GB596846A - Improvements in or relating to modified otto cycle internal combustion engines - Google Patents

Improvements in or relating to modified otto cycle internal combustion engines

Info

Publication number
GB596846A
GB596846A GB1711743A GB1711743A GB596846A GB 596846 A GB596846 A GB 596846A GB 1711743 A GB1711743 A GB 1711743A GB 1711743 A GB1711743 A GB 1711743A GB 596846 A GB596846 A GB 596846A
Authority
GB
United Kingdom
Prior art keywords
fuel
air
nozzle
mixture
injection
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
Application number
GB1711743A
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.)
Texaco Development Corp
Original Assignee
Texaco Development Corp
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 Texaco Development Corp filed Critical Texaco Development Corp
Publication of GB596846A publication Critical patent/GB596846A/en
Expired legal-status Critical Current

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
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/02Engines characterised by air compression and subsequent fuel addition with positive ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/42Texaco combustion process
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2720/00Engines with liquid fuel
    • F02B2720/15Mixture compressing engines with ignition device and mixture formation in the cylinder
    • F02B2720/152Mixture compressing engines with ignition device and mixture formation in the cylinder with fuel supply and pulverisation by injecting the fuel under pressure during the suction or compression stroke
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/12Other methods of operation

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)
  • Ignition Installations For Internal Combustion Engines (AREA)

Abstract

596,846. Working cycles. TEXACO DEVELOPMENT CORPORATION. Oct. 18, 1943, No. 17117. Convention date, Oct. 23, 1942. [Class 7 (ii)] A method of and means for operating an internal combustion engine comprises introducing into the cylinder air without sufficient fuel to produce combustion, compressing the air therein, injecting fuel into the compressed air at a temperature and pressure ensuring that at least a portion of the fuel is instantly vaporized and forming a local area of combustible mixture adjacent the injection nozzle, igniting the mixture by a spark and establishing a flame front before sufficient fuel has been injected to cause knock and continuing the injection of the fuel in a narrow zone in advance of the flame front to form additional local areas of combustible mixture which are promptly ignited and burned. Fuel is injected tangentially into the combustion space through a nozzle 20, Fig. 2, directed along the whirling air stream produced by introducing the air tangentially through a shrouded inlet valve 14, the fuel being introduced at such a rate that the flame front 38 remains stationary or does not progress by more than 90 degrees of the swirl. The injection nozzle 60, Fig. 5, may be arranged radially and the swirling motion of the air be omitted, the fuel then forming a segment 61 of combustible mixture which forms a flame front which travels across the combustion chamber with the point of injection as a pivot, the nozzle delivering movements of fuel to the area immediately in front of the flame as it progresses across the combustion space. Alternatively, the nozzle may form two opposed segments 61, 68 of mixture which approach each other across the combustion space. In another form, the injection nozzle is central and narrow sectors replace the segments. The fuel may be heated to ensure that it vaporizes immediately and the control of the fuel be the sole control of the engine, a full charge of air or weak air-fuel mixture being drawn into the cylinder on each induction stroke. The method permits a low octane fuel to be used with a high compression ratio.
GB1711743A 1942-10-23 1943-10-18 Improvements in or relating to modified otto cycle internal combustion engines Expired GB596846A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US596846XA 1942-10-23 1942-10-23

Publications (1)

Publication Number Publication Date
GB596846A true GB596846A (en) 1948-01-13

Family

ID=22024562

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1711743A Expired GB596846A (en) 1942-10-23 1943-10-18 Improvements in or relating to modified otto cycle internal combustion engines

Country Status (3)

Country Link
DE (1) DE898824C (en)
FR (1) FR917212A (en)
GB (1) GB596846A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2188370B (en) * 1985-07-19 1989-07-26 Orbital Eng Pty Timing of fuel injected engines

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE966044C (en) * 1951-06-15 1957-07-04 Texaco Development Corp Method for operating a two-stroke internal combustion engine
DE1032024B (en) * 1952-06-23 1958-06-12 Texaco Development Corp Internal combustion engine
DE1019502B (en) * 1952-08-30 1957-11-14 Texaco Development Corp Internal combustion engine with a disk-shaped combustion chamber that works with air compression and self-ignition
DE1229778B (en) * 1957-07-05 1966-12-01 Texaco Development Corp Internal combustion engine with circular disk-shaped combustion chamber
DE2944339A1 (en) * 1979-11-02 1981-05-14 Volkswagenwerk Ag, 3180 Wolfsburg IC engine with two spark plugs per cylinder - has fuel injector directing separate fuel jets at plugs during idling

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2188370B (en) * 1985-07-19 1989-07-26 Orbital Eng Pty Timing of fuel injected engines
US4949689A (en) * 1985-07-19 1990-08-21 Orbital Engine Company Proprietary Limited Timing of fuel injected engines

Also Published As

Publication number Publication date
FR917212A (en) 1946-12-30
DE898824C (en) 1953-12-03

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