FR2976624B1 - Turbomoteur a double flux pour aeronef, a section de sortie variable du flux secondaire - Google Patents
Turbomoteur a double flux pour aeronef, a section de sortie variable du flux secondaireInfo
- Publication number
- FR2976624B1 FR2976624B1 FR1155245A FR1155245A FR2976624B1 FR 2976624 B1 FR2976624 B1 FR 2976624B1 FR 1155245 A FR1155245 A FR 1155245A FR 1155245 A FR1155245 A FR 1155245A FR 2976624 B1 FR2976624 B1 FR 2976624B1
- Authority
- FR
- France
- Prior art keywords
- flow
- turbomoteur
- variable output
- aircraft
- double
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1155245A FR2976624B1 (fr) | 2011-06-15 | 2011-06-15 | Turbomoteur a double flux pour aeronef, a section de sortie variable du flux secondaire |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1155245A FR2976624B1 (fr) | 2011-06-15 | 2011-06-15 | Turbomoteur a double flux pour aeronef, a section de sortie variable du flux secondaire |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2976624A1 FR2976624A1 (fr) | 2012-12-21 |
FR2976624B1 true FR2976624B1 (fr) | 2015-04-03 |
Family
ID=44359742
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1155245A Active FR2976624B1 (fr) | 2011-06-15 | 2011-06-15 | Turbomoteur a double flux pour aeronef, a section de sortie variable du flux secondaire |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2976624B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3077847B1 (fr) * | 2018-02-09 | 2020-02-14 | Safran Nacelles | Inverseur de poussee a volets pour ensemble propulsif d’aeronef |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1343676A (fr) * | 1962-10-09 | 1963-11-22 | Bronzavia Sa | Dispositif pour le réglage de la section de passage d'une tuyère |
US3231197A (en) * | 1964-04-17 | 1966-01-25 | Boeing Co | Expansible nozzle |
US3785567A (en) * | 1972-11-02 | 1974-01-15 | Goodrich Co B F | Movable wall for engine nozzle |
US3988889A (en) * | 1974-02-25 | 1976-11-02 | General Electric Company | Cowling arrangement for a turbofan engine |
CA2460598C (fr) * | 2001-10-23 | 2012-12-18 | The Nordam Group, Inc. | Tuyere d'echappement variable confluente |
WO2008045057A1 (fr) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Tuyère à surface de dérivation variable, du type à vessie |
FR2907421B1 (fr) * | 2006-10-19 | 2009-06-05 | Airbus France Sas | Element de panneau deformable et panneau le comprenant |
-
2011
- 2011-06-15 FR FR1155245A patent/FR2976624B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR2976624A1 (fr) | 2012-12-21 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 5 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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Year of fee payment: 8 |
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