GB793325A - Improvements in or relating to combustion apparatus - Google Patents

Improvements in or relating to combustion apparatus

Info

Publication number
GB793325A
GB793325A GB33186/55A GB3318655A GB793325A GB 793325 A GB793325 A GB 793325A GB 33186/55 A GB33186/55 A GB 33186/55A GB 3318655 A GB3318655 A GB 3318655A GB 793325 A GB793325 A GB 793325A
Authority
GB
United Kingdom
Prior art keywords
shell
combustion
combustion apparatus
fins
nov
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
GB33186/55A
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.)
GEN THERMIQUE PROCEDES BROLA S
Original Assignee
GEN THERMIQUE PROCEDES BROLA S
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 GEN THERMIQUE PROCEDES BROLA S filed Critical GEN THERMIQUE PROCEDES BROLA S
Publication of GB793325A publication Critical patent/GB793325A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • 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 
    • F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
    • 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 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

793,325. Combustion apparatus. SOC. ANON. GENERALE THERMIQUE - PROCEDES BROLA. Nov. 21, 1955 [Nov. 24, 1954], No. 33186/55. Class 51 (1). The combustion apparatus, Fig. 1, comprises a tubular member 12 inserted at one end in an aperture formed in one wall of a casing 25 the end so inserted mounting the unit structure shown in Fig. 3. This structure comprises a shell member 1 having holes 3, 4, 5, an annular ring member 7 and fins 6 which connect the shell and the member 7 forming slot-like apertures 11 therebetween. The shell is also formed with a central opening 2 into which, when the structure is in position in the apparatus, is pointed a fuel injector 14 and a sparking plug 15. In operation, all combustion air is supplied from the casing 25, primary, secondary and tertiary air entering the combustion chamber, comprised by the shell and the member 12, through the opening 2, the holes 3, 4, 5 and the slots 11 respectively. The shell 1 may be hemispherical or paraboloidal in shape and the base edges 9, 10, Fig. 2, of the fins are such that the air passing through the slots 11 is caused to eddy in vortices 17.
GB33186/55A 1954-11-24 1955-11-21 Improvements in or relating to combustion apparatus Expired GB793325A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1115481T 1954-11-24

Publications (1)

Publication Number Publication Date
GB793325A true GB793325A (en) 1958-04-16

Family

ID=9628966

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33186/55A Expired GB793325A (en) 1954-11-24 1955-11-21 Improvements in or relating to combustion apparatus

Country Status (4)

Country Link
US (1) US2901032A (en)
FR (1) FR1115481A (en)
GB (1) GB793325A (en)
NL (1) NL98183C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5256352A (en) * 1992-09-02 1993-10-26 United Technologies Corporation Air-liquid mixer
US5267851A (en) * 1992-03-16 1993-12-07 General Electric Company Swirl gutters for isolating flow fields for combustion enhancement at non-baseload operating conditions
US5331815A (en) * 1992-03-23 1994-07-26 General Electric Company Impact resistant combustor
US5658358A (en) * 1993-04-08 1997-08-19 Abb Management Ag Fuel supply system for combustion chamber

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1166664A (en) * 1957-02-05 1958-11-13 Improvements to the combustion chambers which can be used, in particular, in reactors
FR998079A (en) * 1958-08-22 1952-01-14 Snecma Device for the entry of air into the primary zone of a turbo-machine combustion chamber
NL111857C (en) * 1959-04-28
US3130773A (en) * 1959-05-04 1964-04-28 Drake Block Co Inc Air-cooled burner ring
US3169369A (en) * 1963-06-19 1965-02-16 Gen Electric Combustion system
US3304982A (en) * 1964-07-09 1967-02-21 H B Smith Company Inc Windbox for furnace
US3273343A (en) * 1965-03-08 1966-09-20 Dickens Inc Combustion chamber construction in gas turbine power plant
US3414362A (en) * 1966-04-15 1968-12-03 F Schoppe Dr Ing Burner for firing a combustion chamber
JPS4724483Y1 (en) * 1970-12-22 1972-08-02
US3700173A (en) * 1970-12-30 1972-10-24 Combustion Eng Diffuser
GB2043868B (en) * 1979-03-08 1982-12-15 Rolls Royce Gas turbine
US5149261A (en) * 1985-11-15 1992-09-22 Nippon Sanso Kabushiki Kaisha Oxygen heater and oxygen lance using oxygen heater
US8979525B2 (en) * 1997-11-10 2015-03-17 Brambel Trading Internacional LDS Streamlined body and combustion apparatus
DE10158295B4 (en) * 2001-11-23 2005-11-24 Bramble-Trading Internacional Lda, Funchal flow body
FR2881813B1 (en) * 2005-02-09 2011-04-08 Snecma Moteurs TURBOMACHINE COMBUSTION CHAMBER FAIRING
US8622737B2 (en) * 2008-07-16 2014-01-07 Robert S. Babington Perforated flame tube for a liquid fuel burner
US8998605B2 (en) * 2010-10-07 2015-04-07 Carrier Corporation Inshot burner flame retainer
US9410698B2 (en) * 2011-10-11 2016-08-09 Rinnai Corporation Tubular burner

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA510584A (en) * 1955-03-01 C. Benedict Marcus Adjustable flame holder for jet power plant
DE547338C (en) * 1932-03-31 Babcock & Wilcox Dampfkessel W Pulverized coal burners
US1665786A (en) * 1924-06-16 1928-04-10 Morse Dry Dock & Repair Co Furnace front
CH178351A (en) * 1934-07-02 1935-07-15 Brevo A G Fuer Explosions Und Atomizing burners for liquid fuel.
US2411181A (en) * 1943-04-10 1946-11-19 Allis Chalmers Mfg Co Combustion turbine burner
US2689457A (en) * 1949-03-15 1954-09-21 Hermann Oestrich Burner, particularly for gas turbines
US2725718A (en) * 1950-04-10 1955-12-06 Goodyear Aircraft Corp Ignition systems for jet motors and the like
US2701608A (en) * 1951-02-03 1955-02-08 Thermal Res And Engineering Co Burner
US2693083A (en) * 1951-03-26 1954-11-02 Roy W Abbott Combination flame-holder and fuel nozzle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5267851A (en) * 1992-03-16 1993-12-07 General Electric Company Swirl gutters for isolating flow fields for combustion enhancement at non-baseload operating conditions
US5331815A (en) * 1992-03-23 1994-07-26 General Electric Company Impact resistant combustor
US5256352A (en) * 1992-09-02 1993-10-26 United Technologies Corporation Air-liquid mixer
US5658358A (en) * 1993-04-08 1997-08-19 Abb Management Ag Fuel supply system for combustion chamber

Also Published As

Publication number Publication date
US2901032A (en) 1959-08-25
FR1115481A (en) 1956-04-25
NL98183C (en)

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