FR944310A - Burners - Google Patents

Burners

Info

Publication number
FR944310A
FR944310A FR944310DA FR944310A FR 944310 A FR944310 A FR 944310A FR 944310D A FR944310D A FR 944310DA FR 944310 A FR944310 A FR 944310A
Authority
FR
France
Prior art keywords
burners
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
Other languages
French (fr)
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation 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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Application granted granted Critical
Publication of FR944310A publication Critical patent/FR944310A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • 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
FR944310D 1946-01-09 1947-01-09 Burners Expired FR944310A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US944310XA 1946-01-09 1946-01-09

Publications (1)

Publication Number Publication Date
FR944310A true FR944310A (en) 1949-04-01

Family

ID=22245150

Family Applications (1)

Application Number Title Priority Date Filing Date
FR944310D Expired FR944310A (en) 1946-01-09 1947-01-09 Burners

Country Status (1)

Country Link
FR (1) FR944310A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1284157B (en) * 1963-12-04 1968-11-28 Rolls Royce Combustion device for gas turbine engines
FR2379698A1 (en) * 1977-02-04 1978-09-01 Rolls Royce PERFECTED COMBUSTION EQUIPMENT FOR GAS TURBINE ENGINES
EP0387532A1 (en) * 1989-03-15 1990-09-19 Asea Brown Boveri Ag Gas turbine combustion chamber
EP0401529A1 (en) * 1989-06-06 1990-12-12 Asea Brown Boveri Ag Gas turbine combustion chamber
US5193995A (en) * 1987-12-21 1993-03-16 Asea Brown Boveri Ltd. Apparatus for premixing-type combustion of liquid fuel
FR2694799A1 (en) * 1992-08-12 1994-02-18 Snecma Conventional annular combustion chamber with several injectors - includes base mounted circumferentially alternately for pilot and full gas providing idling or take off power with air blown to fuel cone

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1284157B (en) * 1963-12-04 1968-11-28 Rolls Royce Combustion device for gas turbine engines
FR2379698A1 (en) * 1977-02-04 1978-09-01 Rolls Royce PERFECTED COMBUSTION EQUIPMENT FOR GAS TURBINE ENGINES
US5193995A (en) * 1987-12-21 1993-03-16 Asea Brown Boveri Ltd. Apparatus for premixing-type combustion of liquid fuel
EP0387532A1 (en) * 1989-03-15 1990-09-19 Asea Brown Boveri Ag Gas turbine combustion chamber
CH678757A5 (en) * 1989-03-15 1991-10-31 Asea Brown Boveri
US5081844A (en) * 1989-03-15 1992-01-21 Asea Brown Boveri Ltd. Combustion chamber of a gas turbine
EP0401529A1 (en) * 1989-06-06 1990-12-12 Asea Brown Boveri Ag Gas turbine combustion chamber
CH680084A5 (en) * 1989-06-06 1992-06-15 Asea Brown Boveri
US5154059A (en) * 1989-06-06 1992-10-13 Asea Brown Boveri Ltd. Combustion chamber of a gas turbine
FR2694799A1 (en) * 1992-08-12 1994-02-18 Snecma Conventional annular combustion chamber with several injectors - includes base mounted circumferentially alternately for pilot and full gas providing idling or take off power with air blown to fuel cone

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