BE842433A - Moteur a turbine a gaz a by-pass reglables et procede pour commander ce moteur - Google Patents

Moteur a turbine a gaz a by-pass reglables et procede pour commander ce moteur

Info

Publication number
BE842433A
BE842433A BE167509A BE167509A BE842433A BE 842433 A BE842433 A BE 842433A BE 167509 A BE167509 A BE 167509A BE 167509 A BE167509 A BE 167509A BE 842433 A BE842433 A BE 842433A
Authority
BE
Belgium
Prior art keywords
engine
adjustable
procedure
pass
controlling
Prior art date
Application number
BE167509A
Other languages
English (en)
French (fr)
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 filed Critical
Publication of BE842433A publication Critical patent/BE842433A/xx

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
    • F02K3/075—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 controlling flow ratio between flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
BE167509A 1975-06-02 1976-06-01 Moteur a turbine a gaz a by-pass reglables et procede pour commander ce moteur BE842433A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/583,055 US4069661A (en) 1975-06-02 1975-06-02 Variable mixer propulsion cycle

Publications (1)

Publication Number Publication Date
BE842433A true BE842433A (fr) 1976-10-01

Family

ID=24331511

Family Applications (1)

Application Number Title Priority Date Filing Date
BE167509A BE842433A (fr) 1975-06-02 1976-06-01 Moteur a turbine a gaz a by-pass reglables et procede pour commander ce moteur

Country Status (8)

Country Link
US (1) US4069661A (cs)
JP (1) JPS6018826B2 (cs)
BE (1) BE842433A (cs)
CA (1) CA1053011A (cs)
DE (1) DE2624282C2 (cs)
FR (1) FR2313565A1 (cs)
GB (1) GB1544454A (cs)
IT (1) IT1060787B (cs)

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Also Published As

Publication number Publication date
FR2313565B1 (cs) 1983-01-07
CA1053011A (en) 1979-04-24
JPS521221A (en) 1977-01-07
JPS6018826B2 (ja) 1985-05-13
IT1060787B (it) 1982-09-30
DE2624282C2 (de) 1986-04-24
GB1544454A (en) 1979-04-19
DE2624282A1 (de) 1976-12-16
FR2313565A1 (fr) 1976-12-31
US4069661A (en) 1978-01-24

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