EP0095789A1 - Procédé et installation pour la commande de la recirculation des gaz d'échappement dans un compresseur à ondes de pression pour un moteur à combustion interne - Google Patents

Procédé et installation pour la commande de la recirculation des gaz d'échappement dans un compresseur à ondes de pression pour un moteur à combustion interne Download PDF

Info

Publication number
EP0095789A1
EP0095789A1 EP83200493A EP83200493A EP0095789A1 EP 0095789 A1 EP0095789 A1 EP 0095789A1 EP 83200493 A EP83200493 A EP 83200493A EP 83200493 A EP83200493 A EP 83200493A EP 0095789 A1 EP0095789 A1 EP 0095789A1
Authority
EP
European Patent Office
Prior art keywords
pressure
pressure wave
intake air
recirculation
exhaust gas
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
Application number
EP83200493A
Other languages
German (de)
English (en)
Other versions
EP0095789B1 (fr
Inventor
Andreas Mayer
Ibrahim El-Nashar
Fritz Spinnler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BBC Brown Boveri AG Switzerland
Original Assignee
BBC Brown Boveri AG Switzerland
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by BBC Brown Boveri AG Switzerland filed Critical BBC Brown Boveri AG Switzerland
Priority to AT83200493T priority Critical patent/ATE16626T1/de
Publication of EP0095789A1 publication Critical patent/EP0095789A1/fr
Application granted granted Critical
Publication of EP0095789B1 publication Critical patent/EP0095789B1/fr
Expired legal-status Critical Current

Links

Images

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
    • F02B33/00—Engines characterised by provision of pumps for charging or scavenging
    • F02B33/32—Engines with pumps other than of reciprocating-piston type
    • F02B33/42—Engines with pumps other than of reciprocating-piston type with driven apparatus for immediate conversion of combustion gas pressure into pressure of fresh charge, e.g. with cell-type pressure exchangers
    • 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
    • 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
    • F02M26/40—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories with timing means in the recirculation passage, e.g. cyclically operating valves or regenerators; with arrangements involving pressure pulsations

Definitions

  • the present invention relates to a method and a device for controlling the recirculation of exhaust gas in a pressure wave charger for an internal combustion engine according to the preamble of claims 1 and 5.
  • a primary, ie, recirculation of exhaust gas into the compressed charge air which functions without additional devices
  • the mixing of air and exhaust gas at the separating front of the two media in the pressure wave charger can be achieved in a certain speed and load range of the engine, for example in the center of gravity of a driving cycle, by arranging the control edges, in which the relaxed exhaust gas is not completely flushed out in the low-pressure part .
  • the portion of the exhaust gas that is not flushed out is compressed in the high-pressure section together with the fresh air and enters the engine with it.
  • This primary recirculation control via the control edge geometry worsens the effectiveness of the high-pressure side and also the idling properties. Since this recirculation control is carried out via the low-pressure flushing, it is also influenced by the low-pressure resistors, which can change over the course of time, particularly due to filter contamination.
  • this solution has the disadvantage that the difference between charge air pressure and high pressure exhaust gas and also the boost pressure are reduced due to the removal of high pressure exhaust gas. But it works in this way a better adaptation of the degree of recirculation to the respective operating state of the engine than by primary exhaust gas recirculation alone.
  • FIG. 1 shows part of the developed central section through the rotor space and the adjacent channels in the air or gas housing of a pressure wave charger for a diesel engine.
  • the rotor space is designated 1
  • the gas housing 2 and the air housing 3 each have one of the two high and low pressure exhaust gas channels, namely 4 and 5 ? and high and low pressure air channels 6 and 7 shown.
  • the arrow 8 indicates the direction of rotation of the rotor, the arrows 9, 10, 11 and 12 the flow directions of the high-pressure exhaust gas coming from the engine, the compressed high-pressure air pushed out of the rotor, ie the charge air, of the low-pressure exhaust gas emitting from the rotor or the low-pressure air flowing into the rotor, ie the intake air.
  • This degree of recirculation can be influenced by arranging baffles 13 or 14 either in the low-pressure air duct 7 or in the low-pressure exhaust gas duct 5 or in both ducts.
  • baffles 13 or 14 either in the low-pressure air duct 7 or in the low-pressure exhaust gas duct 5 or in both ducts.
  • both an intake damper 13 in the low-pressure air duct 7 and an exhaust damper 14 in the low-pressure exhaust gas duct 5 are provided.
  • the axes of rotation 15, 16 'of these baffles lie in the middle of the baffles or the cross sections of the channels.
  • Other flap arrangements or types of throttles, such as rotary slide valves or the like, are of course also possible, but they should deteriorate the intake resistance or the exhaust resistance as little as possible compared to the resistance of the free channels when the opening is fully open.
  • baffles which, as mentioned, can be provided in one or in both channels, is explained with reference to FIG. 2, in which two rotor cells 17 are entered in the rotor space, the illustration of which has been omitted in FIG. 1.
  • the baffles 13, 14 are omitted in FIG. 2.
  • the dashed line 18 represents the course of the separating front, as it forms from the high-pressure area between the high-pressure exhaust gas duct 4 and the high-pressure air duct 6 when there is no recirculation of exhaust gas.
  • the separating front 18 then remains in the high pressure area and in its further course up to the entry into the area of the low-pressure channels 5 and 7 always within the rotor space 1.
  • no exhaust gas can enter channel 6, ie in the charge air, enter.
  • the separating front 21 between the intake air and the exhaust gas to be returned remains until it enters the The next high pressure area is obtained approximately as in the upper part of FIG. 2 and is then pushed against and into the high pressure air duct by the front of the high pressure exhaust gases. Since a pressure wave machine generally has two high and two low pressure parts, the separating front 21 entered in the lower part of FIG. 2 does not come from the low pressure part 5 + 7 in the upper part of FIG. 2, but from the second, not shown, low pressure part, while the upper part Separating front 21 merges into the second high pressure part, not shown.
  • FIG. 3 A block diagram of a pressure wave charger with controllable recirculation is shown in FIG. 3.
  • 22 designate an intake air filter, 23 an intake silencer, 24 the pressure wave charger, 25 an exhaust silencer, 26 the intake line, 27 the exhaust line, 28 the high-pressure exhaust line, 29 the charge air line, 30 an intake port upstream of the air filter 22, in which the intake air side damper 31 is provided .
  • this could also be arranged immediately before the junction of the low-pressure air duct in the rotor space, but also at any other point between the filter and the inlet of the intake air that is more convenient for installation, maintenance or actuation linkage the rotor space.
  • a compensation element such as a pressure cell, can be provided in the actuating linkage for the storage flap.
  • the control for the baffle flap will preferably be designed so that the flap is fully open when idling and in the upper load range and from a certain speed. Only a primary recirculation is effective in these areas.
  • FIG. 4 shows an ideal recirculation map, wherein in the hatched area, the so-called "recirculation island" 32, the swivel angle ⁇ , see FIG. 6, the baffle flap can be constant or can be controlled in order to obtain the desired course of the degree of recirculation.
  • the mussel curve 33 applies to constant recirculation.
  • FIG. 7 schematically shows a device for controlling the flap position in a diesel engine as a function of the accelerator pedal position to compensate for a change in the intake resistance depending on the degree of contamination of the air filter and the speed.
  • the intake air line 34 is flowed through in the direction indicated by the two flow arrows 35, i.e. the damper 36 lies in front of the air filter 37.
  • the stowage flap 36 is actuated in the desired load or speed-dependent manner by the gas linkage 38, 39 via a resilient element installed between the rods 40, 41 in the form of a pressure can 42 shown in the secondary figure. In the main figure, this pressure can 42 is shown schematically as a spring.
  • the double arrow 44 indicates this relationship.
  • the adjustment of the flap 36 as would occur with a rigid connection of the gas linkage to the flap, is overlaid by the pressure cell 42, a correction movement which compensates for a change in the intake resistance as a result of filter contamination and / or a change in speed.
  • the housing of the pressure cell 42 is connected to the rod 40 and its spring-loaded membrane 43, which is pressurized on both sides, is rigidly connected to the rod 41.
  • the static pressures PvK and p nK in the intake air line upstream or downstream of the flap 36 can be used to apply the membrane 43.
  • a different pressure difference preferably in the suction area of the pressure wave charger, could also prove useful for this.
  • the compensation of a change in the intake resistance can also be achieved by a pressure cell 45, in which the pressure difference between the ambient air and the intake air line 49 after the air filter 46 is used to compensate for the change in the intake resistance, for which purpose a pressure decrease line 50 between the spring-loaded Top of the pressure cell 45 and the intake air line 49 is provided behind the filter.
  • a stop that limits the flap swivel angle so that the intake air line can never be completely closed.
  • a stop will preferably be provided as close as possible to the valve axis.
  • Another advantageous measure for this purpose is to connect the flap to the snifting valve, through which the engine can suck the combustion air directly from the atmosphere during the start-up period, in such a way that the latter is opened when the flap is closed.
  • Another option is to use a return spring that swings the flap back to the fully open position in the event of an accident.
  • Simpler measures consist of using the flap To provide holes or to measure them only so large that they still keep part of the cross-section of the intake air line free at the largest possible swivel angle.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Exhaust-Gas Circulating Devices (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
EP83200493A 1982-06-02 1983-04-07 Procédé et installation pour la commande de la recirculation des gaz d'échappement dans un compresseur à ondes de pression pour un moteur à combustion interne Expired EP0095789B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT83200493T ATE16626T1 (de) 1982-06-02 1983-04-07 Verfahren und einrichtung zur steuerung der rezirkulation von abgas in einem druckwellenlader fuer einen verbrennungsmotor.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH337182 1982-06-02
CH3371/82 1982-06-02

Publications (2)

Publication Number Publication Date
EP0095789A1 true EP0095789A1 (fr) 1983-12-07
EP0095789B1 EP0095789B1 (fr) 1985-11-21

Family

ID=4254514

Family Applications (1)

Application Number Title Priority Date Filing Date
EP83200493A Expired EP0095789B1 (fr) 1982-06-02 1983-04-07 Procédé et installation pour la commande de la recirculation des gaz d'échappement dans un compresseur à ondes de pression pour un moteur à combustion interne

Country Status (5)

Country Link
US (1) US4517950A (fr)
EP (1) EP0095789B1 (fr)
JP (1) JPS58222964A (fr)
AT (1) ATE16626T1 (fr)
DE (1) DE3361269D1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH668292A5 (en) * 1985-12-02 1988-12-15 Bbc Brown Boveri & Cie Throttle flap for pressure pulse charge engine - has controlled leak-rate at zero setting to prevent engine overheating
CH681738A5 (fr) * 1989-11-16 1993-05-14 Comprex Ag
DE102009029880A1 (de) * 2009-06-22 2010-12-23 Continental Automotive Gmbh Turbolader und Verfahren zur Montage einer Regeleinrichtung eines Turboladers

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0152870A3 (fr) * 1984-02-21 1985-10-09 Comprex Ag Procédé de régénération de filtre d'échappement pour moteurs à combustion
US5839416A (en) * 1996-11-12 1998-11-24 Caterpillar Inc. Control system for pressure wave supercharger to optimize emissions and performance of an internal combustion engine
ES2210485T3 (es) * 1997-08-29 2004-07-01 Swissauto Engineering S.A. Maquina de onda de compresion dinamica de gas.
FR2886673A1 (fr) 2005-06-01 2006-12-08 Renault Sas Systeme et procede d'alimentation d'un moteur
DE102006020522A1 (de) 2006-05-03 2007-11-08 Robert Bosch Gmbh Verfahren zum Betreiben einer Brennkraftmaschine
FR2907505B1 (fr) * 2006-10-23 2008-12-26 Renault Sas Procede d'evaluation du debit de gaz fourni a un moteur par un compresseur, et groupe motopropulseur exploitant ce procede
JP4301295B2 (ja) * 2007-01-18 2009-07-22 トヨタ自動車株式会社 内燃機関のｅｇｒシステム
DE102010054505B4 (de) * 2010-12-14 2014-06-12 Benteler Automobiltechnik Gmbh Druckwellenladeranordnung und Verfahren zum Betreiben einer Druckwellenladeranordnung
DE112013001942T5 (de) * 2012-05-03 2014-12-24 Borgwarner Inc. Abgasturbolader

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2215092A5 (fr) * 1972-11-29 1974-08-19 Bbc Brown Boveri & Cie

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2853987A (en) * 1957-09-19 1958-09-30 Ite Circuit Breaker Ltd Diesel engine supercharged by the aerodynamic wave machine
ATE19676T1 (de) * 1981-08-11 1986-05-15 Bbc Brown Boveri & Cie Aufgeladene brennkraftmaschine mit abgaspartikelfilter.

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2215092A5 (fr) * 1972-11-29 1974-08-19 Bbc Brown Boveri & Cie

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH668292A5 (en) * 1985-12-02 1988-12-15 Bbc Brown Boveri & Cie Throttle flap for pressure pulse charge engine - has controlled leak-rate at zero setting to prevent engine overheating
CH681738A5 (fr) * 1989-11-16 1993-05-14 Comprex Ag
DE102009029880A1 (de) * 2009-06-22 2010-12-23 Continental Automotive Gmbh Turbolader und Verfahren zur Montage einer Regeleinrichtung eines Turboladers

Also Published As

Publication number Publication date
EP0095789B1 (fr) 1985-11-21
DE3361269D1 (en) 1986-01-02
JPS58222964A (ja) 1983-12-24
US4517950A (en) 1985-05-21
ATE16626T1 (de) 1985-12-15

Similar Documents

Publication Publication Date Title
EP1274928B1 (fr) Dispositif turbocompresseur pour un moteur a combustion interne
EP2097620B1 (fr) Ventilation de carter de vilebrequin
DE60024776T2 (de) Turbolader und abgasrückführungssystem
DE69815882T2 (de) Anlage einer brennkraftmaschine
DE102006054117B4 (de) Im Teil- und Volllastbetrieb gesteuerte Kurbelgehäuse-Belüftung einer Brennkraftmaschine
DE2534295A1 (de) Maschinenanlage
DE10048237A1 (de) Abgasturbolader, aufgeladene Brennkraftmaschine und Verfahren hierzu
DE2911727A1 (de) Kolben-brennkraftmaschine mit mindestens zwei abgasturboladern
WO2001044650A1 (fr) Dispositif de recirculation de gaz d'echappement
DE3212910C2 (fr)
DE2823067A1 (de) Entlastungssteuerung fuer einen turbolader
EP0095789B1 (fr) Procédé et installation pour la commande de la recirculation des gaz d'échappement dans un compresseur à ondes de pression pour un moteur à combustion interne
DE102004044895A1 (de) Abgasrückführeinrichtung und Verfahren zum Betreiben der Abgasrückführeinrichtung
DE2926373A1 (de) Auspuff-umgehungsventilanordnung
WO2006119866A1 (fr) Moteur thermique a compresseur et recyclage des gaz d'echappement
DE69612420T2 (de) Turboaufgeladene Dieselbrennkraftmaschine
DE10357925A1 (de) Brennkraftmaschine mit Abgasturbolader und Abgasrückführung
DE10258022A1 (de) Brennkraftmaschine mit einem Abgasturbolader
DE19622891A1 (de) Abgasrückführungssystem
WO2006111280A1 (fr) Moteur thermique a recyclage des gaz d'echappement
DE19709910A1 (de) Kurbelgehäuseentlüftung für eine Brennkraftmaschine
DE102012001458A1 (de) Brennkraftmaschine
DE3439999C1 (de) Viertakt-Brennkraftmaschine mit zwei Abgasturboladern
DE19826355A1 (de) Vorrichtung und Verfahren zur Steuerung einer Abgasturboladerturbine
DE3743056A1 (de) Ansaugstrang fuer eine hubkolben-brennkraftmaschine

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

AK Designated contracting states

Designated state(s): AT CH DE FR GB IT LI SE

17P Request for examination filed

Effective date: 19840218

ITF It: translation for a ep patent filed

Owner name: DE DOMINICIS & MAYER S.R.L.

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Designated state(s): AT CH DE FR GB IT LI SE

REF Corresponds to:

Ref document number: 16626

Country of ref document: AT

Date of ref document: 19851215

Kind code of ref document: T

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Effective date: 19851130

REF Corresponds to:

Ref document number: 3361269

Country of ref document: DE

Date of ref document: 19860102

ET Fr: translation filed
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
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Effective date: 19890430

Ref country code: CH

Effective date: 19890430

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 19900315

Year of fee payment: 8

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 19900323

Year of fee payment: 8

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19900331

Year of fee payment: 8

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: 19910407

Ref country code: AT

Effective date: 19910407

GBPC Gb: european patent ceased through non-payment of renewal fee
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Effective date: 19911230

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20000502

Year of fee payment: 18

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20020201