proportional to a volume of the pre-chamber.

Claims

1. A spark-ignition internal combustion engine having a system for feeding a gas, the engine comprising: an engine block with a plurality of cylinders and a cylinder head defining a main combustion chamber associated with each cylinder, an ignition spark plug associated with each cylinder, a plurality of electromagnetically-controlled main gas injectors, each associated with an intake duct of a respective cylinder of the engine, a gas distribution manifold, communicating with said main gas injectors, a gas tank connected via a connection to the distribution manifold, where gas under pressure is accumulated, wherein: the spark plug of each cylinder is mounted within a support body that is mounted within a cavity of said cylinder head opening out in said main combustion chamber, said support body defines a combustion pre-chamber having a first end facing electrodes of the respective spark plug and a second end communicating with the respective main combustion chamber through a plurality of orifices, said support body also defines a channel for auxiliary gas injection into said combustion pre-chamber, said channel having a first end opening out in said combustion pre-chamber, adjacent to said spark plug, said channel being in communication with a respective auxiliary electromagnetically-controlled gas injector, mounted on the cylinder head in a remote position with respect to said combustion pre-chamber, and in said auxiliary gas injection channel associated with each combustion pre-chamber there are arranged in series a non-return valve which enables gas to flow only towards the combustion pre-chamber, and a restricted passage, wherein said engine further comprises: an electronically-controlled pressure regulation valve, interposed in the connection between the gas tank and the distribution manifold, and an electronic control unit configured to control opening and closing of each main gas injector, according to operating conditions of said gas feeding system, and according to operating conditions of the engine, for controlling said pressure regulation valve in order to establish a gas pressure in the gas distribution manifold, the gas pressure being determined according to the operating conditions of said gas feeding system and according to the operating conditions of the engine, and wherein: the auxiliary gas injectors associated with the combustion pre-chambers are all in communication with said distribution manifold, downstream of said electronically-controlled pressure regulation valve, with reference to flow of the gas coming from the gas tank, said electronic control unit also being configured to control opening and closing of each of said auxiliary gas injectors, and said restricted passage is defined by a hole of a bushing inserted within said channel for auxiliary gas injection defined within said support body, said hole having a diameter (D) such that a D/V ratio between said diameter and a volume (V) of the combustion pre-chamber is between 310.sup.4 and 610.sup.4 mm.sup.2, thereby providing for passage of a gas flow proportional to the volume of the combustion pre-chamber.

2. The engine according to claim 1, wherein said support body comprises an upper portion and a lower portion, rigidly connected to each other to define the combustion pre-chamber, said upper portion of the support body having a cylindrical configuration and the cavity having a substantially cylindrical configuration, and said upper portion of the support body being received within the cavity formed in the cylinder head, wherein an outer surface of said upper portion has a circumferential groove that defines a circumferential chamber with a surface of said cylindrical cavity, said circumferential chamber communicating with the respective auxiliary gas injector by a second channel formed in the cylinder head, and wherein a second end of said auxiliary gas injection channel communicates with said circumferential chamber.

3. The engine according to claim 2, wherein said auxiliary gas injection channel extends through the upper portion of the support body and has: a lower channel portion, opening out in the combustion pre-chamber, in which the bushing is inserted defining the restricted passage, and an upper channel portion opening out in said circumferential chamber, wherein which the non-return valve is inserted.

4. The engine according to claim 1, wherein the volume of the combustion pre-chamber is less than 3% of a volume of the main combustion chamber of each cylinder.

5. The engine according to claim 1, wherein the combustion pre-chamber has a main portion of elongated cylindrical shape, having an L/D ratio between its length (L) and its diameter (D) which is between 3 and 6.

6. The engine according to claim 5, wherein the orifices for communication between the combustion pre-chamber and the main combustion chamber are inclined with respect to a main axis of said elongated main portion of the combustion pre-chamber by an angle from 50 to 70.

Description

DETAILED DESCRIPTION OF THE EMBODIMENTS OF THE INVENTION

(1) Further characteristics and advantages of the invention will become apparent from the description that follows with reference to the attached drawings, provided purely by way of non-limiting example, wherein:

(2) FIG. 1 is a diagram of an internal combustion engine equipped with a gas feeding system, according to the present invention,

(3) FIG. 2 is a partial cross-sectional view of a cylinder head of an embodiment of the engine of FIG. 1,

(4) FIG. 3 is another partial cross-sectional view of the cylinder head of FIG. 2,

(5) FIGS. 4 and 5 are two different views, in cross-section and on an enlarged scale, of a spark plug-pre-chamber assembly shown in FIG. 3, and

(6) FIG. 6 illustrates an enlarged detail of FIG. 4,

(7) FIG. 7 illustrates an enlarged detail of FIG. 5, and

(8) FIG. 8 is a perspective view of the spark plug-pre-chamber assembly shown in FIGS. 4 and 5.

(9) In FIG. 1, the reference numeral 1 indicates, in its entirety, a multi-cylinder internal combustion engine (in the example illustrated, a three-cylinder engine) provided with a gas feeding system, in particular a system for feeding CNG (Compressed Natural Gas) or methane, the system being indicated in its entirety with reference number 2.

(10) The engine 1 has a block 1A in which the cylinders 3 are formed. Each of the cylinders 3 has at least one intake duct 4 that receives air from an intake manifold 5. The illustrated example refers to an internal combustion engine of the turbocharged type, in which the intake manifold 5 receives compressed air from a compressor 6. The compressor 6 receives air through an air supply duct 7 in which an air filter 8 is interposed. The outlet for the compressed air from the compressor 6 communicates with the intake manifold 5 through a duct 9 in which a heat exchanger 10 is interposed, for cooling the air fed to the engine.

(11) Each of the cylinders 3 has at least one exhaust duct 11 communicating with an exhaust manifold 12. The exhaust gases leaving the exhaust manifold 12 are used to drive a turbine 13 mechanically connected to the compressor 6 by means of a shaft 14, in order to actuate the compressor 6. The outlet of the exhaust gases from the turbine 13 communicates with an exhaust line 15.

(12) The gas for feeding the internal combustion engine 1 is accumulated under high pressure (for example 200 bar) in a gas tank 16. The outlet of the tank 16 is equipped with a conventional-type interceptor valve (not illustrated). The tank 16 outlet is also connected via a line 17 to a distribution manifold 18 (also called rail) that communicates with a plurality of main gas injectors 19 mounted on the engine 1, to inject gas into respective air supply ducts 4. The main injectors 19 are controlled by an electronic control unit E. In the line 17 that connects the outlet of the tank 16 to the distribution manifold 18, an electronically-controlled pressure regulation valve 20 is interposed to regulate the gas pressure in the distribution manifold 18.

(13) According to the prior art, the electronic control unit E controls the pressure regulation valve 20, preferably in a PWM mode, to establish a pressure value in the distribution manifold 18, which is determined each time according to the operating conditions of the gas feeding system and the operating conditions of the engine 1. To this end, the electronic control unit receives a plurality of signals S1, S2, S3, S4, etc., indicative of the operating parameters of the engine and gas feeding system, such as the engine load (position of the accelerator pedal), the engine rotational speed, the pressure in the distribution manifold 18, the pressure of the gas leaving the tank 16, etc. To this end, the system comprises a pressure sensor P1 at the outlet of the tank 16, and a pressure sensor P2 capable of detecting the pressure in the rail 18.

(14) Referring now to FIGS. 2-6, numeral 21 indicates the body of the cylinder head of the engine 1, the lower surface 22 of which has a cavity 23 at each cylinder 3 of the engine block, defining the main combustion chamber associated with the cylinder.

(15) Associated with each cylinder 3, a spark plug 24 is provided (in the illustrated example, a spark plug with a diameter of 10 mm). The spark plug 24 associated with each cylinder is mounted, for example screwed, within an axial cylindrical cavity 250 of a cylindrical body 25A forming the upper part of a support 25 carrying the spark plug 24. The upper body 25A is, in turn, mounted, for example by screwing, within a cavity 26 formed in the cylinder head 21. In the illustrated example, the body 25A has a lower portion having a threaded outer surface 251 for engaging a corresponding threaded portion of the surface of the lower end portion of the cavity 26. The body 25A has an outer surface with circumferential grooves that receive sealing rings 255, which are in contact with the cavity surface 26.

(16) As clearly shown in FIGS. 4 and 5, the axial cavity 250 of the upper body 25A extends at its lower end into an enlarged cylindrical cavity 252, opening out at the lower end of the body 25A. Moreover, the same axial cavity 250 of the upper body 25A extends at its upper end into an enlarged cylindrical cavity 253, opening out at the upper end of the body 25A. The enlarged cavity 253 defines an abutment surface 254 for an enlarged portion 240 of the body of the spark plug 24. The arrangement is such that when the spark plug rests on the abutment surface 254, its electrodes face the enlarged cavity 252 at the lower end of the body 25A. In this cavity 252, the upper end portion of a body 25B defining the lower part of the support 25 is mounted, for example, by an interference-fit.

(17) The body 25B is also cylindrical and has an axial cylindrical cavity 28, which is blind at its lower end. The bottom wall of the body 25B is dome-shaped and has a circumferential series of orifices 29 for communication the cavity 28 to the combustion chamber 23. The orifices 29 have axes inclined with respect to the axis of the body 25B by an angle preferably between 50 and 70, and preferably equal to 60.

(18) In the illustrated example, the upper end of the axial cavity 28 has a flared shape.

(19) In the assembled condition, in which the bodies 25A and 25B are rigidly connected to each other, their cavities 252 and 28 define a substantially elongated combustion pre-chamber 30, having one end facing the spark plug electrodes 27 and the opposite end communicating with the main combustion chamber through the orifices 29.

(20) The body 25B is inserted through an end portion 260 of the cavity 26 formed in the head, which leads into the combustion pre-chamber 23.

(21) As an alternative to the solution illustrated in which the body 25A is screwed into the cavity 26, it is possible to envisage that the entire assembly formed of the bodies 25A, 25B and the spark plug 24 is secured into position by screwing the body 25B into the cavity 260. In this case, the outer surface of the body 25B and the surface of the cavity 260 have threaded portions cooperating with each other.

(22) In the preferred embodiment, the volume of the combustion pre-chamber 30 is less than 3% of the volume of the main combustion chamber 23 of each cylinder.

(23) The predominant portion of the combustion pre-chamber is defined by the elongated cylindrical cavity 28 of the lower body 25B. This cavity preferably has an L/D ratio between its length and its diameter from 3 to 6.

(24) In the support body 25A, a channel for auxiliary feeding of gas into the combustion pre-chamber 30 is also formed, which is indicated by the reference 31. The channel 31 extends through the support body 25A, alongside the cavity 250 that receives the spark plug 24. The channel 31 has two portions 31A, 31B arranged in an inclined manner to each other. The upper portion 31A leads onto a circumferential groove 256 of the outer surface of the body 25A. The lower portion 31B leads onto the enlarged cavity 252 defining the upper part of the combustion pre-chamber.

(25) In the lower portion 31B of the channel 31, a bushing 32 is inserted with a reduced diameter hole 32A (see FIG. 6) defining a restricted passage for the gas flow. The restricted passage 32A has a diameter D so that the D/V ratio between said diameter and the volume of the combustion pre-chamber is between 310.sup.4 and 610.sup.4 mm.sup.2, in order to allow the passage of a gas flow proportional to the volume of the combustion pre-chamber 30.

(26) In the upper portion 31A of the channel 31, a non-return valve 33 is inserted, which allows gas to flow only towards the combustion pre-chamber 30. FIG. 7 illustrates an exemplary embodiment of the non-return valve 33. In this example, the valve 33 has a body 330 mounted with an interference-fit within the portion 31A of the channel 31. The body 330 extends into a portion of reduced diameter 331, having an axial through-hole. The portion 331 contains a helical spring 332 that pushes a ball 333 against a valve seat defined by a sealing ring mounted within the body 330. When a gas flow occurs in the channel 31 towards the pre-chamber 30, the ball 333 retracts, compressing the spring 332, and the gas flows through passages 334 formed in the body 331. When there is a flow of gas coming from the pre-chamber, this flow finds the passage closed by ball 333.

(27) The auxiliary gas feeding channel 31 communicates with a circumferential chamber 34 (FIG. 3) defined by the circumferential groove 256 and the surface of the cylindrical cavity 26. The chamber 34, in turn, communicates with a channel 35 formed in the cylinder head serving for the communication of the auxiliary gas feeding channel 31 with an auxiliary gas injector 36, which is mounted in the head 21 (FIG. 3).

(28) Returning to the diagram of FIG. 1, therefore, in the engine according to the invention, an auxiliary gas injector 36 is also associated with each cylinder 3 of the engine.

(29) The auxiliary gas injectors 36 associated with the cylinders 3 of the engine, and in particular associated with the combustion pre-chambers 30 of the cylinders of the engine 3, also communicate with the distribution manifold 18. In the example illustrated in FIG. 1, the three auxiliary injectors 36 communicate with a separate manifold body 180 which, in turn, communicates through a line 42 with the manifold 18 of the main injectors 19. The line 42 communicates with the manifold 18 downstream of the pressure regulation valve 20, with reference to the flow direction of the gas leaving the tank 16. Therefore, the pressure regulation valve 20 establishes the same pressure both in the manifold 18 and in the manifold 180.

(30) Of course, the electronic control unit E is configured to control both the pressure regulation valve 20, in order to control the pressure value of the gas in the distribution manifolds 18 and 180, and the main injectors 19 and the injectors 36, in order to regulate the opening and closing of each of these injectors. Finally, the electronic control unit E also controls the activation of the ignition spark plugs 24 associated with the cylinders of the engine.

(31) The diagram of FIG. 1 shows the non-return valve 33 and the restricted passage 32A arranged in series along each auxiliary gas feeding channel in the combustion pre-chambers.

(32) FIG. 2 shows the arrangement of a main injector 19 associated with an intake duct 4. FIG. 2 also illustrates the rail 18. FIGS. 2 and 3 show the auxiliary injector 36 and the rail 180.

(33) The restricted passage 32A has a diameter D so that the D/V ratio between said diameter and the volume of the combustion pre-chamber is between 310.sup.4 and 610.sup.4 mm.sup.2, in order to allow the passage of a gas flow proportional to the volume of the combustion pre-chamber 30.

(34) During operation, the electronic control unit activatesfor each cylinderthe auxiliary gas injector, the spark plug 24 and the main gas injector 19, in order to obtain the following operating sequence: the auxiliary gas injector 36 injects a flow of gas into the combustion pre-chamber 30; this injection can take place in the intake stage of each cylinder, or even in the subsequent compression stage; during the compression step in the cylinder, the piston rises in the cylinder, pushing a certain amount of air into the pre-chamber 30 through the aforesaid orifices 29, the gas previously injected into the pre-chamber 30 is compressed, enabling entry of said amount of air into the pre-chamber; the mixture thus obtained is a rich mixture, for example with between 0.6 and 0.7, the spark plug ignites the mixture in the combustion pre-chamber, the combustion propagates from the combustion pre-chamber 30 to the combustion chamber 23, through the orifices 29 for communication of the combustion pre-chamber 30 with the combustion chamber 23, the main combustion chamber 23 is previously filled with a poor mixture of air and gas (for example, with approximately equal to 2), by injection of gas into the intake duct (FIG. 2) by means of the aforesaid main injector 19.

(35) As already indicated, the engine according to the invention can achieve a series of important advantages: first of all, the main gas injectors 19 as well as the auxiliary gas injectors 36 communicate with the gas distribution manifold 18, which can be formed as a single body or with separate bodies 18, 180, communicating with each other, as illustrated herein. Secondly, the electronic control unit establishes the ideal gas pressure level in the distribution gas manifold 18,180, which communicates both with the main injectors 19 and with the auxiliary injectors 36, the pressure level being calculated according to the operating conditions of the engine (engine load and engine rotational speed) and according to the operating conditions of the gas feeding system. At the same time, the ignition of the gas in the combustion pre-chamber allows the provision of a poor mixture in the cylinder, in order to minimize fuel consumption. Furthermore, each new injection of gas into each combustion pre-chamber carries out a scavenging of the pre-chamber, allowing any unburned fuel from the previous combustion to flow into the cylinder.

(36) Another advantage of the invention is that the above-described arrangement can also be easily obtained, by means of simple modifications, in a cylinder head originally designed with a conventional configuration, without combustion pre-chambers and without auxiliary injectors.

(37) Another advantage of the invention lies in the fact that it is possible to use standard injectors that are identical to each other, both for the main injectors and for the auxiliary injectors, since the aforesaid restricted passage in the auxiliary injection channel limits the gas flow to a value proportional to the volume of the combustion pre-chamber.

(38) Naturally, without prejudice to the principle of the invention, the details of construction and the embodiments may vary widely with respect to those described and illustrated purely by way of example, without departing from the scope of the present invention.