FR3061241B1 - Turbopropulseur a flux inverse - Google Patents
Turbopropulseur a flux inverse Download PDFInfo
- Publication number
- FR3061241B1 FR3061241B1 FR1663312A FR1663312A FR3061241B1 FR 3061241 B1 FR3061241 B1 FR 3061241B1 FR 1663312 A FR1663312 A FR 1663312A FR 1663312 A FR1663312 A FR 1663312A FR 3061241 B1 FR3061241 B1 FR 3061241B1
- Authority
- FR
- France
- Prior art keywords
- casing
- turbopropeller
- reverse flow
- accessories
- gas generator
- 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
- 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
- F02C6/20—Adaptations of gas-turbine plants for driving vehicles
- F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/325—Application in turbines in gas turbines to drive unshrouded, high solidity propeller
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- 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
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)
- Supercharger (AREA)
Abstract
L'invention concerne un turbopropulseur à flux inversé 300 comportant un générateur de gaz et, positionnés à l'arrière dudit générateur de gaz : - un carter d'entrée d'air 320, - un boitier d'entrainement 310 des accessoires 311 comportant un arbre d'entrée 325, - un arbre d'entrainement 340 traversant le carter d'entrée d'air 320 et entrainant en rotation l'arbre d'entrée, le turbopropulseur comportant un carter intermédiaire 314 formant une jonction entre le carter d'entrée d'air 320 et le boitier d'entrainement 310 des accessoires 311, ledit carter intermédiaire 314 comportant au moins un équipement des systèmes externes du turbopropulseur.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1663312A FR3061241B1 (fr) | 2016-12-23 | 2016-12-23 | Turbopropulseur a flux inverse |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1663312A FR3061241B1 (fr) | 2016-12-23 | 2016-12-23 | Turbopropulseur a flux inverse |
FR1663312 | 2016-12-23 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3061241A1 FR3061241A1 (fr) | 2018-06-29 |
FR3061241B1 true FR3061241B1 (fr) | 2021-01-01 |
Family
ID=58010088
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1663312A Active FR3061241B1 (fr) | 2016-12-23 | 2016-12-23 | Turbopropulseur a flux inverse |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3061241B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3116303B1 (fr) * | 2020-11-16 | 2022-10-14 | Safran Helicopter Engines | Turbomachine à propulsion hybride et aéronef comportant une telle turbomachine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2399046A (en) * | 1940-03-26 | 1946-04-23 | Gen Electric | Gas turbine power plant |
US2546420A (en) * | 1944-03-28 | 1951-03-27 | Power Jets Res & Dev Ltd | Internal-combustion turbine power plant |
GB603283A (en) * | 1946-06-27 | 1948-06-11 | Power Jets Res & Dev Ltd | Improvements in or relating to internal combustion turbine power plants |
US3152443A (en) * | 1959-07-17 | 1964-10-13 | United Aircraft Canada | Gas turbine powerplant |
-
2016
- 2016-12-23 FR FR1663312A patent/FR3061241B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3061241A1 (fr) | 2018-06-29 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20180629 |
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Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |