FR1093961A - Gas turbine engine improvements - Google Patents

Gas turbine engine improvements

Info

Publication number
FR1093961A
FR1093961A FR1093961DA FR1093961A FR 1093961 A FR1093961 A FR 1093961A FR 1093961D A FR1093961D A FR 1093961DA FR 1093961 A FR1093961 A FR 1093961A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine improvements
gas
turbine
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 FR1093961A publication Critical patent/FR1093961A/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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
FR1093961D 1951-04-25 1952-04-23 Gas turbine engine improvements Expired FR1093961A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1093961X 1951-04-25

Publications (1)

Publication Number Publication Date
FR1093961A true FR1093961A (en) 1955-05-11

Family

ID=10873569

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1093961D Expired FR1093961A (en) 1951-04-25 1952-04-23 Gas turbine engine improvements

Country Status (1)

Country Link
FR (1) FR1093961A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1081722B (en) * 1956-11-27 1960-05-12 Snecma Combustion device for steel engines with uninterrupted flow
EP0315486A2 (en) * 1987-11-05 1989-05-10 General Electric Company Aircraft engine frame construction

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1081722B (en) * 1956-11-27 1960-05-12 Snecma Combustion device for steel engines with uninterrupted flow
EP0315486A2 (en) * 1987-11-05 1989-05-10 General Electric Company Aircraft engine frame construction
EP0315486A3 (en) * 1987-11-05 1990-01-17 General Electric Company Aircraft engine frame construction
US5020318A (en) * 1987-11-05 1991-06-04 General Electric Company Aircraft engine frame construction

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