FR1516321A - Moteur pour hélicoptères - Google Patents
Moteur pour hélicoptèresInfo
- Publication number
- FR1516321A FR1516321A FR96169A FR96169A FR1516321A FR 1516321 A FR1516321 A FR 1516321A FR 96169 A FR96169 A FR 96169A FR 96169 A FR96169 A FR 96169A FR 1516321 A FR1516321 A FR 1516321A
- Authority
- FR
- France
- Prior art keywords
- helicopters
- engine
- 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
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- 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
-
- 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
- F02K3/025—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 by-pass flow being at least partly used to create an independent thrust component
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB31208/66A GB1108454A (en) | 1966-07-12 | 1966-07-12 | Improvements in or relating to gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1516321A true FR1516321A (fr) | 1968-03-08 |
Family
ID=10319639
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR96169A Expired FR1516321A (fr) | 1966-07-12 | 1967-02-23 | Moteur pour hélicoptères |
Country Status (4)
Country | Link |
---|---|
US (1) | US3375996A (fr) |
DE (1) | DE1626109A1 (fr) |
FR (1) | FR1516321A (fr) |
GB (1) | GB1108454A (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2195548A1 (fr) * | 1972-08-14 | 1974-03-08 | Mtu Muenchen Gmbh | |
FR3055357A1 (fr) * | 2016-08-30 | 2018-03-02 | Guillaume Pelcot | Turbomachine a deux turbines motrices libres de travail et independantes l'une de l'autre ainsi que son dispositif unique de permutation entre ses deux modes de fonctionnement reversibles |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1481610A1 (de) * | 1966-07-02 | 1969-04-03 | Man Turbo Gmbh | Hubschrauberantrieb |
GB1120658A (en) * | 1967-04-20 | 1968-07-24 | Rolls Royce | Power plant for a helicopter |
US3449914A (en) * | 1967-12-21 | 1969-06-17 | United Aircraft Corp | Variable flow turbofan engine |
US3520138A (en) * | 1969-02-27 | 1970-07-14 | United Aircraft Corp | Convertible enginf |
US4899957A (en) * | 1971-03-08 | 1990-02-13 | Karl Eickmann | Air borne craft, for example helicopter, and related devices |
US3893638A (en) * | 1974-02-14 | 1975-07-08 | Boeing Co | Dual cycle fan jet engine for stol aircraft with augmentor wings |
DE2410139C3 (de) * | 1974-03-02 | 1981-10-15 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Gasturbinenanlage |
GB2130984B (en) * | 1982-12-01 | 1986-07-02 | Rolls Royce | Compound helicopter and power plant therefor |
US4610410A (en) * | 1983-07-22 | 1986-09-09 | Rolls-Royce Limited | Compound helicopter and powerplant therefor |
GB8927785D0 (en) * | 1989-12-08 | 1990-05-30 | Westland Helicopters | Helicopters |
US5485717A (en) * | 1994-06-29 | 1996-01-23 | Williams International Corporation | Multi-spool by-pass turbofan engine |
US7246482B2 (en) * | 2004-07-16 | 2007-07-24 | Honeywell International, Inc. | Gas turbine engine bleed air power assist system and method |
FR2912782B1 (fr) * | 2007-02-19 | 2009-05-22 | Snecma Sa | Procede de prelevement d'energie auxiliaire sur un turboreacteur d'avion et turboreacteur equipe pour mettre en oeuvre un tel procede |
DE102008024022A1 (de) * | 2008-05-16 | 2009-11-19 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinentriebwerk, insbesondere Flugtriebwerk |
JP2010185363A (ja) * | 2009-02-12 | 2010-08-26 | Toyota Motor Corp | ターボファンエンジン |
CN112081684A (zh) * | 2019-06-12 | 2020-12-15 | 程浩鹏 | 一种喷气风扇发动机 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2650666A (en) * | 1946-07-25 | 1953-09-01 | Dorand Rene | Rotary-wing aircraft with jet-driven rotor |
US2941749A (en) * | 1955-04-06 | 1960-06-21 | United Aircraft Corp | Jet propelled convertiplane with jet driven rotor |
GB1003734A (en) * | 1963-08-22 | 1965-09-08 | Rolls Royce | Improvements in gas turbine engines of the by-pass type |
-
1966
- 1966-07-12 GB GB31208/66A patent/GB1108454A/en not_active Expired
-
1967
- 1967-02-16 US US616629A patent/US3375996A/en not_active Expired - Lifetime
- 1967-02-22 DE DE19671626109 patent/DE1626109A1/de active Pending
- 1967-02-23 FR FR96169A patent/FR1516321A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2195548A1 (fr) * | 1972-08-14 | 1974-03-08 | Mtu Muenchen Gmbh | |
FR3055357A1 (fr) * | 2016-08-30 | 2018-03-02 | Guillaume Pelcot | Turbomachine a deux turbines motrices libres de travail et independantes l'une de l'autre ainsi que son dispositif unique de permutation entre ses deux modes de fonctionnement reversibles |
Also Published As
Publication number | Publication date |
---|---|
US3375996A (en) | 1968-04-02 |
DE1626109A1 (de) | 1971-03-11 |
GB1108454A (en) | 1968-04-03 |
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