BE463635A - - Google Patents

Info

Publication number
BE463635A
BE463635A BE463635DA BE463635A BE 463635 A BE463635 A BE 463635A BE 463635D A BE463635D A BE 463635DA BE 463635 A BE463635 A BE 463635A
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 BE463635A publication Critical patent/BE463635A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/072Plants 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 with counter-rotating, e.g. fan rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/065Plants 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 with front and aft fans

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE463635D 1944-01-31 BE463635A (lt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB271479X 1944-01-31

Publications (1)

Publication Number Publication Date
BE463635A true BE463635A (lt)

Family

ID=10254984

Family Applications (1)

Application Number Title Priority Date Filing Date
BE463635D BE463635A (lt) 1944-01-31

Country Status (2)

Country Link
BE (1) BE463635A (lt)
CH (1) CH271479A (lt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE963203C (de) * 1952-05-06 1957-05-02 Alfred Buechi Propellerturbinentriebwerk
DE1043722B (de) * 1954-01-16 1958-11-13 Oskar August Schaetzle Dipl In Dreiwellenstrahltriebwerk mit biegungssteifen UEbertragungsgliedern
DE1052821B (de) * 1955-01-25 1959-03-12 Georges Caillette Einrichtung zum Kompensieren der Kreiselmomente von Gasturbinen, insbesondere bei Luftfahrzeugen
GB805418A (en) * 1955-10-05 1958-12-03 Power Jets Res & Dev Ltd Jet propulsion plant
DE1084981B (de) * 1957-01-25 1960-07-07 Konink Luchtvaart Mij N V Flugzeugtriebwerk
DE1236867B (de) * 1960-09-13 1967-03-16 Rolls Royce Geblaese fuer eine Triebwerksanlage in Flugzeugen
DE1242415B (de) * 1960-09-29 1967-06-15 Rolls Royce Gasturbinenstrahltriebwerk
GB992931A (en) * 1964-02-21 1965-05-26 Rolls Royce Gas turbine jet propulsion engine
DE102007013826A1 (de) * 2007-03-22 2008-09-25 Rolls-Royce Deutschland Ltd & Co Kg Axiallager mit einem radial inneren und einem radial äußeren Wälzlager
US8292570B2 (en) * 2008-01-25 2012-10-23 United Technologies Corporation Low pressure turbine with counter-rotating drives for single spool

Also Published As

Publication number Publication date
CH271479A (de) 1950-10-31

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