FR1198599A - Groupe propulseur à réaction, notamment pour aéronefs - Google Patents

Groupe propulseur à réaction, notamment pour aéronefs

Info

Publication number
FR1198599A
FR1198599A FR1198599DA FR1198599A FR 1198599 A FR1198599 A FR 1198599A FR 1198599D A FR1198599D A FR 1198599DA FR 1198599 A FR1198599 A FR 1198599A
Authority
FR
France
Prior art keywords
powertrain
aircraft
jet
jet powertrain
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bristol Aero Engines Ltd
Original Assignee
Bristol Aero Engines 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 Bristol Aero Engines Ltd filed Critical Bristol Aero Engines Ltd
Application granted granted Critical
Publication of FR1198599A publication Critical patent/FR1198599A/fr
Expired legal-status Critical Current

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
    • F02K3/025—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 by-pass flow being at least partly used to create an independent thrust component
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1198599D 1957-01-29 1958-01-28 Groupe propulseur à réaction, notamment pour aéronefs Expired FR1198599A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1198599X 1957-01-29

Publications (1)

Publication Number Publication Date
FR1198599A true FR1198599A (fr) 1959-12-08

Family

ID=10881727

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1198599D Expired FR1198599A (fr) 1957-01-29 1958-01-28 Groupe propulseur à réaction, notamment pour aéronefs

Country Status (1)

Country Link
FR (1) FR1198599A (fr)

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