DE8521358U1 - Piston for a diesel internal combustion engine - Google Patents
Piston for a diesel internal combustion engineInfo
- Publication number
- DE8521358U1 DE8521358U1 DE8521358U DE8521358U DE8521358U1 DE 8521358 U1 DE8521358 U1 DE 8521358U1 DE 8521358 U DE8521358 U DE 8521358U DE 8521358 U DE8521358 U DE 8521358U DE 8521358 U1 DE8521358 U1 DE 8521358U1
- Authority
- DE
- Germany
- Prior art keywords
- piston
- internal combustion
- swirl
- combustion engine
- diesel internal
- 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 description 9
- 238000002347 injection Methods 0.000 claims description 3
- 239000007924 injection Substances 0.000 claims description 3
- 244000309464 bull Species 0.000 claims description 2
- 239000003795 chemical substances by application Substances 0.000 claims 1
- 230000015572 biosynthetic process Effects 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Classifications
-
- 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
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0636—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space having a substantially flat and horizontal bottom
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F3/00—Pistons
- F02F3/28—Other pistons with specially-shaped head
-
- 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
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
-
- 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
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
- F02B23/0624—Swirl flow
-
- 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
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
- F02B23/063—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion the combustion space in the piston interacting fluid dynamically with the cylinder head, the injector body or the cylinder wall
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
• t · · · · &eegr; m• t · · · · η m
4111 I ■· · ·· t f *4111 I ■· · ·· t f *
Kolben für eine Diesel-BrennkraftroaschinePiston for a diesel engine
Die Erfindung besieht sich auf einen Kolben für eine Diesel-Brennkraftmaschine mit Direkteinspritzung und einem drallerzeugenden Einlaßkanal, wobei im Kolbenboden eine Kolbenmulde und Ventiltasehen für Einlaß- und Auslaßventile vorgesehen sind.The invention relates to a piston for a diesel internal combustion engine with direct injection and a swirl-generating intake port, wherein a piston recess and valve pockets for intake and exhaust valves are provided in the piston crown.
Es ist bekannt, daß bei derartigen Diesel-Brennkraftmaschinen mit Direkteinspritzung die Gemischbildung im Zylinder bedeutend verbessert werden kann, wenn die Verbrennungsluft mit einem Drall in den Zylinder eintritt, sodaß ein Luftwirbel um die Zylinderlängsachse erzeugt wird. Am Ende des Verdichtungshubes entsteht außerdem TO eine radial zur Kolbenmulde hin gerichtete Quetschströiiurg.It is known that in such diesel internal combustion engines with direct injection, the mixture formation in the cylinder can be significantly improved if the combustion air enters the cylinder with a swirl, so that an air vortex is generated around the cylinder's longitudinal axis. At the end of the compression stroke, a squish flow is also created that is directed radially towards the piston recess.
Für eine zufriedenstellende Gemischbildung ist bei niedrigen Drehzahlen ein stärkerer Drall erforderlich als bei hohen Drehzahlen, und der Einlaßkanal muß so ausgebildet sein, daß der benötigte starke Drall bei niedrigen Drehzahlen erzeugt wird. Da die Drosselwirkung des Einlaßkanals obo größer ist, je stärker der Drall ist, entstehen mit einem für den Drall bei niedrigen Drehzahlen optimierten Einlaßkanal verhältnismäßig große Drosselverluste bei hohen Dreh zahlen, wodurch die Leistung und der Wirkungsgrad der Brennkraftmaschine bei hohen Drehzahlen verringert wird. Es sind bereits M^ßnahmen bekannt, um den Drall in Abhängigkeit von der Drehzahl zu verändern,sodaß der Einlaßkanal für hohe Drehzahlen optimiert wird und der Drall für niedrige Drehzahlen durch Klappen &ogr;&aacgr;&kgr;&tgr; sonstige Mittel auf das zur Gemischbildung bei diesen Drehzahlen erforderliche Maß erhöht wird. Diese Maßnahmen sind jedoch aufwendig und haben sich in der Praxis nicht durchsetzen können.For satisfactory mixture formation, a stronger swirl is required at low speeds than at high speeds, and the intake port must be designed in such a way that the required strong swirl is generated at low speeds. Since the throttling effect of the intake port is greater the stronger the swirl, an intake port optimized for swirl at low speeds results in relatively large throttling losses at high speeds, which reduces the performance and efficiency of the internal combustion engine at high speeds. Measures are already known to change the swirl depending on the speed, so that the intake port is optimized for high speeds and the swirl for low speeds is increased by flaps or other means to the level required for mixture formation at these speeds. However, these measures are complex and have not been able to prevail in practice.
Der Erfindung liegt die Aufgabe zugrunde, eine Diesel-Brennkraftmaschine der eingangs genanntan Art zu schaffen, bei der ohne Klappen oder sonstige bewegliche Steuerelemente ein starker Drall bei niedrigen Drehzahlen erreicht wird, die Drosselwirkung des drallerzeugenden Einlaßkanals bei hohen Drehze-hlen jedoch beträchtlich vermindert wird. The invention is based on the object of creating a diesel internal combustion engine of the type mentioned at the beginning, in which a strong swirl is achieved at low speeds without flaps or other movable control elements, but the throttling effect of the swirl-generating inlet channel is considerably reduced at high speeds.
' Il Mtl' The Mtl
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Diese Aufgabe wird erfindungsgemäß dadurch gelöst, daß der Rand der Ventiltaschen Im Kolbenboden abgerundet und/oder abgeschrägt ist.This object is achieved according to the invention in that the edge of the valve pockets in the piston crown is rounded and/or bevelled.
Überraschenderweise hat sich herausgestellt, daß durch den Rand der Ventiltaschen, der bisher scharfkantig ausgeführt wurde, wobei die ümfangswand der Ventiltaschen im rechten Winkel zum Kolbenboden steht, der Drall der einströmenden Brennluft sehr stark abgebremst wird. Daher mußte der Einlaßkanal so ausgeführt werden, daß bei niedrigen Drehzahlen ein sehr starker Drall entsteht, der trotz der erwähnten Ab-Surprisingly, it has been found that the edge of the valve pockets, which has previously been sharp-edged, with the peripheral wall of the valve pockets at a right angle to the piston crown, greatly slows down the swirl of the incoming combustion air. Therefore, the intake port had to be designed in such a way that at low speeds a very strong swirl is created, which despite the mentioned
iö bremsung stark genüg 1st, -csn eine zufriedenstellende Gemischbildung zu ermöglichen, der jedoch andererseits zu beträchtlichen Leistungsverlusten bei hohen Drehzahlen führte. iö braking strongly enough to enable satisfactory mixture formation, but on the other hand led to considerable power losses at high speeds.
Durch den erf indungsgemäßen Vorschlag wird der Drall wesentlich weniger abgebremst, sodaß der Einlaßkanal so ausgelegt werden kann, daß er einen geringeren Drall bei niedrigen Drehzahlen erzeugt, wodurch die Drosselwirkung bei hohen Drehzahlen verringert und die Leistung und der Wirkungsgrad entsprechend erhöht werden.The proposal according to the invention slows down the swirl considerably less, so that the intake port can be designed to produce less swirl at low speeds, thereby reducing the throttling effect at high speeds and increasing the power and efficiency accordingly.
Ein Ausfünrungsbeispiel der Erfindung wird im folgenden unter Bezugnahme auf die Zeichnungen beschrieben. Es zeigt:An embodiment of the invention is described below with reference to the drawings. It shows:
Fig. 1 eine Draufsicht des Kolbenbodensy
Fig. 2 einen Schnitt entlang Linie 2 - 2 in Figur *\t und
Fig. 3 einen Schnitt entlang Linie 3 - 3 in Fig. 1 in größerem Maßstab.Fig. 1 a top view of the piston crown y
Fig. 2 is a section along line 2 - 2 in Figure *\ t and Fig. 3 is a section along line 3 - 3 in Fig. 1 on a larger scale.
Der in den Zeichnungen dargestellte Kolben 1 weist in seinem Kolbenboden 2 eine Kolbenmulde 3 sowie Ventiltaschen 4 und 5 auf, in welche die Ventilteller der zugehörigen Ventile in der oberen Totpunktlage des Kolbens 1 hineinragen, wie dies in Figur 3 für das Einlaßventil 6 gestrichelt eingezeichnet ist.The piston 1 shown in the drawings has in its piston crown 2 a piston recess 3 as well as valve pockets 4 and 5 into which the valve plates of the associated valves protrude in the top dead center position of the piston 1, as shown in dashed lines in Figure 3 for the inlet valve 6.
Bisher wurde der Rand der Ventiltaschen scharfkantig ausgeführt, wie dies in Fig. 3 bei 7 gestrichelt angedeutet ist. Dadurch wird der in einem Drall um die Kolbenmittelachse umlaufende Luftstrom, der in Fig. 1 durch die Pfeile 8 veranschaulicht ist, abgebremst, da diese Kante auf der Eintrittsseite des Luftstrcroes in die Ventiltaschen als Abrißkante, die Wirbel erzeugt, und die Kante auf der Austrittsseite als Staufläche wirkt.Previously, the edge of the valve pockets was designed with sharp edges, as indicated by the dashed line at 7 in Fig. 3. This slows down the air flow circulating in a swirl around the piston center axis, which is illustrated by the arrows 8 in Fig. 1, since this edge on the inlet side of the air flow into the valve pockets acts as a separation edge that creates vortices, and the edge on the outlet side acts as a stagnation surface.
üir. diese Abbremsung der Drallbewegung des Luftstromes zu vermeiden oder zumindest zu verringern, ist erfindungsgemäß der Rand 9 der Ventiltaschen 4,5 abgeschrägt, wie dies deutlich aus Fig. 2 und 3 ersichtlich ist. Dadurch wird erreicht, daß der Luftstrom ohne wesentliche Behinderung durch die Ventil taschen strömen kann, wie dies durch die Pfeile 10 in Fig. 3 veranschaulicht ist. Es hat sich gezeigt, daß mit dieser einfachen Maßnahme der Mitteldruck bei niedrigen Drehzahlen beträchtlich erhöht werden kann, sodaß ein Drallkanal mit geringerem Drall und entsprechend geringerer Drosselung bei hohen Drehzahlen verwendet werden kann. Der WinkelGt zwischen der schrägen ümfangswanä 9 und der Senkrechten sollte mindestens 30° betragen. Der Rand 9 braucht nicht von einer geraden Fläche gebildet werden, sondern er kann auch abgerundet sein.In order to avoid or at least reduce this slowing down of the swirling movement of the air flow, the edge 9 of the valve pockets 4, 5 is bevelled according to the invention, as can be clearly seen in Fig. 2 and 3. This ensures that the air flow can flow through the valve pockets without significant obstruction, as is illustrated by the arrows 10 in Fig. 3. It has been shown that with this simple measure the mean pressure can be increased considerably at low speeds, so that a swirl channel with less swirl and correspondingly less throttling can be used at high speeds. The angle Gt between the bevelled peripheral wall 9 and the vertical should be at least 30°. The edge 9 does not have to be formed by a straight surface, but can also be rounded.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE8521358U DE8521358U1 (en) | 1985-07-24 | 1985-07-24 | Piston for a diesel internal combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE8521358U DE8521358U1 (en) | 1985-07-24 | 1985-07-24 | Piston for a diesel internal combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE8521358U1 true DE8521358U1 (en) | 1987-02-12 |
Family
ID=6783481
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8521358U Expired DE8521358U1 (en) | 1985-07-24 | 1985-07-24 | Piston for a diesel internal combustion engine |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE8521358U1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10150721B4 (en) * | 2001-10-13 | 2012-02-09 | Daimler Ag | Diesel engine |
US10233865B2 (en) | 2016-09-30 | 2019-03-19 | Mahle International Gmbh | Piston crown having conical valve pocket |
GB2580905A (en) * | 2019-01-25 | 2020-08-05 | Jaguar Land Rover Ltd | Piston for an internal combustion engine |
-
1985
- 1985-07-24 DE DE8521358U patent/DE8521358U1/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10150721B4 (en) * | 2001-10-13 | 2012-02-09 | Daimler Ag | Diesel engine |
US10233865B2 (en) | 2016-09-30 | 2019-03-19 | Mahle International Gmbh | Piston crown having conical valve pocket |
GB2580905A (en) * | 2019-01-25 | 2020-08-05 | Jaguar Land Rover Ltd | Piston for an internal combustion engine |
GB2580905B (en) * | 2019-01-25 | 2021-08-11 | Jaguar Land Rover Ltd | Piston for an internal combustion engine |
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