CH270943A - Verbrennungseinrichtung. - Google Patents

Verbrennungseinrichtung.

Info

Publication number
CH270943A
CH270943A CH270943DA CH270943A CH 270943 A CH270943 A CH 270943A CH 270943D A CH270943D A CH 270943DA CH 270943 A CH270943 A CH 270943A
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 CH270943A publication Critical patent/CH270943A/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
    • F23D11/26—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space with provision for varying the rate at which the fuel is sprayed
    • F23D11/28—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space with provision for varying the rate at which the fuel is sprayed with flow-back of fuel at the burner, e.g. using by-pass

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
CH270943D 1947-05-23 1948-05-20 Verbrennungseinrichtung. CH270943A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13871/47A GB647344A (en) 1947-05-23 1947-05-23 Improvements in or relating to combustion apparatus

Publications (1)

Publication Number Publication Date
CH270943A true CH270943A (de) 1950-09-30

Family

ID=29726707

Family Applications (1)

Application Number Title Priority Date Filing Date
CH270943D CH270943A (de) 1947-05-23 1948-05-20 Verbrennungseinrichtung.

Country Status (6)

Country Link
US (1) US2781638A (h)
BE (1) BE482650A (h)
CH (1) CH270943A (h)
FR (1) FR971755A (h)
GB (1) GB647344A (h)
NL (1) NL82287C (h)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944398A (en) * 1954-10-20 1960-07-12 Lockheed Aircraft Corp Combustion chamber for jet propulsion motors
US2951341A (en) * 1956-09-19 1960-09-06 Westinghouse Electric Corp Fuel injection system for an aircraft engine
US2974487A (en) * 1957-10-19 1961-03-14 Bristol Siddeley Engines Ltd Combustion system for a gas turbine engine
GB1575410A (en) * 1976-09-04 1980-09-24 Rolls Royce Combustion apparatus for use in gas turbine engines
US4337616A (en) * 1980-04-14 1982-07-06 General Motors Corporation Fuel air ratio controlled fuel splitter
US5187936A (en) * 1990-10-17 1993-02-23 General Electric Company Continuous flow fuel circulation system
US20090111063A1 (en) * 2007-10-29 2009-04-30 General Electric Company Lean premixed, radial inflow, multi-annular staged nozzle, can-annular, dual-fuel combustor

Also Published As

Publication number Publication date
NL82287C (h)
FR971755A (h) 1951-01-22
BE482650A (h)
GB647344A (en) 1950-12-13
US2781638A (en) 1957-02-19

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