GAS ENGINE

Abstract

A gas engine includes: a main combustion chamber; and a precombustion chamber including an ignition plug disposed in a precombustion-chamber upper section and a throat formed in a precombustion-chamber lower section, the throat including a nozzle hole, configured such that mixed gas flows into the throat of the precombustion chamber via the nozzle hole from the main combustion chamber in a compression stroke. The nozzle hole has an opening edge portion on a throat side, the opening edge portion including a curved surface portion formed along a peripheral edge of the opening edge portion. The throat extends linearly along a center axis of the precombustion chamber. A ratio of a length of the throat to an inner diameter of the throat is not smaller than 1.6 and not greater than 2.6, and a value obtained by multiplying a ratio of the inner diameter of the throat to a radius of the curved surface portion by a ratio of the inner diameter of the throat to a precombustion chamber upper portion diameter is not smaller than 18.

Claims

1. A gas engine, comprising: a main combustion chamber; and a precombustion chamber including an ignition plug disposed in a precombustion-chamber upper section and a throat formed in a precombustion-chamber lower section, the throat including a nozzle hole, configured such that mixed gas flows into the throat of the precombustion chamber via the nozzle hole from the main combustion chamber in a compression stroke, wherein the nozzle hole has an opening edge portion on a throat side, the opening edge portion including a curved surface portion formed along a peripheral edge of the opening edge portion, wherein the throat extends linearly along a center axis of the precombustion chamber, and wherein a ratio of a length of the throat to an inner diameter of the throat is not smaller than 1.6 and not greater than 2.6, and a value obtained by multiplying a ratio of the inner diameter of the throat to a radius of the curved surface portion by a ratio of the inner diameter of the throat to a precombustion chamber upper portion diameter is not smaller than 18.

2. The gas engine according to claim 1, wherein a value obtained by multiplying a ratio of a length of the nozzle hole to a diameter of the nozzle hole by a ratio of the inner diameter of the throat to the precombustion chamber upper portion diameter is not smaller than 1.4.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0015] FIG. 1 is a configuration diagram of the vicinity of a combustion chamber of a gas engine according to an embodiment of the present invention.

[0016] FIG. 2 is a diagram showing a half cross-sectional view of a lower section of a precombustion chamber.

[0017] FIG. 3 is a graph showing a relationship between a value obtained by multiplying a ratio of the throat diameter to the radius of the curved surface portion inside the nozzle hole by a ratio of the throat diameter to the diameter of the upper portion of the nozzle hole, and an index of combustion variation inside the precombustion chamber.

[0018] FIG. 4 is a graph showing a relationship between a value obtained by multiplying a ratio of the length of the nozzle hole disposed on the precombustion chamber to the diameter of the nozzle hole by a ratio of the throat diameter to the diameter of the upper portion of the precombustion chamber and an index of combustion variation inside the precombustion chamber.

DETAILED DESCRIPTION

[0019] Embodiments of a gas engine of the present invention will now be described with reference to FIGS. 1 to 4. It is intended, however, that unless particularly specified, dimensions, materials, shapes, relative positions and the like of components described in the embodiments shall be interpreted as illustrative only and not intended to limit the scope of the present invention.

[0020] As shown in FIG. 1, the gas engine 1 includes a cylinder 3, a cylinder head 7 disposed on the upper portion of the cylinder 3, and a piston 5 disposed inside the cylinder 3 so as to be movable in the up-down direction. A main combustion chamber 10 is formed in a region surrounded by the upper surface of the piston 5, the inner surface of the cylinder 3, and the lower surface of the cylinder head 7. An intake port 13 for supplying fuel is connected to the cylinder head 7, such that fuel supply to the main combustion chamber 10 is controlled through opening and closing of the intake valve 14 disposed on the cylinder head 7. Further, an exhaust port 17 for discharging exhaust gas is connected to the cylinder head 7, such that discharge of exhaust gas from the main combustion chamber 10 is controlled through opening and closing of the exhaust valve 18 disposed on the cylinder head 7.

[0021] A precombustion chamber body 30 including a precombustion chamber 31 is disposed on the substantially center part of the upper portion of the cylinder head. The precombustion chamber body 30 extends in the up-down direction and has a bottomed container shape, including a precombustion chamber 31 formed inside, extending in the up-down direction. An ignition plug 40 is disposed on the upper portion of the precombustion chamber 31. The precombustion chamber body 30 includes a precombustion chamber fuel gas passage 34 for supplying the precombustion chamber 31 with fuel. The fuel injected through the precombustion chamber fuel gas passage 34 is mixed with mixed gas supplied to the precombustion chamber 31 through a nozzle hole 37 described below from the main combustion chamber 10 in the compression stroke. The volume of the precombustion chamber 31 is smaller than the volume of the main combustion chamber 10.

[0022] The precombustion chamber 31 includes: a throat 32 extending upward from the bottom portion of the precombustion chamber body 30 and having a bottomed cylindrical shape; and an upper precombustion chamber 33 including a diameter widening portion 33a connected to the upper end of the throat 32 and extending upward, with its diameter increasing gradually upward, and a cylindrical portion 33b connected to the upper end of the diameter widening portion 33a and having a cylindrical shape. The precombustion chamber 31 is formed symmetrically with respect to the center axis line. The above described ignition plug 40 is disposed on the upper precombustion chamber 33. On the bottom portion of the throat 32, a plurality of nozzle holes 37 are disposed at predetermined intervals, penetrating through the throat 32 between the outer surface 30a of the precombustion chamber body 30 and the inner surface 32a of the throat 32. The nozzle holes 37 are inclined downward from the center side toward the radially outer side of the precombustion chamber body 30.

[0023] The nozzle holes 37 extend linearly and each include end portions with respect to the axial direction. An end portion of each nozzle hole 37 has an opening on the outer surface 30a of the precombustion chamber body 30 and another end portion has an opening on the inner surface 32a of the throat 32. The shape of the nozzle holes 37 will be described below in detail.

[0024] In the compression stroke, the gas engine 1 having the above configuration injects mixed gas of the main combustion chamber 10 into the precombustion chamber 31 via the nozzle holes 37, and mixes the mixed gas with fuel injected into the precombustion chamber 31 to achieve a density suitable for ignition. Further, when the piston 5 reaches the vicinity of the compression top dead center, the gas engine 1 ignites mixed gas in the precombustion chamber 31 with the ignition plug 40, and combusts mixed gas in the precombustion chamber 31. Further, combustion flame is injected into the main combustion chamber 10 from the injection nozzle holes 37, and the injected combustion flame ignites the mixed gas in the main combustion chamber 10 to cause combustion.

[0025] As shown in FIG. 2, the nozzle hole 37 includes a curved surface portion 37a having a curved surface of a predetermined radius R on the opening edge portion on the throat side, formed along the periphery of the opening edge portion. The radius R of the curved surface portion 37a has a constant relationship with the inner diameter of the throat 32. That is, the throat curved surface 37a is formed such that a value obtained by multiplying a ratio of the inner diameter s of the throat 32 (hereinafter, referred to as throat diameter s) to the radius R of the curved surface portion 37a by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n is not smaller than 18. Such a curved surface portion 37a can be formed by chamfering the opening edge portion on the throat side along the periphery of the opening edge portion, after forming the nozzle hole 37 by drilling. Furthermore, the curved surface portion 37a may be formed by a method other than the above, for instance, by casting.

[0026] Herein, with the curved surface portion 37a formed along the periphery of the opening edge portion on the throat side of the nozzle hole 37, it is possible to suppress rapid diffusion of mixed gas when mixed gas is discharged from the nozzle hole 37 into the throat 32, which makes it possible to suppress separation of mixed gas in the nozzle hole 37.

[0027] The ratio of the throat diameter s to the radius R of the curved surface portion 37a will be described with reference to FIG. 3. In FIG. 3, x-axis represents a value obtained by multiplying a ratio of the throat diameter s to the radius R of the curved surface portion 37a of the nozzle hole 37 by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n (inner diameter of the above described cylindrical portion 33b), and y-axis represents an index of combustion variation inside the precombustion chamber 31.

[0028] In the graph, the mark .diamond-solid. indicates a measurement value, and the solid line indicates a result estimated from a plurality of measurement values. The index of combustion variation inside the precombustion chamber 31 on the y-axis shows that combustion variation increases toward the upper side of the y-axis, and decreases toward the lower side of the y-axis. As shown in FIG. 3, as the value obtained by multiplying a ratio of the throat diameter s to the radius R of the curved surface portion 37a of the nozzle hole 37 by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n becomes smaller than 18, the increase rate of the index of combustion variation increases. As the value obtained by multiplying a ratio of the throat diameter s to the radius R of the curved surface portion 37a of the nozzle hole 37 by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n exceeds 18, the increase rate of the index of combustion variation decreases and saturates. Thus, the precombustion chamber 31 of the present embodiment is formed such that a value obtained by multiplying a ratio of the throat diameter s to the radius R of the curved surface portion 37a by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n is not smaller than 18.

[0029] As described above, the throat diameter s is relatively large with respect to the radius R of the curved surface portion 37a. Thus, as mixed gas is discharged into the throat 32 from the nozzle hole 37, it is possible to stabilize the flow of mixed gas in the precombustion chamber, and suppress deterioration of combustion variation.

[0030] Further, the throat diameter s has a constant relationship with the length L (see FIG. 1) of the throat 32. That is, the ratio of the length L of the throat 32 to the throat diameter s is not smaller than 1.6 and not greater than 2.6. If the ratio of the length L of the throat 32 to the throat diameter s is smaller than 1.6, there is a greater risk of occurrence of turbulence in the flow of mixed gas injected into the throat 32 through the above described nozzle hole 37. On the other hand, if the ratio of the length L of the throat 32 to the throat diameter s is greater than 2.6, the throat 32 is too long, and it is necessary to change the position of the ignition plug 40. Thus, by forming the above described curved surface portion 37a on the throat-side opening end portion of the nozzle hole 37, with the ratio of the length L of the throat 32 to the throat diameter s being not smaller than 1.6 and not greater than 2.6, it is possible to suppress the risk of occurrence of turbulence in the flow of mixed gas injected into the throat 32.

[0031] Furthermore, the ratio of the length L of the nozzle hole 37 to diameter h of the nozzle hole 37 has a constant relationship. That is, the value obtained by multiplying a ratio of the length L of the nozzle hole 37 to the diameter h of the nozzle hole 37 is not smaller than 1.4. Now, with reference to FIG. 4, the ratio of the length L of the nozzle hole 37 to the diameter h of the nozzle hole 37 will be described. FIG. 4 is a graph showing a relationship between a value obtained by multiplying a ratio of the length L of the nozzle hole 37 to the diameter h of the nozzle hole 37 by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n and an index of combustion variation inside the precombustion chamber. The index of combustion variation inside the precombustion chamber 31 on the y-axis shows that combustion variation increases toward the upper side of the y-axis, and decreases toward the lower side of the y-axis. In the graph, the mark .diamond-solid. indicates a measurement value, and the solid line indicates a result estimate from a plurality of measurement values.

[0032] The measurement value has individual variability with respect to combustion variation, and thus there are two solid lines representing the result. One solid line represents a greater index and the other solid line represents a smaller index. As shown in FIG. 4, if the value obtained by multiplying a ratio of the length L of the nozzle hole 37 to the diameter h of the nozzle hole 37 by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n is smaller than 1.4, the increase rate of the index of combustion variation increases and the individual variability with respect to combustion variation also increases. On the other hand, if the value obtained by multiplying a ratio of the length L of the nozzle hole 37 to the diameter h of the nozzle hole 37 by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n is greater than 1.4, the increase rate of the index of combustion variation decreases and the individual variability with respect to combustion variation also decreases. Thus, in the present embodiment, the nozzle hole 37 is formed such that the value obtained by multiplying a ratio of the length L of the nozzle hole 37 to the diameter h of the nozzle hole 37 by a ratio of the throat diameter s to the precombustion chamber upper portion diameter n is 1.4.

[0033] With the nozzle hole 37 formed as described above, it is possible to rectify the flow at the nozzle hole 37 when mixed gas flows into the precombustion chamber 31 from the main combustion chamber 10. Thus, the flow of mixed gas from the main combustion chamber 10 to the precombustion chamber 31 is stabilized in each engine cycle, and mixed gas having a density that can be easily ignited is formed around the ignition plug 40, and thus it is possible to stabilize combustion inside the precombustion chamber 31 in each cycle.

[0034] The embodiments of the present invention have been described above. However, the present invention is not limited thereto, and various modifications may be applied as long as they do not depart from the object of the present invention. For instance, some of the above described embodiments may be combined upon implementation.

DESCRIPTION OF REFERENCE NUMERALS

[0035] 1 Gas engine [0036] 3 Cylinder [0037] 5 Piston [0038] 7 Cylinder head [0039] 10 Main combustion chamber [0040] 11 Exhaust turbine [0041] 13 Intake port [0042] 14 Intake valve [0043] 17 Exhaust port [0044] 18 Exhaust valve [0045] 30 Precombustion chamber body [0046] 30a Outer surface [0047] 30b Flat surface portion [0048] 31 Precombustion chamber [0049] 32 Throat [0050] 32a Inner surface [0051] 33a Diameter widening portion [0052] 33b Cylindrical portion [0053] 33 Upper combustion chamber [0054] 37 Nozzle hole [0055] 37a Curved surface portion [0056] 40 Ignition plug