BE482650A - - Google Patents

Info

Publication number
BE482650A
BE482650A BE482650DA BE482650A BE 482650 A BE482650 A BE 482650A BE 482650D A BE482650D A BE 482650DA BE 482650 A BE482650 A BE 482650A
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 BE482650A publication Critical patent/BE482650A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/24Burners 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
    • F23D11/26Burners 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
    • F23D11/28Burners 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)
BE482650D 1947-05-23 BE482650A (US07534539-20090519-C00280.png)

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
BE482650A true BE482650A (US07534539-20090519-C00280.png)

Family

ID=29726707

Family Applications (1)

Application Number Title Priority Date Filing Date
BE482650D BE482650A (US07534539-20090519-C00280.png) 1947-05-23

Country Status (6)

Country Link
US (1) US2781638A (US07534539-20090519-C00280.png)
BE (1) BE482650A (US07534539-20090519-C00280.png)
CH (1) CH270943A (US07534539-20090519-C00280.png)
FR (1) FR971755A (US07534539-20090519-C00280.png)
GB (1) GB647344A (US07534539-20090519-C00280.png)
NL (1) NL82287C (US07534539-20090519-C00280.png)

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
FR971755A (US07534539-20090519-C00280.png) 1951-01-22
GB647344A (en) 1950-12-13
US2781638A (en) 1957-02-19
NL82287C (US07534539-20090519-C00280.png)
CH270943A (de) 1950-09-30

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