FR1020989A - Perfectionnements aux moteurs à turbines à gaz - Google Patents

Perfectionnements aux moteurs à turbines à gaz

Info

Publication number
FR1020989A
FR1020989A FR1020989DA FR1020989A FR 1020989 A FR1020989 A FR 1020989A FR 1020989D A FR1020989D A FR 1020989DA FR 1020989 A FR1020989 A FR 1020989A
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
engines
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
English (en)
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 FR1020989A publication Critical patent/FR1020989A/fr
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
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
    • 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)
  • Combustion Of Fluid Fuel (AREA)
  • Gas Burners (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR1020989D 1949-06-27 1950-06-26 Perfectionnements aux moteurs à turbines à gaz Expired FR1020989A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1695549A GB686382A (en) 1949-06-27 1949-06-27 Improvements in or relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
FR1020989A true FR1020989A (fr) 1953-02-12

Family

ID=10086673

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1020989D Expired FR1020989A (fr) 1949-06-27 1950-06-26 Perfectionnements aux moteurs à turbines à gaz

Country Status (3)

Country Link
BE (1) BE496626A (pt)
FR (1) FR1020989A (pt)
GB (1) GB686382A (pt)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1153570B (de) * 1959-04-17 1963-08-29 Rolls Royce Verbrennungsvorrichtung fuer Gasturbinenanlagen
US4201046A (en) * 1977-12-27 1980-05-06 United Technologies Corporation Burner nozzle assembly for gas turbine engine

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1047536B (de) * 1956-07-07 1958-12-24 Daimler Benz Ag Brennkammer fuer Gasturbinen
DE1123868B (de) * 1958-08-26 1962-02-15 Schweizerische Lokomotiv Brennkammer, insbesondere fuer Gasturbinen
US3049882A (en) * 1960-05-16 1962-08-21 Gen Electric Combustor construction with means for prevention of hot streaks
DE1230618B (de) * 1964-01-03 1966-12-15 Lucas Industries Ltd Verbrennungsvorrichtung fuer Strahltriebwerke, Gasturbinen od. dgl.
US3344601A (en) * 1966-01-18 1967-10-03 United Aircraft Corp Interconnection for flametubes
US3500639A (en) * 1968-09-10 1970-03-17 Gen Electric Combustion chamber mounting means
US4251986A (en) * 1978-12-05 1981-02-24 General Electric Company Seal vibration-reducing apparatus
GB0918089D0 (en) * 2009-10-16 2009-12-02 Rolls Royce Plc Fuel injector mounting system
US10066837B2 (en) 2015-02-20 2018-09-04 General Electric Company Combustor aft mount assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1153570B (de) * 1959-04-17 1963-08-29 Rolls Royce Verbrennungsvorrichtung fuer Gasturbinenanlagen
US4201046A (en) * 1977-12-27 1980-05-06 United Technologies Corporation Burner nozzle assembly for gas turbine engine

Also Published As

Publication number Publication date
GB686382A (en) 1953-01-21
BE496626A (pt)

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