FR1415215A - Combustion device for gas turbine engine - Google Patents

Combustion device for gas turbine engine

Info

Publication number
FR1415215A
FR1415215A FR996228A FR996228A FR1415215A FR 1415215 A FR1415215 A FR 1415215A FR 996228 A FR996228 A FR 996228A FR 996228 A FR996228 A FR 996228A FR 1415215 A FR1415215 A FR 1415215A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
combustion device
combustion
engine
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
FR996228A
Other languages
French (fr)
Inventor
Harry Moxon
Terence Durrant
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
Priority to FR996228A priority Critical patent/FR1415215A/en
Application granted granted Critical
Publication of FR1415215A publication Critical patent/FR1415215A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR996228A 1964-11-25 1964-11-25 Combustion device for gas turbine engine Expired FR1415215A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR996228A FR1415215A (en) 1964-11-25 1964-11-25 Combustion device for gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR996228A FR1415215A (en) 1964-11-25 1964-11-25 Combustion device for gas turbine engine

Publications (1)

Publication Number Publication Date
FR1415215A true FR1415215A (en) 1965-10-22

Family

ID=8843315

Family Applications (1)

Application Number Title Priority Date Filing Date
FR996228A Expired FR1415215A (en) 1964-11-25 1964-11-25 Combustion device for gas turbine engine

Country Status (1)

Country Link
FR (1) FR1415215A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2947390B1 (en) * 2014-05-16 2018-06-06 Rolls-Royce plc A combustion chamber arrangement

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2947390B1 (en) * 2014-05-16 2018-06-06 Rolls-Royce plc A combustion chamber arrangement
US10295189B2 (en) 2014-05-16 2019-05-21 Rolls-Royce Plc Combustion chamber arrangement

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