FR2634519A1 - INTERNAL COMBUSTION ENGINE WITH TURBOCHARGER IN WHICH THE ARRIVAL OF THE FUEL IN CERTAIN CYLINDERS CAN BE CUT - Google Patents
INTERNAL COMBUSTION ENGINE WITH TURBOCHARGER IN WHICH THE ARRIVAL OF THE FUEL IN CERTAIN CYLINDERS CAN BE CUT Download PDFInfo
- Publication number
- FR2634519A1 FR2634519A1 FR8909525A FR8909525A FR2634519A1 FR 2634519 A1 FR2634519 A1 FR 2634519A1 FR 8909525 A FR8909525 A FR 8909525A FR 8909525 A FR8909525 A FR 8909525A FR 2634519 A1 FR2634519 A1 FR 2634519A1
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- FR
- France
- Prior art keywords
- engine
- cylinders
- exhaust
- service
- cut
- 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.)
- Granted
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
- F02D9/04—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits concerning exhaust conduits
-
- 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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/001—Engines characterised by provision of pumps driven at least for part of the time by exhaust using exhaust drives arranged in parallel
- F02B37/002—Engines characterised by provision of pumps driven at least for part of the time by exhaust using exhaust drives arranged in parallel the exhaust supply to one of the exhaust drives can be interrupted
-
- 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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/007—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in parallel, e.g. at least one pump supplying alternatively
-
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/01—Internal exhaust gas recirculation, i.e. wherein the residual exhaust gases are trapped in the cylinder or pushed back from the intake or the exhaust manifold into the combustion chamber without the use of additional passages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/13—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
- F02M26/42—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories having two or more EGR passages; EGR systems specially adapted for engines having two or more cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/52—Systems for actuating EGR valves
- F02M26/59—Systems for actuating EGR valves using positive pressure actuators; Check valves therefor
- F02M26/61—Systems for actuating EGR valves using positive pressure actuators; Check valves therefor in response to exhaust pressure
- F02M26/615—Systems for actuating EGR valves using positive pressure actuators; Check valves therefor in response to exhaust pressure the exhaust back pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/02—EGR systems specially adapted for supercharged engines
- F02M26/08—EGR systems specially adapted for supercharged engines for engines having two or more intake charge compressors or exhaust gas turbines, e.g. a turbocharger combined with an additional compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/02—EGR systems specially adapted for supercharged engines
- F02M26/09—Constructional details, e.g. structural combinations of EGR systems and supercharger systems; Arrangement of the EGR and supercharger systems with respect to the engine
- F02M26/10—Constructional details, e.g. structural combinations of EGR systems and supercharger systems; Arrangement of the EGR and supercharger systems with respect to the engine having means to increase the pressure difference between the exhaust and intake system, e.g. venturis, variable geometry turbines, check valves using pressure pulsations or throttles in the air intake or exhaust system
-
- 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)
- Supercharger (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
Moteur à combustion interne à turbocompresseurs dans lequel l'alimentation en carburant de certains cylindres 12 peut être coupée. Le moteur 10 est suralimenté par plusieurs turbocompresseurs 16, 17, 18 montés en parallèle, dont l'un au moins 16, 17 peut être mis hors service. Les périodes d'admission et d'échappement des cylindres se chevauchent. La tubulure 33 d'admission des gaz des turbocompresseurs 18, qui fonctionnent constamment, contient une dispositif 34 obturateur automatique, composé d'un papillon que le courant de gaz peut ouvrir, contre la force de fermeture d'un ressort, lorsque le moteur fonctionne à plein régime, et qui est percé d'une ouverture, non obturable, calibrée pour que ce papillon ne s'ouvre pas au ralenti ou sous faible charge du moteur. Application notamment aux moteurs à grande puissance pour véhicules.A turbocharged internal combustion engine in which the fuel supply to certain cylinders 12 can be cut off. The engine 10 is supercharged by several turbochargers 16, 17, 18 connected in parallel, at least one of which 16, 17 can be taken out of service. The intake and exhaust periods of the cylinders overlap. The gas intake manifold 33 of the turbochargers 18, which are constantly operating, contains an automatic shut-off device 34, consisting of a butterfly valve which the gas stream can open, against the closing force of a spring, when the engine is running. at full speed, and which has an opening, which cannot be closed, calibrated so that this throttle does not open at idle speed or under low engine load. Application in particular to high power engines for vehicles.
Description
La présente invention se rapporte à un moteur à combus-The present invention relates to a combustion engine
tion interne à pistons suralimenté, dans lequel l'arrivée du carburant dans certains cylindres peut être coupée et qui est éouiDé d'au moins un turbocompresseur actionné par les gaz d'échappement et pouvant #tre mis en service et coupé, ainsi supercharged internal piston arrangement, in which the fuel supply in certain cylinders can be cut off and which is exhausted by at least one exhaust gas turbocharger which can be put into service and cut, and
que d'un turbocompresseur à gaz d'échappement restant constam- that an exhaust gas turbocharger
ment en service pendant que le moteur fonctionne. in service while the engine is running.
Le but d'un agencement de ce genre est de garantir qu'en régime permanent le moteur est surali:enté de manière optimale et la consommation de carburant est minimale. A cet effet, en marche au ralenti et sous charge partielle, seule The purpose of such an arrangement is to ensure that in steady state the engine is optimally engaged and the fuel consumption is minimal. For this purpose, while idling and under partial load, only
quelques cylindres (actifs) fournissent de l'énergie. some (active) cylinders provide energy.
On connait par le brevet DE-C1-3 704 967 un moteur du genre précité, dans lequel les cylindres, coupés de la source Patent DE-C1-3 704 967 discloses a motor of the above kind, in which the cylinders, cut from the source
de carburant, continuent à fonctionner sans délivrer d'énergie. fuel, continue to operate without delivering energy.
Les cycles d'admission et d'échappement de ces cylindres ne sont pas différents de ceux des cylindres actifs, de sorte que même lorsqu'ils scnt isolés, ils sont encore alimentés, mais The intake and exhaust cycles of these cylinders are not different from those of the active cylinders, so that even when they are isolated, they are still powered, but
unioue4ent avec de l'air. Comme JE n'y a pas d'apport de cha- unioue4ent with air. Since I do not have any contribution of
leur par combustion, ces cycles d'admission et d'échappement des cylindres isolés se déroulent à un niveau de température bien inférieur à celui des cylindres actifs. La température moyenne de ces cylindres isolés est donc bien inférieure à By their combustion, these intake and exhaust cycles of the insulated cylinders take place at a much lower temperature level than that of the active cylinders. The average temperature of these insulated cylinders is therefore much lower than
celle des cylindres actifs.that of active cylinders.
Lorsque la charge appliquée augmente et oblige a met- When the applied load increases and forces
tre ern service &es cylindres qui n'étaient pas alimentés en being serviced by cylinders that were not powered
carburant, il se produit, en fonction de la température am- fuel, it occurs, depending on the ambient temperature
biante et de celle du z.oteur, une émission indésirable et inad- and that of the engine, an undesirable and inappropriate
missible de gaz d'échappement.exhaust gas missile.
L'invention a pour but d'empêcher une émission inad- The object of the invention is to prevent an inadmissible
missible de gaz d'échappement quand la charge appliquée au exhaust missible when the load applied to the
moteur atteint une valeur à laquelle des cvylindres non alimen- engine reaches a value at which non-powered cylinders
tés en carburant sont remis en service. fuel are returned to service.
Dans un moteur à combustion interne suralimenté et conforme à l'invention, dans lequel l'arrivée du carburant In a supercharged internal combustion engine according to the invention, in which the fuel supply
dans certains cylindres peut être coupée et avec lequel coopS- in some cylinders can be cut and with which coopS-
rent' plusieurs turbocompresseurs montés en parallèle, dont l'un au moins peut être mis en service et arrêté, chacun des turbocompresseurs pouvant être arrêtés comporte, en amont de l'orifice d'admission des gaz dans sa turbine, un dispositif obturateur réglable, et en amont de l'orifice d'admission d'air de son compresseur, un dispositif obturateur automatique, et a plurality of parallel-connected turbochargers, at least one of which can be put into service and stopped, each of the turbochargers which can be stopped comprises, upstream of the gas inlet orifice in its turbine, an adjustable shutter device, and upstream of the air inlet of its compressor, an automatic shutter device, and
l'un des autres turbocompresseurs comporte un dispositif d'ar- one of the other turbochargers comprises a device for
rêt des gaz d'échappement, qui est formé d'un papillon que le courant des gaz d'échappement peut amener automatiquement en exhaust gas, which is formed of a throttle that the exhaust gas stream can automatically bring into
position d'ouverture contre l'action d'un ressort, et le méca- opening position against the action of a spring, and the mechanism
nisme de distribution du moteur fait se chevaucher les périodes engine timing causes the periods to overlap
d'admission et d'échappement des cylindres. intake and exhaust cylinders.
Dans une forme de réalisation de l'invention, lorsque le papillon d'arrêt des gaz, qui tourne sur un axe, coopère avec un turbocompresseur constamment en service, ce papillon In one embodiment of the invention, when the throttle butterfly, which rotates on an axis, cooperates with a turbocharger constantly in service, this butterfly
peut comporter une ouverture non obturable, calibrée en fonc- may have a non-closable opening, calibrated according to
tion du débit des gaz d'échappement pendant la marche au ralen- exhaust flow during idling.
ti. Cet axe peut avoir une position excentrée par rapport au ti. This axis may have an off-center position with respect to
centre de gravité du papillon.center of gravity of the butterfly.
En marche au ralenti et sous charge partielle faible, lorsque cer- Idling and low partial load, when
tains cylindres et les turbocompresseurs correspondants sont mis hors service, les gaz d'échappement sont refoulés dans la some cylinders and the corresponding turbochargers are put out of service, the exhaust gases are forced back into the
tubulure d'échappement commune à tous les cylindres, car la pa- exhaust pipe common to all cylinders, because the
pillon d'arrêt se ferme automatiquement sous l'action du ressort en raison du faible débit de ces gaz. En coopération avec le Stopper is automatically closed by spring action due to the low flow rate of these gases. In cooperation with
chevauchement des durées d'admission et d'échappement des cy- overlap of the intake and exhaust times of
lindres, ce refoulement provoque un reflux des gaz dans tous lindres, this repression causes a reflux of gases in all
les cylindres, même ceux qui ne sont pas alimentés en carbu- cylinders, even those not fueled
rant. Cela augmente notablement avant tout la température mo- rant. This significantly increases the temperature above all
yenne de ces derniers cylindres non alimentés. Cette augmenta- yenne of these last non-powered cylinders. This increase
tion de la température améliore de la manière voulue le dérou- the temperature improves the desired
lement de l'émission des gaz d'échappement du moteur, quand the emission of engine exhaust, when
celui-ci est soumis à une surcharge. it is overloaded.
Les avantages apportés par l'invention consistent notamment entce que les températures des organes du moteur sont uniformes dans toute la plage de fonctionnement du moteur; qu'il n'y a pas besoin d'équipement Advantages provided by the invention include that the temperatures of the engine components are uniform throughout the operating range of the engine; that there is no need for equipment
spécial pour commander et régler le papillon-obturateur auto- to control and adjust the self-closing butterfly
matique; et qu'il est possible d'équiper ultérieurement et é- matic; and that it is possible to equip later and
conomiquement de cet agencement un moteur existant. economically of this arrangement an existing engine.
Un exemple de réalisation de l'invention va être décrit ci-dessous de manière plus détaillée à titre illustratif et nullement limitatif, en regard du dessin annexé, sur lequel An exemplary embodiment of the invention will be described below in more detail by way of illustration and in no way limiting, with reference to the appended drawing, in which:
la figure 1 représente schématiquement un moteur à com- FIG. 1 schematically represents a motor with
bustion interne comportant deux turbocompresseurs pouvant être mis hors service et un autre turbocompresseur constamment internal combustion with two turbochargers that can be decommissioned and another turbocharger constantly
en service, ainsi que des cylindres dont l'aLimentation en car- in service, as well as cylinders whose car-
burant peut être coupée; etburant can be cut off; and
la figure 2 représente le détail I de la figure 1, mon- FIG. 2 represents the detail I of FIG.
trant le papillon automatique de la tubulure d'admission des the automatic throttle of the intake manifold
gaz d'échappement.exhaust gas.
Un moteur 10 à combustion interne et à pistons comporte deux groupes de cylindres 11 et 12, qu'une tubulure com=une 13 An internal combustion engine 10 with pistons comprises two groups of cylinders 11 and 12, which a tube com = a 13
alimente en air comprimé de suralimentation. Un collecteur d'é- feeds in supercharged compressed air. A collector of
chappement 14 coopère avec ces cylindres 11 et 12. L'air de su- 14 cooperates with these cylinders 11 and 12. The air of su-
ralirentation est fourni au mote-r 10 par trois turbocompresseurs raliration is provided to the mote-r 10 by three turbochargers
16, 17, 1ú à gaz d'échappement,;ontés en parallèle, qui com- 16, 17, 1º with exhaust gas, in parallel, which com-
prennent chacurn une turbine 19, 20, 21 alimentée par les gaz take each one a turbine 19, 20, 21 fed by the gases
d'échanpement et un compresseur 22, 23, 24 d'air de suralizen- and a compressor 22, 23, 24 of overflow air
tation.tation.
Les turbocompresseurs 16 et 17 peuvent être mis en servi- Turbochargers 16 and 17 can be put into service.
ce et hors service par l'intermédiaire de dispositifs 27, 2E this and out of service via devices 27, 2E
réglables d'obturation de gaz, qui sont montés dans les tubulu- adjustable gas shutters, which are mounted in the tubulu-
res 25, 26 respectives d'admission de gaz et de dispositifs 25, 26 respectively for the admission of gases and devices
29, 30 automatiques obturateurs d'air, Cui commandent les tu- 29, 30 automatic air shutters, which control the
_ures 31,,2 d'admission d'air de s.ralimenzation. Lorsuue _ures 31,, 2 air intake airing. Lorsuue
le moteur 10 fonctionne à plein régime et que tous les cylin- the engine 10 is running at full speed and all cylinders
dres 11 et 12 fournissent de l'énergie, les trois turbocompres- 11 and 12 provide energy, the three turbochargers
seurs 16, 17, 18 sont en service. En marche au ralenti et sous faible charge partielle, seul le turbocompresseur 18, qui ne peut pas être coupé, fonctionne en fournissant au moteur 10 de l'air de 16, 17, 18 are in use. In idling and under low partial load, only the turbocharger 18, which can not be shut down, operates by supplying the engine with 10
suralimentation. Les cylindres 12 sont alors isolés de la sour- overeating. The cylinders 12 are then isolated from the source
ce d'alimenrtation en carburant et ils fonctionnent sans délivrer d'énergie. Le mécanisme de distribution, qui commande tous les it's fueling and they work without delivering energy. The distribution mechanism, which controls all
cylindres- 11 et 12 du moteur 10, fait se chevaucher les pério- cylinders 11 and 12 of the engine 10 overlap the
des d'admission et d1échappement de ces cylindres. intake and exhaust of these cylinders.
Un dispositif 34 obturateur de gaz d'échappement est monté dans la tubulure 33 d'alimentation en gaz d'échappement de la turbine 21 du turbocompresseur 18 qui ne peut être mis hors service. Ce dispositif 34 est composé d'un papillon 35, solidaire en rotation d'un axe 39, et d'un levier 37, qui est aussi solidaire en rotation de cet axe 39 et auquel est fixé un ressort 38 maintenant ce papillon 35 en position de fermeture. L'axe 39 est excentré par rapport au centre de gravité de la surface du papillon 35. Par conséquent, un courant de gaz d'échappement venant frapper ce papillon 35 fermé crée un couple de rota-., An exhaust gas shutoff device 34 is mounted in the exhaust gas feed pipe 33 of the turbine 21 of the turbocharger 18 which can not be taken out of service. This device 34 is composed of a throttle 35, integral in rotation with an axis 39, and a lever 37, which is also integral in rotation with this axis 39 and to which is fixed a spring 38 holding this throttle 35 in position closure. The axis 39 is eccentric with respect to the center of gravity of the surface of the throttle valve 35. Consequently, an exhaust gas stream impinging on this closed throttle 35 creates a rotational torque.
tion oui agit dans le sens de l'ouverture. Le Papillon 35 s'ou- yes it works in the sense of openness. The Butterfly 35 is
vre automaticuement lorsque la valeur de ce couple est supérieu- automatically when the value of this couple is higher than
re à celle de la force de fermeture exercée par le ressort 38. re to that of the closing force exerted by the spring 38.
Une ouverture 36 non obturable est formée dans le papillon 35. A non-closable opening 36 is formed in the butterfly 35.
La force du ressort 38 et les dimensions de cette ouverture 36 sont déterminées de façon que le papillon reste fermé contre The force of the spring 38 and the dimensions of this opening 36 are determined so that the butterfly remains closed against
aci d es gaz d'écnaprement produits par le moteur 10 pen- gas emissions from the engine 10
dant au'il fonctionne au ralenti ou sous faible charge partielle. Ces gaz refluent donc dans le collecteur 14 d'échappement, en amont du disposit_if obturateur 34. En coopération avec le chevauchement while idling or under light load. These gases flow back into the exhaust manifold 14, upstream of the shutter device 34. In cooperation with the overlap
des péorodes d'admission et d'échappement des cylindres, ce re- the cylinder inlet and outlet peorodes, this
flux fait revenir les gaz dans des cylindres 11 et 12, ce qui augmente sensiblement la température moyenne des cylindres 12 non alimentés en carburant, si bien qu'au moment d'une nouvelle surcharge provoquant la mise en service de tous les cylindres flow returns the gases in cylinders 11 and 12, which substantially increases the average temperature of the cylinders 12 not supplied with fuel, so that at the time of a new overload causing the commissioning of all the cylinders
11 et 12, le moteur 10 fonctionne sans dégager une quantité inad- 11 and 12, the engine 10 operates without releasing an inappropriate amount.
missible de gaz d'échappement.exhaust gas missile.
Il va de soi qu'il est possible sans s'écarter du domai- It goes without saying that it is possible without departing from
ne de l'invention,d'apporter diverses modifications au moteur of the invention, to make various modifications to the engine
à turbocompresseur à grande puissance pour véhicules, représen- turbocharger with high power for vehicles,
té et décrit.described and described.
Claims (3)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3824406A DE3824406C1 (en) | 1988-07-19 | 1988-07-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2634519A1 true FR2634519A1 (en) | 1990-01-26 |
FR2634519B1 FR2634519B1 (en) | 1991-08-16 |
Family
ID=6358986
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR898909525A Expired - Lifetime FR2634519B1 (en) | 1988-07-19 | 1989-07-13 | INTERNAL COMBUSTION ENGINE WITH TURBOCHARGERS IN WHICH THE FUEL INTAKE IN CERTAIN CYLINDERS CAN BE CUT |
Country Status (5)
Country | Link |
---|---|
JP (1) | JPH0242125A (en) |
DE (1) | DE3824406C1 (en) |
FR (1) | FR2634519B1 (en) |
GB (1) | GB2220987B (en) |
IT (1) | IT1230216B (en) |
Families Citing this family (10)
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DE19816840C2 (en) * | 1998-04-16 | 2003-02-27 | Mtu Friedrichshafen Gmbh | Internal combustion engine with several exhaust gas turbochargers that can be optionally switched on and off |
DE19823014C2 (en) * | 1998-05-22 | 2003-11-13 | Udo Mailaender Gmbh | Method of charging an internal combustion engine |
DE19831251C2 (en) * | 1998-07-11 | 2000-04-27 | Daimler Chrysler Ag | Rechargeable internal combustion engine with cylinder deactivation |
US6715289B2 (en) * | 2002-04-08 | 2004-04-06 | General Motors Corporation | Turbo-on-demand engine with cylinder deactivation |
DE102004035323A1 (en) | 2004-07-21 | 2006-02-16 | Bayerische Motoren Werke Ag | Sequential loader control with cylinder deactivation |
GB0510160D0 (en) * | 2005-05-18 | 2005-06-22 | Leavesley Malcolm G | Twin turbocharger apparatus |
GB2430708B (en) * | 2005-10-03 | 2010-09-22 | Ford Global Tech Llc | Turbo charging in a variable displacement engine |
EP2006506A1 (en) * | 2007-06-22 | 2008-12-24 | ABB Turbo Systems AG | Charging system for a combustion engine |
CN102767420A (en) * | 2012-07-16 | 2012-11-07 | 上海交通大学 | Partitioning device for connecting pipes |
US10746089B2 (en) | 2018-01-25 | 2020-08-18 | Caterpillar Inc. | Inline turbocharger arrangement and method |
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US4249382A (en) * | 1978-05-22 | 1981-02-10 | Caterpillar Tractor Co. | Exhaust gas recirculation system for turbo charged engines |
JPS59231134A (en) * | 1983-06-13 | 1984-12-25 | Mazda Motor Corp | Engine with turbocharger |
DE3631284C1 (en) * | 1986-09-13 | 1987-04-16 | Mtu Friedrichshafen Gmbh | Multi-cylinder diesel internal combustion engine with a low compression ratio in the cylinders |
DE3704967C1 (en) * | 1987-02-17 | 1988-05-11 | Mtu Friedrichshafen Gmbh | Supercharged multi-cylinder reciprocating internal combustion engine with several exhaust gas turbochargers working in parallel |
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---|---|---|---|---|
DE3030265C2 (en) * | 1980-08-09 | 1984-02-16 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Internal combustion engine |
JPS598646A (en) * | 1982-07-07 | 1984-01-17 | Nippon Telegr & Teleph Corp <Ntt> | Coating of optical fiber |
JPS6055747A (en) * | 1983-09-07 | 1985-04-01 | Nippon Telegr & Teleph Corp <Ntt> | Acquisition device |
-
1988
- 1988-07-19 DE DE3824406A patent/DE3824406C1/de not_active Expired
-
1989
- 1989-05-26 IT IT8920663A patent/IT1230216B/en active
- 1989-06-08 JP JP1144300A patent/JPH0242125A/en active Pending
- 1989-07-13 FR FR898909525A patent/FR2634519B1/en not_active Expired - Lifetime
- 1989-07-19 GB GB8916463A patent/GB2220987B/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4249382A (en) * | 1978-05-22 | 1981-02-10 | Caterpillar Tractor Co. | Exhaust gas recirculation system for turbo charged engines |
JPS59231134A (en) * | 1983-06-13 | 1984-12-25 | Mazda Motor Corp | Engine with turbocharger |
DE3631284C1 (en) * | 1986-09-13 | 1987-04-16 | Mtu Friedrichshafen Gmbh | Multi-cylinder diesel internal combustion engine with a low compression ratio in the cylinders |
DE3704967C1 (en) * | 1987-02-17 | 1988-05-11 | Mtu Friedrichshafen Gmbh | Supercharged multi-cylinder reciprocating internal combustion engine with several exhaust gas turbochargers working in parallel |
Non-Patent Citations (1)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 9, no. 111 (M-379)(1834) 15 mai 1985, & JP-A-59 231134 (MAZDA) 25 décembre 1984, * |
Also Published As
Publication number | Publication date |
---|---|
GB2220987B (en) | 1992-04-15 |
IT1230216B (en) | 1991-10-18 |
DE3824406C1 (en) | 1989-05-24 |
JPH0242125A (en) | 1990-02-13 |
GB8916463D0 (en) | 1989-09-06 |
IT8920663A0 (en) | 1989-05-26 |
GB2220987A (en) | 1990-01-24 |
FR2634519B1 (en) | 1991-08-16 |
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