CH263760A - Brenner in einer Verbrennungskammer von Verbrennungsturbinen. - Google Patents

Brenner in einer Verbrennungskammer von Verbrennungsturbinen.

Info

Publication number
CH263760A
CH263760A CH263760DA CH263760A CH 263760 A CH263760 A CH 263760A CH 263760D A CH263760D A CH 263760DA CH 263760 A CH263760 A CH 263760A
Authority
CH
Switzerland
Prior art keywords
hub
burner
nozzle
combustion
chamber
Prior art date
Application number
Other languages
German (de)
English (en)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH263760A publication Critical patent/CH263760A/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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
CH263760D 1946-03-26 1947-02-26 Brenner in einer Verbrennungskammer von Verbrennungsturbinen. CH263760A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB934446A GB614553A (en) 1946-03-26 1946-03-26 Improvements in or relating to burner assemblies for internal combustion turbines

Publications (1)

Publication Number Publication Date
CH263760A true CH263760A (de) 1949-09-15

Family

ID=9870143

Family Applications (1)

Application Number Title Priority Date Filing Date
CH263760D CH263760A (de) 1946-03-26 1947-02-26 Brenner in einer Verbrennungskammer von Verbrennungsturbinen.

Country Status (3)

Country Link
BE (1) BE488537A (US06262066-20010717-C00315.png)
CH (1) CH263760A (US06262066-20010717-C00315.png)
GB (1) GB614553A (US06262066-20010717-C00315.png)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0132213A2 (en) * 1983-07-19 1985-01-23 United Technologies Corporation Fuel nozzle for gas turbine engine

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1476748B1 (de) * 1965-10-12 1970-12-17 Daimler Benz Ag Filtervorrichtung
US8387391B2 (en) 2010-12-17 2013-03-05 General Electric Company Aerodynamically enhanced fuel nozzle
US11230976B2 (en) 2017-07-14 2022-01-25 General Electric Company Integrated fuel nozzle connection

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0132213A2 (en) * 1983-07-19 1985-01-23 United Technologies Corporation Fuel nozzle for gas turbine engine
EP0132213A3 (en) * 1983-07-19 1986-02-12 United Technologies Corporation Fuel nozzle for gas turbine engine

Also Published As

Publication number Publication date
GB614553A (en) 1948-12-17
BE488537A (US06262066-20010717-C00315.png)

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