FR2657121B1 - Turbo-soufflante a deux rotors de soufflante tournant en sens opposes. - Google Patents
Turbo-soufflante a deux rotors de soufflante tournant en sens opposes.Info
- Publication number
- FR2657121B1 FR2657121B1 FR909015832A FR9015832A FR2657121B1 FR 2657121 B1 FR2657121 B1 FR 2657121B1 FR 909015832 A FR909015832 A FR 909015832A FR 9015832 A FR9015832 A FR 9015832A FR 2657121 B1 FR2657121 B1 FR 2657121B1
- Authority
- FR
- France
- Prior art keywords
- blower
- turbo
- opposite direction
- rotors rotating
- rotating
- 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 - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
- B64D35/06—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors the propellers or rotors being counter-rotating
-
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3941852A DE3941852A1 (de) | 1989-12-19 | 1989-12-19 | Propfantriebwerk mit zwei entgegengesetzt drehenden fanrotoren |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2657121A1 FR2657121A1 (fr) | 1991-07-19 |
FR2657121B1 true FR2657121B1 (fr) | 1994-09-02 |
Family
ID=6395760
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR909015832A Expired - Fee Related FR2657121B1 (fr) | 1989-12-19 | 1990-12-18 | Turbo-soufflante a deux rotors de soufflante tournant en sens opposes. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5137425A (fr) |
DE (1) | DE3941852A1 (fr) |
FR (1) | FR2657121B1 (fr) |
GB (1) | GB2240591B (fr) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AUPO735397A0 (en) * | 1997-06-13 | 1997-07-10 | Cameron, Ron | Contra-rotating ducted impellers |
DE19828562B4 (de) * | 1998-06-26 | 2005-09-08 | Mtu Aero Engines Gmbh | Triebwerk mit gegenläufig drehenden Rotoren |
US7513103B2 (en) * | 2005-10-19 | 2009-04-07 | General Electric Company | Gas turbine engine assembly and methods of assembling same |
US7752836B2 (en) * | 2005-10-19 | 2010-07-13 | General Electric Company | Gas turbine assembly and methods of assembling same |
US7685808B2 (en) * | 2005-10-19 | 2010-03-30 | General Electric Company | Gas turbine engine assembly and methods of assembling same |
US7526913B2 (en) * | 2005-10-19 | 2009-05-05 | General Electric Company | Gas turbine engine assembly and methods of assembling same |
US7966806B2 (en) * | 2006-10-31 | 2011-06-28 | General Electric Company | Turbofan engine assembly and method of assembling same |
FR2928977B1 (fr) * | 2008-03-21 | 2010-04-09 | Snecma | Systeme d'helices contrarotatives disposant d'un dispositif de mise en drapeau des pales d'helices |
US10669946B2 (en) | 2015-06-05 | 2020-06-02 | Raytheon Technologies Corporation | Geared architecture for a gas turbine engine |
FR3087849B1 (fr) * | 2018-10-26 | 2020-11-20 | Safran Aircraft Engines | Turbomachine a double helices non carenees |
GB201820919D0 (en) | 2018-12-21 | 2019-02-06 | Rolls Royce Plc | Turbine engine |
US11204037B2 (en) | 2018-12-21 | 2021-12-21 | Rolls-Royce Plc | Turbine engine |
GB201820925D0 (en) * | 2018-12-21 | 2019-02-06 | Rolls Royce Plc | Turbine engine |
GB201820924D0 (en) | 2018-12-21 | 2019-02-06 | Rolls Royce Plc | Turbine engine |
DE102019128081A1 (de) * | 2019-10-17 | 2021-04-22 | Rolls-Royce Deutschland Ltd & Co Kg | Planetengetriebe und Gasturbinentriebwerk mit Planetengetriebe |
US11725590B2 (en) | 2020-10-22 | 2023-08-15 | General Electric Company | Turbomachine and gear assembly |
US11873767B2 (en) | 2021-10-22 | 2024-01-16 | Ge Avio S.R.L. | Gearbox configurations for clockwise and counterclockwise propeller rotation |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1381939A (en) * | 1919-12-15 | 1921-06-21 | Robert E Small | Propelling mechanism |
US1879142A (en) * | 1930-02-17 | 1932-09-27 | Mathew M Egan | Propeller |
US1881080A (en) * | 1930-12-04 | 1932-10-04 | William D Hubert | Aircraft propeller |
US2050283A (en) * | 1934-05-19 | 1936-08-11 | Jr Harry V Dixon | Propeller driving mechanism |
FR998574A (fr) * | 1945-11-02 | 1952-01-21 | Perfectionnement aux hélices coaxiales à pas variables | |
US4237751A (en) * | 1978-08-11 | 1980-12-09 | Davis Roland O | Motion transmitting device |
US4251987A (en) * | 1979-08-22 | 1981-02-24 | General Electric Company | Differential geared engine |
GB2180892B (en) * | 1985-09-28 | 1990-03-07 | Dowty Rotol Ltd | A control system for a bladed rotor assembly |
GB2182397B (en) * | 1985-11-02 | 1989-10-04 | Rolls Royce Plc | Propeller module for an aero gas turbine engine |
GB2186918B (en) * | 1986-02-25 | 1989-11-15 | Rolls Royce | Propeller module for an aero gas turbine engine |
DE3714990A1 (de) * | 1987-05-06 | 1988-12-01 | Mtu Muenchen Gmbh | Propfan-turbotriebwerk |
GB2209575A (en) * | 1987-09-05 | 1989-05-17 | Rolls Royce Plc | A gearbox arrangement for driving contra-rotating multi-bladed rotors |
DE3812027A1 (de) * | 1988-04-11 | 1989-10-26 | Mtu Muenchen Gmbh | Propfan-turbotriebwerk |
US4936746A (en) * | 1988-10-18 | 1990-06-26 | United Technologies Corporation | Counter-rotation pitch change system |
DE3837994A1 (de) * | 1988-11-09 | 1990-05-10 | Mtu Muenchen Gmbh | Vorrichtung zur verstellung der rotorschaufeln eines propfan/turboproptriebwerkes |
US5010729A (en) * | 1989-01-03 | 1991-04-30 | General Electric Company | Geared counterrotating turbine/fan propulsion system |
GB2231623B (en) * | 1989-05-17 | 1993-10-20 | Rolls Royce Plc | A variable pitch propeller module for an aero gas turbine engine powerplant |
JPH0727277Y2 (ja) * | 1989-08-28 | 1995-06-21 | 石川島播磨重工業株式会社 | 二重反転軸の動力伝達装置 |
-
1989
- 1989-12-19 DE DE3941852A patent/DE3941852A1/de active Granted
-
1990
- 1990-12-06 US US07/628,181 patent/US5137425A/en not_active Expired - Lifetime
- 1990-12-18 FR FR909015832A patent/FR2657121B1/fr not_active Expired - Fee Related
- 1990-12-19 GB GB9027493A patent/GB2240591B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE3941852A1 (de) | 1991-06-20 |
GB9027493D0 (en) | 1991-02-06 |
DE3941852C2 (fr) | 1992-11-05 |
GB2240591B (en) | 1993-09-22 |
US5137425A (en) | 1992-08-11 |
FR2657121A1 (fr) | 1991-07-19 |
GB2240591A (en) | 1991-08-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20060831 |