BE569712A - - Google Patents

Info

Publication number
BE569712A
BE569712A BE569712DA BE569712A BE 569712 A BE569712 A BE 569712A BE 569712D A BE569712D A BE 569712DA BE 569712 A BE569712 A BE 569712A
Authority
BE
Belgium
Application number
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.)
Publication of BE569712A publication Critical patent/BE569712A/xx
Priority claimed from GB2400755A external-priority patent/GB812404A/en

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
    • F23R3/60—Support structures; Attaching or mounting means
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE569712D 1954-08-18 BE569712A (xx)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB2400755A GB812404A (en) 1955-07-28 1954-08-18 Internal combustion turbine units
GB2179255 1955-07-28
GB23819/57A GB865762A (en) 1954-08-18 1957-07-26 Internal combustion turbine units

Publications (1)

Publication Number Publication Date
BE569712A true BE569712A (xx)

Family

ID=27258037

Family Applications (2)

Application Number Title Priority Date Filing Date
BE540594D BE540594A (xx) 1954-08-18
BE569712D BE569712A (xx) 1954-08-18

Family Applications Before (1)

Application Number Title Priority Date Filing Date
BE540594D BE540594A (xx) 1954-08-18

Country Status (6)

Country Link
US (1) US2968924A (xx)
BE (2) BE569712A (xx)
CH (1) CH358990A (xx)
DE (1) DE1086089B (xx)
FR (2) FR1129767A (xx)
GB (1) GB865762A (xx)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2147405A (en) * 1983-09-28 1985-05-09 Rolls Royce Gas turbine engine combustion chamber mounting
US6116013A (en) * 1998-01-02 2000-09-12 Siemens Westinghouse Power Corporation Bolted gas turbine combustor transition coupling
US8938976B2 (en) * 2011-05-20 2015-01-27 Siemens Energy, Inc. Structural frame for gas turbine combustion cap assembly

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1599457A (en) * 1924-02-02 1926-09-14 Rateau Soc Fuel burner
US2563744A (en) * 1942-03-06 1951-08-07 Lockheed Aircraft Corp Gas turbine power plant having internal cooling means
DE807574C (de) * 1942-10-02 1951-07-02 Armstrong Siddeley Motors Ltd Brennkraftturbine
CH263382A (de) * 1945-02-20 1949-08-31 Power Jets Res & Dev Ltd Gasturbinen-Antriebsaggregat.
DE850087C (de) * 1945-02-27 1952-09-22 Maschf Augsburg Nuernberg Ag Verfahren und Vorrichtung zur Erzeugung eines gasfoermigen Treib-mittels, insbesondere fuer Turbinen
GB606526A (en) * 1945-10-09 1948-08-16 Bristol Aeroplane Co Ltd Improvements in or relating to means for supporting gas-turbine power-plants
US2531810A (en) * 1946-06-05 1950-11-28 Kellogg M W Co Air inlet arrangement for combustion chamber flame tubes
CH267195A (de) * 1947-06-12 1950-03-15 Bristol Aeroplane Company Limi Gasturbinenanlage.
US2676459A (en) * 1947-06-12 1954-04-27 Bristol Aeroplane Co Ltd Gas turbine engine having a continuous outer stress bearing shell and means allowing access through the shell to the combustion space of the engine
GB644031A (en) * 1947-06-16 1950-10-04 Bristol Aeroplane Co Ltd Improvements in or relating to gas turbine engines
US2670600A (en) * 1947-06-17 1954-03-02 Bristol Aeroplane Co Ltd Air distribution system for flame tubes of gas turbine engines
US2645412A (en) * 1949-09-28 1953-07-14 United Aircraft Corp Locking device for split-compressor type turbopower plants
FR1038694A (fr) * 1950-05-17 1953-09-30 Rolls Royce Perfectionnements aux générateurs de puissance à turbine à gaz comportant des dégivreurs
GB703002A (en) * 1951-02-14 1954-01-27 Rolls Royce Improvements in or relating to gas turbines
GB715910A (en) * 1952-02-01 1954-09-22 Rolls Royce Improvements in or relating to combustion equipment of gas-turbine engines

Also Published As

Publication number Publication date
GB865762A (en) 1961-04-19
FR73887E (fr) 1960-09-12
CH358990A (fr) 1961-12-15
FR1129767A (fr) 1957-01-25
BE540594A (xx)
US2968924A (en) 1961-01-24
DE1086089B (de) 1960-07-28

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