The present disclosure relates generally to a piston for an internal combustion engine, and more particularly to a piston having features proportioned for enhanced flame speed and compression ratio.
Internal combustion engines are widely used throughout the world for purposes ranging from vehicle propulsion to operation of pumps and compressors, to generation of electrical power. Typical internal combustion engines employ a plurality of pistons that reciprocate in cylinder bores to rotate a crankshaft in response to a controlled combustion reaction producing a rapid pressure and temperature rise to drive the pistons. For decades engineers have experimented with a wide variety of different fuels, various exhaust treatment apparatuses and technologies, and different operating strategies in efforts to improve engine operation, reliability, and performance.
In recent years considerable engineering resources have been directed at developing pistons optimized for various applications. Depending upon engine type, a piston is commonly formed with a specified combustion face geometry intended to interact with flows of fuel, air, and/or exhaust during operation to various ends including optimizing emissions and/or efficiency, to mitigate or otherwise control in-cylinder temperatures and/or mechanical wear or corrosion, and for various other purposes. It has been observed that oftentimes seemingly quite minor changes to piston geometry can have outsized effects upon engine operation and performance, and the results of toggling any one variable respecting piston geometry can often be quite unpredictable. Moreover, compounding the difficulties in optimizing piston design, the addition or removal of piston volume, particularly upon the combustion face, affects geometric compression ratio, oftentimes requiring other modifications to piston or overall engine and supporting system design to maintain compression ratio at a desired level. Depending upon fuel type and a great many different operating parameters and different engine applications, optimized piston designs can have widely varying geometries. One known piston is set forth in U.S. Pat. No. 9,670,829 to Bowing et al.
In one aspect, a piston for an internal combustion engine includes a piston skirt having a wrist pin bore formed therein and defining a wrist pin axis, and a piston crown having a combustion face forming a piston rim extending circumferentially around a piston center axis, and a combustion bowl having a bowl floor extending radially outward of the piston center axis to a bowl outer wall. The combustion face further includes a bowl edge defining an intersection of a combustion bowl and the piston rim, and a reentrant surface extending between the bowl edge and the bowl outer wall. A bowl depth dimension coincident with the piston center axis is defined between the piston rim and the bowl floor, and a compression height dimension coincident with the piston center axis is defined between the piston rim and the wrist pin axis. A ratio of the bowl depth dimension to the compression height dimension is from about 0.30 to about 0.35.
In another aspect, a piston for an internal combustion engine includes a piston skirt having a wrist pin bore formed therein and defining a wrist pin axis, and a piston crown including a combustion face forming a piston rim extending circumferentially around a piston center axis, and a combustion bowl. The combustion face further includes a bowl edge defining an intersection of the combustion bowl and the piston rim, and a reentrant surface defining a bowl reentrancy angle. The combustion bowl has a U-shaped profile, axially below the reentrant surface, relative to the piston center axis, in a plane including the piston center axis. A ratio of a bowl depth dimension coincident with the piston center axis to a compression height dimension coincident with the piston center axis is 0.3 or greater.
In still another aspect, an internal combustion engine system includes an engine housing having a cylinder bore formed therein, an engine head, and a piston movable within the cylinder bore between a bottom-dead-center (BDC) position and a top-dead-center (TDC) position. The piston includes a piston skirt having a wrist pin bore formed therein and defining a wrist pin axis, and a piston crown including a combustion face forming a piston rim extending circumferentially around a piston center axis, and a reentrant combustion bowl. A ratio of a bowl depth dimension coincident with the piston center axis to a compression height dimension coincident with the piston center axis is from about 0.30 to about 0.35.
Referring to
A cylinder liner 20 is positioned within cylinder block 14, and a piston 22 is movable in cylinder 18 between a bottom-dead-center (BDC) position and a top-dead-center (TDC) position in a generally conventional manner. Engine 12 will typically, but not necessarily, be configured to operate in a four-stroke engine cycle. Piston 22 is coupled to a connecting rod 24 in turn coupled to a crankshaft 26. An oil sprayer 28 may be oriented to spray cooling and lubricating oil onto an underside of piston 22 and into an oil gallery therein also in a generally conventional manner.
Engine system 10 also includes an intake system 30. Intake system 30 includes an intake conduit 32 structured to convey intake air for combustion to cylinder 18. Intake system 30 also includes an intake manifold 40 and an intake runner 41 extending from intake manifold 40 to an intake port 43 feeding cylinder 18. Those skilled in the art will appreciate an intake manifold would typically be coupled to a plurality of intake runners each extending to one of a plurality of cylinders. Engine system 10 also includes a turbocharger 34 having a compressor 36 positioned to pressurize an incoming flow of intake air in response to rotation of a turbine 38. Engine system 10 also includes an exhaust manifold 42 configured to receive a flow of exhaust from cylinder 18 and to convey the same by way of an exhaust conduit 44 to turbine 38.
Engine system 10 also includes a fuel admission valve 48 positioned to admit a flow of fuel from a fuel supply 46 to intake conduit 32. The illustrated arrangement will be recognized as a fumigated fuel admission arrangement. In other instances, engine system 10 might be port injected, including a fuel injection valve extending into or close to intake port 43, or manifold injected. It is contemplated engine system 10 will typically operate on a gaseous fuel, such as natural gas. Natural gas or other gaseous fuels might be supplied from a pressurized fuel tank, a gas line, from a mine, or various other sources. Engine system 10 may also be operated on various fuel blends including natural gas and gaseous molecular hydrogen, or various other gaseous hydrocarbon fuels and blends such as methane, ethane, biogas, landfill gas, or still others.
An intake valve 52 is shown supported in engine head 16 and movable to open or close fluid communications between intake port 43 and cylinder 18. An exhaust valve 54 analogously selectively fluidly connects cylinder 18 to exhaust manifold 42. In a typical application a total of two intake valves and a total of two exhaust valves might be provided for each cylinder in an engine. Engine system 10 may also be spark-ignited and includes a sparkplug 56 positioned to extend through engine head 16 into cylinder 18 to produce an electrical spark for igniting a mixture of fuel and air in cylinder 18. Sparkplug 56 may be electrically connected to an electronic control unit 58 or another suitable electrical or magnetic device for generating a spark at a spark gap in cylinder 18. Still other implementations could employ a prechamber sparkplug providing a prechamber within or fluidly connected to cylinder 18 for igniting a prechamber charge that ignites a main charge of a fuel and air in cylinder 18 according to well-known principles.
Referring also now to
In the illustrated embodiment, piston rim 74 extends planarly between a piston outer crown surface 90 and bowl edge 82. Piston outer crown surface 90 may include a plurality of piston ring grooves 91 each extending circumferentially around piston center axis 76 and configured to receive a piston ring containing fluids within cylinder 18 during service. Bowl floor 80 may extend planarly between piston center axis 76 and bowl outer wall. 81. Thus, each of piston rim 74 and bowl floor 81 may be planar and may be parallel to one another. Bowl outer wall 81 may include an arcuate surface 92 extending radially outward and axially upward from bowl floor 80, relative to piston center axis 76, and a cylindrical surface 94 extending axially upward, relative to piston center axis 74, from arcuate surface 92 and circumferentially around piston center axis 76.
Combustion bowl 78 may have a U-shaped profile, axially below reentrant surface 84, relative to piston center axis 76, in a plane including piston center axis 76. Reentrant surface 84 may extend from bowl edge 82 to cylindrical surface 94. Axially below reentrant surface 84, relative to piston center axis 76, combustion face 72 may be understood as formed by a total of three surfaces, including cylindrical surface 94, arcuate surface 92, and bowl floor 80. Combustion face 72 may have a uniform profile of rotation about piston center axis 76. Arcuate surface 92 may define a radius of curvature in the plane of the page in
As noted above, piston 22 is understood to have a piston skirt portion 96 that includes piston skirt 64. Piston skirt portion 96 is attached to piston crown 70, and in the illustrated embodiment may be attached by friction welding such as inertia welding or another strategy. A first weld post 98 and a second weld post 100 each extend circumferentially around piston center axis 76 and together attach piston skirt 64 to piston crown 70. An oil gallery 102 is formed in part in piston crown 70 and in part in piston skirt portion 96 and extends circumferentially around combustion bowl 78. First weld post 98 may extend from oil gallery 102 to combustion bowl 78. Those skilled in the art will recognize that in contrast to certain other piston designs a weld post extends to combustion bowl 78, whereas certain conventional pistons place a friction weld post beneath a combustion bowl.
With continued reference to the drawings generally, but focusing on
With continued reference to the drawings generally, but focusing now on
It has been observed that increased turbulence in the flow of fluids within a combustion cylinder can be associated with enhanced combustion flame speed in at least certain instances. In a general sense, increased turbulence helps promote rapid flame speed, hastening combustion, and in some instances improving engine efficiency, performance, and emissions. In operating engine system 10 as the premixed gaseous fuel and air is compressed during a compression stroke, when piston 22 approaches the TDC position the relatively small clearance distance 104 assists in providing a relatively rapid squish of fuel and air from between piston rim 72 and engine head 16. The squished-fuel-and-air mixture flows over bowl edge 82 and, based at least in part on the reentrant profile of combustion bowl 78, produces turbulence that assists in promoting fast flame speed.
As also noted above, relatively minute changes to piston geometry can have outsized and/or unpredictable effects. Many engines are configured to operate at a relatively tightly specified compression ratio. According to the present disclosure, piston 22 may be understood to approach engine head 16 quite closely at TDC to promote a robust squish of fuel and air. Reducing clearance distance, however, other factors being equal, would affect compression ratio by reducing volume in the cylinder bore. Accordingly, combustion bowl 78 is made relatively deep to maintain a compression ratio for a given stroke distance and compression height. The dimensions and ranges of ratios disclosed herein can assist in providing a piston having a compression ratio of about 13.3:1 whilst providing for faster flame speed resulting from high-squish velocity and turbulence induced by flow into the reentrant combustion bowl.
Certain dimensions and proportions are described herein using the term “about.” The term “about” can be understood to mean generally or approximately as would be understood by a person skilled in the engine and piston design field, such as by way of approximation, convention, or conventional rounding to a consistent number of significant digits. According to the latter of these, “about 0.3” is understood to mean from 0.25 to 0.34. “About 0.32” means from 0.315 to 0.324, and so on. A dimension or proportion listed without a preceding relative term can be understood to mean the dimension or proportion within measurement error.
The present description is for illustrative purposes only, and should not be construed to narrow the breadth of the present disclosure in any way. Thus, those skilled in the art will appreciate that various modifications might be made to the presently disclosed embodiments without departing from the full and fair scope and spirit of the present disclosure. Other aspects, features and advantages will be apparent upon an examination of the attached drawings and appended claims. As used herein, the articles “a” and “an” are intended to include one or more items, and may be used interchangeably with “one or more.” Where only one item is intended, the term “one” or similar language is used. Also, as used herein, the terms “has,” “have,” “having,” or the like are intended to be open-ended terms. Further, the phrase “based on” is intended to mean “based, at least in part, on” unless explicitly stated otherwise.
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