FR3016408B1 - Ensemble d'entrainement d'accessoires pour turbomachine d'aeronef - Google Patents
Ensemble d'entrainement d'accessoires pour turbomachine d'aeronef Download PDFInfo
- Publication number
- FR3016408B1 FR3016408B1 FR1450351A FR1450351A FR3016408B1 FR 3016408 B1 FR3016408 B1 FR 3016408B1 FR 1450351 A FR1450351 A FR 1450351A FR 1450351 A FR1450351 A FR 1450351A FR 3016408 B1 FR3016408 B1 FR 3016408B1
- Authority
- FR
- France
- Prior art keywords
- accessory
- input
- drive shaft
- turbine engine
- radial drive
- 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
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 230000005540 biological transmission Effects 0.000 abstract 3
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
- 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
-
- 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
-
- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- 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
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
-
- 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
- F05D2260/00—Function
- F05D2260/40—Transmission of power
- F05D2260/403—Transmission of power through the shape of the drive components
- F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
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)
Abstract
L'invention concerne un ensemble d'entrainement d'accessoires pour turbomachine d'aéronef comprenant : - un arbre d'entrainement radial (41), - une boîte d'engrenage d'entrée (20) comprenant un pignon d'entrée propre à être fixé sur un arbre de transmission (12) reliant une turbine (11) à un compresseur (10) de la turbomachine, et un pignon de sortie solidaire de l'arbre d'entrainement radial (41), - un accessoire (51) comprenant un stator propre à être fixé à un carter (2) de la turbomachine, et un rotor monté rotatif par rapport au stator, - une boîte d'engrenage de transfert (41) comprenant un pignon d'entrée solidaire en rotation de l'arbre d'entrainement radial (41), et un pignon de sortie solidaire en rotation du rotor de l'accessoire (51), le pignon d'entrée (45) engrenant avec le pignon de sortie (46) de sorte que lorsque l'arbre de transmission (12) est entrainé en rotation, l'arbre de transmission entraine en rotation le rotor de l'accessoire (51) via la boîte d'engrenage d'entrée (20), l'arbre d'entrainement radial (41) et la boîte d'engrenage de transfert (41).
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1450351A FR3016408B1 (fr) | 2014-01-16 | 2014-01-16 | Ensemble d'entrainement d'accessoires pour turbomachine d'aeronef |
US15/111,785 US20160333793A1 (en) | 2014-01-16 | 2015-01-16 | Accessory gearbox assembly for an aircraft turbine engine |
PCT/FR2015/050115 WO2015107308A1 (fr) | 2014-01-16 | 2015-01-16 | Ensemble d'entraînement d'accessoires pour turbomachine d'aeronef |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1450351A FR3016408B1 (fr) | 2014-01-16 | 2014-01-16 | Ensemble d'entrainement d'accessoires pour turbomachine d'aeronef |
FR1450351 | 2014-01-16 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3016408A1 FR3016408A1 (fr) | 2015-07-17 |
FR3016408B1 true FR3016408B1 (fr) | 2019-05-31 |
Family
ID=50290148
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1450351A Active FR3016408B1 (fr) | 2014-01-16 | 2014-01-16 | Ensemble d'entrainement d'accessoires pour turbomachine d'aeronef |
Country Status (3)
Country | Link |
---|---|
US (1) | US20160333793A1 (fr) |
FR (1) | FR3016408B1 (fr) |
WO (1) | WO2015107308A1 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4023871A4 (fr) * | 2019-08-30 | 2023-10-18 | Kawasaki Jukogyo Kabushiki Kaisha | Moteur à turbine à gaz |
FR3107735B1 (fr) * | 2020-02-27 | 2022-02-04 | Safran Aircraft Engines | Turbomachine a double flux comprenant au moins un accessoire ou equipement |
FR3110933B1 (fr) * | 2020-05-27 | 2022-09-02 | Safran Trans Systems | Turbomachine equipee de machines electriques |
US11365706B2 (en) | 2020-11-04 | 2022-06-21 | William Todd Hodges | Turbine engine system utilizing an augmented combustion module |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5343778A (en) * | 1992-11-09 | 1994-09-06 | Alliedsignal Inc. | Multifunction secondary power system |
GB9313905D0 (en) * | 1993-07-06 | 1993-08-25 | Rolls Royce Plc | Shaft power transfer in gas turbine engines |
GB9606546D0 (en) * | 1996-03-28 | 1996-06-05 | Rolls Royce Plc | Gas turbine engine system |
US6260351B1 (en) * | 1998-12-10 | 2001-07-17 | United Technologies Corporation | Controlled spring rate gearbox mount |
GB0315894D0 (en) * | 2003-07-08 | 2003-08-13 | Rolls Royce Plc | Aircraft engine arrangement |
US7246482B2 (en) * | 2004-07-16 | 2007-07-24 | Honeywell International, Inc. | Gas turbine engine bleed air power assist system and method |
US7552582B2 (en) * | 2005-06-07 | 2009-06-30 | Honeywell International Inc. | More electric aircraft power transfer systems and methods |
US7481062B2 (en) * | 2005-12-30 | 2009-01-27 | Honeywell International Inc. | More electric aircraft starter-generator multi-speed transmission system |
US8192143B2 (en) * | 2008-05-21 | 2012-06-05 | United Technologies Corporation | Gearbox assembly |
US9121351B2 (en) * | 2008-10-30 | 2015-09-01 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine accessory system |
FR2941744B1 (fr) * | 2009-01-30 | 2011-09-16 | Hispano Suiza Sa | Ensemble d'un boitier de relais d'accessoires et d'un reservoir d'huile |
US8966911B2 (en) * | 2009-12-29 | 2015-03-03 | Rolls-Royce North American Technologies, Inc. | Turbofan engine with HP and LP power off-takes |
CN103459807B (zh) * | 2011-04-07 | 2016-08-17 | 川崎重工业株式会社 | 航空器发电装置 |
DE102011112253A1 (de) * | 2011-09-02 | 2013-03-07 | Rolls-Royce Deutschland Ltd & Co Kg | Baueinheit für ein Triebwerk eines Luftfahrzeugs |
US9062611B2 (en) * | 2011-10-19 | 2015-06-23 | United Technologies Corporation | Split accessory drive system |
DE102013114638A1 (de) * | 2013-12-20 | 2015-06-25 | Rolls-Royce Deutschland Ltd & Co Kg | Vorrichtung eines Strahltriebwerks mit wenigstens einem in einem Gehäuse angeordneten und gegenüber dem Gehäuse drehbar ausgeführten Bauteil |
-
2014
- 2014-01-16 FR FR1450351A patent/FR3016408B1/fr active Active
-
2015
- 2015-01-16 WO PCT/FR2015/050115 patent/WO2015107308A1/fr active Application Filing
- 2015-01-16 US US15/111,785 patent/US20160333793A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US20160333793A1 (en) | 2016-11-17 |
FR3016408A1 (fr) | 2015-07-17 |
WO2015107308A1 (fr) | 2015-07-23 |
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Owner name: HISPANO SUIZA, FR Effective date: 20170725 |
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