CH261477A - Verbrennungseinrichtung. - Google Patents

Verbrennungseinrichtung.

Info

Publication number
CH261477A
CH261477A CH261477DA CH261477A CH 261477 A CH261477 A CH 261477A CH 261477D A CH261477D A CH 261477DA CH 261477 A CH261477 A CH 261477A
Authority
CH
Switzerland
Prior art keywords
incinerator
Prior art date
Application number
Other languages
German (de)
English (en)
Inventor
Power Jets Research De Limited
Original Assignee
Power Jets Res & Dev Ltd
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 Power Jets Res & Dev Ltd filed Critical Power Jets Res & Dev Ltd
Publication of CH261477A publication Critical patent/CH261477A/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/062—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with aft fan
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Gas Burners (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
CH261477D 1945-01-16 1946-01-10 Verbrennungseinrichtung. CH261477A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1354/45A GB591113A (en) 1945-01-16 1945-01-16 Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus

Publications (1)

Publication Number Publication Date
CH261477A true CH261477A (de) 1949-05-15

Family

ID=29725418

Family Applications (1)

Application Number Title Priority Date Filing Date
CH261477D CH261477A (de) 1945-01-16 1946-01-10 Verbrennungseinrichtung.

Country Status (6)

Country Link
US (1) US2575264A (xx)
BE (1) BE462369A (xx)
CH (1) CH261477A (xx)
FR (2) FR920036A (xx)
GB (1) GB591113A (xx)
NL (1) NL70888C (xx)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1198130B (de) * 1958-08-22 1965-08-05 Snecma Brenner fuer ringfoermige Brennkammern

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2675675A (en) * 1954-04-20 Muctlpefi combustion chamber jet
US2670600A (en) * 1947-06-17 1954-03-02 Bristol Aeroplane Co Ltd Air distribution system for flame tubes of gas turbine engines
US2697032A (en) * 1949-05-05 1954-12-14 Phillips Petroleum Co Acetylene gas producer
US2711631A (en) * 1949-06-21 1955-06-28 Hartford Nat Bank & Trust Co Gas turbine power plant
US2692478A (en) * 1951-02-24 1954-10-26 Boeing Co Turbine burner incorporating removable burner liner
US2690648A (en) * 1951-07-03 1954-10-05 Dowty Equipment Ltd Means for conducting the flow of liquid fuel for feeding burners of gas turbine engines
US3062482A (en) * 1952-08-25 1962-11-06 A V Roe Canada Ltd Gas turbine engined aircraft
US3741483A (en) * 1971-12-10 1973-06-26 Mitsubishi Heavy Ind Ltd Combustion air supply arrangement for gas turbines
US5630319A (en) * 1995-05-12 1997-05-20 General Electric Company Dome assembly for a multiple annular combustor

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2439273A (en) * 1948-04-06 Turbo-jet engine for aircraft
US2432359A (en) * 1947-12-09 Internal-combustion turbine power
US1517422A (en) * 1922-08-05 1924-12-02 Leo G Hall Combination land and water vehicle
US1466006A (en) * 1922-09-14 1923-08-28 Trood Samuel Apparatus for producing and utilizing combustible mixture
US1950046A (en) * 1933-05-12 1934-03-06 Surface Combustion Corp Gas burner
US1995417A (en) * 1933-05-12 1935-03-26 Surface Combustion Corp Gas burner
US2072731A (en) * 1934-12-03 1937-03-02 Steam Motors Inc Oil burner
US2224472A (en) * 1938-05-02 1940-12-10 Chandler Evans Corp Pressure fed carburetor
US2360130A (en) * 1941-03-26 1944-10-10 Armstrong Siddeley Motors Ltd High-speed propulsion plant
US2422214A (en) * 1944-08-17 1947-06-17 Westinghouse Electric Corp Fuel injector mounting for combustion chambers

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1198130B (de) * 1958-08-22 1965-08-05 Snecma Brenner fuer ringfoermige Brennkammern

Also Published As

Publication number Publication date
NL70888C (xx)
GB591113A (en) 1947-08-07
FR920036A (fr) 1947-03-25
BE462369A (xx)
US2575264A (en) 1951-11-13
FR920038A (fr) 1947-03-25

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