FR1199576A - Improvements made to power plants with gas turbines, in particular for jet propulsion - Google Patents

Improvements made to power plants with gas turbines, in particular for jet propulsion

Info

Publication number
FR1199576A
FR1199576A FR1199576DA FR1199576A FR 1199576 A FR1199576 A FR 1199576A FR 1199576D A FR1199576D A FR 1199576DA FR 1199576 A FR1199576 A FR 1199576A
Authority
FR
France
Prior art keywords
power plants
improvements made
gas turbines
jet propulsion
propulsion
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
French (fr)
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1199576A publication Critical patent/FR1199576A/en
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
    • F02K3/04—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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1199576D 1957-03-06 1958-03-06 Improvements made to power plants with gas turbines, in particular for jet propulsion Expired FR1199576A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB738457A GB838602A (en) 1957-03-06 1957-03-06 Improvements in or relating to gas turbine plant

Publications (1)

Publication Number Publication Date
FR1199576A true FR1199576A (en) 1959-12-15

Family

ID=9832098

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1199576D Expired FR1199576A (en) 1957-03-06 1958-03-06 Improvements made to power plants with gas turbines, in particular for jet propulsion

Country Status (2)

Country Link
FR (1) FR1199576A (en)
GB (1) GB838602A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3095696A (en) * 1959-09-25 1963-07-02 Roy W Rumble Combustion-engine exhaust systems
DE1270891B (en) * 1963-12-17 1968-06-20 Hans Georg Muenzberg Gas turbine engine with a short axial length
FR2378182A1 (en) * 1977-01-19 1978-08-18 Rolls Royce GAS TURBINE PROPELLER IMPROVEMENTS
EP0022692A1 (en) * 1979-07-16 1981-01-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Turbofan with variable by-pass ratio

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1483743A (en) * 1965-12-02 1967-06-09 Snecma Turbomachine with contra-rotating compressor
DE1626110B1 (en) * 1966-03-02 1969-12-18 Rolls Royce Gas turbine fan engine
US3375997A (en) * 1966-06-10 1968-04-02 Gen Electric Compound aircraft and propulsion system
FR2181472B1 (en) * 1972-04-25 1975-08-29 Snecma
GB2309745A (en) * 1996-02-02 1997-08-06 John Peter Miller Multi-stage compressor
CN104937251B (en) * 2013-01-18 2017-11-28 通用电气公司 Engine framework with reverse rotation monoblock type driver and without stator turbine
CN108757509B (en) * 2018-05-30 2020-09-29 中国航发动力股份有限公司 Low-pressure compressor structure of gas turbine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3095696A (en) * 1959-09-25 1963-07-02 Roy W Rumble Combustion-engine exhaust systems
DE1270891B (en) * 1963-12-17 1968-06-20 Hans Georg Muenzberg Gas turbine engine with a short axial length
FR2378182A1 (en) * 1977-01-19 1978-08-18 Rolls Royce GAS TURBINE PROPELLER IMPROVEMENTS
EP0022692A1 (en) * 1979-07-16 1981-01-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Turbofan with variable by-pass ratio
FR2461820A1 (en) * 1979-07-16 1981-02-06 Snecma MULTIFLUX TURBOREACTOR WITH A DILUTION RATE

Also Published As

Publication number Publication date
GB838602A (en) 1960-06-22

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