NL67338C - - Google Patents

Info

Publication number
NL67338C
NL67338C NL67338DA NL67338C NL 67338 C NL67338 C NL 67338C NL 67338D A NL67338D A NL 67338DA NL 67338 C NL67338 C NL 67338C
Authority
NL
Netherlands
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 NL67338C publication Critical patent/NL67338C/xx

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
NL67338D 1944-11-28 NL67338C (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB262382X 1944-11-28

Publications (1)

Publication Number Publication Date
NL67338C true NL67338C (fr)

Family

ID=10240490

Family Applications (1)

Application Number Title Priority Date Filing Date
NL67338D NL67338C (fr) 1944-11-28

Country Status (5)

Country Link
BE (1) BE468998A (fr)
CH (1) CH262382A (fr)
FR (1) FR943200A (fr)
GB (1) GB588847A (fr)
NL (1) NL67338C (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2648950A (en) * 1949-08-24 1953-08-18 Westinghouse Electric Corp Gas turbine engine apparatus designed to burn wet pulverized fuel
US3003316A (en) * 1953-02-10 1961-10-10 Rolls Royce Cooling means for forked exhaust ducts of gas turbine engines
US2861424A (en) * 1954-04-09 1958-11-25 Douglas Aircraft Co Inc Fuel supply means for combustion apparatus
US2944388A (en) * 1955-02-24 1960-07-12 Thompson Ramo Wooldridge Inc Air atomizing spray bar
US2942414A (en) * 1956-07-03 1960-06-28 Thompson Ramo Wooldridge Inc Umbrella spraybar afterburner arrangement
BE795529A (fr) * 1972-02-17 1973-06-18 Gen Electric Allumeur monte sur un dispositif d'augmentation de la poussee de turboreacteurs et refroidi a l'air
US4070826A (en) * 1975-12-24 1978-01-31 General Electric Company Low pressure fuel injection system
FR2471480A1 (fr) * 1979-12-13 1981-06-19 Snecma Dispositif d'injection pour chambre a combustion de moteur a turbine
CH666340A5 (en) * 1985-05-29 1988-07-15 Bbc Brown Boveri & Cie Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
US4955201A (en) * 1987-12-14 1990-09-11 Sundstrand Corporation Fuel injectors for turbine engines
US4798048A (en) * 1987-12-21 1989-01-17 United Technologies Corporation Augmentor pilot
US4887425A (en) * 1988-03-18 1989-12-19 General Electric Company Fuel spraybar
DE59208193D1 (de) * 1992-07-03 1997-04-17 Abb Research Ltd Nachbrenner
US8869941B2 (en) * 2009-11-16 2014-10-28 Textron Innovations Inc. Dual-path fluid injection jet
US9638422B2 (en) * 2012-06-22 2017-05-02 Delavan Inc. Active purge mechanism with backflow preventer for gas turbine fuel injectors
WO2015054136A1 (fr) 2013-10-07 2015-04-16 United Technologies Corporation Injecteur de carburant refroidi à l'air pour moteur à turbine
EP3109550B1 (fr) * 2015-06-19 2019-09-04 Rolls-Royce Corporation Air de refroidissement refroidi de turbine circulant par un agencement tubulaire

Also Published As

Publication number Publication date
CH262382A (de) 1949-06-30
BE468998A (fr)
FR943200A (fr) 1949-03-01
GB588847A (en) 1947-06-04

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