FR1561980A - - Google Patents

Info

Publication number
FR1561980A
FR1561980A FR132312A FR1561980DA FR1561980A FR 1561980 A FR1561980 A FR 1561980A FR 132312 A FR132312 A FR 132312A FR 1561980D A FR1561980D A FR 1561980DA FR 1561980 A FR1561980 A FR 1561980A
Authority
FR
France
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
FR132312A
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
Application granted granted Critical
Publication of FR1561980A publication Critical patent/FR1561980A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/026—Multi-stage pumps with a plurality of shafts rotating at different speeds
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/024—Multi-stage pumps with contrarotating parts
FR132312A 1967-12-14 1967-12-14 Expired FR1561980A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR132312 1967-12-14

Publications (1)

Publication Number Publication Date
FR1561980A true FR1561980A (fr) 1969-04-04

Family

ID=8643234

Family Applications (1)

Application Number Title Priority Date Filing Date
FR132312A Expired FR1561980A (fr) 1967-12-14 1967-12-14

Country Status (3)

Country Link
US (1) US3524318A (fr)
FR (1) FR1561980A (fr)
GB (1) GB1233718A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2551488A3 (fr) * 2011-07-29 2016-10-26 United Technologies Corporation Configuration de paliers pour moteur triple corps
EP2235329A4 (fr) * 2007-12-20 2018-02-21 GKN Aerospace Sweden AB Turbine à gaz

Families Citing this family (40)

* Cited by examiner, † Cited by third party
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US3861139A (en) * 1973-02-12 1975-01-21 Gen Electric Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
US4155684A (en) * 1975-10-17 1979-05-22 Bbc Brown Boveri & Company Limited Two-stage exhaust-gas turbocharger
US4132064A (en) * 1977-05-26 1979-01-02 The Garrett Corporation Turbine engine with differential gearing between high pressure turbine and compressor
US4159624A (en) * 1978-02-06 1979-07-03 Gruner George P Contra-rotating rotors with differential gearing
US4274261A (en) * 1978-09-25 1981-06-23 United Technologies Corporation Closed cycle contrarotating gas turbine power plant utilizing helium as the working medium
US4286430A (en) * 1979-09-17 1981-09-01 Teledyne Industries, Inc. Gas turbine engine
FR2506840A1 (fr) * 1981-05-29 1982-12-03 Onera (Off Nat Aerospatiale) Turboreacteur a roues contra-rotatives
US4790133A (en) * 1986-08-29 1988-12-13 General Electric Company High bypass ratio counterrotating turbofan engine
US4860537A (en) * 1986-08-29 1989-08-29 Brandt, Inc. High bypass ratio counterrotating gearless front fan engine
US4916894A (en) * 1989-01-03 1990-04-17 General Electric Company High bypass turbofan engine having a partially geared fan drive turbine
US4969325A (en) * 1989-01-03 1990-11-13 General Electric Company Turbofan engine having a counterrotating partially geared fan drive turbine
US4951461A (en) * 1989-03-20 1990-08-28 General Electric Company Power turbine support arrangement
GB2232720B (en) * 1989-06-15 1993-11-10 Rolls Royce Business Ventures Gas turbine engine power unit
DE4122008A1 (de) * 1991-07-03 1993-01-14 Mtu Muenchen Gmbh Propfantriebwerk mit gegenlaeufigem niederdruckverdichter (booster)
GB2288640B (en) * 1994-04-16 1998-08-12 Rolls Royce Plc A gas turbine engine
US6711887B2 (en) * 2002-08-19 2004-03-30 General Electric Co. Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines
GB2401651B (en) * 2003-05-14 2006-03-01 Rolls Royce Plc A gas turbine engine
GB0502324D0 (en) * 2005-03-14 2005-03-16 Rolls Royce Plc A multi-shaft arrangement for a turbine engine
US20100229568A1 (en) * 2007-08-02 2010-09-16 Kevork Nercessian Gas turbine engine
US20100126178A1 (en) * 2008-10-08 2010-05-27 Searete Llc, A Limited Liability Corporation Of The State Of Delaware Hybrid propulsive engine including at least one independently rotatable turbine stator
US8549833B2 (en) * 2008-10-08 2013-10-08 The Invention Science Fund I Llc Hybrid propulsive engine including at least one independently rotatable compressor stator
IT1401662B1 (it) * 2010-08-27 2013-08-02 Nuova Pignone S R L Dispositivo espansore multistadio assiale con ingranaggi, sistema e metodo.
US9938898B2 (en) 2011-07-29 2018-04-10 United Technologies Corporation Geared turbofan bearing arrangement
US9534608B2 (en) 2012-02-17 2017-01-03 Embry-Riddle Aeronautical University, Inc. Multi-stage axial compressor with counter-rotation
US9353754B2 (en) 2012-03-13 2016-05-31 Embry-Riddle Aeronautical University, Inc. Multi-stage axial compressor with counter-rotation using accessory drive
KR20140125894A (ko) * 2013-03-26 2014-10-30 두산중공업 주식회사 가스 터빈 장치
US9528706B2 (en) * 2013-12-13 2016-12-27 Siemens Energy, Inc. Swirling midframe flow for gas turbine engine having advanced transitions
US9410430B2 (en) * 2014-06-19 2016-08-09 Jay HASKIN Turbine apparatus with counter-rotating blades
US10337401B2 (en) 2015-02-13 2019-07-02 United Technologies Corporation Turbine engine with a turbo-compressor
US10125722B2 (en) 2015-02-13 2018-11-13 United Technologies Corporation Turbine engine with a turbo-compressor
US10100731B2 (en) * 2015-02-13 2018-10-16 United Technologies Corporation Turbine engine with a turbo-compressor
WO2017041197A1 (fr) * 2015-09-09 2017-03-16 苏犁 Combinaison de turbine du type à transmission à multiples douilles et à ventilateur à roue de rotation bidirectionnelle et de compresseur de gaz du type à ventilateur à roue à douille
CN105507954B (zh) * 2015-12-29 2017-04-05 中国航空工业集团公司沈阳发动机设计研究所 一种发动机叶片角度控制系统
US9745860B1 (en) * 2016-11-02 2017-08-29 Jay HASKIN Power transmission system for turbine or compressor having counter-rotating blades
US10260367B2 (en) 2016-11-02 2019-04-16 Jay HASKIN Power transmission system for turbines or compressors having counter-rotating blades
US10677159B2 (en) * 2017-10-27 2020-06-09 General Electric Company Gas turbine engine including a dual-speed split compressor
JP7059028B2 (ja) * 2018-02-01 2022-04-25 本田技研工業株式会社 ガスタービンエンジン
EP3578763A1 (fr) 2018-06-07 2019-12-11 Haskin, Jay Système de transmission de puissance pour turbine, turbocompresseur, compresseur ou pompe
US11549463B2 (en) 2021-02-22 2023-01-10 General Electric Company Compact low-pressure compressor
CN113503264A (zh) * 2021-07-22 2021-10-15 浙江华擎航空发动机科技有限公司 一种采用组合轴系结构的多级压气机

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430399A (en) * 1942-11-05 1947-11-04 Armstrong Siddeley Motors Ltd Jet augmenter for combustion turbine propulsion plants
FR1514932A (fr) * 1965-06-24 1968-03-01 Snecma Compresseur axial à double rotor contrarotatif
FR1455278A (fr) * 1965-08-05 1966-04-01 Snecma Turboréacteur à double flux
US3465524A (en) * 1966-03-02 1969-09-09 Rolls Royce Fan gas turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2235329A4 (fr) * 2007-12-20 2018-02-21 GKN Aerospace Sweden AB Turbine à gaz
EP2551488A3 (fr) * 2011-07-29 2016-10-26 United Technologies Corporation Configuration de paliers pour moteur triple corps

Also Published As

Publication number Publication date
US3524318A (en) 1970-08-18
DE1814367A1 (de) 1969-07-26
DE1814367B2 (de) 1976-10-28
GB1233718A (fr) 1971-05-26

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Legal Events

Date Code Title Description
ST Notification of lapse