FR1206830A - Improvements to combustion equipment for gas turbine engines - Google Patents

Improvements to combustion equipment for gas turbine engines

Info

Publication number
FR1206830A
FR1206830A FR1206830DA FR1206830A FR 1206830 A FR1206830 A FR 1206830A FR 1206830D A FR1206830D A FR 1206830DA FR 1206830 A FR1206830 A FR 1206830A
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
combustion equipment
combustion
equipment
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1206830A publication Critical patent/FR1206830A/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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1206830D 1958-05-19 1958-05-19 Improvements to combustion equipment for gas turbine engines Expired FR1206830A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1206830T 1958-05-19

Publications (1)

Publication Number Publication Date
FR1206830A true FR1206830A (en) 1960-02-11

Family

ID=9673779

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1206830D Expired FR1206830A (en) 1958-05-19 1958-05-19 Improvements to combustion equipment for gas turbine engines

Country Status (1)

Country Link
FR (1) FR1206830A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1224989B (en) * 1960-05-18 1966-09-15 Rolls Royce Annular combustion chamber for gas turbine engines
FR2199059A1 (en) * 1972-09-07 1974-04-05 Rolls Royce
FR2295235A1 (en) * 1974-12-18 1976-07-16 United Technologies Corp COMBUSTION CHAMBER
FR2363700A1 (en) * 1976-09-04 1978-03-31 Rolls Royce GAS TURBINE ENGINE COMBUSTION EQUIPMENT
FR2446442A1 (en) * 1979-01-15 1980-08-08 United Technologies Corp BURNER SYSTEM AND METHOD OF USING BURNER SYSTEM
FR2488942A1 (en) * 1980-08-25 1982-02-26 Hitachi Ltd COMBUSTION PROCESS AND APPARATUS FOR GAS TURBINE
CN115727354A (en) * 2022-11-11 2023-03-03 中国航发哈尔滨东安发动机有限公司 Turbofan engine flame tube structure for aircraft

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1224989B (en) * 1960-05-18 1966-09-15 Rolls Royce Annular combustion chamber for gas turbine engines
FR2199059A1 (en) * 1972-09-07 1974-04-05 Rolls Royce
FR2295235A1 (en) * 1974-12-18 1976-07-16 United Technologies Corp COMBUSTION CHAMBER
FR2363700A1 (en) * 1976-09-04 1978-03-31 Rolls Royce GAS TURBINE ENGINE COMBUSTION EQUIPMENT
FR2446442A1 (en) * 1979-01-15 1980-08-08 United Technologies Corp BURNER SYSTEM AND METHOD OF USING BURNER SYSTEM
FR2488942A1 (en) * 1980-08-25 1982-02-26 Hitachi Ltd COMBUSTION PROCESS AND APPARATUS FOR GAS TURBINE
CN115727354A (en) * 2022-11-11 2023-03-03 中国航发哈尔滨东安发动机有限公司 Turbofan engine flame tube structure for aircraft

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