FR2922265B1 - Turboreacteur incorporant un generateur de courant electrique. - Google Patents
Turboreacteur incorporant un generateur de courant electrique.Info
- Publication number
- FR2922265B1 FR2922265B1 FR0707187A FR0707187A FR2922265B1 FR 2922265 B1 FR2922265 B1 FR 2922265B1 FR 0707187 A FR0707187 A FR 0707187A FR 0707187 A FR0707187 A FR 0707187A FR 2922265 B1 FR2922265 B1 FR 2922265B1
- Authority
- FR
- France
- Prior art keywords
- current generator
- electric current
- generator
- turboreactor
- incorporating
- 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.)
- Active
Links
Classifications
-
- 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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0707187A FR2922265B1 (fr) | 2007-10-12 | 2007-10-12 | Turboreacteur incorporant un generateur de courant electrique. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0707187A FR2922265B1 (fr) | 2007-10-12 | 2007-10-12 | Turboreacteur incorporant un generateur de courant electrique. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2922265A1 FR2922265A1 (fr) | 2009-04-17 |
FR2922265B1 true FR2922265B1 (fr) | 2013-11-22 |
Family
ID=39387751
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0707187A Active FR2922265B1 (fr) | 2007-10-12 | 2007-10-12 | Turboreacteur incorporant un generateur de courant electrique. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2922265B1 (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3087819B1 (fr) | 2018-10-26 | 2020-11-13 | Safran Aircraft Engines | Turbomachine d'aeronef equipee d'une machine electrique |
FR3087820B1 (fr) | 2018-10-26 | 2020-10-16 | Safran Aircraft Engines | Turbomachine d'aeronef equipee d'une machine electrique |
FR3103853B1 (fr) | 2019-12-03 | 2021-11-05 | Safran Aircraft Engines | Raccordement electrique d’une machine electrique dans une turbomachine d’aeronef |
FR3103851B1 (fr) | 2019-12-03 | 2021-11-05 | Safran Aircraft Engines | Barre rigide pour le raccordement electrique d’une machine dans une turbomachine d’aeronef |
FR3103852B1 (fr) | 2019-12-03 | 2021-10-22 | Safran Aircraft Engines | Module electrique pour une turbomachine d’aeronef |
FR3103854B1 (fr) | 2019-12-03 | 2022-01-28 | Safran Aircraft Engines | Raccordement electrique d’une machine electrique dans une turbomachine d’aeronef |
FR3108654B1 (fr) | 2020-03-25 | 2022-03-04 | Safran Aircraft Engines | Turbomachine d’aeronef equipee d’une machine electrique |
FR3114351B1 (fr) | 2020-09-18 | 2022-08-12 | Safran Aircraft Engines | Raccordement electrique d’une machine electrique dans une turbomachine d’aeronef |
FR3124543B1 (fr) | 2021-06-23 | 2023-05-12 | Safran Aircraft Engines | Turbomachine d’aeronef equipee d’une machine electrique |
FR3124544A1 (fr) | 2021-06-23 | 2022-12-30 | Safran Aircraft Engines | Turbomachine comprenant un carter sectorisé |
FR3129427A1 (fr) | 2021-11-22 | 2023-05-26 | Safran Aircraft Engines | Carter d’echappement comportant un bras creux traverse par un element conducteur de transmission de puissance |
FR3129537B1 (fr) | 2021-11-22 | 2023-12-01 | Safran Aircraft Engines | Systeme de connexion electrique protegee par boitier imperdable |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1268437B (de) * | 1962-08-27 | 1968-05-16 | Bristol Siddeley Engines Ltd | Gasturbinentriebwerk |
GB1174969A (en) * | 1967-10-20 | 1969-12-17 | Rolls Royce | Gas Turbine Engine Provided with an Alternator |
US3900274A (en) * | 1974-06-25 | 1975-08-19 | Gen Electric | Remote controlled actuation system for the rotor of a gas turbine engine |
US5282719A (en) * | 1991-05-13 | 1994-02-01 | Alliedsignal Inc. | Quad mode fan pitch actuation system for a gas turbine engine |
FR2712250B1 (fr) * | 1993-11-10 | 1995-12-29 | Hispano Suiza Sa | Procédé et dispositif de commande de variation du pas des pales d'un rotor. |
EP1841960B1 (fr) * | 2004-12-01 | 2011-05-25 | United Technologies Corporation | Ailettes de rotor de soufflante pour moteur a turbine en bout |
-
2007
- 2007-10-12 FR FR0707187A patent/FR2922265B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2922265A1 (fr) | 2009-04-17 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 15 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |