CH271479A - Gasturbinen-Kraftanlage. - Google Patents

Gasturbinen-Kraftanlage.

Info

Publication number
CH271479A
CH271479A CH271479DA CH271479A CH 271479 A CH271479 A CH 271479A CH 271479D A CH271479D A CH 271479DA CH 271479 A CH271479 A CH 271479A
Authority
CH
Switzerland
Prior art keywords
guide vane
compressor
rotor
power plant
turbine
Prior art date
Application number
Other languages
German (de)
English (en)
Inventor
Power Jets Research De Limited
Original Assignee
Power Jets Res & Dev 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 Power Jets Res & Dev Ltd filed Critical Power Jets Res & Dev Ltd
Publication of CH271479A publication Critical patent/CH271479A/de

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
    • F02K3/072—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 with counter-rotating, e.g. fan rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-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
    • F02C3/067—Gas-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
    • 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
    • F02K3/065—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 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)
CH271479D 1944-01-31 1946-02-18 Gasturbinen-Kraftanlage. CH271479A (de)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
CH271479A true CH271479A (de) 1950-10-31

Family

ID=10254984

Family Applications (1)

Application Number Title Priority Date Filing Date
CH271479D CH271479A (de) 1944-01-31 1946-02-18 Gasturbinen-Kraftanlage.

Country Status (2)

Country Link
BE (1) BE463635A (en:Method)
CH (1) CH271479A (en:Method)

Cited By (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
DE1043721B (de) * 1955-10-05 1958-11-13 Power Jets Res & Dev Ltd Strahltriebwerk
DE1052821B (de) * 1955-01-25 1959-03-12 Georges Caillette Einrichtung zum Kompensieren der Kreiselmomente von Gasturbinen, insbesondere bei Luftfahrzeugen
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
DE1264871B (de) * 1964-02-21 1968-03-28 Rolls Royce Gasturbinenstrahltriebwerk
DE102007013826A1 (de) * 2007-03-22 2008-09-25 Rolls-Royce Deutschland Ltd & Co Kg Axiallager mit einem radial inneren und einem radial äußeren Wälzlager
EP2085586A3 (en) * 2008-01-25 2012-11-21 United Technologies Corporation Low pressure turbine and corresponding gas turbine engine

Cited By (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
DE1043721B (de) * 1955-10-05 1958-11-13 Power Jets Res & Dev Ltd Strahltriebwerk
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
DE1264871B (de) * 1964-02-21 1968-03-28 Rolls Royce Gasturbinenstrahltriebwerk
DE102007013826A1 (de) * 2007-03-22 2008-09-25 Rolls-Royce Deutschland Ltd & Co Kg Axiallager mit einem radial inneren und einem radial äußeren Wälzlager
EP2085586A3 (en) * 2008-01-25 2012-11-21 United Technologies Corporation Low pressure turbine and corresponding gas turbine engine

Also Published As

Publication number Publication date
BE463635A (en:Method)

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