CH345499A - Verbrennungseinrichtung mit wenigstens einer Brennkammer - Google Patents

Verbrennungseinrichtung mit wenigstens einer Brennkammer

Info

Publication number
CH345499A
CH345499A CH345499DA CH345499A CH 345499 A CH345499 A CH 345499A CH 345499D A CH345499D A CH 345499DA CH 345499 A CH345499 A CH 345499A
Authority
CH
Switzerland
Prior art keywords
combustion
chamber
combustion chamber
combustion device
Prior art date
Application number
Other languages
English (en)
Inventor
Bonsall Frank
Sidney Massey Bernard
Original Assignee
Bristol Aero Engines Limited
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
Priority claimed from GB615754A external-priority patent/GB791752A/en
Priority claimed from US491098A external-priority patent/US3018624A/en
Application filed by Bristol Aero Engines Limited filed Critical Bristol Aero Engines Limited
Publication of CH345499A publication Critical patent/CH345499A/de

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH345499D 1954-03-02 1955-12-28 Verbrennungseinrichtung mit wenigstens einer Brennkammer CH345499A (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB615754A GB791752A (en) 1954-03-02 1954-03-02 Improvements in or relating to flame tubes for use in combustion systems of gas turbine engines
US491098A US3018624A (en) 1954-03-02 1955-02-28 Flame tubes for use in combustion systems of gas turbine engines
US837319A US2994196A (en) 1954-03-02 1959-08-25 Flame tubes for use in combustion systems of gas turbine engines

Publications (1)

Publication Number Publication Date
CH345499A true CH345499A (de) 1960-03-31

Family

ID=32397630

Family Applications (1)

Application Number Title Priority Date Filing Date
CH345499D CH345499A (de) 1954-03-02 1955-12-28 Verbrennungseinrichtung mit wenigstens einer Brennkammer

Country Status (3)

Country Link
US (1) US2994196A (de)
CH (1) CH345499A (de)
FR (1) FR1126424A (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9322335B2 (en) * 2013-03-15 2016-04-26 Siemens Energy, Inc. Gas turbine combustor exit piece with hinged connections
EP3124749B1 (de) * 2015-07-28 2018-12-19 Ansaldo Energia Switzerland AG Turbinenschaufelanordnung von erster stufe
US12416262B2 (en) 2023-02-17 2025-09-16 General Electric Company Reverse flow gas turbine engine having electric machine
US12221894B2 (en) * 2023-03-20 2025-02-11 General Electric Company Polska Sp. Z O.O. Compressor with anti-ice inlet

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2680951A (en) * 1948-01-02 1954-06-15 Power Jets Res & Dev Ltd Combustion apparatus for burning particles of solid or heavy liquid fuel in a fast moving stream
GB697027A (en) * 1950-11-27 1953-09-16 Lucas Ltd Joseph Combustion chambers for prime movers

Also Published As

Publication number Publication date
FR1126424A (fr) 1956-11-22
US2994196A (en) 1961-08-01

Similar Documents

Publication Publication Date Title
CH330271A (de) Zylindrische Verbrennungskammer
CH330987A (de) Brennkammer
CH351647A (de) Brennstoffelement
FR1098104A (fr) Projectile
CH345499A (de) Verbrennungseinrichtung mit wenigstens einer Brennkammer
AT187016B (de) Repetier-Handschußwaffe
FR1104957A (fr) Embrayage électro-centrifuge
CH327319A (de) Zeichengerät
AT185012B (de) Ölbrenner mit Eigendampfzerstäubung
AT186476B (de) Drosselventil
AT190243B (de) Verschiebevorrichtung
AT192582B (de) Brenneranlage mit pulsierender Verbrennung
AT189323B (de) Ölbrenner mit Eigendampfzerstäubung
FR1147426A (fr) Carburant
CH328212A (de) Drehzahlabhängige Regelungsvorrichtung
AT189773B (de) Dochtvergaser
ES43290Y (es) Aparato economizador de combustible
ES40658Y (es) Economizador de gasolina
FR1132765A (fr) Injecteur
FR1143337A (fr) Carburateur
FR1113238A (fr) Carburateur
FR1130173A (fr) Carburateur
ES44519Y (es) Hornillo
FR1105947A (fr) Brûleurs
FI26992A (fi) Keittoliesi