EP2752561B1 - Verfahren und Vorrichtung zur Steuerung des Betriebs eines Verbrennungsmotors - Google Patents

Verfahren und Vorrichtung zur Steuerung des Betriebs eines Verbrennungsmotors Download PDF

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Publication number
EP2752561B1
EP2752561B1 EP13150429.2A EP13150429A EP2752561B1 EP 2752561 B1 EP2752561 B1 EP 2752561B1 EP 13150429 A EP13150429 A EP 13150429A EP 2752561 B1 EP2752561 B1 EP 2752561B1
Authority
EP
European Patent Office
Prior art keywords
operating lever
lever support
valve operating
inlet valve
fuel injection
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP13150429.2A
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English (en)
French (fr)
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EP2752561A1 (de
Inventor
Eike Joachim Sixel
Hendrik Johannes Lange
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Caterpillar Motoren GmbH and Co KG
Original Assignee
Caterpillar Motoren GmbH and Co KG
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Publication date
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Priority to EP13150429.2A priority Critical patent/EP2752561B1/de
Publication of EP2752561A1 publication Critical patent/EP2752561A1/de
Application granted granted Critical
Publication of EP2752561B1 publication Critical patent/EP2752561B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/0015—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
    • F01L13/0021—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque by modification of rocker arm ratio
    • F01L13/0026—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque by modification of rocker arm ratio by means of an eccentric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/0015—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
    • F01L13/0036—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque the valves being driven by two or more cams with different shape, size or timing or a single cam profiled in axial and radial direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L13/00—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations
    • F01L13/0015—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
    • F01L13/0063—Modifications of valve-gear to facilitate reversing, braking, starting, changing compression ratio, or other specific operations for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque by modification of cam contact point by displacing an intermediate lever or wedge-shaped intermediate element, e.g. Tourtelot

Definitions

  • the present disclosure generally relates to a method and device for controlling the operation of an internal combustion engine.
  • an internal combustion engine may be equipped with an exhaust after treatment system and/or may be charged via an exhaust gas turbocharger.
  • large internal combustion engines configured to bum diesel and/or gas as used, for example, on ships, with heavy road vehicles and construction vehicles, or in power plants may be controlled according to the present disclosure.
  • EP 2 136 054 Al shows a device for controlling the operation of a diesel engine equipped with a rotatable shaft provided with three eccentrics.
  • Each eccentric supports an operating lever.
  • a first eccentric supports an inlet valve operating lever formed, for example, as an oscillating arm, which may trace a stroke of an inlet cam via, for example, a roll supported thereon, and may transmit it to the inlet valve via, for example, an inlet valve operating lifter, in order to operate the inlet valve.
  • a second eccentric supports an outlet valve operating lever, which may trace the stroke of an outlet cam via, for example, a roll supported thereon, and may transmit it to an outlet valve operating lifter.
  • a stroke of a fuel pump cam may be traced by, for example, a roll arranged at the end of a pump operating lever and transmitted to a pump piston via, for example, a pressure spring.
  • the pump operating lever is supported on the third eccentric.
  • the eccentrics may be formed integrally with the rotatable shaft.
  • the eccentricities of the preferably circular cylindrical circumferential surfaces of the eccentrics relative to the axis of the rotatable shaft, as well as the relative position of the eccentricities relative to the rotational position of the shaft may be selected individually according to the respective requirements.
  • An actuator and gear wheels form an adjusting device.
  • the diesel engine is operated at a load greater than 25 % of the full load with two valve lifting curves, i.e. in the Miller cycle.
  • the shaft is twisted, so that the diesel engine is operated with two different valve lifting curves.
  • This technology is also known as flexible camshaft technology (FCT).
  • the present disclosure is directed, at least in part, to improving or overcoming one or more aspects of prior systems.
  • exemplary internal combustion engines may be, for example, an internal combustion engine operable in a low load liquid fuel mode and a high load liquid fuel mode.
  • Other exemplary internal combustion engines may be dual fuel engines operable in a liquid fuel mode and a gaseous fuel mode (also referred to as gas mode), or gas engines.
  • a rotatable shaft configured to engage with first to third eccentrics may be rotatable by an adjusting device.
  • Three different rotational positions of the shaft in combination with individual designs and arrangements of the first, second and third eccentrics may result in respective different appropriate opening and closing timings of inlet and outlet valves, and an adjusted injection of fuel, for example, liquid fuel during a low load liquid fuel mode and a high load liquid fuel mode.
  • a device for controlling the operation of an internal combustion engine comprises an inlet valve operating lever support rotationally supported, the inlet valve operating lever support being provided with a first eccentric configured to support an inlet valve operating lever for controlling an inlet valve, an outlet valve operating lever support rotationally supported, the outlet valve operating lever support being provided with a second eccentric configured to support an outlet valve operating lever for controlling an outlet valve, and a fuel injection operating lever support rotationally supported, the fuel injection operating lever support being provided with a third eccentric configured to support a fuel injection operating lever for controlling a fuel injection.
  • the device further comprises a shaft rotationally supported, the shaft being provided with a first engagement portion, a second engagement portion and a third engagement portion, the first engagement portion being configured to engage with the inlet valve operating lever support to rotate the same between a first inlet valve operating position and a second inlet valve operating position, the second engagement portion being configured to engage with the outlet valve operating lever support to rotate the same between a first outlet valve operating position and a second outlet valve operating position, and the third engagement portion being configured to engage with the fuel injection operating lever support to rotate the same between a first fuel injection operating position and a second fuel injection operating position.
  • At least two of the inlet valve operating lever support, the outlet valve operating lever support and the fuel injection operating lever support are configured to rotate independent from each other, the at least two of the inlet valve operating lever support, the outlet valve operating lever support and the fuel injection operating lever support and the associated engagement portions of the shaft being configured to engage with each other at different rotational positions of the shaft.
  • a method for controlling the operation of an internal combustion engine comprising an inlet valve operating lever support rotationally supported, the inlet valve operating lever support being provided with a first eccentric configured to support an inlet valve operating lever for controlling an inlet valve, an outlet valve operating lever support rotationally supported, the outlet valve operating lever support being provided with a second eccentric configured to support an outlet valve operating lever for controlling an outlet valve, a fuel injection operating lever support rotationally supported, the fuel injection operating lever support being provided with a third eccentric configured to support a fuel injection operating lever for controlling a fuel injection, and a shaft rotationally supported, the shaft being configured to engage with the inlet valve operating lever support, the outlet valve operating lever support, and the fuel injection operating lever support to rotate the same, comprises the steps of rotating the shaft from a first rotational position to a second rotational position to rotate at least one first operating lever support while at least one second operating lever support remains stationary, and rotating the shaft from the second rotational position to a third rotational position to rotate the at least one second operating lever support
  • Dual fuel engine may mean any type of internal combustion engine configured to bum both liquid fuels, for example, diesel, heavy fuel oil (HFO) or marine diesel oil (MDO), and gaseous fuels.
  • liquid fuels for example, diesel, heavy fuel oil (HFO) or marine diesel oil (MDO), and gaseous fuels.
  • HFO heavy fuel oil
  • MDO marine diesel oil
  • late may mean inter alia that the inlet valve opening begins later than the inlet valve opening in the high load liquid fuel mode.
  • “Early” may mean inter alia that the injection of liquid fuel begins earlier than in the high load liquid fuel mode.
  • gas fuel mode gas mode
  • gas mode gaseous fuel mode
  • All these terms may refer to that kind of operation mode of the internal combustion engine in which the internal combustion engine bums a gaseous fuel such as, for example, gas of any gas quality, particularly non-pipeline quality gas as associated with gas in oil fields.
  • a pilot injection system may inject a very small amount of liquid fuel when a dual fuel engine is operating in gas mode.
  • the pilot injection system injects a small amount of liquid fuel to ignite a gas/air mixture.
  • Such pilot injection systems are well-known in the art and common in dual fuel engines.
  • a conventional injection system is used when the dual fuel engine runs on liquid fuel such as heavy fuel oil or diesel oil. If a stop of liquid fuel is mentioned herein in respect to a gas mode, the stop of supply of liquid fuel to the conventional injection system is meant, not to the pilot injection system.
  • any reference to an inlet valve, an outlet valve or a fuel injection device, for example, a fuel pump does not limit the present disclosure to one single valve or pump.
  • one or more inlet and outlet valves or one ore more fuel pumps may be controlled by one ore more eccentrics.
  • a not illustrated internal combustion engine charged via an exhaust gas turbocharger, includes, for example, a camshaft 10 which is preferably formed integrally with several cams, for example, an inlet cam 12, an outlet cam 14 and an injection cam 16 (shown in Fig. 2 ).
  • Inlet cam 12 may operate an inlet valve that is arranged in an inlet of a combustion chamber of a cylinder of the internal combustion engine and operated via, for example, an inlet valve operating arrangement 18.
  • Outlet cam 14 may operate an outlet valve arranged in an outlet of the combustion chamber via, for example, an outlet valve operating arrangement 20.
  • Injection cam 16 may operate an injection device, for example, a pump piston (not shown) of an injection pump via, for example, a pump operating arrangement 22.
  • Inlet valve operating arrangement 18 comprises an inlet valve operating lever 26 formed, for example, as an oscillating arm, which may trace the stroke of inlet cam 12 via, for example, a roll 25 supported thereon, and transmit it to the inlet valve via, for example, an inlet valve operating lifter 28 in order to operate said inlet valve.
  • inlet valve operating lever 26 formed, for example, as an oscillating arm, which may trace the stroke of inlet cam 12 via, for example, a roll 25 supported thereon, and transmit it to the inlet valve via, for example, an inlet valve operating lifter 28 in order to operate said inlet valve.
  • outlet valve operating arrangement 20 is provided with an outlet valve operating lever 30, which may trace the stroke of outlet cam 14 via, for example, a roll 29 supported thereon, and transmit it to an outlet valve operating lifter 32.
  • the stroke of injection cam 16 may be traced by, for example, a roll 33 arranged at the end of a fuel injection operating lever 34 and transmitted to the injection device.
  • eccentric disks 36, 38 and 40 are preferably formed integrally with separate rotatable shafts 128, 132, 133 to form rotatable operating lever supports that may be rotatably supported on an engine housing (not shown).
  • the eccentricities of the preferably circular cylindrical circumferential surfaces of the eccentric disks 36, 38, 40 relative to the axis of the corresponding shaft, as well as the relative position of the eccentricities relative to the rotational position of the corresponding shaft, may be selected individually according to the respective requirements outlined herein.
  • An inlet valve operating lever support 126 includes shaft 128 and eccentric 36 and is configured to support inlet valve operating lever 26 for controlling the inlet valve.
  • An outlet valve operating lever support 130 includes shaft 132 and eccentric 38 and is configured to support outlet valve operating lever 30 for controlling the outlet valve.
  • a fuel injection operating lever support 134 includes shaft 133 and eccentric 40 and is configured to support fuel injection operating lever 34 for controlling the fuel injection.
  • a rotatable shaft 42 that is supported, for example, on the engine housing extends adjacent to operating lever supports 126-134.
  • Shaft 42 is provided with a first engagement portion 136 configured to engage with inlet valve operating lever support 126, in particular, shaft 128, to rotate the same between a first inlet valve operating position and a second inlet valve operating position.
  • shaft 42 is provided with a second engagement portion 138 configured to engage with outlet valve operating lever support 130, in particular, shaft 132, to rotate the same between a first outlet valve operating position and a second outlet valve operating position.
  • Shaft 42 is also provided with a third engagement portion 140 configured to engage with fuel injection operating lever support 134, in particular, shaft 133, to rotate the same between a first fuel injection operating position and a second fuel injection operating position.
  • First engagement portion 136, second engagement portion 138 and third engagement portion 140 are spaced apart from each other in a longitudinal direction of shaft 42, i.e. first engagement portion 136 is provided adjacent to inlet valve operating lever support 126, second engagement portion 138 is provided adjacent to outlet valve operating lever support 130, and third engagement portion 140 is provided adjacent to fuel injection operating lever support 134. As will be described in more detail below, at least two of first engagement portion 136, second engagement portion 138 and third engagement portion 140 are offset from one another in a circumferential direction of shaft 42 to engage with the associated lever supports at different rotational positions of shaft 42.
  • shaft 42 may be connected, for example, torsionally stiff, to a gearwheel 44 or any other applicable element meshing with, for example, teeth of a segmental gearwheel which may be adjustable via, for example, an actuator unit (not shown).
  • the actuator unit together with the segmental gearwheel and gearwheel 44 may form an adjusting device.
  • a hydraulic or pneumatic cylinder may be used as a longitudinally adjustable element.
  • a linear motor or any other technical element may be suitable to rotate shaft 42 in an appropriate manner, for example, via a rack and pinion mechanism or the like.
  • an actuator configured to adjust shaft 42 in at least three different rotational positions may be used.
  • an actuator configured to continuously vary the rotational angle of shaft 42 may be used for adjusting shaft 42.
  • an actuator or a combination of actuators configured to continuously vary the rotational angle of shaft 42 in a first range, and discretely adjust the rotational angle of shaft 42 in a second range may be used.
  • an electronic control device for controlling the actuator unit, may be provided, which preferably comprises a microprocessor with appropriate program and data memories, and which may be provided with several outputs, at least one of said outputs being connected to the actuator unit.
  • the electronic control device is preferably provided with several inputs, one of said inputs being connected with, for example, a load adjusting element, by means of which the load of the internal combustion engine is mechanically selectable or adjustable.
  • FIG. 2 shows engagement portions 136, 138 formed on shaft 42 and the configuration of operating lever supports 126-134 in more detail. It should be appreciated that engagement portion 140 has a configuration similar to engagement portions 136, 138.
  • each operating lever support may be formed with a separate rotatable shaft which may be supported by the internal combustion engine.
  • Each operating lever support may be supported in a separate support structure, for example, a housing or the like.
  • a housing 234 for fuel injection operating lever support 134 is shown in Figs. 1 and 2 . It should be appreciated, however, that corresponding support structures are also provided for inlet valve operating lever support 126 and outlet valve operating lever support 130.
  • First engagement portion 136 associated with inlet valve operating lever support 126 may be formed as a flange 146 integrally formed with shaft 42. On an outer circumferential surface of flange 146, a nose 147 may be provided. Nose 147 may be configured to engage with a corresponding groove 157 formed in the shaft of inlet valve operating lever support 126.
  • a biasing mechanism for example, one or more biasing springs (not shown), may be provided to bias operating lever support 126 (and, in a similar manner, operating lever supports 130, 134) against shaft 42 for reliable engagement of nose 147 and groove 157 during rotation of shaft 42.
  • inlet valve operating lever 26 When nose 147 comes into engagement with groove 157, rotation of shaft 42 will result in rotation of inlet valve operating lever support 126 and eccentric 36 associated with the same. According to the position of eccentric 36, inlet valve operating lever 26 may be adjusted to different orientations resulting in different opening and closing timings of the associated inlet valve.
  • Second engagement portion 138 includes a second flange 148 and a second nose 149 formed on an outer peripheral surface of second flange 148. Second nose 149 is configured to engage with a corresponding groove 159 formed in outlet valve operating lever support 130.
  • the configuration of second engagement portion 138 and outlet valve operating lever support 130 is similar to the configuration of first engagement portion 136 and inlet valve operating lever support 126, such that a detailed description will be omitted.
  • third engagement portion 150 associated with fuel injection operating lever support 134 is configured in a similar manner, including a third flange 150 (see Fig. 1 ) and a third nose 151 formed on an outer peripheral surface of third flange 150 and configured for engagement with a corresponding groove 161 formed in shaft 133 of fuel injection operating lever support 134 (see Figs. 6A-7C ).
  • Rotation of inlet valve operating lever support 126, outlet valve operating lever support 130 and fuel injection operating lever support 134 may be limited to a rotation between a first limiting position and a second limiting position, respectively.
  • a corresponding stop mechanism for each operating lever support may, for example, include noses 127, 131, 135 formed on the shafts of the corresponding operating lever supports.
  • Each of noses 127, 131, 135 may be configured to abut against mechanical stops 187, 189, 191, 193, 195, 197 to limit the movement of the associated operating lever support.
  • nose 135 of fuel injection operating lever support 134 may be guided in a notch or groove of housing 234 supporting fuel injection operating lever support 134 and may abut against stop 197 (see Fig. 1 ).
  • stop mechanisms for the other operating lever supports may have a similar configuration, as will be described in more detail below. It will be appreciated that, in other exemplary embodiments of the present disclosure, different stop mechanisms may be provided for each of the three operating lever supports. In the same manner, one or more brake mechanisms (not shown) may be provided for operating lever supports 126, 130, 134 for maintaining the respective operating lever supports in their respective limiting positions when they are not engaged by shaft 42, for example, via friction.
  • shaft 42 and inlet valve operating lever support 126 may be configured such that, when shaft 42 is in a position in which nose 147 is not engaged with groove 157 and is disposed on one side of shaft 128 of inlet valve operating lever support 126, inlet valve operating lever support 126 and the corresponding eccentric 36 are in a first position, in particular, a first limiting position, in which nose 127 abuts against a first stop 189.
  • inlet valve operating lever support 126 When shaft 42 is rotated counter clockwise, nose 147 is brought into engagement with groove 157. Accordingly, inlet valve operating lever support 126 is rotated clockwise. The clockwise rotation of inlet valve operating lever support 126 may be stopped by nose 147 abutting against a second stop 187. Accordingly, inlet valve operating lever support 126 may be rotated from the first position shown on the left of Fig. 3 to the second position shown on the right of Fig. 3 by rotation of shaft 42. This results in that eccentric 36 is also rotated clockwise, and inlet valve operating lever 26 (not shown) is displaced to the right in Fig. 3 , resulting in an adjusted inlet valve timing.
  • inlet valve operating lever support 126 Upon further rotation of shaft 42, as shown in Fig. 4 , inlet valve operating lever support 126 will remain in the second position, i.e. a second limiting position, and nose 147 will be out of engagement with groove 157. Accordingly, the position of inlet valve operating lever support 126 will remain stationary while shaft 42 continues to rotate. In this manner, as will be described in more detail below, it is possible to individually rotate each of inlet valve operating lever support 126, outlet valve operating lever support 130 and fuel injection operating lever support 134 when noses 147, 149, 151 are disposed at different positions along the circumferential direction of shaft 42.
  • shaft 42 could be configured such that, when shaft 42 is in the position shown on the right of Fig. 4 , nose 151 is in engagement with corresponding groove 161 formed in fuel injection operating lever support 134. Accordingly, the timing of the fuel pump could be adjusted independent from the timing of, for example, the inlet valve.
  • shaft 42 is configured such that, when nose 147 is in engagement with groove 157, noses 149 and 151 are not in engagement with corresponding grooves 159, 161, the timing of the inlet valve may be continuously varied without changing the timing of the outlet valve and the fuel injection. It will be readily apparent to the skilled person that using appropriate configurations for shaft 42 and operating lever supports 126, 130, 134 allows many different combinations for individually adjusting the timing of the corresponding valves and the fuel injection.
  • engagement portions 136, 138, 140 have been described herein as flanges formed on shaft 42, each flange being provided with a corresponding nose for engaging a groove of the associated operating lever support, many different configurations may be used for the corresponding engagement portions.
  • noses 147-151 could also be provided on the shafts of operating lever supports 126-134, with corresponding grooves being formed in shaft 42 at appropriate positions.
  • biasing springs may also be provided to bias operating lever supports and shaft 42 against each other in an appropriate manner.
  • flanges 146, 148, 150 may be annular, in other embodiments, flanges 146, 148, 150 may have a different configuration or may be omitted.
  • operating lever supports 126-134 and shaft 42 are possible without departing from the scope of the present disclosure.
  • only two of the operating lever supports may be provided separately to rotate independent from each other, i.e. two of operating lever supports 126-134 may be coupled to each other to rotate together.
  • engagement portions 136-140 may be identical and operating lever supports 126-134 may be arranged differently or have different configurations to result in the engagement with engagement portions 136-140 at different rotational angles of shaft 42.
  • two of operating lever supports 126-134 may be offset from each other.
  • control device may have many different configurations, depending on the desired application.
  • control device may be applied to a dual fuel engine.
  • dual fuel engines may need at least three sets of combinations for the valve timings and the timing of a main injection of liquid fuel, for example, diesel fuel, provided by a fuel pump.
  • shaft 42 and operating lever supports 126, 130, 134 may be configured such that, when shaft 42 is in a first position as shown in Fig. 6A , noses 147, 149, 151 are out of engagement with grooves 157, 159, 161 and are all disposed on one side of each operating lever support shaft. Nose 151 may be offset from noses 147, 149.
  • Each of operating lever supports 126, 130, 134 may be in a first limiting position.
  • the corresponding eccentrics 36, 38, 40 may be configured such that, in the first limiting position, the inlet valve is operated with an early inlet valve timing, the exhaust valve is operated with a late exhaust valve timing, and the fuel pump is operated with a "normal" injection timing corresponding to a high load diesel mode with a strong Miller cycle.
  • shaft 42 When the dual fuel engine is to be operated in the gas mode, shaft 42 is rotated counter clockwise to the position shown in Fig. 6B .
  • nose 151 associated with fuel injection operating lever support 134 is offset from noses 147, 149, when shaft 42 is rotated counter clockwise to a second position, noses 147, 149 are brought into engagement with grooves 157, 159 and rotate inlet valve operating lever support 126 and outlet valve operating lever support 130 in a clockwise direction, while nose 151 is not brought into engagement with groove 161 and fuel injection operating lever 34 remains stationary.
  • the second limiting position of inlet valve operating lever support 126 may correspond to a late inlet valve timing
  • the second limiting position of outlet valve operating lever support 130 may correspond to an early exhaust valve timing
  • control device it is possible to provide at least three different configurations for the operation of a dual fuel engine in a high load diesel fuel mode, a low load diesel fuel mode and a gas mode by rotating shaft 42 to one of three different positions.
  • transitions from the gas mode to one of the low load diesel fuel mode and the high load diesel fuel mode may be effected by rotation between the position of shaft 42 shown in Fig. 6B and the positions of shaft 42 shown in Figs. 6A, 6C , respectively.
  • the control device may be used with a diesel engine with an exhaust after treatment system such as an SCR system.
  • a diesel engine generally requires two configurations, a low load diesel fuel mode and a high load diesel fuel mode.
  • additional control may be required for the timing of the exhaust valve. This additional control may be a load dependent control.
  • shaft 42 and operating lever supports 126, 130, 134 may be configured such that, when shaft 42 is in a first position, as shown in Fig. 7A , inlet valve operating lever support 126 is in its first limiting position, outlet valve operating lever support 130 is in its second limiting position, and fuel injection operating lever support 134 is in its first limiting position.
  • the first limiting position of inlet valve operating lever support 126 may correspond to an early inlet valve timing
  • the second limiting position of outlet valve operating lever support 130 may correspond to a late exhaust valve timing
  • the first limiting position of fuel injection operating lever support 134 may correspond to a "normal" injection timing of the fuel pump, for example, in the high load diesel fuel mode.
  • shaft 42 When the diesel engine is to be operated in the low load diesel fuel mode, shaft 42 may be turned counter clockwise. Noses 147, 149, 151 may be arranged on shaft 42 such that, when shaft 42 is rotated counter clockwise from the first position shown in Fig. 7A to the second position shown in Fig. 7B , noses 147, 151 are brought into engagement with grooves 157, 161, while nose 149 is not in engagement with groove 159 formed on outlet valve operating lever support 130. Accordingly, rotation of shaft 42 to the position shown in Fig. 7B may result in the inlet valve timing being adjusted from an early inlet valve timing to a late inlet valve timing and the injection timing being adjusted from a "normal" injection timing to an early injection timing, while the late exhaust valve timing is not adjusted.
  • the configuration shown in Fig. 7B may correspond to the low load diesel fuel mode with nearly no Miller cycle, a smaller valve overlap and an early injection timing.
  • shaft 42 may be rotated clockwise from the first position shown in Fig. 7A to a third position shown in Fig. 7C .
  • Shaft 42 and operating lever support 126, 130, 134 may be configured such that, upon rotation of shaft 42 from the position shown in Fig. 7A to the position shown in Fig. 7C , nose 149 is brought into engagement with groove 159 formed on outlet valve operating lever support 130.
  • noses 147, 151 may be arranged on shaft 42 such that, at the same time, noses 147, 151 do not come into engagement with grooves 157, 161. Accordingly, in the position of shaft 42 shown in Fig. 7C , it is possible to continuously vary the timing of the outlet valve while maintaining the early inlet valve timing and the "normal" injection timing of the high load diesel fuel mode shown in Fig. 7A .
  • control device may be applied to many different internal combustion engines, for example, gas engines, without departing from the scope of the present disclosure.
  • any appropriate fuel injection device such as a fuel pump or the like may be used for injecting liquid fuel or gaseous fuel in accordance with the present disclosure.
  • an internal combustion engine may be any kind of large internal combustion engine having an output range of 1,000 kW or more.
  • Internal combustion engines as disclosed herein may be suitable for operation with heavy fuel oil (HFO), marine diesel oil (MDO), diesel oil (DO) and gas.
  • an internal combustion engine according to the present disclosure may include any number of cylinders in any known cylinder configuration.
  • Shaft 42 may be embodied as a single shaft for a number of cylinders of the internal combustion engine, or a separate shaft 42 may be provided for each cylinder of the internal combustion engine.

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Claims (15)

  1. Vorrichtung zum Steuern des Betriebs einer Brennkraftmaschine mit innerer Verbrennung, mit:
    einem drehgelagerten Einlassventilbetätigungshebelträger (126), der mit einem ersten Exzenter (36) versehen ist, der zum Tragen eines Einlassventilbetätigungshebels (26) zum Steuern eines Einlassventils ausgebildet ist;
    einem drehgelagerten Auslassventilbetätigungshebelträger (130), der mit einem zweiten Exzenter (38) versehen ist, der zum Tragen eines Auslassventilbetätigungshebels (30) zum Steuern eines Auslassventils ausgebildet ist;
    einem drehgelagerten Kraftstoffeinspritzbetätigungshebelträger (134), der mit einem dritten Exzenter (40) versehen ist, der zum Tragen eines Kraftstoffeinspritzbetätigungshebels (34) zum Steuern einer Kraftstoffeinspritzvorrichtung ausgebildet ist; und
    einer drehgelagerten Welle (42), die mit einem ersten Eingriffsabschnitt (136), einem zweiten Eingriffsabschnitt (138) und einem dritten Eingriffsabschnitt (140) versehen ist, wobei der erste Eingriffsabschnitt (136) zum Eingriff mit dem Einlassventilbetätigungshebelträger (126) zur Drehung desselben zwischen einer ersten Einlassventilbetätigungsposition und einer zweiten Einlassventilbetätigungsposition ausgebildet ist, der zweite Eingriffsabschnitt (138) zum Eingriff mit dem Auslassventilbetätigungshebelträger (130) zur Drehung desselben zwischen einer ersten Auslassventilbetätigungsposition und einer zweiten Auslassventilbetätigungsposition ausgebildet ist und der dritte Eingriffsabschnitt (140) zum Eingriff mit dem Kraftstoffeinspritzbetätigungshebelträger (134) zur Drehung desselben zwischen einer ersten Kraftstoffeinspritzbetätigungsposition und einer zweiten Kraftstoffeinspritzbetätigungsposition ausgebildet ist,
    wobei mindestens zwei von dem Einlassventilbetätigungshebelträger (126), dem Auslassventilbetätigungshebelträger (130) und dem Kraftstoffeinspritzbetätigungshebelträger (134) zur Drehung unabhängig voneinander ausgebildet sind, und
    die mindestens zwei von dem Einlassventilbetätigungshebelträger (126), dem Auslassventilbetätigungshebelträger (130) und dem Kraftstoffeinspritzbetätigungshebelträger (134) sowie die zugehörigen Eingriffsabschnitte der Welle (42) zum Eingriff miteinander an unterschiedlichen Drehpositionen der Welle (42) ausgebildet sind.
  2. Vorrichtung nach Anspruch 1, bei der der erste Eingriffsabschnitt (136), der zweite Eingriffsabschnitt (138) und der dritte Eingriffsabschnitt (140) jeweils einen Flansch (146, 148, 150) und eine Nase (147, 149, 151) oder eine Nut enthalten, die an dem Flansch (146, 148, 150) vorgesehen ist, wobei die Flansche (146, 148, 150) in einer Längsrichtung der Welle (42) voneinander beabstandet sind, wobei mindestens zwei der Nasen (147, 149, 151) oder Nuten in einer Umfangsrichtung der Welle (42) zueinander versetzt sind und zum Eingriff mit einer entsprechenden Nut (157, 159, 161) oder Nase, die an dem zugeordneten Betätigungshebelträger vorgesehen ist, zur Drehung derselben ausgebildet sind.
  3. Vorrichtung nach Anspruch 1 oder 2, bei der der Einlassventilbetätigungshebelträger (126) über eine erste separate Welle (128) drehgelagert ist, der Auslassventilbetätigungshebelträger (130) über eine zweite separate Welle (132) drehgelagert ist und der Kraftstoffeinspritzbetätigungshebelträger (134) über eine dritte separate Welle (133) drehgelagert ist, wobei die erste separate Welle (128), die zweite separate Welle (132) und die dritte separate Welle (133) koaxial zueinander sind.
  4. Vorrichtung nach einem der Ansprüche 1 bis 3, ferner mit mindestens einem ersten Stoppmechanismus (127, 187, 189), der zum Begrenzen der Drehung des Einlassventilbetätigungshebelträgers (126) zwischen der ersten Einlassventilbetätigungsposition und der zweiten Einlassventilbetätigungsposition ausgebildet ist, einem zweiten Stoppmechanismus (131, 191, 193), der zum Begrenzen der Drehung des Auslassventilbetätigungshebelträgers (130) zwischen der ersten Auslassventilbetätigungsposition und der zweiten Auslassventilbetätigungsposition ausgebildet ist, oder einem dritten Stoppmechanismus (135, 195, 197), der zum Begrenzen der Drehung des Kraftstoffeinspritzbetätigungshebelträgers (134) zwischen der ersten Kraftstoffeinspritzbetätigungsposition und der zweiten Kraftstoffeinspritzbetätigungsposition ausgebildet ist.
  5. Vorrichtung nach einem der Ansprüche 1 bis 4, ferner mit mindestens einem ersten Bremsmechanismus, der zum Halten des Einlassventilbetätigungshebelträgers (126) an der ersten Einlassventilbetätigungsposition und der zweiten Einlassventilbetätigungsposition ausgebildet ist, einem zweiten Bremsmechanismus, der zum Halten des Auslassventilbetätigungshebelträgers (130) an der ersten Auslassventilbetätigungsposition und der zweiten Auslassventilbetätigungsposition ausgebildet ist, oder einem dritten Bremsmechanismus, der zum Halten des Kraftstoffeinspritzbetätigungshebelträgers (134) an der ersten Kraftstoffeinspritzbetätigungsposition und der zweiten Kraftstoffeinspritzbetätigungsposition ausgebildet ist.
  6. Vorrichtung nach einem der Ansprüche 1 bis 5, ferner mit einer Einstellvorrichtung, die zum Einstellen der Welle (42) auf mindestens eine erste Drehposition, eine zweite Drehposition, die sich von der ersten Drehposition unterscheidet, und eine dritte Drehposition, die sich von der ersten Drehposition und der zweiten Drehposition unterscheidet, ausgebildet ist.
  7. Vorrichtung nach Anspruch 6, bei der der erste Eingriffsabschnitt (136), der zweite Eingriffsabschnitt (138), der dritte Eingriffsabschnitt (140), der Einlassventilbetätigungshebelträger (126), der Auslassventilbetätigungshebelträger (130) und der Kraftstoffeinspritzbetätigungshebelträger (134) derart angeordnet sind, dass bei einer Drehung der Welle (42) von der ersten Drehposition zu der zweiten Drehposition der Einlassventilbetätigungshebelträger (126) von der ersten Einlassventilbetätigungsposition zu der zweiten Einlassventilbetätigungsposition gedreht wird, der Auslassventilbetätigungshebelträger (130) von der ersten Auslassventilbetätigungsposition zu der zweiten Auslassventilbetätigungsposition gedreht wird und der Kraftstoffeinspritzbetätigungshebelträger (134) an der zweiten Kraftstoffeinspritzbetätigungsposition bleibt, und bei Drehung der Welle (42) von der zweiten Drehposition zu der dritten Drehposition der Kraftstoffeinspritzbetätigungshebelträger (134) von der ersten Kraftstoffeinspritzbetätigungsposition zu der zweiten Kraftstoffeinspritzbetätigungsposition gedreht wird, während der Einlassventilbetätigungshebelträger (126) an der zweiten Einlassventilbetätigungsposition bleibt und der Auslassventilbetätigungshebelträger (130) an der zweiten Auslassventilbetätigungsposition bleibt.
  8. Vorrichtung nach Anspruch 6 oder 7, bei der die Vorrichtung zum Steuern eines Zweikraftstoffmotors ausgebildet ist, wobei die erste Drehposition einem Hochlastflüssigkraftstoffbetriebsmodus entspricht, die zweite Drehposition einem Gaskraftstoffbetriebsmodus entspricht und die dritte Drehposition einem Niedriglastflüssigkraftstoffmodus des Zweikraftstoffmotors entspricht.
  9. Vorrichtung nach Anspruch 8, bei der der Einlassventilbetätigungshebelträger (126) derart ausgebildet ist, dass an der ersten Einlassventilbetätigungsposition das zugehörige Einlassventil früh öffnet und an der zweiten Einlassventilbetätigungsposition das zugehörige Einlassventil spät öffnet, der Auslassventilbetätigungshebelträger (130) derart ausgebildet ist, dass an der ersten Auslassventilbetätigungsposition das zugehörige Auslassventil spät öffnet und an der zweiten Auslassventilbetätigungsposition das zugehörige Auslassventil früh öffnet, der Kraftstoffeinspritzbetätigungshebel (134) derart ausgebildet ist, dass an der zweiten Kraftstoffeinspritzbetätigungsposition die Kraftstoffeinspritzung derart gesteuert wird, dass eine Einspritzung von Flüssigkraftstoff früh durchgeführt wird.
  10. Vorrichtung nach Anspruch 6, bei der der erste Eingriffsabschnitt (136), der zweite Eingriffsabschnitt (138), der dritte Eingriffsabschnitt (140), der Einlassventilbetätigungshebelträger (126), der Auslassventilbetätigungshebelträger (130) und der Kraftstoffeinspritzbetätigungshebelträger (134) derart angeordnet sind, dass bei einer Drehung der Welle (42) von der ersten Drehposition zu der zweiten Drehposition der Einlassventilbetätigungshebelträger (126) von der ersten Einlassventilbetätigungsposition zu der zweiten Einlassventilbetätigungsposition gedreht wird, der Auslassventilbetätigungshebelträger (130) an der ersten Auslassventilbetätigungsposition bleibt und der Kraftstoffeinspritzbetätigungshebelträger (134) von der ersten Kraftstoffeinspritzbetätigungsposition zu der zweiten Kraftstoffeinspritzbetätigungsposition gedreht wird.
  11. Vorrichtung nach Anspruch 10, bei der bei einer Drehung der Welle (42) von der zweiten Drehposition zu der dritten Drehposition der Auslassventilbetätigungshebelträger (130) von der ersten Auslassventilbetätigungsposition zu der zweiten Auslassventilbetätigungsposition gedreht wird, während der Einlassventilbetätigungshebelträger (126) an der zweiten Einlassventilbetätigungsposition bleibt und der Kraftstoffeinspritzbetätigungshebelträger (134) an der zweiten Auslassventilbetätigungsposition bleibt.
  12. Vorrichtung nach einem der Ansprüche 6, 10 oder 11, bei der die Vorrichtung zum Steuern einer Brennkraftmaschine mit innerer Verbrennung ausgebildet ist, die ein Abgasbehandlungssystem aufweist, wobei die erste Drehposition einem Niedriglastbetriebsmodus entspricht, die zweite Drehposition einem Hochlastbetriebsmodus entspricht und die dritte Drehposition einem emissionsgesteuerten Betriebsmodus der Brennkraftmaschine mit innerer Verbrennung entspricht.
  13. Vorrichtung nach Anspruch 12, bei der der Einlassventilbetätigungshebelträger (126) derart ausgebildet ist, dass an der ersten Einlassventilbetätigungsposition das zugehörige Einlassventil spät öffnet und an der zweiten Einlassventilbetätigungsposition das zugehörige Einlassventil früh öffnet, der Auslassventilbetätigungshebel (130) derart ausgebildet ist, dass an der ersten Auslassventilbetätigungsposition das zugehörige Auslassventil spät öffnet und an der zweiten Auslassventilbetätigungsposition das zugehörige Auslassventil früh öffnet, der Kraftstoffeinspritzbetätigungshebelträger (134) derart ausgebildet ist, dass an der ersten Kraftstoffeinspritzbetätigungsposition die Kraftstoffeinspritzung derart gesteuert wird, dass eine Einspritzung von Flüssigkraftstoff früher als an der zweiten Kraftstoffeinspritzbetätigungsposition durchgeführt wird.
  14. Vorrichtung nach einem der Ansprüche 6 bis 13, bei der die Einstellvorrichtung zum stufenlosen Variieren der Drehposition der Welle (42) zum Einstellen mindestens des Einlassventilbetätigungshebelträgers (126), des Auslassventilbetätigungshebelträgers (130) und des Kraftstoffeinspritzbetätigungshebelträgers in einem Kontinuum von Positionen zwischen der ersten Betätigungsposition und der zweiten Betätigungsposition ausgebildet ist.
  15. Verfahren zum Steuern des Betriebs einer Brennkraftmaschine mit innerer Verbrennung, die einen drehgelagerten Einlassventilbetätigungshebelträger (126), der mit einem ersten Exzenter (36) versehen ist, der zum Tragen eines Einlassventilbetätigungshebels (26) zum Steuern eines Einlassventils ausgebildet ist, einen drehgelagerten Auslassventilbetätigungshebelträger (130), der mit einem zweiten Exzenter (38) versehen ist, der zum Tragen eines Auslassventilbetätigungshebels (30) zum Steuern eines Auslassventils ausgebildet ist, einen drehgelagerten Kraftstoffeinspritzbetätigungshebelträger (134), der mit einem dritten Exzenter (40) versehen ist, der zum Tragen eines Kraftstoffeinspritzbetätigungshebels (34) zum Steuern einer Kraftstoffpumpe ausgebildet ist, und eine drehgelagerte Welle (42) aufweist, die zum Eingriff mit dem Einlassventilbetätigungshebelträger (126), dem Auslassventilbetätigungshebelträger (130) und dem Kraftstoffeinspritzbetätigungshebelträger (134) zur Drehung derselben ausgebildet ist, mit folgenden Schritten:
    Drehen der Welle (42) von einer ersten Drehposition zu einer zweiten Drehposition zur Drehung mindestens eines ersten Betätigungshebelträgers, während mindestens ein zweiter Betätigungshebelträger stationär bleibt, und
    Drehen der Welle (42) von der zweiten Drehposition zu einer dritten Drehposition zur Drehung des mindestens einen zweiten Betätigungshebelträgers.
EP13150429.2A 2013-01-07 2013-01-07 Verfahren und Vorrichtung zur Steuerung des Betriebs eines Verbrennungsmotors Not-in-force EP2752561B1 (de)

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Family Cites Families (15)

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Publication number Priority date Publication date Assignee Title
CH390617A (de) 1962-01-31 1965-04-15 Sulzer Ag Ventilantrieb für Kolbenbrennkraftmaschinen
DE3213565A1 (de) 1982-04-13 1983-10-13 Hans Eugen 7760 Radolfzell Barth Regelbarer ventiltrieb fuer brennkraftmaschinen
DE3313313C2 (de) 1983-04-13 1986-09-25 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8900 Augsburg Hubkolbenbrennkraftmaschine mit einer Einrichtung zur Einspritzzeitpunktverstellung
DE69110342T2 (de) * 1990-03-14 1995-10-12 Suzuki Co Ltd Ventiltriebvorrichtung für Viertaktbrennkraftmaschine.
DE4207980A1 (de) 1992-03-13 1993-09-16 Mak Maschinenbau Krupp Vorrichtung zur betaetigung einer einspritzpumpe
US5713335A (en) 1995-09-12 1998-02-03 Cummins Engine Company, Inc. Variable injection timing and injection pressure control arrangement
US5666913A (en) 1996-05-29 1997-09-16 Cummins Engine Company, Inc. Variable timing cam follower lever assembly
JPH1136833A (ja) 1997-07-22 1999-02-09 Otix:Kk 可変動弁機構
US6431134B1 (en) 2001-04-20 2002-08-13 Caterpillar Motoren Gmbh & Co. Kg Camshaft follower arrangement and method
ATE299555T1 (de) 2001-07-04 2005-07-15 Caterpillar Motoren Gmbh & Co Verfahren und vorrichtung zum einspritzen von kraftstoff
EP1477638B1 (de) 2003-05-08 2008-12-24 Caterpillar Motoren GmbH & Co. KG Variable Ventilsteuerungseinrichtung
DE10359087B3 (de) 2003-12-17 2005-05-19 Caterpillar Motoren Gmbh & Co. Kg Variable Ventilsteuerungseinrichtung
DE102004057438A1 (de) 2004-11-27 2006-06-01 Man B & W Diesel Ag Ventiltrieb für Gaswechselventile einer Brennkraftmaschine mit einem verstellbaren Schwinghebel, der einerseits mit einer Exzenterwelle und andererseits mit einer auf einem Nocken einer Nockenwelle laufenden Rolle zusammenwirkt
JP2009228555A (ja) 2008-03-24 2009-10-08 Hitachi Ltd 内燃機関の可変動弁装置及び該可変動弁装置の制御軸
EP2136054B1 (de) 2008-06-18 2011-09-07 Caterpillar Motoren GmbH & Co. KG Vorrichtung zur Steuerung des Betriebs eines Verbrennungsmotors

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