Combustion engine, has exhaust gas return line opening into intake line downstream of compressor, and pre-cooling device arranged upstream of or in region of non-return valve that is arranged upstream of exhaust gas recirculation cooler
Abstract
The invention relates to an internal combustion engine (1) having an inlet line (2) and an exhaust line (3), with at least one of a compressor (4) and an exhaust gas turbine (5) having an exhaust gas turbocharger with a high pressure exhaust gas recirculation system with at least one exhaust gas recirculation line (6) , which starts upstream of the exhaust gas turbine (5) from the exhaust line (3) and downstream of the compressor (4) in the inlet line (2) opens, where in the exhaust line (3) at least one first exhaust gas recirculation cooler (7), at least one exhaust gas recirculation valve (8) and at least one non-return valve (9) is arranged and wherein the check valve (9) upstream of the first exhaust gas recirculation cooler (7) is arranged. In order to allow strict emission criteria low fuel consumption, it is provided that upstream of or in the region of the check valve (9) at least one pre-cooler (20) is arranged.

Term
5 yearsleft in the term
Expires 6 October 2031.
- Priority and filed
- Granted
- Today
- Expires
10 claims: 1 independent, 9 dependent
- 1Patentansprüche 1. Brennkraftmaschine (1) mit einem Einlassstrang (2) und einem Abgasstrang (3), mit zumindest einem einen Verdichter (4) und eine Abgasturbine (5) aufweisenden Abgasturbolader, mit einem Hochdruck-Abgasrückführsystem mit zumindest einer Abgasrückführleitung (6), welche stromaufwärts der Abgasturbine (5) vom Abgasstrang (3) ausgeht und stromabwärts des Verdichters (4) in den Einlassstrang (2) einmündet, wobei in der Abgasrückführleitung (6) zumindest ein erster Abgasrückführkühler (7), zumindest ein Abgasrückführventil (8) und zumindest ein Rückschlagventil (9) angeordnet ist und wobei das Rückschlagventil (9) stromaufwärts des ersten Abgasrückführkühlers (7) angeordnet ist, wobei stromaufwärts oder im Bereich des Rückschlagventils (9) zumindest eine Vorkühleinrichtung (20) angeordnet ist, dadurch gekennzeichnet, dass die Vorkühleinrichtung (20) durch eine Kühlleitung (21) innerhalb des Zylinderkopfes (15) gebildet ist.
- 2Brennkraftmaschine (1) nach Anspruch 1, dadurch gekennzeichnet, dass die Vorkühleinrichtung (20) durch Kühlrippen an einem zum Rückschlagventil (9) führenden Abschnitt der Abgasrückführleitung (6) gebildet ist.
- 3Brennkraftmaschine (1) nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Vorkühleinrichtung (20) durch eine Luftkühlung, erzielt durch gezieltes Anströmen eines zum Rückschlagventil (9) führenden Abschnittes der Abgasrückführleitung (6) und/oder durch Anströmen des Rückschlagventils (9), gebildet ist. 3/6 AT511 604 B1 2013-01-15 österreichisches Patentamt
- 4Brennkraftmaschine (1) nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass die Vorkühleinrichtung (20) durch einen zweiten Abgasrückführkühler (22) gebildet ist.
- 5Brennkraftmaschine (1) nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass das Abgasrückführventil (8) stromabwärts des Rückschlagventils (9) und/oder des ersten Abgasrückführkühlers (7) angeordnet ist.
- 6Brennkraftmaschine (1) nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass die Abgasrückführleitung (6) sich in zumindest zwei, vorzugsweise symmetrische, Zweigleitungen (10) aufspaltet, wobei die Zweigleitungen (10) zylinderindividuell jeweils in einen Einlasskanal (11) unterschiedlicher Zylinder (12) einmünden.
- 7Verfahren zum Betreiben einer Brennkraftmaschine (1) mit einem HochdruckAbgasrückführsystem, insbesondere nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass in zumindest einem Betriebsbereich der Brennkraftmaschine (1) die Steuerzeit zumindest eines Einlassventils und/oder eines Auslassventils so verändert wird, dass eine negative Ventilüberschneidung auftritt.
- 8Verfahren nach Anspruch 7, dadurch gekennzeichnet, dass die negative Ventilüberschneidung - bezogen auf 1 mm Ventilhub - 40° bis 120° Kurbelwinkel (KW), vorzugsweise 60° bis 100° Kurbelwinkel (KW) beträgt.
- 9Verfahren nach Anspruch 7 oder 8, dadurch gekennzeichnet, dass der Einlassschluss, insbesondere in Betriebsphasen mit negativer Ventilüberschneidung, bei 1 mm Ventilhub später als 590° Kurbelwinkel nach dem oberen Totpunkt der Zündung erfolgt.
- 10Verfahren nach einem der Ansprüche 7 bis 9, dadurch gekennzeichnet, dass der Wechsel von positiver zu negativer Ventilüberschneidung durch Vorverstellen der Auslasssteuerzeiten erfolgt.
Independent claims10
37 paragraphs, as filed
Patent office
description
The invention relates to an internal combustion engine with an inlet line and an exhaust line, with at least one exhaust gas turbocharger having a compressor and an exhaust gas turbine, with a high-pressure exhaust gas recirculation system with at least one exhaust gas recirculation line, which emanates from the exhaust gas line upstream of the exhaust gas turbine and into the inlet line downstream of the compressor opens, wherein in the exhaust gas recirculation line at least one first exhaust gas recirculation cooler, at least one exhaust gas recirculation valve and at least one check valve is arranged and the check valve is arranged upstream of the first exhaust gas recirculation cooler, with at least one pre-cooling device being arranged upstream or in the area of the check valve. The invention also relates to a method for operating this internal combustion engine.
From JP 2007-085 248 A an internal combustion engine with high pressure exhaust gas recirculation is known, an exhaust gas recirculation valve and a check valve being arranged in parallel branch lines of the exhaust gas recirculation line in the exhaust gas recirculation line upstream of an exhaust gas recirculation cooler.
EP 0 840 000 A1 describes an internal combustion engine with a high-pressure exhaust gas recirculation system, an exhaust gas recirculation valve being arranged in the exhaust gas recirculation line in the area of the extraction point from the exhaust gas line and a check valve being arranged in the area of the opening into the inlet line. An exhaust gas recirculation cooler is arranged between the exhaust gas recirculation valve and the check valve.
GB 2 473 821 A discloses an internal combustion engine with a high-pressure exhaust gas recirculation system, two exhaust gas recirculation coolers being arranged one behind the other in an exhaust gas recirculation line. Both coolers can be bypassed by a bypass line, each bypass line can be controlled separately via a bypass valve.
The publications DE 10 2008 050 368 A1, WO 2009/151 080 A1, WO 2009/105 463 A1 and JP 2007/303 355 A disclose internal combustion engines with an inlet line and an outlet line, an exhaust gas turbocharger and a high pressure exhaust gas recirculation system between Outlet line and inlet line, wherein an exhaust gas recirculation cooler, an exhaust gas recirculation valve and a check valve are arranged in the exhaust gas recirculation line, which is positioned upstream of a first exhaust gas recirculation cooler. A pre-cooling device is arranged upstream of the check valve.
Furthermore, it is from the publications EP 1 835 155 A2, JP 2007-303 355 A, JP 2007332 913 A, US 7,275,514 B2, US 7,360,523 B2, US 7,367,313 B2, US 7,370,0633 B2 and US 2009/0150052 A1 known to use a negative valve overlap for inlet and outlet valves in connection with exhaust gas recirculation. Due to the negative valve overlap, the pressure difference between the exhaust line and the intake line can be positively influenced in order to increase the exhaust gas recirculation quantities.
The object of the invention is to achieve a reduction in consumption while adhering to the strictest exhaust gas guidelines.
According to the invention this is achieved in that the pre-cooling device is formed by a cooling line within the cylinder head.
The pre-cooling device can also be formed by cooling fins on a section of the exhaust gas recirculation line leading to the check valve or by air cooling, achieved by targeted flow against a section of the exhaust gas recirculation line leading to the check valve and / or by flow against the check valve.
It when the pre-cooling device is formed by a second exhaust gas recirculation cooler, wherein the exhaust gas recirculation valve is preferably arranged downstream of the check valve and / or the first exhaust gas recirculation cooler is particularly advantageous.
By the high pressure exhaust gas recirculation with check valve can through the pressure 1/6
AT511 604 B1 2013-01-15 Austrian
Patent Office pulsations can be fed back into the inlet line even with a low or negative pressure difference between the outlet and inlet ducts. In order to enable a cylinder-specific exhaust gas recirculation, it can furthermore be provided that the exhaust gas recirculation line splits into at least two branch lines, the branch line opening into an inlet channel of different cylinders for each individual cylinder. The feed line to the distribution strip is preferably carried out in the middle; the services branching off from the distribution bar to the cylinders are preferably symmetrical.
The pre-cooler in front of the check valve prevents overheating of the check valve and makes it possible to maintain the temperature limits of the components. In addition, gas dynamic effects are less disturbed.
In a further embodiment of the invention it is provided that in at least one operating range in which exhaust gas recirculation is desired, the control time of at least one inlet valve and / or one outlet valve is changed so that a negative valve overlap occurs, preferably the inlet closure at 1 mm valve lift, especially in operating phases with negative valve overlap, takes place later than 590 ° crank angle after the top dead center of the ignition. It can also be provided that the change from positive to negative valve overlap takes place by advancing the exhaust control times.
The negative valve overlap (based on 1 mm valve lift) is 40 ° to 120 ° crank angle, preferably 60 ° to 100 ° crank angle.
The negative valve overlap ensures that sufficiently high amounts of exhaust gas can be returned from the outlet line to the inlet line. Furthermore, losses due to opening the outlet too late - especially when the outlet valves are open for a short time - are avoided.
The invention is explained in more detail below with reference to the figures.
It show schematically
1 shows an internal combustion engine according to the invention in a first variant,
2 shows an internal combustion engine according to the invention in a second embodiment variant,
Figure 3
4 shows the control times of the inlet and outlet valves with positive valve overlap and the control times of the inlet and outlet valves with negative valve overlap.
Parts with the same function are provided with the same reference numerals in the design variants.
1 and 2 each show an internal combustion engine 1 with an inlet branch 2 and an outlet branch 3. Reference numeral 4 denotes a compressor arranged in the inlet branch 2, and reference numeral 5 denotes a turbine of an exhaust gas turbocharger which is arranged in the exhaust branch 3. An exhaust gas recirculation line 6 of a high-pressure exhaust gas recirculation system is arranged between the outlet line and the inlet line 2, which branches off from the exhaust line 3 upstream of the turbine 5 and opens into the inlet line 2 downstream of the compressor 4. In the exhaust gas recirculation line 6, a first exhaust gas recirculation cooler 7, an exhaust gas recirculation valve 8 and - upstream of the exhaust gas recirculation cooler 7 and the exhaust gas recirculation valve 8, a check valve 9 are arranged, which can be designed as a so-called reed valve. The exhaust gas recirculation line 6 opens downstream of the exhaust gas recirculation valve 8 centrally into an exhaust gas distribution line 10, via which cylinder-selective exhaust gas is fed to the inlet channels 11 of the individual cylinders 12. In the exhaust line 3, at least one exhaust gas aftertreatment device 12 is further arranged downstream of the turbine 5. A charge air cooler 13 and a throttle valve 14 are arranged in the inlet branch 2 downstream of the compressor 4.
2/6
AT511 604 B1 2013-01-15 Austrian
Patent office
Both embodiments shown in Fig. 1 and 2 have in common that upstream of the check valve 9, a pre-cooling device 20 is arranged to lower the temperatures of the exhaust gas to values compatible for the check valve 9 without destroying the necessary gas dynamics.
In the embodiment shown in Fig. 1, the pre-cooling device 20 is formed by a cooling line 21 arranged within the cylinder head 15 of the internal combustion engine, through which a pre-cooling of the exhaust gas is achieved.
In the embodiment shown in FIG. 2, the pre-cooling device 20 is formed by a second exhaust gas recirculation cooler 22.
3 and 4 show valve lift-crank angle diagrams, the valve lift h of the exhaust valve and the intake valve being plotted against the crank angle KW. The lift curve of the exhaust valve is denoted by E, and the lift curve of the inlet valve is denoted by I.
3 shows the case of a positive valve overlap with a late-late strategy (late outlet closure - late inlet closure). Residual gas is sucked back into the cylinder by closing the outlet late. The engine can be de-throttled further (Atkinson cycle) by closing the inlet late. The disadvantage of such an operating strategy is that if the outlet is open for a short time, the outlet will open after the lower gate point (180 ° CA). There are losses when pushing out, which can compensate for the advantages of closing the outlet late.
4 shows a negative valve overlap, with which the pressure ratio between the exhaust line and the inlet line can be improved in favor of increased exhaust gas recirculation quantities by opening the outlet early. In addition, residual gas control (internal exhaust gas recirculation) can be achieved, which avoids the late opening of the exhaust and thus the exhaust losses. The negative valve overlap (based on 1 mm valve lift) is 40 ° 120 ° crank angle KW, preferably 60-100 ° crank angle KW. Another advantage is the avoidance of deep valve pockets in the piston crown, which are necessary when the outlet closes late or the inlet opens early.
Both in Fig. 3 and in Fig. 4, the inlet closure of the inlet valves - considered at 1mm valve lift - is later than 590 ° crank angle! KW, the duration of the camshaft opening being relatively short.
4 sheets
Sheet 1 Sheet 2 Sheet 3 Sheet 4
Every citation, both ways
| Document | Relation | Office | Cited during |
|---|---|---|---|
| EP0840000A1 | Cites | European Patent Office (EPO) | Search report |
| DE10018503A1 | Cites | Germany | Search report |
| DE102008050368A1 | Cites | Germany | Search report |
| EP1835155A2 | Cites | European Patent Office (EPO) | Search report |
| JP2007085248A | Cites | Japan | Search report |
| JP2007303355A | Cites | Japan | Search report |
| JP2007332913A | Cites | Japan | Search report |
| WO2009093114A1 | Cites | World Intellectual Property Organization (WIPO) | Search report |
| WO2009105463A2 | Cites | World Intellectual Property Organization (WIPO) | Search report |
| US2009150052A1 | Cites | United States of America | Search report |
| WO2009151080A1 | Cites | World Intellectual Property Organization (WIPO) | Search report |
| GB2473821A | Cites | United Kingdom | Search report |
| US7275514B2 | Cites | United States of America | Search report |
| US7360523B2 | Cites | United States of America | Search report |
| US7367313B2 | Cites | United States of America | Search report |
3 members in 2 offices
Priority claims2
| Document | Office | Kind | Date |
|---|---|---|---|
| 14482011 | Austria | A | |
| AT20110001448 | – | – | – |
Members3
| Document | Office | Kind | |
|---|---|---|---|
| AT511604A4 | Austria | A4 | |
| AT511604B1This record | Austria | B1 | |
| DE102012109270A1 | Germany | A1 |
Numbers
- Publication
- 511604
- Publication, DOCDB
- 511604
- Publication, EPODOC
- AT511604B
- Application
- 1448
- Application, DOCDB
- 14482011
- Application, EPODOC
- AT20110001448
Titles2
- English
- INTERNAL COMBUSTION ENGINE WITH AN INTAKE STRAND
- German
- BRENNKRAFTMASCHINE MIT EINEM EINLASSSTRANG
Classification
- CPC, 6
- F02D13/0265
- F02B29/0406
- F02M26/40
- F02M26/05
- F02M26/24
- Y02T10/12
- IPC, 2
- F02M25 07
- F02D13 02