WO1981003048A1 - Procede et chambre de combustion de synthese a turbulence variable - Google Patents

Procede et chambre de combustion de synthese a turbulence variable Download PDF

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Publication number
WO1981003048A1
WO1981003048A1 PCT/RO1981/000002 RO8100002W WO8103048A1 WO 1981003048 A1 WO1981003048 A1 WO 1981003048A1 RO 8100002 W RO8100002 W RO 8100002W WO 8103048 A1 WO8103048 A1 WO 8103048A1
Authority
WO
WIPO (PCT)
Prior art keywords
combustion chamber
combustion
chamber
piston
circulation
Prior art date
Application number
PCT/RO1981/000002
Other languages
English (en)
French (fr)
Inventor
M Paul
E Sarateanu
Original Assignee
Inst Nat Motoare Termice
M Paul
E Sarateanu
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 Inst Nat Motoare Termice, M Paul, E Sarateanu filed Critical Inst Nat Motoare Termice
Publication of WO1981003048A1 publication Critical patent/WO1981003048A1/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B19/00Engines characterised by precombustion chambers
    • F02B19/02Engines characterised by precombustion chambers the chamber being periodically isolated from its cylinder
    • F02B19/04Engines characterised by precombustion chambers the chamber being periodically isolated from its cylinder the isolation being effected by a protuberance on piston or cylinder head
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Definitions

  • the invention relates to a process and a combustion chamber with variable turbulence used in high speed engines.
  • the method and the unitary combustion chamber are also known, in which the absence of throttles in the path of the working fluid ensures a relatively reduced consumption of fuel, but has the disadvantage that they cannot operate at high speeds, following d '' a reduced level of organization of turbulence.
  • the method and the synthetic combustion chamber, in accordance with the present invention overcome the disadvantages presented above, in that, in order to achieve reduced fuel consumption and increased flexibility of compression-ignition engines both as regards the range of turns and / or load, as regards the dimensional range, ensures the integral organization by volume of the circulation of fluid in the combustion chamber by the only temporary separation of the space from the tower room.
  • the chamber forming a unitary whole, the combustion process as a whole constituting a synthesis between the chamber process unitary and the divided chamber method, the reinforcement of the turbulence being obtained as a result of the vectorial sum of at least three vortices, vortices with three-dimensional circulation and also by the enhancement of the threshold effect (squish) created by the piston, which accentuates the effect of transfer of the fluid between the one two enclosures which are separated by spatial profile which penetrates into the separation channel, profile defined by at least three steering surfaces, which produce vortices with three-dimensional circulation and constitute as a mobile braking threshold of the vortex enclosure, by concentrating the rich mixture which burns in the zone d u transfer channel, the circulation of the fluid in the swirling enclosure being thus determined, in order to meet the jet of fuel by equi-current and to move part of the fuel over the incandescent head of a candle.
  • FIGS. 1 ... 7 Three examples of embodiments of the combustion chambers which apply the method according to the present invention are given, in relation to FIGS. 1 ... 7, which represent:
  • injectors with several orifices allows the application of the method and of constructive solutions, in accordance with the present invention also for engines of large dimensions.
  • the air circulation in the final compression faze first encounters an ignition rod and then enters the injection zone, entraining the jet of fuel by equicurrent.

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)
PCT/RO1981/000002 1980-04-27 1981-04-21 Procede et chambre de combustion de synthese a turbulence variable WO1981003048A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RO80100981A RO77086A2 (ro) 1980-04-27 1980-04-27 Procedeu si camera de ardere de sinteza cu turbulenta variabila
RO100981 1980-04-27

Publications (1)

Publication Number Publication Date
WO1981003048A1 true WO1981003048A1 (fr) 1981-10-29

Family

ID=20108442

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RO1981/000002 WO1981003048A1 (fr) 1980-04-27 1981-04-21 Procede et chambre de combustion de synthese a turbulence variable

Country Status (4)

Country Link
EP (1) EP0050665A1 (ro)
GB (1) GB2088952B (ro)
RO (1) RO77086A2 (ro)
WO (1) WO1981003048A1 (ro)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8421445D0 (en) * 1984-08-23 1984-09-26 Greenhough J H Ic engine
US9791494B2 (en) 2012-01-20 2017-10-17 Lear Corporation Apparatus and method for diagnostics of a capacitive sensor

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2826185A (en) * 1954-08-25 1958-03-11 Gen Motors Corp Combustion chamber for engines
DE1526302A1 (de) * 1965-11-23 1970-04-02 Inst Francais Du Petrol Motor mit Kompressionszuendung

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2826185A (en) * 1954-08-25 1958-03-11 Gen Motors Corp Combustion chamber for engines
DE1526302A1 (de) * 1965-11-23 1970-04-02 Inst Francais Du Petrol Motor mit Kompressionszuendung

Also Published As

Publication number Publication date
GB2088952B (en) 1984-08-22
RO77086A2 (ro) 1983-02-01
RO77086B1 (ro) 1983-01-30
EP0050665A1 (fr) 1982-05-05
GB2088952A (en) 1982-06-16

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Designated state(s): FR