INTERNAL COMBUSTION ENGINE

Abstract: The internal combustion engine is provided with a fuel injection nozzle. The injection ports of which are arranged concentrically in two rows around the axis (L) of the injection nozzle in such a manner that the injection ports in the upper and lower rows are staggered. The axes (P) of the injection ports in the lower row are on a circle having as its centre a point (O) on the axis of the injection nozzle. The axes (P) of the injection ports in the lower row are on a circle having as its centre a point (O') which is on the axis of the injection nozzle and spaced by a predetermined distance (Z) from the centre of the injection ports in the upper row.

Description: The present invention relates to an internal combustion engine and more particularly to an internal combustion engine including a fuel injection device. In general, to assure that an internal combustion engine has an increased combustion efficiency and an increased output, it is required that it has an improved combustion matching. To have such an improved combustion matching, items required particularly for a fuel injection system are such that a period of time for injecting a required amount of fuel is shortened as far as possible and moreover uniformity of distribution of sprayed fuel in a combustion chamber is improved further. Hitherto, a nozzle in a fuel injection device used for a conventional internal combustion engine, particularly for a conventional high speed diesel engine, is usually so designed that a plurality of injection holes formed at the fore end part of the injection nozzle are arranged in a single row on the periphery of a circle whose centre coincides with a centre axis of the injection nozzle, which has 4 to 6 injection holes formed therein so that combustion matching and uniformity of distribution of injected fuel are improved. However, required performances fail to be attained at present. To assure that a period of fuel injection time is shortened further to improve combustion matching with such a high speed diesel engine, it has been considered that the injection holes formed at the fore end part of the injection nozzle should preferably have an enlarged diameter, in other words, have an increased total area. However, when the injection holes have an increased total area merely by enlarging their diameter, it has been found that a streaming force generated by fuel injection becomes excessively intense, this causes fuel injection to be achieved in a deviated state on a periphery area of the combustion chamber and this leads to a high magnitude of fluctuation in distribution of injected fuel in the combustion chamber, resulting in combustion efficiency being reduced adversely. Accordingly, an excessively enlarged diameter of the injection holes can not contribute to improvement in combustion efficiency with the internal combustion engine and increase in output therefrom. In addition, it has been considered that when the number of injection holes is increased without any increase in diameter thereof, their total area is likewise increased and this enables a period of fuel injection time to be shortened. However, when the number of injection holes is practically increased, it follows that a distance between adjacent injection holes is reduced and this causes overlapping to occur between successive spray injections even with a reduced intensity of swirl in the combustion chamber, resulting in a high magnitude of fluctuation in distribution of sprayed fuel appearing in the combustion chamber. Accordingly, the conventional internal combustion engine can not improve the combustion efficiency thereof and increase an output therefrom, irrespective of how much the number of injection holes is increased. On the other hand, with the foregoing circumstances in mind, the inventors have proposed a fuel injection nozzle under Japanese Utility Model Application No. 195511/1982 whose purport consists in that an area assumed by injection holes is increased, depth of a cavity is determined more than that of a conventional non-swirl type combustion chamber and a period of fuel injection time is shortened as far as possible to improve uniformity of distribution of sprayed fuel in combustion chamber. The injection nozzle proposed under Japanese Utility Model Application No. 195511/1982 is so designed that a plurality of injection holes are arranged in two upper and lower rows concentrically relative to the centre axis of the injection nozzle, centre axes of the radially extending injection holes in the upper row coincide with those in the lower row at a single position on the centre axis of the injection nozzle and the injection holes in the upper row are arranged in a zigzag fashion relative to those in the lower row. When injection holes are arranged in that way, it follows that the number of injection holes is increased to increase their total area and a period of fuel injection time is shortened. Additionally, since the injection holes are arranged in a zigzag fashion, a danger that overlapping occurs between fuel injection effected through adjacent injection holes is removed as far as possible, resulting in uniformity of distribution of injected fuel being improved as far as possible. The injection nozzle proposed under Japanese Utility Model Application No. 195511/1982 is shown in Fig. 13 which is a fragmental sectional view illustrating the fore end part of the injection nozzle. According to the prior invention proposed under Japanese Utility Model Application No. 195511/1982 as shown in Fig. 13, the injection nozzle is so constructed that a plurality of injection holes arranged in upper and lower rows in a zigzag fashion are formed concentrically relative to the centre axis L of the injection nozzle in such a manner that their radially extending centre axes P′ and P converge on a single position O on the centre axis L. Thus, starting points Q and Q′ of the respective injection holes arranged in the upper and lower rows have a reduced distance therebetween, causing a crack to occur between adjacent holes after the injection nozzle is used for a long period of time. Consequently, the injection nozzle has a degraded durability. In other words, the conventional internal combustion engine including the aforementioned injection nozzle has a degraded durability. An internal combustion engine according to the pre-characterising parts of claims 1 and 3 is disclosed in GB-A-1 214 595. The present invention has as an object to provide an internal combustion engine which assures that a period of time required for injecting a required amount of fuel is determined as short as possible, uniformity of distribution of sprayed fuel in a combustion chamber is improved further and moreover durability of an injection nozzle is improved further. Another object of the present invention is to provide an internal combustion engine which assures that a period of fuel injection time is shortened, uniformity of distribution of sprayed fuel in the combustion chamber is improved, the depth of a cavity is determined more than that of a conventional non-swirl type combustion chamber and moreover the injection nozzle has an excellent durability. Another object of the present invention is to provide an internal combustion engine which assures that the cavity serving as a combustion chamber has a shallow-bottomed sectional contour corresponding to an increased output from the engine, a period of fuel injection time is shortened even with such a combustion chamber having a shallow-bottomed sectional contour, uniformity of distribution of sprayed fuel in the combustion chamber is improved and moreover the injection nozzle has an excellent durability. According to the present invention from one aspect, there is provided an internal combustion engine including a fuel injection device for feeding fuel into a combustion chamber through an injection nozzle, wherein: said injection nozzle has a plurality of injection holes arranged in a first row and a second row concentrically relative to a centre axis of the injection nozzle; the injection holes in the first row are more distant from a fore end of the nozzle than the injection holes in the second row; the injection holes in the first row are arranged in a zig zag fashion with those in the second row; radially extending centre axes of the injection holes in the first row are arranged on the periphery of a circle whose centre is located at a first position on the centre axis of the injection nozzle; radially extending centre axes of the injection holes in the second row are arranged on the periphery of a circle whose centre is located at a second position on the centre axis of the injection nozzle, said first position being spaced from said second position by a distance Z so as to be more distant from the fore end of the injection nozzle than said second position; and the number of injection holes arranged in both the first and second rows is in the range from 14 to 20 in total; the engine including a piston having a diameter D, characterised in that a top portion of the piston is formed with a cavity having a diameter F and which provides said combustion chamber, and the following conditions are satisfied:- (i) d < Z < 4d (ii) 45 < X < 60 (ii) 75 < Y < 85 (iv) 0.5 < F/D< 0.7 where:d is a diameter of each of said injection holes; X is an angle between the centre axes of the injection holes in the second row and the centre axis of the injection nozzle; and Y is an angle between the centre axes of the injection holes in the first row and the centre axis of the injection nozzle. According to the present invention from another aspect, there is provided an internal combustion engine including a fuel injection device for feeding fuel into a combustion chamber through an injection nozzle, wherein: said injection nozzle has a plurality of injection holes arranged in a first row and a second row concentrically relative to a centre axis of the injection nozzle; the injection holes in the first row are more distant from a fore end of the nozzle than the injection holes in the second row; the injection holes in the first row are arranged in a zig zag fashion with those in the second row; radially extending centre axes of the injection holes in the first row are arranged on the periphery of a circle whose centre is located at a first position on the centre axis of the injection nozzle; radially extending centre axes of the injection holes in the second row are arranged on the periphery of a circle whose centre is located at a second position on the centre axis of the injection nozzle, said first position being spaced from said second position by a distance Z so as to be more distant from the fore end of the injection nozzle than said second position; and the number of injection holes arranged in both the first and second rows is in the range from 10 to 16 in total; the engine being provided with a piston having a diameter D, characterised in that a top portion of the piston is formed with a cavity having a diameter F and a depth H and which provides said combustion chamber, and the following conditions are satisfied:- (i) d1 ≧ d2 (ii) d1 < Z < 5d1 (iii) 55 ≦ X ≦ 70 (iv) 75 ≦ Y ≦ 80 (v) 0.55 ≦ F/D ≦ 0.80 (vi) H/F < 0.45 where: d1 is a diameter of an injection hole in the first row; d2 is a diameter of an injection hole in the second row; X is an angle between the centre axes of the injection holes in the second row and the centre axis of the injection nozzle; and Y is an angle between the centre axes of the injection holes in the first row and the centre axis of the injection nozzle. The present invention will now be described, by way of example, with reference to the accompanying drawings, in which: Fig. 1 is a fragmental sectional view illustrating an essential part of an internal combustion engine in accordance with an embodiment of the present invention; Fig. 2 is a plan view of an injection nozzle as seen in the direction identified by arrow I in Fig. 1; Fig. 3 is a fragmental sectional view illustrating the fore end part of the injection nozzle; Figs. 4 to 6 are graphs showing characteristics of the internal combustion engine in accordance with the embodiment of the present invention; Fig. 7 is a fragmental sectional view illustrating an essential part of an internal combustion engine in accordance with another embodiment of the present invention; Fig. 8 is a plan view of an injection nozzle as seen in the direction identified by arrow II in Fig. 7; Fig. 9 is a fragmental sectional view illustrating the fore end part of the injection nozzle shown in Fig. 8; Figs. 10 to 12 are graphs showing characteristics of the internal combustion engine in accordance with the other embodiment of the present invention; and Fig. 13 is a fragmental sectional view illustrating an essential part of an injection nozzle usable for a conventional internal combustion engine. Fig. 1 is a fragmental sectional view illustrating an essential part of an internal combustion engine in accordance with an embodiment of the present invention and particularly illustrating in more detail a combustion chamber and an injection nozzle. This internal combustion engine is a direct fuel injection type diesel engine which includes a piston 2 just beneath an injection nozzle 1. The piston 2 is formed with a cavity at its upper part which constitutes a so-called deep-bottomed tray type combustion chamber 3. As will be apparent from Fig. 2 which is a plan view as seen in the direction identified by an arrow I in Fig. 1, the injection nozzle 1 is formed with a plurality of injection holes 4 arranged in two rows comprising an upper row A and a lower row B concentrically relative to a centre axis L in a zigzag fashion at its foremost end. In addition, as will be apparent from Fig. 3 which is a sectional view illustrating an essential part of the injection nozzle 1 shown in Fig. 2, the radially extending injection holes 4 arranged in the upper row A are formed at a predetermined pitch on the periphery of a circle whose centre is located at a position O on the centre axis L, while the radially extending injection holes 4 arranged in the lower row B are formed at a predetermined pitch on the periphery of a circle whose centre is located at a position O′ on the centre axis L spaced away from the position O by a distance Z. In the illustrated embodiment, the injection holes 4 number from 14 to 20 in total. In addition, in the foregoing embodiment, as shown in Fig. 3, the injection centres O and O′ in the injection nozzle 1 are spaced away from one another by a distance Z on the centre axis L as mentioned above, on the assumption that the fore end part of the injection nozzle 1 assumes a cylindrical configuration. Concretely speaking, the distance Z is determined relative to a diameter d of the respective injection holes 4 in accordance with the following relationship:- d < Z < 4d Additionally, in the foregoing embodiment as shown in Fig. 3, angles assumed relative to the centre axis L of the injection nozzle by the centre axes P and P′ of the respective injection holes 4 arranged in the upper and lower rows are determined in accordance with the following relationship when an angle assumed for the lower row B is represented by X · and an angle assumed for the upper row A is represented b Y · :- 45 < X < 60 75 < Y < 85 Consequently, fuel injected through the injection holes 4 arranged in two rows is sprayed within a comparatively narrow range extended round the centre axis L as identified by arrows A′ and B′ in Fig. 1 and this makes it possible to determine a depth H of the cavity more than that of a conventional non-swirl type combustion chamber. Incidentally, in the embodiment shown in Fig. 1, the range assumed by the ratio of diameter of cavity / diameter of piston (F/D) is determined in accordance with the following relationship:- 0.5 < F/D < 0.7 When a relationship between value of F/D and fuel consumption rate is examined on the basis of results derived from a number of experiments conducted with respect to the internal combustion engine having the deep-bottomed type combustion chamber as shown in Fig. 1, a graph in Fig. 4 is obtained which represents that the engine has the lowest fuel consumption rate in the range represented by 0.5 < F/D < 0.7 which is in accordance with the inequality (4). In other words, the engine has a high combustion efficiency. In addition, when a relationship between angle X assumed by the injection holes 4 arranged in the lower row B and fuel consumption rate is likewise examined on the basis of results derived from a number of experiments, a graph in Fig. 5 is obtained which represents that the engine exhibits the lowest fuel consumption rate in the range represented by 45 < X < 60 which is in accordance with the inequality (2). Additionally, when a relationship between angle Y assumed by the injection holes 4 arranged in the upper row A and fuel consumption rate is examined on the basis of results derived from a number of experiments, a graph in Fig. 6 is obtained which shows that the engine exhibits the lowest fuel consumption rate in the range represented by 75 < Y < 85 which is determined in accordance with the inequality (3). As will be apparent from the above description, since the foregoing embodiment is practiced such that the engine has an increased total area assumed by the injection holes compared with that of a conventional engine and a depth of cavity is determined more than that of a conventional non-swirl type combustion chamber, it is assured that a period of fuel injection time is shortened, uniformity of distribution of sprayed fuel in the combustion chamber is improved further and fuel combustion efficiency is increased further. By virtue of the arrangement that a centre of a circle round which the injection holes are arranged in the upper row is spaced away from a centre of a circle round which the injection holes are arranged in the lower row, by a predetermined distances as viewed in the direction of extension of the centre axis of the injection nozzle, starting positions R and R′ of the injection holes arranged in two rows in that way are spaced from one another while maintaining a certain distance therebetween (see Fig. 3). Consequently, a danger of causing a crack between the adjacent injection holes after the injection nozzle is used for a long period of time can be reduced as far as possible and thereby an internal combustion engine having a remarkably improved durability can be provided. By the way, due to the fact that a configuration assumed by the combustion chamber of a piston in an internal combustion engine is unavoidably determined in dependence on a load exerted on the piston, in some case a sectional contour (exhibiting a deep-bottomed tray shape) of the piston having a considerably large magnitude of cavity depth can not necessarily be determined for the internal combustion engine as shown in Fig. 1. In general, as an engine generates an increased output, a thermal load active on the piston increases, causing the cavity in a combustion chamber to unavoidably have a reduced depth. Accordingly, as the thermal load increases further, the upper end part of the combustion chamber tends to exhibit an expanded shape. According to the embodiment of the present invention as shown in Fig. 1, a deep-bottomed tray type cavity for the combustion chamber assures an improved uniform distribution of injected fuel and prevents an occurrence of cracking on the nozzle having a number of injection holes formed therein as far as possible. However, it should of course be understood that the present invention should not be limited only to the foregoing embodiment. Alternatively, the present invention may be applied to a case where a cavity for the combustion chamber has a reduced depth while assuring an uniform distribution of injected fuel and preventing an occurrence of cracking of the nozzle having a number of injection holes formed therein. Next, description will be made below as to an internal combustion engine in accordance with another embodiment of the present invention wherein a shallow-bottomed tray type cavity serving as a combustion chamber has a reduced depth. Fig. 7 is a fragmental sectional view illustrating an essential part of an internal combustion engine in accordance with the other embodiment of the present invention and particularly illustrating in more detail a combustion chamber and an injection nozzle. This internal combustion engine is a direct fuel injection type diesel engine which includes a piston 12 just beneath an injection nozzle 11. The piston 12 is formed with a cavity at its upper part which constitutes a shallow-bottomed tray type combustion chamber 13. As will be apparent from Fig. 8 which is a plan view as seen in the direction identified by an arrow II in Fig. 7, a plurality of injection holes 14 arranged in the periphery of the fore end part of the injection nozzle 11 in two rows concentrically relative to the centre axis L of the injection nozzle 11 are formed in such a manner that the injection holes 14 of the upper row A are arranged in a zigzag fashion relative to those of the lower row B. In addition, as will be apparent from Fig. 9 which is a sectional view of the fore end part of the injection nozzle 11 shown in Fig. 7, the radially extending injection holes 14 of the upper row A are formed at a predetermined pitch on the periphery of a circle whose centre is located at a position O on the centre axis L of the injection nozzle 11, while the radially extending injection holes 14 of the lower row B are formed at a predetermined pitch on the periphery of a circle whose centre is located at a position O′ on the centre axis L of the injection nozzle 11. The position O is spaced away from the piston O′ by a predetermined distance Z. In the illustrated embodiment, the injection holes 14 number from 10 to 16 in total. As shown in Fig. 9, according to the foregoing embodiment, the injection centres O and O′ for the injection nozzle 11 are spaced away from one another by a distance Z on the centre axis L of the injection nozzle 11 on the assumption that the fore end part of the injection nozzle 11 exhibits a cylindrical configuration. Concretely speaking, the distance Z is determined in accordance with the following relationship when it is assumed that a diameter of the respective injection holes in the upper row is represented by d₁ and a diameter of the respective injection holes in the lower row B is represented by d₂:- d₁ ≧ d₂ and d₁ < Z< 5 d₁ In the foregoing embodiment, angles assumed by centre axes P and P′ of the injection holes 14 relative to the centre axis L of the injection nozzle 11 are determined in accordance with the following relationships when an angle assumed by the respective injection holes in the lower row B is represented X ○ and an angle assumed by the respective injection holes in the upper row A is represented by Y ○ :- 55 ≦ X ≦ 70 75 ≦ Y ≦ 80 Consequently, fuel injected through the injection holes 14 arranged in two upper and lower rows is distributed within a comparatively wide range extended round the centre axis L of the injection nozzle 11 as identified by arrows A′ and B′. Thus, according to the foregoing embodiment, a depth H of the cavity can be determined less than that of a conventional non-swirl type combustion chamber. Incidentally, in the embodiment shown in Fig. 7, the range assumed by the ratio of diameter of cavity / diameter of piston (F/D) is determined in accordance with the following relationship:- 0.55 ≦ F/D ≦ 0.80 Moreover, the ratio H/F of depth H of the combustion chamber to diameter F of the cavity is determined in accordance with the following relationship:- H/F < 0.45 When a relationship between angle X assumed by the injection holes 14 in the lower row B and fuel cost rate is examined on the basis of results derived from a number of experiments conducted with respect to an internal combustion engine having a shallow-bottomed tray type combustion chamber as shown in Fig. 7, a graph in Fig. 10 is obtained which shows that the range identified by 55 ≦ X ≦ 70 in accordance with the inequality (7) exhibits the lowest fuel consumption rate. In other words, it exhibits a high combustion efficiency. In addition, when a relationship between angle Y assumed by the injection holes 14 in the upper row A and fuel consumption rate is likewise examined on the basis of results derived from a number of experiments, a graph in Fig. 11 is obtained which shows that the range identified by 75 ≦ Y ≦ 80 in accordance with the inequality (8) exhibits the lowest fuel consumption rate. Additionally, when a relationship between the ratio F/D and fuel consumption rate is examined on the basis of results derived from a number of experiments, a graph in Fig. 12 is obtained which shows that the range identified by 0.55 ≦ F/D ≦ 0.80 in accordance with the inequality (9) exhibits the lowest fuel consumption rate. In other words, it exhibits a high combustion efficiency. As will be readily apparent from the above description, according to the aforementioned second embodiment, by selecting the number of injection holes and a diameter of each of the injection holes within a properly determined range, a period of fuel injection time can be shortened corresponding to a reduced depth of the cavity for the combustion chamber accompanied by an increased output from the engine, uniformity of distribution of injected fuel within the interior of the combustion chamber can be improved and a combustion efficiency can be increased further. Since a centre of a circle in the upper row round which a series of injection holes are arranged is offset along the centre axis L of the injection nozzle 11 by a predetermined distance Z from a centre of a circle in the lower row round which a series of injection holes are arranged, this assures that starting positions R and R′ of injection holes arranged in two rows are located while maintaining a certain distance therebetween (see Fig. 9). Consequently, a danger that a crack may occur between adjacent injection holes after the injection nozzle is used for a long period of time can be reduced as far as possible whereby an internal combustion engine having a remarkably improved durability can be provided. As described hereinbefore, an internal combustion engine in accordance with the present invention is suitably employable for such an internal combustion engine that improvement on fuel consumption rate and output, and particularly, durability for a long period of time are required.

Claims: 1. An internal combustion engine including a fuel injection device for feeding fuel into a combustion chamber (3) through an injection nozzle (1), wherein: said injection nozzle has a plurality of injection holes (4) arranged in a first row (A) and a second row (B) concentrically relative to a centre axis (L) of the injection nozzle; the injection holes in the first row are more distant from a fore end of the nozzle than the injection holes in the second row; the injection holes in the first row are arranged in a zig zag fashion with those in the second row; radially extending centre axes (P′) of the injection holes in the first row are arranged on the periphery a circle whose centre is located at a first position (O) on the centre axis of the injection nozzle; radially extending centre axes (P) of the injection holes in the second row are arranged on the periphery of a circle whose centre is located at a second position (O′) on the centre axis of the injection nozzle, said first position being spaced from said second position by a distance Z so as to be more distant from the fore end of the injection nozzle than said second position; and the number of injection holes arranged in both the first and second rows is in the range from 14 to 20 in total; the engine including a piston (2) having a diameter D, characterised in that a top portion of the piston is formed with a cavity having a diameter F and which provides said combustion chamber, and the following conditions are satisfied:- (i) d < Z < 4d (ii) 45 < X < 60 (iii) 75 < Y < 85 (iv) 0.5 < F/D < 0.7 where: d is a diameter of each of said injection holes; X is an angle between the centre axes of the injection holes in the second row and the centre axis of the injection nozzle; and Y is an angle between the centre axes of the injection holes in the first row and the centre axis of the injection nozzle. 2. An internal combustion engine as claimed in claim 1, characterised in that it is a direct fuel injection type diesel engine. 3. An internal combustion engine including a fuel injection device for feeding fuel into a combustion chamber (13) through an injection nozzle (11), wherein: said injection nozzle has a plurality of injection holes (14) arranged in a first row (A) and a second row (B) concentrically relative to a centre axis (L) of the injection nozzle; the injection holes in the first row and more distant from the fore end of the nozzle than the injection holes in the second row; the injection holes in the first row are arranged in a zig zag fashion with those in the second row; radially extending centre axes (P′) of the injection holes in the first row are arranged on the periphery of a circle whose centre is located at a first position (O) on the centre axis of the injection nozzle; radially extending centre axes (P) of the injection holes in the second row are arranged on the periphery of a circle whose centre is located at a second position (O′) on the centre axis of the injection nozzle, said first position being spaced from said second position by a distance Z so as to be more distant from the fore end of the injection nozzle than said second position; and the number of injection holes arranged in both the first and second rows is in the range from 10 to 16 in total; the engine being provided with a piston (12) having a diameter D, characterised in that a top portion of the piston is formed with a cavity having a diameter F and a depth and H which provides said combustion chamber, and the following conditions are satisfied:- (i) d1 ≧ d2 (ii) d1 < Z < 5d1 (iii) 55 ≦ X ≦ 70 (iv) 75 ≦ Y ≦ 80 (v) 0.55 ≦ F/D ≦ 0.80 (vi) H/F < 0.45 where: d1 is a diameter of an injection hole in the first row; d2 is a diameter of an injection hole in the second row; X is an angle between the centre axes of the injection holes in the second row and the centre axis of the injection nozzle; and Y is an angle between the centre axes of the injection holes in the first row and the centre axis of the injection nozzle. 4. An internal combustion engine as claimed in claim 3, characterised in that it is a direct fuel injection type diesel engine.

Inventors: HIRAKI, HIKOSABURO, KUSAKABE, AKIRA, MURAKAMI,TOSHIBUMI
Applicants: KABUSHIKI KAISHA KOMATSU SEISAKUSHO
Application year: 1988
Main classification: F02M61
IPC codes: F02M61