CH418733A - Nebenstromgasturbinentriebwerk - Google Patents
NebenstromgasturbinentriebwerkInfo
- Publication number
- CH418733A CH418733A CH657363A CH657363A CH418733A CH 418733 A CH418733 A CH 418733A CH 657363 A CH657363 A CH 657363A CH 657363 A CH657363 A CH 657363A CH 418733 A CH418733 A CH 418733A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- turbine engine
- bypass gas
- bypass
- engine
- Prior art date
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
- F02K3/06—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 fan
-
- 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
- F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
-
- 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
- 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
- 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
- F02K3/077—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 the plant being of the multiple flow type, i.e. having three or more flows
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB21106/62A GB978658A (en) | 1962-05-31 | 1962-05-31 | Gas turbine by-pass engines |
GB3665063 | 1963-05-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH418733A true CH418733A (de) | 1966-08-15 |
Family
ID=26255145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH657363A CH418733A (de) | 1962-05-31 | 1963-05-27 | Nebenstromgasturbinentriebwerk |
Country Status (4)
Country | Link |
---|---|
US (1) | US3182898A (de) |
CH (1) | CH418733A (de) |
DE (1) | DE1428220C3 (de) |
GB (1) | GB978658A (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2506500A1 (de) * | 1974-02-25 | 1975-08-28 | Gen Electric | Turbofantriebwerk mit variablem bypass-verhaeltnis |
DE102005021446B3 (de) * | 2005-05-04 | 2006-06-29 | Technische Universität Dresden | Gasturbine |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB978462A (en) * | 1963-10-28 | 1964-12-23 | Rolls Royce | Gas turbine by-pass engine |
GB992931A (en) * | 1964-02-21 | 1965-05-26 | Rolls Royce | Gas turbine jet propulsion engine |
US3330475A (en) * | 1965-04-12 | 1967-07-11 | United Aircraft Corp | Vane construction in turbofan engine |
US3283995A (en) * | 1965-04-28 | 1966-11-08 | United Aircraft Corp | Splitter vane construction for turbofan engine |
GB1436796A (en) * | 1972-08-22 | 1976-05-26 | Mtu Muenchen Gmbh | Gas turbine ducted fan engines of multi-shaft and multi-flow construction |
US4043121A (en) * | 1975-01-02 | 1977-08-23 | General Electric Company | Two-spool variable cycle engine |
GB1535765A (en) * | 1975-01-02 | 1978-12-13 | Gen Electric | Variable cycle turbofan engines |
US4240250A (en) * | 1977-12-27 | 1980-12-23 | The Boeing Company | Noise reducing air inlet for gas turbine engines |
US4704862A (en) * | 1985-05-29 | 1987-11-10 | United Technologies Corporation | Ducted prop engine |
FR2645911B1 (fr) * | 1989-04-18 | 1991-06-07 | Snecma | Moteur a grand taux de dilution a soufflante amont et soufflante aval |
GB2353983B (en) * | 2000-07-04 | 2003-10-15 | Adrian Alexander Hubbard | Variable mode jet engine-suitable for STOVL |
US7144221B2 (en) * | 2004-07-30 | 2006-12-05 | General Electric Company | Method and apparatus for assembling gas turbine engines |
US7225607B2 (en) * | 2004-08-27 | 2007-06-05 | Pratt & Whitney Canada Corp. | Gas turbine braking apparatus and method |
US7631484B2 (en) * | 2006-03-13 | 2009-12-15 | Rollin George Giffin | High pressure ratio aft fan |
DE102008021683A1 (de) | 2008-04-30 | 2009-11-05 | Rolls-Royce Deutschland Ltd & Co Kg | Rotierende Einheit für einen Axialkompressor |
BE1022364B1 (fr) * | 2014-10-27 | 2016-03-17 | Techspace Aero S.A. | Compresseur de turbomachine axiale avec double rotors contrarotatifs |
US9982676B2 (en) | 2014-11-18 | 2018-05-29 | Rolls-Royce North American Technologies Inc. | Split axial-centrifugal compressor |
US10329943B2 (en) | 2014-11-18 | 2019-06-25 | Rolls-Royce North American Technologies Inc. | Split axial-centrifugal compressor |
CN106567746A (zh) * | 2015-10-10 | 2017-04-19 | 熵零控股股份有限公司 | 复合流叶轮机构 |
CN105756716A (zh) * | 2016-04-22 | 2016-07-13 | 中国船舶重工集团公司第七�三研究所 | 可倒车涡轮用双层整体静叶环 |
GB201813674D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813671D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813672D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813670D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
GB201813675D0 (en) | 2018-08-22 | 2018-10-03 | Rolls Royce Plc | Turbomachine |
CN110259600A (zh) * | 2019-06-25 | 2019-09-20 | 中国航空发动机研究院 | 双外涵自适应循环发动机 |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL65557C (de) * | ||||
US2450745A (en) * | 1942-11-12 | 1948-10-05 | Vickers Electrical Co Ltd | Axial flow compressor |
US2702985A (en) * | 1944-01-31 | 1955-03-01 | Power Jets Res & Dev Ltd | Gas turbine power plant with power take-off from rotatable guide blading |
GB676769A (en) * | 1948-07-20 | 1952-08-06 | Rolls Royce | Improvements relating to gas compressor systems |
US2659528A (en) * | 1948-09-29 | 1953-11-17 | Lockheed Aircraft Corp | Gas turbine compressor system |
-
1962
- 1962-05-31 GB GB21106/62A patent/GB978658A/en not_active Expired
-
1963
- 1963-05-23 US US282788A patent/US3182898A/en not_active Expired - Lifetime
- 1963-05-27 CH CH657363A patent/CH418733A/de unknown
- 1963-05-28 DE DE1428220A patent/DE1428220C3/de not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2506500A1 (de) * | 1974-02-25 | 1975-08-28 | Gen Electric | Turbofantriebwerk mit variablem bypass-verhaeltnis |
DE102005021446B3 (de) * | 2005-05-04 | 2006-06-29 | Technische Universität Dresden | Gasturbine |
Also Published As
Publication number | Publication date |
---|---|
US3182898A (en) | 1965-05-11 |
DE1428220A1 (de) | 1969-07-17 |
DE1428220C3 (de) | 1974-05-09 |
DE1428220B2 (de) | 1973-10-04 |
GB978658A (en) | 1964-12-23 |
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