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GB838326A - Method and means for control of combustion in internal combustion engines - Google Patents

Method and means for control of combustion in internal combustion engines

Info

Publication number
GB838326A
GB838326A GB37104/57A GB3710457A GB838326A GB 838326 A GB838326 A GB 838326A GB 37104/57 A GB37104/57 A GB 37104/57A GB 3710457 A GB3710457 A GB 3710457A GB 838326 A GB838326 A GB 838326A
Authority
GB
United Kingdom
Prior art keywords
chamber
nozzle
combustion
gas turbine
entry
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
GB37104/57A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB838326A publication Critical patent/GB838326A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00—Subject-matter not provided for in other groups of this subclass
    • F23C99/003—Combustion process using sound or vibrations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01T—SPARK GAPS; OVERVOLTAGE ARRESTERS USING SPARK GAPS; SPARKING PLUGS; CORONA DEVICES; GENERATING IONS TO BE INTRODUCED INTO NON-ENCLOSED GASES
    • H01T13/00—Sparking plugs
    • H01T13/54—Sparking plugs having electrodes arranged in a partly-enclosed ignition chamber

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

838,326. Gas turbine plant. MEYER, A. J. Nov. 28, 1957 [Dec. 3, 1956], No. 37104/57. Class 110 (3). [Also in Groups XI, XII and XXVII] In a gas turbine engine, fuel from a nozzle 28 is sprayed into air supplied to a combustion chamber 13 at a pressure equal to, or more than, twice that in the main combustion zone 22, is ignited by a glow plug 29 and issues from a De Laval nozzle 15 at supersonic speed to form shock waves which cause rapid combustion and reduce detonation tendencies in the chamber 22. The nozzle 15 may be made up of three straightsided sections, may have an exit area between 10 and 60% larger than its throat area, and its orifice coefficient may be lowered by omitting its convergent entry or forming this entry in an annular projection into the chamber 13.
GB37104/57A 1956-12-03 1957-11-28 Method and means for control of combustion in internal combustion engines Expired GB838326A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US838326XA 1956-12-03 1956-12-03

Publications (1)

Publication Number Publication Date
GB838326A true GB838326A (en) 1960-06-22

Family

ID=22180981

Family Applications (1)

Application Number Title Priority Date Filing Date
GB37104/57A Expired GB838326A (en) 1956-12-03 1957-11-28 Method and means for control of combustion in internal combustion engines

Country Status (1)

Country Link
GB (1) GB838326A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4127095A (en) * 1976-04-22 1978-11-28 Nippon Soken, Inc. Torch-ignition internal combustion engine
GB2202274A (en) * 1987-03-20 1988-09-21 Westmoreland & Company Limited I.C. engine spark plug fitment
GB2443839A (en) * 2006-11-17 2008-05-21 Siemens Ag Interconnected Combustion Chambers
EP2261559A1 (en) * 2009-06-09 2010-12-15 Universität Stuttgart Combustor assembly for gas turbine with combustion-induced total pressure gain
CN110728048A (en) * 2019-10-08 2020-01-24 中国航发沈阳发动机研究所 Method and device for judging success of boosting ignition

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4127095A (en) * 1976-04-22 1978-11-28 Nippon Soken, Inc. Torch-ignition internal combustion engine
GB2202274A (en) * 1987-03-20 1988-09-21 Westmoreland & Company Limited I.C. engine spark plug fitment
GB2443839A (en) * 2006-11-17 2008-05-21 Siemens Ag Interconnected Combustion Chambers
EP2261559A1 (en) * 2009-06-09 2010-12-15 Universität Stuttgart Combustor assembly for gas turbine with combustion-induced total pressure gain
CN110728048A (en) * 2019-10-08 2020-01-24 中国航发沈阳发动机研究所 Method and device for judging success of boosting ignition
CN110728048B (en) * 2019-10-08 2023-10-20 中国航发沈阳发动机研究所 Method and device for judging success of boosting ignition

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