Methods and systems are provided for adjusting a flow profile of a windage tray. In one example, a method for operation an engine system is provided that includes operating an engine to perform combustion, determining an engine speed, and adjusting a flow profile of a plurality of deflectors in a windage tray positioned in a crankcase based on the engine speed.

Patent
   10385742
Priority
Nov 28 2017
Filed
Nov 28 2017
Issued
Aug 20 2019
Expiry
Mar 07 2038
Extension
99 days
Assg.orig
Entity
Large
2
6
currently ok
1. A method for operating an engine system comprising:
operating an engine to perform combustion;
determining an engine speed; and
adjusting a flow profile of a plurality of deflectors in a windage tray positioned in a crankcase based on the engine speed.
16. A method for operating an engine system comprising:
operating an engine with an engine speed is greater than a threshold value; and
in response to operating the engine with the engine speed greater than the threshold value, adjusting a position of flow deflectors in a windage tray to decrease the flowrate of crankcase gas through openings in the windage tray.
7. An engine system comprising:
a lubricant reservoir receiving lubricant from lubricated components;
a lubricant pump positioned in the lubricant reservoir;
a crankshaft positioned in a crankcase vertically above the lubricant reservoir and receiving rotational input from a piston rod;
a windage tray positioned vertically between the lubricant pump and the crankshaft, the windage tray including a plurality of deflectors extending longitudinally along the windage tray; and
code stored in memory executable by a processor to:
increase a degree of opening of the plurality of deflectors in response to a decrease in engine speed.
2. The method of claim 1, where adjusting a flow profile of deflectors in the windage tray includes increasing a degree of opening of the deflectors when an engine speed is less than a threshold value and decreasing a degree of opening of the deflectors when the engine speed is greater than the threshold value.
3. The method of claim 2, further comprising adjusting the threshold value based on a flowrate of crankcase gas into an intake system through a crankcase ventilation system.
4. The method of claim 3, where adjusting the threshold value includes decreasing the threshold value in response to an increase in a flowrate of crankcase gas into the intake system through the crankcase ventilation system.
5. The method of claim 1, further comprising adjusting a flow profile of the plurality of deflectors based on engine vibration.
6. The method of claim 1, where adjusting the deflectors includes for each of the deflectors, rotating the deflector at one end about a pivot.
8. The engine system of claim 7, where the plurality of deflectors are louver plates.
9. The engine system of claim 8, where the louver plates have a length greater than a width.
10. The engine system of claim 7, where the plurality of deflectors pivot about pivots during the increase in the degree of opening of the plurality of deflectors.
11. The engine system of claim 7, further comprising code stored in memory executable by the processor to decrease a degree of opening of the plurality of deflectors in response to an increase in engine speed.
12. The engine system of claim 11, where the increase in engine speed includes an increase in engine speed above a threshold value.
13. The engine system of claim 7, further comprising code stored in memory executable by the processor to adjust the threshold value based on a flowrate of crankcase gas into the intake system through a crankcase ventilation system.
14. The engine system of claim 7, where adjusting the threshold value includes increasing the threshold value in response to a decrease in a flowrate of crankcase gas into the intake system through the crankcase ventilation system or decreasing the threshold value in response to an increase in the flowrate of crankcase gas into the intake system through the crankcase ventilation system.
15. The engine system of claim 7, further comprising code stored in memory executable by the processor to increase a degree of opening of the plurality of deflectors based on engine vibration.
17. The method of claim 16, further comprising:
operating the engine with an engine speed less than the threshold value; and
in response to operating the engine with the engine speed less than the threshold value, adjusting a position of the plurality of deflectors in the windage tray to increase the flowrate of crankcase gas through the openings in the windage tray.
18. The method of claim 16, further comprising adjusting the threshold value based on a flowrate of crankcase gas into the intake system through a crankcase ventilation system.
19. The method of claim 18, where adjusting the threshold value includes at least one of increasing the threshold value in response to a decrease in a flowrate of crankcase gas into an intake system through the crankcase ventilation system and decreasing the threshold value in response to an increase in the flowrate of crankcase gas into the intake system through the crankcase ventilation system.
20. The method of claim 16, where adjusting the position of the plurality of deflectors includes for each of the deflectors, rotating the deflector at one end about a deflector pivot.

The present description relates generally to an engine with an engine system including an adjustable windage tray and a method for operation of said engine system.

Engines have utilized windage trays positioned in crankcases to modify flow dynamics in the crankcase. The use of windage trays is particularly prevalent in high performance engines, due to the propensity of high performance engines to be operated at high speeds for extended periods. However, the necessity of the windage tray varies based on engine operating conditions. During lower engine speeds the turbulence in the crankcase may not cause the oil aeration issues that are so prevalent at the high engine speeds. However, as the engine speed increases, the momentum of the crankcase flowfield and oil leakage via component bearings, perturb and impinge with high velocity on the free surface of the oil within the oil reservoir. Aeration is an inherent consequence of the oil interacting with the highly turbulent flowfield within the crankcase. A more quiescent oil free surface is one of the design goals of previous windage trays. However, during lower engine speeds oil aeration considerably decreases and may not pose a significant problem. Therefore, during lower engine speeds flow interruption created by the windage tray may not be needed. Furthermore, during low engine speeds the windage tray may interfere with oil draining. For instance, oil may impinge on surfaces of windage trays, thereby interfering with oil draining operation. Specifically, the amount and/or speed of oil returning to the oil pan may be reduced due to windage tray interference. Furthermore, some windage trays may also create losses in crankcase ventilation systems.

U.S. Pat. No. 6,019,071 discloses a windage tray with an oil flow path provided in the windage tray with integrated oil squirters directing oil towards the undersides of the engine pistons. However, the windage tray discloses in U.S. Pat. No. 6,019,071 suffers from the abovementioned problems of slow oil draining and crankcase ventilation losses.

Recognizing the problems described above and in an attempt to address at least some of the problems the inventors developed a method for operating an engine system. The method includes operating an engine to perform combustion, determining an engine speed and adjusting a flow profile of a plurality of deflectors in a windage tray positioned in a crankcase based on the engine speed. In this way, the flow profile of the windage tray may be dynamically adjusted to alter flow characteristics in the crankcase over a wide range of engine speeds. Consequently, the functionality of the windage tray can be varied to suit engine operating conditions, enabling the windage tray to reduce oil aeration during selected operating conditions while reducing windage tray flow interference during other operating conditions to increase oil draining, for instance.

In one example, the deflectors in the windage tray may be opened when the engine is operated below a threshold speed and closed when the engine is operated above the threshold speed. In this way, the windage tray acts to decrease crankcase turbulence around the lubricant reservoir, thereby decreasing oil aeration during high speed operation. Conversely, during lower speed engine operation the lubricant drainage interference is mitigated by opening the deflectors in the windage tray, thereby increasing the lubrication system efficiency.

It should be understood that the summary above is provided to introduce in simplified form a selection of concepts that are further described in the detailed description. It is not meant to identify key or essential features of the claimed subject matter, the scope of which is defined uniquely by the claims that follow the detailed description. Furthermore, the claimed subject matter is not limited to implementations that solve any disadvantages noted above or in any part of this disclosure.

FIG. 1 shows a schematic depiction of an internal combustion engine including a windage tray with adjustable deflectors.

FIG. 2 shows an illustration of a cross-section of a first example of a windage tray with adjustable deflectors in a closed configuration.

FIG. 3 shows an illustration of a cross-section of the first example of the windage tray with the adjustable deflectors in an open configuration.

FIG. 4 shows a perspective view of another exemplary windage tray with adjustable deflectors.

FIG. 5 shows a method for operation of an engine system with an adjustable windage tray.

FIG. 6 shows another method for operation of an engine system with an adjustable windage tray.

FIG. 7 shows a timing diagram of an exemplary windage tray control strategy.

The following description relates to an engine system and method for varying the flow profile of a windage tray based on engine speed, enabling the windage tray to act to interrupt crankcase turbulence during targeted conditions. The engine system includes a windage tray with adjustable deflectors (e.g., louvers) to achieve flow interference adaptability. The deflectors may be pivoted or otherwise moved to increase and decrease the amount of crankcase gas passing through the windage tray. In one example, the deflectors may be moved into open positions during lower speed operation to increase lubricant draining. Continuing with such an example, during higher speed operation the deflectors may be closed to reduce the likelihood of crankcase turbulence causing lubricant aeration. As a result, engine lubrication is enhanced during both high and low speed engine operation, thereby increasing engine reliability and longevity.

FIG. 1 shows a schematic depiction of an engine system with a windage tray. FIG. 2 shows an example of the engine system with the windage tray with deflectors in the windage tray in a closed position. FIG. 3 shows the engine system and windage tray shown in FIG. 2 with the deflectors in an open position. FIG. 4 shows a perspective view of another exemplary windage tray. FIGS. 5 and 6 show methods for operation of engine systems with windage trays to vary flow patterns in the crankcase and lubricant reservoir based on engine operating conditions. FIG. 7 shows a timing diagram associated with a windage tray control strategy which decreases lubricant aeration and increases lubricant draining in a lubricant system.

Turning to FIG. 1, an engine 10 with an engine system 12 in a vehicle 14 is schematically illustrated. Although, FIG. 1 provides a schematic depiction of various engine and engine system, it will be appreciated that at least some of the components may have a different spatial positions and greater structural complexity than the components shown in FIG. 1. The structural details of the components are discussed in greater detail herein with regard to FIGS. 2-4.

An intake system 16 providing intake air to a combustion chamber 18, is also depicted in FIG. 1. A piston 20 is positioned in the combustion chamber 18. The piston 20 is coupled to a crankshaft 22 via a mechanical component 24 (e.g., piston rod). The combustion chamber 18 is formed by a cylinder block 26 coupled to a cylinder head 28. Although, FIG. 1 depicts the engine 10 with one combustion chamber. The engine 10 may have additional combustion chambers, in other examples. For instance, the engine 10 may include a plurality of combustion chambers which may in some instances be positioned in banks.

The intake system 16 includes an intake conduit 30 and a throttle 32 coupled to the intake conduit. The throttle 32 is configured to regulate the amount of airflow provided to the combustion chamber 18. In the depicted example, the intake conduit 30 feeds air to an intake manifold 34. In turn, the intake manifold 34 directs air to an intake valve 36. However, in other examples, such as in a multi-cylinder engine intake runners may branch off of the intake manifold and feed intake air to other intake valves.

The intake valve 36 may be actuated by an intake valve actuator 38. Likewise, an exhaust valve 40 may be actuated by an exhaust valve actuator 42. In one example, the intake valve actuator 38 and the exhaust valve actuator 42 may employ cams coupled to intake and exhaust camshafts (not shown), respectively, to open/close the valves. Continuing with the cam driven valve actuator example, the intake and exhaust camshafts may be rotationally coupled to the crankshaft 22. Further in such an example, the valve actuators may utilize one or more of cam profile switching (CPS), variable cam timing (VCT), variable valve timing (VVT), and/or variable valve lift (VVL) systems to vary valve operation. Thus, cam timing devices may be used to vary the valve timing, if desired. It will therefore be appreciated that valve overlap may occur. In another example, the intake and/or exhaust valve actuators, 38 and 42, may be controlled by electronic valve actuation. For example, the valve actuators, 38 and 42, may be electronic valve actuators controlled via electronic actuation. In yet another example, the engine 10 may alternatively include exhaust valves controlled via electric valve actuation and intake valves controlled via cam actuation including CPS and/or VCT systems or vice versa. In still other embodiments, the intake and exhaust valves may be controlled by a common valve actuator or actuation system.

The engine 10 further includes a lubrication system 44 providing lubricant to engine components such as the piston 20, crankshaft 22, mechanical component 24, etc. The lubrication system 44 includes a lubricant reservoir 46 that receiving lubricant from the lubricated components (e.g., pistons, crankshaft, piston rods, etc.). Thus, the lubricant reservoir 46 in the lubrication system 44 may be designed to receive lubricant draining from the lubricated components such as the pistons 20, crankshaft 22, mechanical component 24, etc. For instance, the lubricant reservoir 46 may be positioned below the lubricated components to receive oil that has been sprayed or otherwise delivered to the lubricated components. A lubricant pump 48 is positioned in the lubricant reservoir 46 in the illustrated example. However, in other examples, the lubricant pump 48 may be positioned external to the lubricant reservoir with a pick-up line extending into the reservoir. The lubricant pump 48 is configured to flow pressurized lubricant to a plurality of lubrication lines 50. The plurality of lubrication lines 50 are schematically illustrated. However it will be appreciated that the lubrication lines may extend through different sections of the cylinder block 26 and/or cylinder head 28 to provide lubricant to the piston 20, the crankshaft 22, the mechanical component 24, etc. The lubrication system 44 may further include nozzles designed to spray or otherwise direct lubricant to the piston, crankshaft, etc., and are discussed in greater detail herein with regard to FIGS. 2 and 3. The lubrication system 44 also includes valves that are designed to regulate the flowrate of the lubricant provided to the lubricated components, discussed in greater detail herein with regard to FIGS. 2 and 3.

The engine 10 may also include an engine cooling system (not shown). The engine cooling system may include coolant jackets circulating coolant through the cylinder head and/or cylinder block as well as a heat exchanger (e.g., radiator) removing heat from the coolant.

A fuel delivery system 52 is also shown in FIG. 1. The fuel delivery system 52 provides pressurized fuel to a fuel injector 54. In the illustrated example, the fuel injector 54 is a direct fuel injector coupled to combustion chamber 18. Additionally or alternatively, the fuel delivery system 52 may also include a port fuel injector designed to inject fuel upstream of the combustion chamber 18 into the intake system 16. The fuel delivery system 52 includes a fuel tank 56 and a fuel pump 58 designed flow pressurized fuel to downstream components. A fuel line 60 provides fluidic communication between the fuel pump 58 and the fuel injector 54. The fuel delivery system 52 may include conventional components such as a high pressure fuel pump, check valves, return lines, etc., to enable fuel to be provided to the injectors at desired pressures.

An exhaust system 62 configured to manage exhaust gas from the combustion chamber 18 is also included in the vehicle 14 depicted in FIG. 1. The exhaust system 62 includes the exhaust valve 40 designed to open and close to allow and inhibit exhaust gas flow to downstream components from the combustion chamber. The exhaust system 62 also includes an emission control device 64 coupled to an exhaust conduit 66 downstream of an exhaust manifold 68. The emission control device 64 may include filters, catalysts, absorbers, etc., for reducing tailpipe emissions. The engine 10 also includes an ignition system 70 including an energy storage device 72 designed to provide energy to an ignition device 74. Additionally or alternatively, the engine 10 may perform compression ignition.

The engine system 12 is designed to vary the flow pattern in the lubricant reservoir 46 and a crankcase 82. The engine system 12 includes a windage tray 84. The windage tray 84 includes adjustable deflectors that may be actively controlled to alter the amount of crankcase gas flowing through the windage tray. For instance, the deflectors may be opened to allow crankcase gas to flow through the windage tray during low engine speeds. Continuing with such an example, the deflectors may be closed to inhibit crankcase gas from flowing through the windage tray during high engine speeds. The deflectors are described in greater detail herein with regard to FIGS. 2-4. Further in one example, the engine system 12 may also include the lubricant reservoir 46, the lubricant pump 48, and/or the crankshaft 22.

During engine operation, the combustion chamber 18 typically undergoes a four stroke cycle including an intake stroke, compression stroke, expansion stroke, and exhaust stroke. During the intake stroke, generally, the exhaust valve closes and intake valve opens. Air is introduced into the combustion chamber via the corresponding intake conduit, and the piston moves to the bottom of the combustion chamber so as to increase the volume within the combustion chamber. The position at which the piston is near the bottom of the combustion chamber and at the end of its stroke (e.g., when the combustion chamber is at its largest volume) is typically referred to by those of skill in the art as bottom dead center (BDC). During the compression stroke, the intake valve and the exhaust valve are closed. The piston moves toward the cylinder head so as to compress the air within combustion chamber. The point at which the piston is at the end of its stroke and closest to the cylinder head (e.g., when the combustion chamber is at its smallest volume) is typically referred to by those of skill in the art as top dead center (TDC). In a process herein referred to as injection, fuel is introduced into the combustion chamber. In a process herein referred to as ignition, the injected fuel in the combustion chamber is ignited via compression, resulting in combustion. However, in other examples, additionally or alternatively, spark from an ignition device may be used to ignite the air fuel mixture in the combustion chamber. During the expansion stroke, the expanding gases push the piston back to BDC. A crankshaft converts this piston movement into a rotational torque of the rotary shaft. During the exhaust stroke, in a traditional design, exhaust valve is opened to release the residual combusted air-fuel mixture to the corresponding exhaust passages and the piston returns to TDC.

FIG. 1 also shows a controller 100 in the vehicle 14. Specifically, controller 100 is shown in FIG. 1 as a conventional microcomputer including: microprocessor unit 102, input/output ports 104, read-only memory 106, random access memory 108, keep alive memory 110, and a conventional data bus. Controller 100 is configured to receive various signals from sensors coupled to the engine 10. The sensors may include engine coolant temperature sensor 130, exhaust gas composition sensor 132, exhaust gas airflow sensor 134, an intake airflow sensor 136, manifold pressure sensor 137, engine speed sensor 138, vibration sensor 140, etc. Additionally, the controller 100 is also configured to receive throttle position (TP) from a throttle position sensor 112 coupled to a pedal 114 actuated by an operator 116.

Additionally, the controller 100 may be configured to trigger one or more actuators and/or send commands to components. For instance, the controller 100 may trigger adjustment of the throttle 32, lubrication system 44, intake valve actuator 38, exhaust valve actuator 42, engine system 12, fuel delivery system 52, and/or the ignition system 70. Specifically, the controller 100 may be configured to send signals to the windage tray 84 to adjust the position of deflectors (e.g., louvers) in the windage tray. The controller 100 may also be configured to send control signals to the lubrication system 44 to control the amount of lubricant delivered to targeted lubricated components. Furthermore, the controller 100 may be configured to send control signals to the fuel pump 58 and the fuel injector 54 to control the amount and timing of fuel injection provided to the combustion chamber 18. The controller 100 may also send control signals to the throttle 32 to vary engine speed.

Therefore, the controller 100 receives signals from the various sensors and employs the various actuators to adjust engine operation based on the received signals and instructions stored in memory (e.g., non-transitory memory) of the controller. Thus, it will be appreciated that the controller 100 may send and receive signals from the engine system 12. For example, adjusting deflectors in the windage tray may include adjusting deflector actuators to adjust the deflectors in the windage tray. In yet another example, adjusting the degree of opening of deflectors in the windage tray, may be empirically determined and stored in predetermined lookup tables and/or functions. For example, one table may correspond to determining an amount of deflector opening in the windage tray when the engine is operating within a first speed range and another table may correspond to determining an amount deflector opening in the windage tray when the engine is operating within a second speed range that is less than the first speed range. The tables may be indexed to engine operating conditions such as engine speed, engine load, among other engine operating conditions. Furthermore, the tables may output an amount of fuel to inject via the fuel injectors to the combustion chamber at each cylinder cycle. Thus, it will be appreciated that the controller 100 may be configured to implement the methods, control strategies, etc., described herein with regard to an engine system including a windage tray.

FIG. 2 shows a first example of an internal combustion engine 200 and engine system 202 in cross-section. A z-axis and x-axis are provided in FIG. 2 as well as FIG. 3, for reference. FIG. 4 also shows a y-axis along with the z-axis and the x-axis for reference. In one example, the z-axis may be parallel to a gravitational axis. The x-axis may be a lateral axis, in one example. Furthermore, the y-axis may be a longitudinal axis, in one instance. However in other examples, other, x-axis, y-axis, and z-axis orientations have been contemplated. It will be appreciated that the engine 200 and the engine system 202, shown in FIG. 2, are examples of the engine 10 and the engine system 12, shown in FIG. 1. Therefore, features in the engine 10 and engine system 12 shown in FIG. 1 may be included in the engine 200 and engine system 202, shown in FIG. 2, or vice versa.

FIG. 2 shows the engine 200 including a cylinder block 204 coupled to a cylinder head 206 forming a combustion chamber 208. Although only one cylinder is depicted in FIG. 2, it will be appreciated that the engine 200 may include additional combustion chambers. In such an example, a windage tray 210 included in the engine system 202 may extend underneath pistons and associated piston rods, for instance.

Additionally, an exhaust valve 212 and an intake valve 214 are shown coupled to the combustion chamber 208. The intake valve 214 includes an intake valve stem 215 and the exhaust valve 212 includes an exhaust valve stem 217. Correspondingly, intake conduit 216 and exhaust conduit 218 providing fluidic communication between upstream intake system components and downstream exhaust system components, are also depicted in FIG. 2.

A piston 220 is positioned within the combustion chamber 208. The piston 220 include piston rings 222 designed to seal the combustion chamber 208. A piston rod 224 is attached to the piston 220 and a crankshaft 226.

A direct fuel injector 228 is also shown coupled to the combustion chamber 208. However, a port fuel injector may additionally or alternatively be included in the engine. A lubrication system 230 is also shown in FIG. 2. The lubrication system 230 includes a lubricant pump 232 designed to circulate lubricant through lubricant lines in the lubrication system. Furthermore, the lubricant pump 232 may be driven via rotational energy extracted from the crankshaft, in one example. However, in other examples, the lubricant pump 232, may be an electrical pump. Suitable pumps such as a gear pump, trochoid pump, vane pump, etc., have been contemplated. The lubricant pump 232 includes a pick-up line 234 with an inlet 236 directing lubricant 283 from a lubricant reservoir 238 into the pump. The lubricant pump 232 also includes an outlet 240 in fluidic communication with a lubricant line 242. A lubricant valve 244 coupled to the lubricant line 242. The lubricant valve 244 is configured to vary the amount of lubricant flowing through the lubricant line 242. For instance, the lubricant valve 244 may be fully opened, fully closed, and/or may have varying degrees of opening and closure. The lubricant valve 244 as well as other lubricant valves described herein may be an on/off electrically actuated solenoid valve, an on/off pneumatically actuated solenoid valve, an on/off electrically actuated piezoelectric stack valve, an electrically actuated proportioning valve, or a pneumatically actuated proportioning valve. A nozzle 246 is coupled to an end of the lubricant line 242. The nozzle 246 is designed to direct lubricant spray towards an underside 248 of the piston 220 to lubricate said piston. It will be appreciated that the lubrication system 230 may also include additional lubricant lines directing lubricant towards other lubricated components such as the crankshaft 226, the intake valve stem 217, the exhaust valve stem 215, etc.

The lubricant reservoir 238 is also included in the lubrication system 230 shown in FIG. 2. The lubricant reservoir 238 includes a housing 250 defining an interior section 252 of the lubricant reservoir 238 storing lubricant (e.g., oil).

A crankcase 254 is also shown in FIG. 2. The crankcase 254 houses the crankshaft 226. A crankcase housing 256 may for at least a portion of the boundary of the crankcase 254. Further in one example, the cylinder block 204 may also form a boundary of the crankcase 254.

FIG. 2 also shows a crankcase ventilation system 258. The crankcase ventilation system 258 includes a ventilation conduit 260 extending through the crankcase housing 256 into the crankcase 254. Thus, a first end 262 of the ventilation conduit 260 opens into the crankcase. The ventilation conduit 260 extend between the crankcase 254 and the intake conduit 216. A crankcase ventilation valve 264 is also coupled to the ventilation conduit 260. The crankcase ventilation valve 264 may be opened when there is a sufficient vacuum generated in the intake conduit 216 and crankcase ventilation flow is desired. The crankcase ventilation valve 264 may be controlled via pressure gradients between the intake system and crankcase. The crankcase ventilation valve and oil separator pressure drop requirements may be determined based on engine architecture and operating regimes, in one example. It will be appreciated that the controller 100 may send and receive signals from the valves, sensors, etc., shown in FIGS. 2 and 3. For instance, the controller 100 may adjust operation of the crankcase ventilation valve 264, the lubricant pump 232, windage tray 210, lubricant valve 244, etc.

The engine system 202 includes the windage tray 210. The engine system 202 may also include the lubricant reservoir 238, the lubricant pump 232, and/or the crankshaft 226. The windage tray 210 is positioned below (e.g., vertically below) the crankshaft and above (e.g., vertically above) the lubricant pump 232. The windage tray 210 also shown positioned in the lubricant reservoir 238. It will be appreciated that in other examples the windage tray 210 may extend into the crankcase 254. Thus, in some examples, the windage tray 210 may be attached (e.g., fixedly attached) to the lubricant reservoir housing 250 and/or the crankcase housing 256.

The windage tray 210 is shown including deflectors 266. The deflectors 266 are positioned in inclined sections 268 of the base 270 of the tray. However, other deflector positions have been contemplated. In the closed positioned the deflectors 266 may be aligned with upper surfaces 274 of the inclined sections 268, to substantially reduce (e.g., inhibit) crankcase gas flow through the windage tray. The deflectors 266 are moveably coupled (e.g., pivotally coupled) to the base 270. Specifically, the deflectors 266 are designed to pivot about deflector pivots 272. However, deflectors with alternate adjustment mechanisms have been contemplated.

FIG. 2 also shows a fixed deflector 276 and an opening 278 in the windage tray 210. The opening 278 enables lubricant to drain and pass through the windage tray and into the lubricant reservoir 238. In this way, lubricant build up on the windage tray may be avoided, thereby reducing interference between the lubrication system 230 and the windage tray 210. Consequently, lubrication system 230 efficiency may be increased.

Actuators 280 configured to adjust the positions of the deflectors are shown coupled to the deflectors. It will be appreciated that in other examples, a single actuator may actuate all of the deflectors or the actuators may actuate more than one deflector. In one example, the actuators 280 may be hydraulic actuators controlling the position of the deflectors 266 (e.g., louvers) via hydraulics. However, other suitable actuators have been contemplated.

Arrows 282 indicate the general direction of crankcase gas flow around the windage tray 210. Thus, when the deflectors 266 are in a closed position crankcase gas is substantially inhibited from flowing through the interior of the windage tray 210. However, in other examples when the deflectors 266 are in the closed position crankcase gas flow through the windage tray may be substantially reduced. As illustrated in FIG. 2, crankcase gas is direct towards the periphery of the windage tray near the lubricant reservoir housing 250. As a result, crankcase gas interference with lubricant 283 (e.g., oil) in the lubricant reservoir 238 is reduced, thereby reducing lubricant aeration. It will be appreciated that the gas flow pattern in around the windage tray 210 has greater complexity than is illustrated in FIG. 2.

It will be appreciated that the windage tray 210 (e.g., actuators 280), lubricant valve 244, crankcase ventilation valve 264, lubricant pump 232, and/or direct fuel injector 228 may receive control signals from the controller 100, shown in FIG. 1, and may also send signals to the controller. An engine speed sensor 284 coupled to the crankshaft 226 is also shown in FIG. 2. It will be appreciated that the engine speed sensor 284 may send signals to the controller 100, shown in FIG. 1.

FIG. 2 shows the deflectors 266 in a closed position while FIG. 3 shows the engine system 202 with the windage tray 210 with the deflectors in an open position. It will be appreciated that the actuators 280 may be commanded to place the deflectors 266 in the open position. Specifically, as shown in FIG. 3 the deflectors 266 are pivoted about the deflector pivots 272 such that the deflectors extend away from the base 270 of the windage tray 210. When the deflectors 266 are moved in this manner openings 300 in the windage tray 210 are uncovered. However, other deflector adjustment kinematics have been contemplated. When the openings 300 are uncovered crankcase gas can flow through the windage tray 210. Thus, when the deflectors 266 are moved into the open position from the closed position the flowrate of crankcase gas through the windage tray is increased. Conversely, when the deflectors 266 are moved from the open position to the closed position the flowrate of crankcase gas through the windage tray is reduced. Arrows 302 depict the general direction of gas flow through the openings 300. However, it will be appreciated that the gas flow pattern in the crankcase and through the openings has greater complexity than is illustrated.

In a fully open configuration the deflectors 266 may be arranged perpendicular to the base 270 of the windage tray 210. However, other orientations between the fully opened deflectors and the base of the windage tray have been contemplated. Conversely, in the closed position the deflectors 266 may be parallel to the base 270 of the windage tray. However, other orientations between the closed deflectors and the base has been envisioned such as 2°, 5°, 10°, etc., angles formed between the deflectors and the base. In the open position the deflectors 266 allow gas to flow through the windage tray 210 from the crankcase 254 to the lubricant reservoir 238.

Lubricant may also flow through the openings 300 when the deflectors 266 are opened to increase lubricant draining. Lubricant also drains through the opening 278 next to the fixed deflector 276. Arrow 304 indicates the generate path of lubricant flow through the openings 278. Consequently, lubricant can more efficiently drain into the lubricant reservoir 238.

It will be appreciated that the deflectors 266 in the windage tray 210 may be placed in the open configuration shown in FIG. 3 when the engine is operating above a threshold speed (e.g., 5,000 RPM, 5,500 RPM, 6,000 RPM, etc.,) in one instance. Conversely, the deflectors 266 in the windage tray 210 may be placed in the closed configuration shown in FIG. 2 when the engine is operating below the threshold speed.

In another example, the deflectors 266 in the windage tray 210 may be placed in the open configuration, shown in FIG. 3, when the engine speed is increasing. Thus, in such an example, the deflectors may be placed in the closed configuration, shown in FIG. 2, when the engine speed is decreasing. Control strategies for the deflectors in the windage tray are discussed in greater detail herein with regard to FIGS. 5, 6, and 7.

FIG. 3 again shows the engine 200, engine system 202, cylinder block 204, cylinder head 206, combustion chamber 208, piston 220, piston rod 224, crankshaft 226, crankcase housing 256, and engine speed sensor 284. The intake valve 214, the exhaust valve 212, intake conduit 216, exhaust conduit 218, direct fuel injector 228, lubricant pump 232, lubricant valve 244, lubricant line 242, nozzle 246, lubricant reservoir 238, crankcase ventilation system 258, ventilation conduit 260, and crankcase ventilation valve 264 are also shown in FIG. 3.

FIG. 4 shows a perspective view of an exemplary windage tray 400. The windage tray 400 shown in FIG. 4 is an example of the windage tray 210, shown in FIGS. 2 and 3. Therefore, the windage tray 400 may be included in the engine system 202, shown in FIGS. 2 and 3. Furthermore, the windage tray 400 shown in FIG. 4 may receive signals from the controller 100, shown in FIG. 1, to adjust operation thereof.

The windage tray 400 includes a first end 402, a second end 404, a first side 406, and a second side 408. The windage tray 400 also includes flanges 410 configured to attach to a section of a crankcase housing, cylinder block, lubricant reservoir housing, etc.

The windage tray 400 includes different sets 412 of deflectors, each set having a plurality of deflectors 414. As shown, the plurality of deflectors included in each set overlap with one another, in the closed position shown in FIG. 4. However, in other examples the deflectors in each set may be spaced away from one another. Each set of deflectors is positioned at different longitudinal positions along the windage tray 400. However, in other examples, the windage tray may include deflectors extending longitudinally down the length of the tray. It will be appreciated that numerous deflector profiles that enable the flow profile of the windage tray to be actively adjusted have been contemplated. It will also be appreciated that the second side 408 of the windage tray 210 may include sets of deflectors similar to the first side 406 of the windage tray.

The deflectors 414 shown in FIG. 4 are depicted as louvers plates. Each of the louver plates have a similar geometry in the illustrated example. However, in other examples the profile of the louver plates may vary within the sets of the louver plates and/or from set to set, for example. Specifically, in the illustrated example, the louver plates have a length 416 that is greater than their width 418. Additionally, a top surface 420 of the deflectors is also illustrated as substantially planar. However, other louver plate geometries have been contemplated. For instance, the louver plates may have a curved (e.g., convex or concave) upper surface and/or may taper in a longitudinal or a lateral direction.

Arrows 422 indicate the direction of deflector movement when the deflectors 414 are shifted from the closed position shown in FIG. 4 to an open position. In one example, the sets 412 of the deflectors may be correspondingly adjusted. That is to say that each of the deflectors 414 may be opened/closed by corresponding amounts. However in other examples, the sets 412 of the deflectors may be independently adjusted. For instance, a first set of deflectors may be opened while another set of deflectors may be closed or the degree of opening or closure in different sets of deflectors may vary between the sets of deflector and/or within specific deflectors in the sets. For instance, a first set of deflectors may be opened while another set of deflectors may be closed. The variations in deflector opening may be determined based on engine operating conditions. For instance, the deflectors may be closed when the engine is operating above a threshold speed and may be opened when the engine is operating below the threshold speed. In other examples, the degree of opening of the deflectors may decrease as the engine speed increases. Correspondingly, the degree of opening of the deflectors may increase as the engine speed decreases.

FIGS. 2-4 show example configurations with relative positioning of the various components. If shown directly contacting each other, or directly coupled, then such elements may be referred to as directly contacting or directly coupled, respectively, at least in one example. Similarly, elements shown contiguous or adjacent to one another may be contiguous or adjacent to each other, respectively, at least in one example. As an example, components laying in face-sharing contact with each other may be referred to as in face-sharing contact. As another example, elements positioned apart from each other with only a space there-between and no other components may be referred to as such, in at least one example. As yet another example, elements shown above/below one another, at opposite sides to one another, or to the left/right of one another may be referred to as such, relative to one another. Further, as shown in the figures, a topmost element or point of element may be referred to as a “top” of the component and a bottommost element or point of the element may be referred to as a “bottom” of the component, in at least one example. As used herein, top/bottom, upper/lower, above/below, may be relative to a vertical axis of the figures and used to describe positioning of elements of the figures relative to one another. As such, elements shown above other elements are positioned vertically above the other elements, in one example. As yet another example, shapes of the elements depicted within the figures may be referred to as having those shapes (e.g., such as being circular, straight, planar, curved, rounded, chamfered, angled, or the like). Further, elements shown intersecting one another may be referred to as intersecting elements or intersecting one another, in at least one example. Further still, an element shown within another element or shown outside of another element may be referred as such, in one example.

FIG. 5 shows a method 500 for operation of an engine system with a windage tray including adjustable deflectors. Method 500 as well as the other methods described herein may be implemented by engines and piston heating systems described above with regard to FIGS. 1-4 or may be implemented by other suitable engines and piston heating systems, in other examples. Instructions for carrying out the method 500 and the other methods described herein may be executed by a controller based on instructions stored in memory (e.g., non-transitory) executable by the controller and in conjunction with signals received from sensors of in the engine and corresponding systems, such as the sensors described above with reference to FIGS. 1-4. The controller may employ engine actuators of the engine systems to adjust engine operation, according to the methods described below.

At 502 the method includes operating the engine with an engine speed. It will be appreciated that the engine speed may be adjusted based on signals from a pedal position sensor or other suitable acceleration request sensor. Moreover, it will be appreciated that operating the engine with an engine speed including operating the engine to perform combustion.

At 504 the method includes determining engine operating conditions. The engine operating conditions may include engine speed, engine load, intake flowrate, engine temperature, exhaust gas flowrate, exhaust gas composition, engine vibration, crankcase ventilation flowrate, etc. The engine operating conditions may be ascertained from signals sent from various sensors in the engine and/or determined (e.g., calculated) based on signals from the sensors.

At 506 the method includes determining if the engine is operating above a threshold speed. The threshold speed may be 4,000 RPM, 4,500 RPM, or 5,000 RPM, in some examples. In another example, oil pressure may be a criterion that could be used to determine the flow return rate to the oil pump and windage tray operating regime.

If it is determined that the engine is not operating above the threshold speed (NO at 506) the method proceeds to 508. At 508 the method includes maintaining the degree of opening of deflectors in the windage tray. For instance, the deflectors may be maintained in a fully opened or a partially opened position. Thus, the windage tray may be operated with deflectors in an open position. In this way, crankcase gas may flow through the windage tray and lubricant draining through the windage tray may be increased. In other examples, the deflectors may be moved into a fully opened or a partially opened position or the degree of opening of the deflectors may be increased at 508.

On the other hand, if it is determined that the engine is operating above the threshold speed (YES at 506) the method advances to 510. At 510 the method includes decreasing a degree of opening of the deflectors. In this way, a flowrate of crankcase gas through the windage tray is decreased. In one example, decreasing a degree of opening of the deflectors may include placing the deflectors in a closed position. Thus, the windage tray may be operated with the deflectors in a closed position. As previously discussed, in the closed position crankcase gas through openings in the windage tray may be substantially inhibited. However in other examples, decreasing a degree of opening of the deflectors may include placing the deflectors in a partially closed position. Furthermore, as previously discussed adjusting a degree of opening or closing of the deflectors may include pivoting the deflectors at one end about a pivot.

At 512 the method includes determining if the engine is operating below the threshold speed. It will be appreciated that the operating conditions may be again determined prior to or during step 512. If it is determined that the engine is not operating below the threshold speed (NO at 512) the method proceeds to 514. At 514 the method includes maintaining the positions of the deflectors. For instance, the deflectors may be maintained in a closed position.

However, if it is determined that the engine is operating below the threshold speed (YES at 512) the method advances to 516. At 516 the method includes increasing a degree of opening of the deflectors. Increasing a degree of opening of the deflectors may include moving the deflectors into a partially opened or fully opened position, in one example.

It will be appreciated that steps 506, 510, 512, and 516 may be included in a more general step of adjusting a flow profile of the plurality of deflectors in the windage tray based on engine speed. In this way, the windage tray may be adapted to suit the current engine operating conditions.

At 518 the method includes determining if there is an increase in crankcase ventilation. The position of a crankcase ventilation valve and/or intake manifold pressure may be used to determine if there is an increase in crankcase ventilation. In other examples, it may be determined if the flowrate of crankcase ventilation gas surpasses a threshold value.

If it is determined that there is not an increase in crankcase ventilation (NO at 518) the method proceeds to 520. At 520 the method includes maintaining the current engine speed threshold. However, if it is determined that there is an increase in crankcase ventilation (YES at 518) the method proceeds to 522 where the method includes decreasing the engine speed threshold. In this way, the engine speed threshold may be decreased when the crankcase ventilation system causes increased turbulence in the crankcase and lubricant reservoir. Consequently, the deflectors in the windage tray may be closed at lower engine speeds to decrease lubricant aeration.

FIG. 6 shows another method 600 for operation of an engine system with a windage tray having adjustable deflectors. As discussed above, the method may be implemented by the engines and engine systems described above with regard to FIGS. 1-4 or may be implemented by other suitable engines and engine systems.

At 602 the method includes determining engine operating conditions. The operating conditions may include engine speed, engine load, intake flowrate, engine temperature, exhaust gas flowrate, exhaust gas composition, engine vibration, crankcase ventilation flowrate, etc. It will be appreciated that the engine may be operated according to the aforementioned operating conditions.

At 604 the method includes determining if there is an increase in engine speed. If there is an increase in engine speed (YES at 604) the method advances to 606. At 606 the method includes decreasing a degree of opening of deflectors in a windage tray. For instance, the deflectors in the windage tray may be placed in a closed position or a partially closed position. However, if there is not an increase in engine speed (NO at 604) the method proceeds to 608. At 608 the method includes determining if there is a decrease in engine speed. If there is a decrease in engine speed (YES at 608) the method proceeds to 610. At 610 the method includes increasing a degree of opening of the deflectors in the windage tray. On the other hand, if there is not a decrease in engine speed (NO at 608) the method moves to 612. At 612 the method includes maintaining the degree of opening of the deflectors in the windage tray. It will be appreciated that in other examples, steps 604 and 608 may include determining if the engine is operating above a threshold speed or below a threshold speed, respectively.

At 614 the method includes determining if engine vibration is greater than a threshold value. If the engine vibration is greater than the threshold value (YES at 614) the method moves to 616 where the method includes decreasing a degree of opening of the deflectors in the windage tray. Therefore it will be appreciated that vibration may be a catalyst of lubricant aeration therefore the windage tray contour may be responsively adjusted based on changes in engine vibration. In this way, the deflectors in the windage tray may be closed during periods of elevated vibration to reduce lubricant aeration. If the engine vibration is not greater than the threshold value (NO at 614) the method moves to 618 where the method includes maintaining the position of the deflectors in the windage tray. Method 600 enables the flow profile of the windage tray to be adjusted to decrease lubricant aeration as the engine speed increases and to increase lubricant draining as the engine speed decreases.

Now turning to FIG. 7, graphs 700 depict example engine system control signals in conjunction with engine speed and crankcase ventilation flowrate plots, such as described in FIGS. 1-6. The example of FIG. 7 is drawn substantially to scale, even though each and every point is not labeled with numerical values. As such, relative differences in timings can be estimated by the drawing dimensions. However, other relative timings may be used, if desired. Furthermore, each of the curves and plots time is represented on the x axis. It will also be appreciated that the plots in FIG. 7 are exemplary in nature and that, in other examples, the timing of the control signals, the threshold values, etc., may vary.

Continuing with FIG. 7, curve 702 depicts the engine speed (along the y axis). Signal 704 indicates a control signal sent to the windage tray with the adjustable deflectors. Curve 706 depicts the flowrate of crankcase gas into the intake system. The control signal 704 sent to the windage tray is shows including two values (i.e., open and close). However, it will be appreciated that more finite adjustments are possible such as stepwise or continuous adjustment of the deflectors to place the deflectors in different partially opened positions. For example, the deflectors may have a plurality of position that have different degrees of opening. Thus, each of the different deflector positions allow a different amount of crankcase gas flow through the windage tray. In this way, the degree of deflector opening/closing may be fine-tuned based on engine operating conditions.

At t1, the engine speeds surpasses a threshold engine speed 708. The threshold engine speed may be ascertained using the previously discussed techniques. Responsive to the engine speed surpassing the engine speed threshold the control signal 704 sent to the windage tray is changed to “open”. Consequently, the deflectors in the windage tray are opened to allow crankcase gas to flow therethrough as well as allow lubricant to drain through the windage tray.

At t2, the engine speed falls below the threshold engine speed 708. Responsive to the engine speed falling below the threshold engine speed 708 the control signal 704 sent to the windage tray is changed to “close” to reduce (e.g., prevent) crankcase gas from flowing through openings in the windage tray. Consequently, the windage tray reduces flow interference between crankcase gas and lubricant in the lubricant reservoir when in the closed configuration, thereby reducing lubricant aeration.

At t3, the crankcase ventilation flowrate surpasses a threshold value 710. When the crankcase ventilation flowrate surpasses the threshold value 710, the threshold engine speed 708 is responsively decreased. The control signal 704 sent to the windage tray is changed to “open” responsive to the crankcase ventilation flowrate surpassing the threshold value. The control strategy shown in FIG. 7 enables the flow profile of the windage tray to be altered based on engine speed and crankcase ventilation flow to enable the windage tray to provide different functions (e.g., oil aeration reduction and increased oil draining) that suit different engine conditions. Consequently, the efficiency of the lubrication system is increased.

The engine systems and methods described herein have the technical effect of decreasing lubricant aeration during high engine speeds and increasing lubricant draining during lower engine speeds. As a results, lubrication system efficiency is increased across a wide range of engine operating conditions.

The invention will further be described in the following paragraphs. In one aspect, a method for operating an engine system is provided, the method including operating an engine to perform combustion operation, determining an engine speed, and adjusting a flow profile of a plurality of deflectors in a windage tray positioned in a crankcase based on the engine speed.

In another aspect an engine system is provided that includes a lubricant reservoir receiving lubricant from lubricated components, a lubricant pump positioned in the lubricant reservoir, a crankshaft positioned in a crankcase vertically above the lubricant reservoir and receiving rotational input from a piston rod, a windage tray positioned vertically between the lubricant pump and the crankshaft, the windage tray including a plurality of deflectors extending longitudinally along the windage tray, and code stored in memory executable by a processor to increase a degree of opening of the plurality of deflectors in response to a decrease in engine speed.

In another aspect, a method for operating an engine system is provided, the method includes operating an engine with an engine speed is greater than a threshold value, and in response to operating the engine with the engine speed greater than a threshold value, adjusting a position of flow deflectors in a windage tray to decrease the flowrate of crankcase gas through openings in the windage tray.

In any of the aspects herein or combinations of the aspects, adjusting a flow profile of deflectors in the windage tray may include increasing a degree of opening of the deflectors when an engine speed is less than a threshold value and decreasing a degree of opening of the deflectors when the engine speed is greater than the threshold value.

In any of the aspects herein or combinations of the aspects, the method may further include adjusting the threshold value based on a flowrate of crankcase gas into an intake system through a crankcase ventilation system.

In any of the aspects herein or combinations of the aspects, adjusting the threshold value may include decreasing the threshold value in response to an increase in a flowrate of crankcase gas into the intake system through the crankcase ventilation system.

In any of the aspects herein or combinations of the aspects, the method may further include adjusting a flow profile of the plurality of deflectors based on engine vibration.

In any of the aspects herein or combinations of the aspects, adjusting the deflectors may include for each of the deflectors, rotating the deflector at one end about a pivot.

In any of the aspects herein or combinations of the aspects, the plurality of deflectors may be louver plates.

In any of the aspects herein or combinations of the aspects, the louver plates may have a length greater than a width.

In any of the aspects herein or combinations of the aspects, the plurality of deflectors may pivot about pivots during the increase in the degree of opening of the plurality of deflectors.

In any of the aspects herein or combinations of the aspects, the engine system may further include code stored in memory executable by the processor to decrease a degree of opening of the plurality of deflectors in response to an increase in engine speed.

In any of the aspects herein or combinations of the aspects, the increase in engine speed may include an increase in engine speed above a threshold value.

In any of the aspects herein or combinations of the aspects, the engine system may further include code stored in memory executable by the processor to adjust the threshold value based on a flowrate of crankcase gas into the intake system through a crankcase ventilation system.

In any of the aspects herein or combinations of the aspects, adjusting the threshold value may include increasing the threshold value in response to a decrease in a flowrate of crankcase gas into the intake system through the crankcase ventilation system or decreasing the threshold value in response to an increase in the flowrate of crankcase gas into the intake system through the crankcase ventilation system.

In any of the aspects herein or combinations of the aspects, the engine system may further include code stored in memory executable by the processor to increase a degree of opening of the plurality of deflectors based on engine vibration.

In any of the aspects herein or combinations of the aspects, the method may include operating the engine with an engine speed less than the threshold value, and in response to operating the engine with the engine speed less than the threshold value, adjusting a position of a plurality of deflectors in a windage tray to increase the flowrate of crankcase gas through openings in the windage tray.

In any of the aspects herein or combinations of the aspects, the method may further include adjusting the threshold value based on a flowrate of crankcase gas into the intake system through a crankcase ventilation system.

In any of the aspects herein or combinations of the aspects, adjusting the threshold value may include at least one of increasing the threshold value in response to a decrease in a flowrate of crankcase gas into an intake system through the crankcase ventilation system and decreasing the threshold value in response to an increase in the flowrate of crankcase gas into the intake system through the crankcase ventilation system.

In any of the aspects herein or combinations of the aspects, adjusting the position of the plurality of deflectors may include for each of the deflectors, rotating the deflector at one end about a deflector pivot.

Note that the example control and estimation routines included herein can be used with various engine and/or vehicle system configurations. The control methods and routines disclosed herein may be stored as executable instructions in non-transitory memory and may be carried out by the control system including the controller in combination with the various sensors, actuators, and other engine hardware. The specific routines described herein may represent one or more of any number of processing strategies such as event-driven, interrupt-driven, multi-tasking, multi-threading, and the like. As such, various actions, operations, and/or functions illustrated may be performed in the sequence illustrated, in parallel, or in some cases omitted. Likewise, the order of processing is not necessarily required to achieve the features and advantages of the example embodiments described herein, but is provided for ease of illustration and description. One or more of the illustrated actions, operations and/or functions may be repeatedly performed depending on the particular strategy being used. Further, the described actions, operations and/or functions may graphically represent code to be programmed into non-transitory memory of the computer readable storage medium in the engine control system, where the described actions are carried out by executing the instructions in a system including the various engine hardware components in combination with the electronic controller.

It will be appreciated that the configurations and routines disclosed herein are exemplary in nature, and that these specific embodiments are not to be considered in a limiting sense, because numerous variations are possible. For example, the above technology can be applied to V-6, I-4, I-6, V-12, opposed 4, and other engine types. The subject matter of the present disclosure includes all novel and non-obvious combinations and sub-combinations of the various systems and configurations, and other features, functions, and/or properties disclosed herein.

The following claims particularly point out certain combinations and sub-combinations regarded as novel and non-obvious. These claims may refer to “an” element or “a first” element or the equivalent thereof. Such claims should be understood to include incorporation of one or more such elements, neither requiring nor excluding two or more such elements. Other combinations and sub-combinations of the disclosed features, functions, elements, and/or properties may be claimed through amendment of the present claims or through presentation of new claims in this or a related application. Such claims, whether broader, narrower, equal, or different in scope to the original claims, also are regarded as included within the subject matter of the present disclosure.

Dunn, Matthew

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