The present disclosure relates to an internal combustion engine with a variable compression ratio.
An internal combustion engine is a heat engine in which the combustion of a fuel occurs with an oxidizer (typically air) in a combustion chamber that is an integral part of the engine. Internal combustion engines are often employed for powering vehicles, either as a primary power source, or as part of a hybrid powertrain. In a reciprocating internal combustion engine, expansion of the high-temperature and high-pressure gases in a combustion chamber space at the top of the cylinder produced by the combustion applies direct force to the engine's piston. The combustion force applied to the piston subsequently acts through the engine's connecting rod to turn the engine's crankshaft.
A compression ratio is one of the fundamental specifications of an internal combustion engine. An internal combustion engine's compression ratio is a value that represents the ratio of the volume of the engine's combustion chamber from its largest capacity to its smallest capacity. In a reciprocating internal combustion engine the compression ratio is typically defined as the ratio between the volume of the cylinder and combustion chamber when the piston is at the bottom of its stroke, and the volume of the combustion chamber when the piston is at the top of its stroke. An internal combustion engine's compression ratio greatly influences the subject engine's torque output and its fuel efficiency.
One embodiment of the disclosure is directed to a variable compression ratio (VCR) internal combustion engine that includes an engine block defining a cylinder and a cylinder head mounted to the engine block and defining at least a part of a combustion chamber. The engine also includes a reciprocating primary piston arranged inside the cylinder and configured to compress a mixture of air and fuel and a crankshaft arranged in the engine block and rotated by an application of a combustion force to the primary piston. The engine additionally includes a secondary piston mounted in the cylinder head, movably with respect to the combustion chamber and a mechanism configured to shift the secondary piston in the cylinder head and thereby vary a volume of the combustion chamber and a compression ratio of the engine.
The cylinder has a cylinder centerline and the mechanism can be configured to generate a linear motion of the secondary piston along the cylinder centerline.
The mechanism can include an electro-mechanical actuator having a stepper motor operatively connected to a worm wheel in mesh with a worm screw.
The engine can also include a fluid pump configured to pressurize engine oil. In such case, the mechanism can include a hydraulic actuator driven by the oil pressurized by the fluid pump.
The engine can additionally include a vacuum pump. In such case, the mechanism can include a pneumatic actuator driven by the vacuum pump.
The cylinder head can define a cavity and the secondary piston can be configured to shift inside the cavity. Accordingly, the secondary piston can be configured to vary the compression ratio of the engine by selectively expanding and contracting the size of the cavity.
The secondary piston can include a secondary piston body having a first surface facing the primary piston, an opposing second surface, and a secondary piston shaft fixed to the second surface of the secondary piston body. The secondary piston shaft can be operatively connected to the mechanism.
The secondary piston can define a gas passage extending from the first surface of the secondary piston body into the shaft. Additionally, the gas passage can be in fluid communication with a blow-off orifice. The secondary piston shaft can include a check-valve arranged inside the gas passage such that the check-valve is configured to relieve pressure from inside the combustion chamber into the blow-off orifice above a predetermined combustion pressure value.
The secondary piston body can define a vent orifice configured to provide pressure equalization between the first surface and the second surface of the secondary piston body.
The engine can also include a plurality of spark plugs arranged inside the combustion chamber and configured to ignite the mixture of air and fuel for initiating combustion thereof.
The engine can operate according to the Miller cycle, and can be either a spark-ignition or a compression-ignition type.
Another embodiment of the present disclosure is directed to a vehicle employing such a VCR internal combustion engine.
The above features and advantages, and other features and advantages of the present disclosure, will be readily apparent from the following detailed description of the embodiment(s) and best mode(s) for carrying out the described disclosure when taken in connection with the accompanying drawings and appended claims.
Referring to the drawings, wherein like reference numbers correspond to like or similar components throughout the several figures,
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As understood by those skilled in the art, a flow of air from the ambient is directed through an intake manifold 32 to each of the combustion chambers 30. Ambient air is combined either in the intake manifold 32 or inside the combustion chambers 30 with an appropriately metered amount of fuel to form a fuel-air mixture for subsequent combustion inside the subject combustion chamber. As also known by those skilled in the art, an intake air compressor device, such as a turbocharger or a supercharger (not shown), can be employed to increase pressure of the ambient air charge to enhance torque output of the engine 20. Although an in-line four-cylinder engine is shown in
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The engine 20 also includes a crankshaft 44 configured to rotate within the engine block 22 by an application of a combustion force to the primary piston 28. Specifically, and as understood by those skilled in the art, the crankshaft 44 is rotated by the primary pistons 28 via connecting rods 34 as a result of an appropriately proportioned of fuel and air being selectively admitted into the combustion chambers 30 via one or more intake valves 36, compressed by the primary pistons 28, and burned in the combustion chambers. After the air-fuel mixture is burned inside a specific combustion chamber 30, the reciprocating motion of a respective primary piston 28 serves to exhaust post-combustion gasses from the respective cylinder 24 via one or more exhaust valves 40.
The cylinder head 26 is also configured to exhaust post-combustion gasses from the combustion chambers 30, such as via an exhaust manifold 46. As shown in
As will be described below, the engine 20 is provided with a Variable Compression Ratio (VCR) and can also include Miller cycle capability. Such capability to vary the compression ratio of the engine 20 can be used to optimize the potential fuel efficiency gains of Miller cycle operation without the inherent spark limitations of a fixed VCR Miller cycle at high engine loads. Accordingly, the engine 20 can also employ mechanically or electromechanically operated phasers (not shown) for the camshafts 38 and 42 to optimize opening and closing events for the respective intake valve 36 and exhaust valve 40, particularly to enable operation of the engine using the Miller cycle.
In the Miller cycle, the intake valve(s) 36 are kept open longer than they would be in a traditional Otto or Diesel cycle. In effect, in the Miller cycle the compression stroke is split into two discrete cycles—the initial portion when the engine's intake valve is open and final portion when the intake valve is closed. As the primary piston 28 initially moves upwards toward the combustion chamber 30 in what is traditionally the compression stroke, the intake charge is partially expelled back out through the still-open intake valve(s) 36. Therefore, in the Miller cycle engine, the piston 28 begins to compress the fuel-air mixture only after the intake valve(s) 36 close, i.e., only during a part of the compression stroke.
While in the Otto and Diesel cycle the expansion ratio and the compression ratio are equal, the Miller cycle has a greater expansion ratio than compression ratio. The increased expansion ratio allows more work to be extracted from the combustion gases as the gases are expanded to nearly atmospheric pressure. Delaying the closing of the intake valve(s) 36 in the Miller cycle in effect shortens the compression stroke compared to the expansion stroke and allows the combustion gases to be expanded to atmospheric pressure, thereby potentially increasing the efficiency of the Miller cycle. As such, it is typically the Miller cycle's greater efficiency that fosters its use in internal combustion engines.
In spark-ignition internal combustion engines, at low engine speeds and loads, the use of the Miller cycle in spark-ignition internal combustion engines provides a significant fuel efficiency benefit, particularly when combined with an elevated compression ratio, such as above 12:1, to take advantage of the thermal efficiency gains. At high engine speeds and loads, however, Miller cycle enabled spark-ignition engines with such elevated compression ratio become spark limited to the degree that the engine's maximum power potential is significantly reduced. A Miller cycle enabled engine with VCR is capable of overcoming such power limitations. The VCR enables operation of the spark-ignition engine using an elevated compression ratio during low engine speeds and loads to maximize thermal efficiency, while a reduced compression ratio can be used at high engine speeds and loads to achieve increased power and acceptable fuel efficiency. In compression-ignition engines, Miller cycle can help reduce emissions of Nitrogen Oxides (NOx) and increase engine efficiency, especially at higher engine loads.
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By shifting inside the cavity 68, the secondary piston body 70 varies the compression ratio of the engine 20 via selectively expanding and contracting the volume of the cavity open to the combustion chamber 30.
As noted above, typically, high engine load at low engine speed results in elevated pressure inside the combustion chambers 30, thereby increasing the likelihood of knock or auto ignition due to uncontrolled combustion. Therefore, at lower engine speeds, increasing the volume of the combustion chamber 30, by shifting the secondary piston 50 away from the primary piston 28, reduces the pre-combustion pressures inside the particular cylinder 24, and reduces the likelihood of knock. On the other hand, at higher engine speeds, reducing the volume of the combustion chamber 30 by shifting the secondary piston 50 toward the primary piston 28 increases the compression ratio of the particular cylinder 24 and permits the cylinder to generate higher peak cylinder pressures and develop increased power.
As a result of the secondary piston 50 being shifted inside the combustion chamber 30 by the mechanism 52, the combustion pressures inside the combustion chamber 30 can be effectively managed via VCR during certain engine operating modes. Overall, the secondary piston 50 operated by the mechanism 52 can be controlled to generate increased VCR in combination with an increased expansion ratio of the Miller cycle operation for enhanced fuel efficiency of the engine 20 at lower engine speeds. Additionally, the secondary piston 50 can be operated by the mechanism 52 to reduce the VCR at higher engine speeds and thereby enhance the engine's power output.
The detailed description and the drawings or figures are supportive and descriptive of the disclosure, but the scope of the disclosure is defined solely by the claims. While some of the best modes and other embodiments for carrying out the claimed disclosure have been described in detail, various alternative designs and embodiments exist for practicing the disclosure defined in the appended claims. Furthermore, the embodiments shown in the drawings or the characteristics of various embodiments mentioned in the present description are not necessarily to be understood as embodiments independent of each other. Rather, it is possible that each of the characteristics described in one of the examples of an embodiment can be combined with one or a plurality of other desired characteristics from other embodiments, resulting in other embodiments not described in words or by reference to the drawings. Accordingly, such other embodiments fall within the framework of the scope of the appended claims.
This application claims the benefit of U.S. Provisional Application Ser. No. 62/314,571 filed Mar. 29, 2016, the entire content of which is hereby incorporated by reference.
Number | Date | Country | |
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62314571 | Mar 2016 | US |