EP0281572B1 - Multi-cylinder diesel internal combustion engine with low compression ratio in the cylinders - Google Patents
Multi-cylinder diesel internal combustion engine with low compression ratio in the cylinders Download PDFInfo
- Publication number
- EP0281572B1 EP0281572B1 EP87904236A EP87904236A EP0281572B1 EP 0281572 B1 EP0281572 B1 EP 0281572B1 EP 87904236 A EP87904236 A EP 87904236A EP 87904236 A EP87904236 A EP 87904236A EP 0281572 B1 EP0281572 B1 EP 0281572B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cylinder
- cylinders
- combustion engine
- diesel internal
- valve
- 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.)
- Expired
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 19
- 230000006835 compression Effects 0.000 title claims abstract description 17
- 238000007906 compression Methods 0.000 title claims abstract description 17
- 239000000446 fuel Substances 0.000 claims abstract description 6
- 230000001419 dependent effect Effects 0.000 claims 1
- 230000006698 induction Effects 0.000 claims 1
- 239000012774 insulation material Substances 0.000 claims 1
- 239000007789 gas Substances 0.000 abstract 1
- 238000004064 recycling Methods 0.000 abstract 1
- 238000001816 cooling Methods 0.000 description 4
- 238000010304 firing Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000033764 rhythmic process Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D21/00—Controlling engines characterised by their being supplied with non-airborne oxygen or other non-fuel gas
- F02D21/06—Controlling engines characterised by their being supplied with non-airborne oxygen or other non-fuel gas peculiar to engines having other non-fuel gas added to combustion air
- F02D21/08—Controlling engines characterised by their being supplied with non-airborne oxygen or other non-fuel gas peculiar to engines having other non-fuel gas added to combustion air the other gas being the exhaust gas of engine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/02—Engines with reciprocating-piston pumps; Engines with crankcase pumps
- F02B33/06—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B65/00—Adaptations of engines for special uses not provided for in groups F02B61/00 or F02B63/00; Combinations of engines with other devices, e.g. with non-driven apparatus
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D17/00—Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling
- F02D17/02—Cutting-out
- F02D17/023—Cutting-out the inactive cylinders acting as compressor other than for pumping air into the exhaust system
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B2075/1804—Number of cylinders
- F02B2075/1848—Number of cylinders twelve
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Definitions
- the invention relates to a multi-cylinder diesel internal combustion engine with a low compression ratio in the cylinders according to the preamble of claim 1.
- a generic diesel internal combustion engine is known from DE-PS-2 648 411.
- the valve can also be an arbitrarily actuated valve as a block.
- the cylinders operating as compressors remain cold in relation to the temperature of an engine cylinder. This effect arises from the delivery of the air compressed in the compressor cylinder, which is heated in the process, to an engine cylinder and the subsequent intake of air which has a lower temperature than the discharged compressed air. It has been shown that the cooling of the compressor cylinders resulting from the loss of air mass is not compensated for by the supply of heat from the cooling system.
- the arrangement causes exhaust gas recirculation from the engine cylinders to the compressor cylinders.
- a temperature increase in the compressor cylinders is achieved when the diesel internal combustion engine is split.
- the same lines are used that are already available for pushing the compressed air out of the compression cylinders on the diesel engine.
- the advantages achieved by the invention are, in particular, that when the diesel internal combustion engine is in divided operation, air with a higher temperature is available from the compressor cylinders for recharging the engine cylinders than without exhaust gas recirculation, that when switching to full-engine operation, the diesel internal combustion engine immediately loads up to Permits full load limit and that the diesel internal combustion engines already designed for the split mode of operation can be easily equipped with the arrangement according to the invention.
- FIG. 2 A diesel internal combustion engine with twelve cylinders 1 to 12 arranged in a V-shape in two rows is shown schematically in FIG. 2.
- the firing order is 1-8-5-10-3-7-6 -11 -2-9 - 4 - 12.
- cylinders 1 to 6 of the first row are engine cylinders
- cylinders 7 to 12 the second row used as a compressor cylinder in start and partial load operation.
- the cylinders 8 and 5, 10 and 3, 7 and 6, 11 and 2, 9 and 4 and 12 and 1 are each connected by a line.
- Fig. 2 only the line between cylinder 8 and cylinder 5 is shown with reference numeral 13.
- the two cylinders belonging together can be arranged in the same row.
- FIG. 1 shows a compressor cylinder 14 with the cylinder 8 and a piston 17, an engine cylinder 15 with the cylinder 5 and a piston 16 and the associated line 13 with the control elements.
- the position of the two crank pins 18, 19 of a crankshaft indicated by 20 is the same for both pistons 16, 17. Due to the V-angle 21 of the cylinder arrangement shown at 90 degrees, the piston 17 of the compressor cylinder 14 also leads 90 degrees ahead of the crankshaft angle relative to the piston 16 of the engine cylinder 15. The piston 17 of the compressor cylinder is shortly before its top dead center and has that of the amount of air sucked in before it is compressed. The piston 16 of the engine cylinder is located shortly after its bottom dead center and thus at the beginning of its compression stroke.
- Each of the lines 13, which is arranged between a pair of cylinders, is controlled by two valves.
- the control system is supplied with compressed air from a compressed air reservoir 30, which is connected via a line 31 and 32 to the reversing slide 26 and to the compressed air distributor 29, respectively.
- the lines 31, 32 are controlled by solenoid valves 33, 34.
- the solenoid valves 33, 34 in lines 31 and 32 are open.
- the compressed air from line 31 reaches a reversing slide 26 and shifts its slide 35 into the open position (as drawn). Compressed air thus passes from line 31 via line 24 to the dispenser valve 22, which is thereby shifted into the position shown.
- the line 13 is thus open. Since the solenoid valve 34 in line 32 is also open at the same time, compressed air also reaches the compressed air distributor 29, the distributor rotor 37 of which rotates at half the crankshaft speed. The position of the distributor rotor 37 is assigned to the position of the associated piston 16 of cylinder 5.
- the air sucked in via the regular inlet valve mixes with the hot exhaust gas arriving via line 13 in cylinder 8. This results in a heating of the compressor cylinder 14 and its filling quantity.
- the duration and time of use of this exhaust gas recirculation is determined by the position and length of the control groove 41 on the compressed air distributor 29. As soon as the distributor rotor 37 has reached the end of the control groove 41, the compressed air to the receiver valve 23 is blocked and the lines 27 are vented. The receiver valve 23 returns to the position shown in FIG. 1, in which the valve 38 is effective.
- the dispenser valve 22 is continuously open, while the receiver valve 23 oscillates back and forth between its two positions in the rhythm of the extension strokes of the engine cylinder 15.
- the solenoid valve 33 is closed. Shutting off the compressed air supply causes the dispenser valve 22 to switch to its closed position and releases the fuel supply to the cylinders 7 to 12.
- the solenoid valve 34 remains open. As a result, the lines 25, 27, 28 of the compressed air distributor 29 are periodically supplied with compressed air as described above.
- Compressed air also passes via line 28 to the reversing slide 26 below the differential piston 36. Since the space under slide 35 is now depressurized after solenoid valve 33 has been closed, the piston area of differential piston 36 is sufficient to slide the slide 35 into the position shown in FIG. 1 move.
- the compressed air in line 28 now opens the check valve 42, closes the check valve 43 and reaches the dispenser valve 22 via slide 35. With the pulses coming from the compressed air distributor 29, the dispenser valve 22 is now in its open position for approximately the duration of the extension stroke of cylinder 5 moved so that exhaust gas from the cylinder 5 can flow via line 13 into the cylinder 8. This exhaust gas recirculation is ended when the compressed air supply from the compressed air reservoir 30 to the compressed air distributor 29 is cut off by switching off the solenoid valve 34.
- a line 45 leading to the compressed air reservoir 30 is connected to at least one of the lines 13 via a non-return valve 46 and serves to refill the compressed air reservoir.
- a filter 47 is arranged in line 45.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Valve Device For Special Equipments (AREA)
Abstract
Description
Die Erfindung bezieht sich auf eine mehrzylindrige Dieselbrennkraftmaschine mit niedrigem Verdichtungsverhältnis in den Zylindern gemäß dem Oberbegriff von Patentanspruch 1.The invention relates to a multi-cylinder diesel internal combustion engine with a low compression ratio in the cylinders according to the preamble of
Mit einer derartigen Anordnung wird eine verbesserte Versorgung der als Motor arbeitenden Zylinder mit vorverdichteter Verbrennungsluft bewirkt, so daß im geteilten Betrieb der Dieselbrennkraftmaschine in den als Motor arbeitenden Zylindern trotz eines niedrigen Verdichtungsverhältnisses die erforderliche Verdichtungsendtemperatur zum Zünden des eingespritzten Brennstoffes erreicht wird.With such an arrangement, an improved supply of the cylinders working as the engine with precompressed combustion air is brought about, so that in split operation of the diesel internal combustion engine in the cylinders working as the engine, the compression end temperature required to ignite the injected fuel is achieved in spite of a low compression ratio.
Aus der DE-PS-2 648 411 ist eine gattungsbildende Dieselbrennkraftmaschine bekannnt. Bei dieser kann anstelle eines Rückschlagventils als Sper der Ventil auch ein willkürlich betätiges Ventil vorgesehen sein. Bei geteiltem betrieb der Dieselbrennkraftmaschine bleiben die als Verdichter arbeitenden Zylinder im Verhältnis zur Temperatur eines Motorzylinders kalt. Dieser Effekt entsteht durch die Abgabe der im Verdichterzylinder verdichteten und dabei erwärmten Luft an einen Motorzylinder und dem nachfolgenden Ansaugen von Luft, die eine niedrigere Temperatur als die abgegebene verdichtete Luft besitzt. Dabei hat sich gezeigt, daß die aus dem Luftmassenverlust resultierende Abkühlung der Verdichterzylinder nicht durch die Wärmezufuhr aus dem Kühlsystem ausgeglichen wird.A generic diesel internal combustion engine is known from DE-PS-2 648 411. In this case, instead of a check valve, the valve can also be an arbitrarily actuated valve as a block. When the diesel internal combustion engine is split, the cylinders operating as compressors remain cold in relation to the temperature of an engine cylinder. This effect arises from the delivery of the air compressed in the compressor cylinder, which is heated in the process, to an engine cylinder and the subsequent intake of air which has a lower temperature than the discharged compressed air. It has been shown that the cooling of the compressor cylinders resulting from the loss of air mass is not compensated for by the supply of heat from the cooling system.
Gemäß DE-A-2 838 682 wird in abgeschaltete Zylinder ein Gemisch aus Abgas Frischluft eingeführt. Dies verhindert Auskülen der Zylinder.According to DE-A-2 838 682, a mixture of exhaust gas fresh air is introduced into switched-off cylinders. This prevents the cylinders from cooling down.
Beim Übergang von geteiltem auf Vollmotor- Betrieb ergeben sich daher bei den Verdichterzylindern Zündprobleme, da die Verdichtungsendtemperatur erst nach einer Warmlaufphase der betroffenen Zylinder erreicht wird. Eine rasche Lastannahme der Dieselbrennkraftmaschine wird dadurch verhindert. Es ist deshalb Aufgabe der Erfindung, bei einer gattungsgemäßen Dieselbrennkraftmaschine die Abkühlung der Zylinderinnenräume bei den als Verdichter betriebenen Zylindern zu vermeiden.When switching from split to full-engine operation, there are ignition problems with the compression cylinders, since the compression end temperature is only reached after the affected cylinders have warmed up. This prevents the diesel engine from being loaded quickly. It is therefore an object of the invention to avoid cooling of the cylinder interior in the case of a generic diesel internal combustion engine in the cylinders operated as compressors.
Diese Aufgabe wird erfindungsgemäß mit den kennzeichnenden Merkmalen von Anspruch 1 gelöst. Die Anordnung bewirkt eine Abgasrückführung aus den Motorzylindern in die Verdichterzylinder. Dadurch wird bei geteiltem Betrieb der Dieselbrennkraftmaschine eine Temperaturanhebung in den Verdichterzylindern erreicht. Für die Abgasrückführung werden die gleichen Leitungen benutzt, die schon für das Überschieben der verdichteten Luft aus den Verdichterzylindern an der Dieselbrennkraftmaschine vorhanden sind.This object is achieved with the characterizing features of
Die weitere Ausgestaltung der Erfindung ergibt sich mit den Merkmalen der Ansprüche 2 bis 4.The further embodiment of the invention results from the features of
Die mit der Erfindung erzielten Vorteile bestehen insbesondere darin, daß bei geteiltem Betrieb der Dieselbrennkraftmaschine aus den Verdichterzylindern für das Nachladen der Motorzylinder Luft mit höherer Temperatur zur Verfügung steht als ohne Abgasrückführung, daß bei Übergang auf Vollmotor-Betrieb die Dieselbrennkraftmaschine eine unverzüglich einsetzende Lastaufschaltung bis zur Vollastgrenze zuläßt und daß sich die bereits für die geteilte Betriebsweise ausgebildeten Dieselbrennkraftmaschinen problemlos mit der erfindungsgemäßen Anordnung ausrüsten lassen.The advantages achieved by the invention are, in particular, that when the diesel internal combustion engine is in divided operation, air with a higher temperature is available from the compressor cylinders for recharging the engine cylinders than without exhaust gas recirculation, that when switching to full-engine operation, the diesel internal combustion engine immediately loads up to Permits full load limit and that the diesel internal combustion engines already designed for the split mode of operation can be easily equipped with the arrangement according to the invention.
Ein Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt und wird nachstehend näher beschrieben. Es zeigt:
- Fig. 1 schematische Anordnung zweier Zylinder einer Dieselbrennkraftmaschine mit Nachladeeinrichtung;
- Fig. 2 schematische Anordnung der Zylinder von Fig. 1 in den Zylinderreihen der Dieselbrennkraftmaschine.
- Figure 1 shows a schematic arrangement of two cylinders of a diesel engine with reloading device.
- Fig. 2 shows a schematic arrangement of the cylinders of Fig. 1 in the cylinder rows of the diesel engine.
Eine Dieselbrennkraftmaschine mit V-förmig in zwei Reihen angeordneten zwölf Zylindern 1 bis 12 ist schematisch in Fig. 2 dargestellt. Die Zündfolge betrage 1-8-5-10-3-7-6 -11 -2-9 - 4 - 12. Im Beispiel sind bei sogenanntem geteilten Betrieb die Zylinder 1 bis 6 der ersten Reihe als Motorzylinder, die Zylinder 7 bis 12 der zweiten Reihe als Verdichterzylinder im Start-und Teillastbetrieb eingesetzt. Die Zylinder 8 und 5, 10 und 3, 7 und 6, 11 und 2, 9 und 4 und 12 und 1 sind jeweils durch eine Leitung verbunden. In Fig. 2 ist nur die Leitung zwischen Zylinder 8 und Zylinder 5 mit Bezugszeichen 13 dargestellt. Natürlich ist es auch möglich, nur einen Teil der vorhandenen Zylinder in Motor und Verdichterzylinder aufzuteilen. Ebenso können bei entsprechender Zündfolge die beiden zusammengehörenden Zylinder in derselben Reihe angeordnet sein.A diesel internal combustion engine with twelve
In Fig. 1 sind ein Verdichterzylinder 14 mit dem Zylinder 8 und einem Kolben 17, ein Motorzylinder 15 mit dem Zylinder 5 und einem Kolben 16 sowie die zugehörige Leitung 13 mit den Steuerungselementen dargestellt.1 shows a
Die Lage der zwei Kurbeizapfen 18, 19 einer mit 20 angedeuteten Kurbelwelle stimmt für beide Kolben 16, 17 überein. Durch den mit 90 Grad dargestellten V-Winkel 21 der Zylinderanordnung ergibt sich ein Vorauseilen des Kolbens 17 des Verdichterzylinders 14 von ebenfalls 90 Grad Kurbelwellenwinkel gegenüber dem Kolben 16 des Motorzylinders 15. Der Kolben 17 des Verdichterzylinders steht kurz vor seinem oberen Totpunkt und hat die von ihm vorher angesaugte Luftmenge verdichtet. Der Kolben 16 des Motorzylinders befindet sich kurz nach seinem unteren Totpunkt und damit am Anfang seines Verdichtungshubes.The position of the two crank pins 18, 19 of a crankshaft indicated by 20 is the same for both
Jede der Leitungen 13, die zwischen einem Zylinderpaar angeordnet ist, wird von zwei Ventilen beherrscht. Das eine, sogenannte Spenderventil 22, das sich in der Nähe des Verdichterzylinders 8 befindet, wird gemeinsam mit einem Brennstoffabsperrventil 44 für die Verdichterzylinder 7 bis 12 über eine Steuerleitung 31 betätigt.Each of the
Das andere, sogenannte Empfängerventil 23, das sich in der Nähe des Motorzylinders 5 befindet, ist gemeinsam mit dem Umsteuerschieber 26 über Steuerleitungen 25, 27, 28 mit einem Druckluftverteiler 29 verbunden. Die Versorgung der Steuerung mit Druckluft erfolgt aus einem Druckluftspeicher 30, der über je eine Leitung 31 und 32 mit dem Umsteuerschieber 26 bzw. mit dem Druckluftverteiler 29 verbunden ist. Die Leitungen 31, 32 werden dabei durch Magnetventile 33, 34 beherrscht.The other, so-called receiver valve 23, which is located in the vicinity of the
Bei geteiltem Betrieb der Dieselbrennkraftmaschine sind die Magnetventile 33, 34 in Leitung 31 und 32 geöffnet. Die Druckluft aus Leitung 31 erreicht einen Umsteuerschieber 26 und verschiebt dessen Schieber 35 in Durchlaßstellung (wie gezeichnet). Damit gelangt Druckluft aus Leitung 31 über Leitung 24 zum Spenderventil 22, das dadurch in die dargestellte Stellung verschoben wird. Die Leitung 13 ist damit geöffnet. Da gleichzeitig auch das Magnetventil 34 in Leitung 32 geöffnet ist, gelangt Druckluft auch zum Druckluftverteiler 29, dessen Verteilerläufer 37 mit der halben Kurbelwellendrehzahl umläuft. Die Stellung des Verteilerläufers 37 ist der Stellung des zugehörigen Kolbens 16 von Zylinder 5 zugeordnet. In der gezeichneten Stellung von Kolben 16 am Beginn des Verdichtungshubes ist der Durchgang zwischen Leitung 32 und 27 am Druckluftverteiler 29 gesperrt. Das Empfängerventil 23 befindet sich daher in der in Fig. 1 dargestellten Stellung. Dabei ist ein im Empfängerventil 23 angeordnetes Ventil 38 wirksam, das gegen die Kraft einer Feder 39 vom Druck der im Zylinder 8 verdichteten Luft geöffnet wird. Mit der Auslegung des Ventils 38 wird der Zeitpunkt der Luftübergabe von Zylinder 8 an Zylinder 5 und die Druckhöhe beim Verdichtungsbeginn in Zylinder 5 bestimmt.When the diesel internal combustion engine is in split operation, the
Nach einer Kurbelwellenumdrehung steht der Kolben 16 des Motorzylinders 5 am Beginn des Ausschiebehubes wieder im unteren Totpunkt und der Kolben 17 des Verdichterzylinders 8 am Beginn des Ansaughubes im oberen Totpunkt. Diese Stellung der Kolben 16, 17 entspricht etwa auch der Darstellung in Fig. 1. Nur mit dem Unterschied, daß der Verteilerläufer 37 des Druckluftverteilers 29 eine um 180 Grad versetzte Stellung eingenommen hat. Dadurch ist der Durchgang zwischen Leitung 32 und 27 nun geöffnet. Die Druckluft gelangt damit in Steuerleitung 25 und verschiebt das Empfängerventil 23 in seine andere Stellung, wodurch der Durchgang 40 wirksam wird. Heißes Abgas strömt nun während des Ausschiebehubes von Zylinder 5 zum Zylinder 8, der gleichzeitig einen Ansaughub ausführt. Dabei mischen sich in Zylinder 8 die über das reguläre Einlaßventil angesaugte Luft mit dem über Leitung 13 ankommenden heißen Abgas. Dadurch ergibt sich eine Erwärmung des Verdichterzylinders 14 und seiner Füllmenge. Dauer und Einsatzzeitpunkt dieser Abgasrückführung wird durch die Lage und Länge der Steuernut 41 am Druckluftverteiler 29 bestimmt. Sobald der Verteilerläufer 37 das Ende der Steuernut 41 erreicht hat, wird die Druckluft zum Empfängerventil 23 gesperrt und die Leitungen 27 entlüftet. Das Empfängerventil 23 kehrt wieder in die in Fig. 1 dargestellte Stellung zurück, bei der das Ventil 38 wirksam ist.After a crankshaft revolution, the piston 16 of the
Während der geteilten Betriebsweise der Dieselbrennkraftmaschine ist das Spenderventil 22 dauernd geöffnet, während das Empfängerventil 23 im Rhythmus der Ausschiebehübe des Motorzylinders 15 zwischen seinen beiden Stellungen hin- und herpendelt. Beim Übergang vom geteilten Betrieb in den Vollmotorbetrieb ist es zur Verbesserung der Lastannahme der vorher als Verdichter betriebenen Zylinder wünschenswert, die Abgasrückführung über Leitung 13 noch eine Zeitlang fortzuführen. Zu diesem Zweck wird nur das Magnetventil 33 geschlossen. Die Absperrung der Druckluftzufuhr bewirkt das Umschalten des Spenderventils 22 in seine Schließstellung und die Freigabe der Brennstoffzufuhr zu den Zylindern 7 bis 12. Das Magnetventil 34 bleibt noch geöffnet. Dadurch werden die Leitungen 25, 27, 28 von Druckluftverteiler 29 wie vorstehend beschrieben periodisch mit Druckluft versorgt. Über Leitung 28 gelangt Druckluft auch zum Umsteuerschieber 26 unter den Differenzkolben 36. Da der Raum unter Schieber 35 jetzt nach Schließen von Magnetventil 33 drucklos ist, reicht die Kolbenfläche von Differenzkolben 36 aus, um den Schieber 35 in die in Fig. 1 dargestellte Stellung zu verschieben. Die in Leitung 28 anstehende Druckluft öffnet nun das Rückschlagventil 42, schließt das Rückschlagventil 43 und erreicht über Schieber 35 das Spenderventil 22. Mit den vom Druckluftverteiler 29 kommenden Impulsen wird nun jeweils das Spenderventil 22 während etwa der Dauer des Ausschiebehubes von Zylinder 5 in seine Durchlaßstellung verschoben, so daß jeweils Abgas aus dem Zylinder 5 über Leitung 13 in den Zylinder 8 strömen kann. Diese Abgasrückführung wird beendet, wenn durch Abschalten des Magnetventiles 34 die Druckluftzufuhr aus dem Druckluftspeicher 30 zum Druckluftverteiler 29 unterbunden ist.During the split mode of operation of the diesel engine, the
An wenigstens eine der Leitungen 13 ist über ein Rückschlagventil 46 eine zum Druckluftspeicher 30 führende Leitung 45 angeschlossen, die zum Nachfüllen des Druckluftspeichers dient. Zu Reinigen der Druckluft ist in der Leitung 45 ein Fiter 47 angeordnet.A
Claims (4)
- A multi-cylinder diesel internal-combustion engine with low compression ratio in the cylinders, wherein in normal operation all the cylinders are supplied with fuel and generate power, and during starting and, optionally, under partial load in a so-called split operation some of the cylinders without fuel supply have a compressor function and feed compressed air to the cylinders having an engine function, wherein a respective compressor cylinder is connected to a respective engine cylinder via a duct which is independent of the usual induction and exhaust ducts and which at one end in the vicinity of the compressor cylinder has a distributor valve which can be actuated under split operation and at its other end in the vicinity of the engine cylinder has a receiving valve shutting off in the compressor cylinder direction, and wherein the piston of each compressor cylinder precedes the piston of the associated engine cylinder by 30° to 150° of crankshaft angle, characterised in that each of the receiving valves (23) is combined with a device for the arbitrary opening of the respective associated duct (13) in the direction of the compressor cylinder (14), in that the actuation of the ducts (13) by the devices takes place during the exhaust stroke of the associated engine cylinder (16), and in that the impulse for actuating the device is derived from an energy store by a distributor (29) dependent on the crankshaft speed of rotation.
- 2. A multi-cylinder diesel internal-combustion engine according to Claim 1, characterised in that a reversing slide (26) is disposed in the control duct (31) of the distributor valve (32) [sic] and is so designed that it can be acted upon by two different actuating impulses.
- 3. A multi-cylinder diesel internal-combustion engine according to Claim 1, characterised in that the energy store is a compressed-air accumulator (30) which is supplied via a non-return valve (46) from at least one of the independent ducts (13).
- 4. A multi-cylinder diesel internal-combustion engine according to Claim 1, characterised in that the ducts (13) are covered with thermal insulation material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT87904236T ATE45783T1 (en) | 1986-09-13 | 1987-07-03 | MULTI-CYLINDER DIESEL ENGINE WITH LOW COMPRESSION RATIO IN THE CYLINDERS. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3631284A DE3631284C1 (en) | 1986-09-13 | 1986-09-13 | Multi-cylinder diesel internal combustion engine with a low compression ratio in the cylinders |
DE3631284 | 1986-09-13 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0281572A1 EP0281572A1 (en) | 1988-09-14 |
EP0281572B1 true EP0281572B1 (en) | 1989-08-23 |
Family
ID=6309580
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP87904236A Expired EP0281572B1 (en) | 1986-09-13 | 1987-07-03 | Multi-cylinder diesel internal combustion engine with low compression ratio in the cylinders |
Country Status (8)
Country | Link |
---|---|
US (1) | US4860716A (en) |
EP (1) | EP0281572B1 (en) |
JP (1) | JPS63502685A (en) |
CN (1) | CN1004719B (en) |
DE (2) | DE3631284C1 (en) |
ES (1) | ES2004778A6 (en) |
RU (1) | RU1806281C (en) |
WO (1) | WO1988002065A1 (en) |
Families Citing this family (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3633405A1 (en) * | 1986-10-01 | 1988-04-14 | Man Nutzfahrzeuge Gmbh | METHOD FOR OPERATING AN EXHAUST TRUBO-CHARGED, LOW-COMPRESSING MULTI-CYLINDER DIESEL INTERNAL COMBUSTION ENGINE |
DE3824406C1 (en) * | 1988-07-19 | 1989-05-24 | Mtu Friedrichshafen Gmbh | |
US6318310B1 (en) | 1999-08-05 | 2001-11-20 | Caterpillar Inc. | Internal combustion engine |
US6382193B1 (en) | 2000-11-20 | 2002-05-07 | Ford Global Technologies, Inc. | Method of supercharging an engine |
DE10204482A1 (en) * | 2002-02-05 | 2003-08-14 | Daimler Chrysler Ag | Internal combustion engine |
US6736121B2 (en) | 2002-06-04 | 2004-05-18 | Ford Global Technologies, Llc | Method for air-fuel ratio sensor diagnosis |
US6725830B2 (en) * | 2002-06-04 | 2004-04-27 | Ford Global Technologies, Llc | Method for split ignition timing for idle speed control of an engine |
US6736120B2 (en) * | 2002-06-04 | 2004-05-18 | Ford Global Technologies, Llc | Method and system of adaptive learning for engine exhaust gas sensors |
US6735938B2 (en) | 2002-06-04 | 2004-05-18 | Ford Global Technologies, Llc | Method to control transitions between modes of operation of an engine |
US7168239B2 (en) * | 2002-06-04 | 2007-01-30 | Ford Global Technologies, Llc | Method and system for rapid heating of an emission control device |
US20050193988A1 (en) * | 2004-03-05 | 2005-09-08 | David Bidner | System for controlling valve timing of an engine with cylinder deactivation |
US7111450B2 (en) * | 2002-06-04 | 2006-09-26 | Ford Global Technologies, Llc | Method for controlling the temperature of an emission control device |
US6758185B2 (en) * | 2002-06-04 | 2004-07-06 | Ford Global Technologies, Llc | Method to improve fuel economy in lean burn engines with variable-displacement-like characteristics |
US6868827B2 (en) | 2002-06-04 | 2005-03-22 | Ford Global Technologies, Llc | Method for controlling transitions between operating modes of an engine for rapid heating of an emission control device |
US6568177B1 (en) * | 2002-06-04 | 2003-05-27 | Ford Global Technologies, Llc | Method for rapid catalyst heating |
US7032572B2 (en) * | 2002-06-04 | 2006-04-25 | Ford Global Technologies, Llc | Method for controlling an engine to obtain rapid catalyst heating |
US6925982B2 (en) * | 2002-06-04 | 2005-08-09 | Ford Global Technologies, Llc | Overall scheduling of a lean burn engine system |
US6931839B2 (en) * | 2002-11-25 | 2005-08-23 | Delphi Technologies, Inc. | Apparatus and method for reduced cold start emissions |
US7021046B2 (en) | 2004-03-05 | 2006-04-04 | Ford Global Technologies, Llc | Engine system and method for efficient emission control device purging |
US7000602B2 (en) * | 2004-03-05 | 2006-02-21 | Ford Global Technologies, Llc | Engine system and fuel vapor purging system with cylinder deactivation |
US7367180B2 (en) * | 2004-03-05 | 2008-05-06 | Ford Global Technologies Llc | System and method for controlling valve timing of an engine with cylinder deactivation |
US7044885B2 (en) * | 2004-03-05 | 2006-05-16 | Ford Global Technologies, Llc | Engine system and method for enabling cylinder deactivation |
US7073494B2 (en) * | 2004-03-05 | 2006-07-11 | Ford Global Technologies, Llc | System and method for estimating fuel vapor with cylinder deactivation |
US7028670B2 (en) * | 2004-03-05 | 2006-04-18 | Ford Global Technologies, Llc | Torque control for engine during cylinder activation or deactivation |
US7086386B2 (en) * | 2004-03-05 | 2006-08-08 | Ford Global Technologies, Llc | Engine system and method accounting for engine misfire |
US7159387B2 (en) | 2004-03-05 | 2007-01-09 | Ford Global Technologies, Llc | Emission control device |
US7073322B2 (en) * | 2004-03-05 | 2006-07-11 | Ford Global Technologies, Llc | System for emission device control with cylinder deactivation |
US7025039B2 (en) * | 2004-03-05 | 2006-04-11 | Ford Global Technologies, Llc | System and method for controlling valve timing of an engine with cylinder deactivation |
DE102007061420B4 (en) * | 2007-12-20 | 2009-11-26 | Knorr-Bremse Systeme für Nutzfahrzeuge GmbH | A device for generating compressed air for a vehicle and method for operating a device for compressed air generation |
US20090229545A1 (en) * | 2008-03-13 | 2009-09-17 | Compressco, Inc. | Crankshaft for integral gas compressor and internal combustion engine |
JP4829994B2 (en) * | 2009-04-06 | 2011-12-07 | 住友ゴム工業株式会社 | Pneumatic tire |
US8763571B2 (en) * | 2009-05-07 | 2014-07-01 | Scuderi Group, Inc. | Air supply for components of a split-cycle engine |
WO2011159756A1 (en) | 2010-06-18 | 2011-12-22 | Scuderi Group, Llc | Split-cycle engine with crossover passage combustion |
DE102010032055B4 (en) * | 2010-07-23 | 2015-01-08 | Hong Kong Meta Co. Ltd. | Method for operating an internal combustion engine and internal combustion engine |
FR2964700B1 (en) * | 2010-09-15 | 2012-10-19 | Univ Orleans | METHOD FOR OPERATING A THERMAL-PNEUMATIC HYBRID ENGINE AND ADAPTED MOTOR |
US8833315B2 (en) | 2010-09-29 | 2014-09-16 | Scuderi Group, Inc. | Crossover passage sizing for split-cycle engine |
KR20130111560A (en) | 2010-10-01 | 2013-10-10 | 스쿠데리 그룹, 인크. | Split-cycle air hybrid v-engine |
CN103443408A (en) | 2011-01-27 | 2013-12-11 | 史古德利集团公司 | Lost-motion variable valve actuation system with valve deactivation |
CA2825804A1 (en) | 2011-01-27 | 2012-08-02 | Scuderi Group, Inc. | Lost-motion variable valve actuation system with cam phaser |
JP5870640B2 (en) * | 2011-11-15 | 2016-03-01 | いすゞ自動車株式会社 | Auxiliary brake device |
US9109468B2 (en) | 2012-01-06 | 2015-08-18 | Scuderi Group, Llc | Lost-motion variable valve actuation system |
EP2657487B1 (en) * | 2012-04-24 | 2019-04-03 | Ford Global Technologies, LLC | Self-ignited combustion engine with partial shut-down and method for operating such a combustion engine with optimised emissions |
EP2657485B1 (en) * | 2012-04-24 | 2015-08-05 | Ford Global Technologies, LLC | Method for operating an externally ignited combustion engine with partial shut-down |
EP2657486A1 (en) * | 2012-04-24 | 2013-10-30 | Ford Global Technologies, LLC | Self-ignited combustion engine with partial shut-down and method for operating such a combustion engine with optimised consumption |
US8857156B2 (en) | 2012-04-27 | 2014-10-14 | General Electric Company | Engine utilizing a plurality of control valves, and a related method thereof |
US10012153B2 (en) | 2012-08-15 | 2018-07-03 | General Electric Company | System and method for engine control |
DE102012214967B3 (en) * | 2012-08-23 | 2014-04-03 | Ford Global Technologies, Llc | Four-cylinder inline engine with partial shutdown and method of operating such a four-cylinder in-line engine |
US9109507B2 (en) * | 2012-10-18 | 2015-08-18 | GM Global Technology Operations LLC | Engine assembly with variable valve displacement on one cylinder bank and method of controlling same |
EP2971636A1 (en) | 2013-03-15 | 2016-01-20 | Scuderi Group, Inc. | Split-cycle engines with direct injection |
US10221798B2 (en) | 2015-12-01 | 2019-03-05 | Ge Global Sourcing Llc | Method and systems for airflow control |
CN115898666B (en) * | 2022-11-18 | 2024-04-19 | 中车戚墅堰机车有限公司 | Control method for improving cold start performance of EGR diesel engine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2648411C2 (en) * | 1976-10-26 | 1984-05-17 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Multi-cylinder diesel internal combustion engine |
DE2838683A1 (en) * | 1977-09-06 | 1980-03-13 | Bayerische Motoren Werke Ag | Partial load control for combustion engine - has some cylinders with pre-exhaust connected via changeover valves to other cylinders for post-expansion operation |
DE2753584A1 (en) * | 1977-12-01 | 1979-06-07 | Motoren Turbinen Union | MULTI-CYLINDER DIESEL ENGINE |
DE2838682A1 (en) * | 1978-09-05 | 1980-03-13 | Bayerische Motoren Werke Ag | Load control for multicylinder otto engine - interrupts fuel supply to some cylinders and connects them to exhaust of other cylinders |
JPS6121537Y2 (en) * | 1980-02-01 | 1986-06-27 | ||
GB2093909A (en) * | 1981-02-19 | 1982-09-08 | Ford Motor Co | I.C. engines operable on less than all cylinders |
-
1986
- 1986-09-13 DE DE3631284A patent/DE3631284C1/en not_active Expired
-
1987
- 1987-07-03 EP EP87904236A patent/EP0281572B1/en not_active Expired
- 1987-07-03 DE DE8787904236T patent/DE3760480D1/en not_active Expired
- 1987-07-03 WO PCT/DE1987/000302 patent/WO1988002065A1/en active IP Right Grant
- 1987-07-03 JP JP62503979A patent/JPS63502685A/en active Granted
- 1987-07-03 US US07/214,714 patent/US4860716A/en not_active Expired - Fee Related
- 1987-08-05 ES ES8702292A patent/ES2004778A6/en not_active Expired
- 1987-09-12 CN CN87106281.XA patent/CN1004719B/en not_active Expired
-
1988
- 1988-05-11 RU SU884355753A patent/RU1806281C/en active
Also Published As
Publication number | Publication date |
---|---|
ES2004778A6 (en) | 1989-02-01 |
JPH0321733B2 (en) | 1991-03-25 |
CN1004719B (en) | 1989-07-05 |
WO1988002065A1 (en) | 1988-03-24 |
CN87106281A (en) | 1988-05-04 |
DE3760480D1 (en) | 1989-09-28 |
DE3631284C1 (en) | 1987-04-16 |
EP0281572A1 (en) | 1988-09-14 |
US4860716A (en) | 1989-08-29 |
RU1806281C (en) | 1993-03-30 |
JPS63502685A (en) | 1988-10-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0281572B1 (en) | Multi-cylinder diesel internal combustion engine with low compression ratio in the cylinders | |
DE19742969C2 (en) | Method for starting a multi-cylinder internal combustion engine | |
DE19849914C1 (en) | Internal combustion engine with auxiliary inlet valve | |
DE3401362C2 (en) | ||
DE3125647C2 (en) | ||
DE2847527C2 (en) | ||
CH636168A5 (en) | MULTI-CYLINDER CHARGED DIESEL ENGINE. | |
DE2648411C2 (en) | Multi-cylinder diesel internal combustion engine | |
EP0141165A2 (en) | Intake and exhaust control device for internal-combustion engines | |
DE3212910A1 (en) | FUEL INLET SYSTEM FOR A PRE-COMPRESSION ENGINE | |
DE2851504C2 (en) | Method for operating an internal combustion engine with internal combustion and variable compression ratio | |
DE102019113738A1 (en) | Internal combustion engine with variable intake and exhaust valve actuation | |
DE3832784A1 (en) | COMBUSTION ENGINE | |
EP0325162B1 (en) | Power control process for an internal-combustion piston engine with controlled cylinder charge | |
DE102014218655B4 (en) | Method for operating a partially switched off self-igniting internal combustion engine and internal combustion engine for carrying out such a method | |
DE4414849A1 (en) | Fluid control system for Otto=cycle IC engine | |
EP3519684B1 (en) | Reciprocating-piston internal combustion engine with device for increasing the torque thereof | |
DE3137471C2 (en) | ||
DE3625223A1 (en) | Internal combustion engine | |
DE102015200074B4 (en) | Method for operating a partially switched-off compression-ignition internal combustion engine with at least two cylinders arranged in a row | |
DE349713C (en) | Flushing and charging process for two-stroke internal combustion engines | |
DE3011974A1 (en) | INTAKE SYSTEM FOR AN INTERNAL COMBUSTION ENGINE | |
DE4036537C1 (en) | IC engine toxics reduction system - involves mixing off-gas from previous cycle to fresh air content | |
DE4411434A1 (en) | IC engine valve operation method with two inlet valves per cylinder | |
CH373220A (en) | Method and device for starting diesel engines |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19880513 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT CH DE FR GB IT LI |
|
GBC | Gb: translation of claims filed (gb section 78(7)/1977) | ||
EL | Fr: translation of claims filed | ||
17Q | First examination report despatched |
Effective date: 19890124 |
|
EM | Fr: revised translation of claims filed | ||
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT CH DE FR GB IT LI |
|
REF | Corresponds to: |
Ref document number: 45783 Country of ref document: AT Date of ref document: 19890915 Kind code of ref document: T |
|
REF | Corresponds to: |
Ref document number: 3760480 Country of ref document: DE Date of ref document: 19890928 |
|
ET | Fr: translation filed | ||
ITF | It: translation for a ep patent filed | ||
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19920507 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 19920615 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 19920616 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19920619 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 19920622 Year of fee payment: 6 |
|
ITTA | It: last paid annual fee | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Effective date: 19930703 Ref country code: AT Effective date: 19930703 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Effective date: 19930731 Ref country code: CH Effective date: 19930731 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19930703 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Effective date: 19940331 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Effective date: 19940401 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20050703 |