JP2012516407A - Agbと油タンクとを含むアセンブリ - Google Patents
Agbと油タンクとを含むアセンブリ Download PDFInfo
- Publication number
- JP2012516407A JP2012516407A JP2011546860A JP2011546860A JP2012516407A JP 2012516407 A JP2012516407 A JP 2012516407A JP 2011546860 A JP2011546860 A JP 2011546860A JP 2011546860 A JP2011546860 A JP 2011546860A JP 2012516407 A JP2012516407 A JP 2012516407A
- Authority
- JP
- Japan
- Prior art keywords
- compartment
- agb
- assembly according
- assembly
- gearbox
- 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.)
- Granted
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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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/18—Lubricating arrangements
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- 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
- 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
- F05D2250/312—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being parallel to each other
-
- 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)
- General Details Of Gearings (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
Abstract
Description
Claims (10)
- ターボジェットエンジン用の補機(9a〜9f)ギアボックス(1)であって、補機(9a〜9f)を機械的に駆動する互いに平行なシャフト(8a〜8f)に接続されるギア装置(7)を備える補機(9a〜9f)ギアボックス(1)と、潤滑油の貯留槽(2)とを備えるアセンブリであって、2つの隔室(5a、5b)と前記シャフト(8a〜8f)に垂直な1つの隔壁(6)であって、隔室(5a、5b)を仕切る隔壁(6)とを有するボックス(4)を備え、1つの隔室(5a)が補機(9a〜9f)ギアボックス(1)を形成し、1つの隔室(5b)が潤滑油貯留槽(2)を形成することを特徴とする、アセンブリ。
- ボックス(4)が、取り付けられることが意図されるターボジェットエンジンの円筒状ケーシングの形状に沿うように設計された曲面形状である、請求項1に記載のアセンブリ。
- 全体に軸に沿って伸びるターボジェットエンジンでは、補機(9a〜9f)ギアボックス(1)のギア装置(7)が、ターボジェットエンジンの軸にほぼ垂直な動力取出シャフトによって駆動されるように作られる、請求項3に記載のアセンブリ。
- 隔室(5a、5b)が、金属製中実ブロックからの機械加工によって製造される、請求項1から3の一項に記載のアセンブリ。
- 隔室(5a、5b)が、互いに固定される2つの半シェル(4a、4b)で形成される、請求項1から4の一項に記載のアセンブリ。
- 半シェル(4a、4b)が、好ましくは、隔壁と共に取り外し可能に、例えば、ねじ留めによって互いに固定される、請求項5に記載のアセンブリ。
- 隔壁(6)が、油貯留槽(2)を形成する半シェル(4b)に取り外し不可能に固定される、例えば、溶接される、請求項5または6に記載のアセンブリ。
- ボックス(4)が、補機(9a〜9f)駆動シャフト(8a〜8f)にほぼ垂直な方向に略細長形状である、請求項1から7の一項に記載のアセンブリ。
- 潤滑油貯留槽(2)を形成する隔室(5b)が、補機(9a〜9f)ギアボックス(1)によって駆動される少なくともいくつかの補機(9a、9c、9e)の支持体の役割を果たす、請求項1から8の一項に記載のアセンブリ。
- 貯留槽(2)を形成する隔室(5b)まで少なくとも部分的に伸びる前記補機(9c、9e)を駆動する駆動シャフト(8c、8e)と共に、前記シャフト(8c、8e)の周囲の保護管(8c’’、8e’’)が貯留槽(2)内に取り付けられる、請求項9に記載のアセンブリ。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0950617 | 2009-01-30 | ||
FR0950617A FR2941744B1 (fr) | 2009-01-30 | 2009-01-30 | Ensemble d'un boitier de relais d'accessoires et d'un reservoir d'huile |
PCT/EP2010/051122 WO2010086422A1 (fr) | 2009-01-30 | 2010-01-29 | Ensemble d'un agb et d'un reservoir d'huile |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2012516407A true JP2012516407A (ja) | 2012-07-19 |
JP5479495B2 JP5479495B2 (ja) | 2014-04-23 |
Family
ID=41060236
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2011546860A Expired - Fee Related JP5479495B2 (ja) | 2009-01-30 | 2010-01-29 | Agbと油タンクとを含むアセンブリ |
Country Status (11)
Country | Link |
---|---|
US (1) | US8905191B2 (ja) |
EP (1) | EP2391803B1 (ja) |
JP (1) | JP5479495B2 (ja) |
CN (1) | CN102301097B (ja) |
BR (1) | BRPI1007421B1 (ja) |
CA (1) | CA2750490C (ja) |
ES (1) | ES2600517T3 (ja) |
FR (1) | FR2941744B1 (ja) |
PL (1) | PL2391803T3 (ja) |
RU (1) | RU2538373C2 (ja) |
WO (1) | WO2010086422A1 (ja) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2017503964A (ja) * | 2014-01-16 | 2017-02-02 | イスパノ スイザ | アクセサリ・ギアボックス |
JP2017508915A (ja) * | 2014-02-18 | 2017-03-30 | サフラン・トランスミッション・システムズ | タービンエンジン用装置を駆動するための筐体 |
Families Citing this family (36)
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---|---|---|---|---|
EP2696058B1 (en) * | 2011-04-07 | 2017-10-11 | Kawasaki Jukogyo Kabushiki Kaisha | Aircraft with a generator apparatus |
US9926849B2 (en) * | 2011-06-14 | 2018-03-27 | Honeywell International Inc. | Transverse mounted accessory gearbox |
FR2977280B1 (fr) * | 2011-06-28 | 2015-04-10 | Hispano Suiza Sa | Boitier perfectionne de relais d'accessoires d'une turbine a gaz |
FR2981986B1 (fr) * | 2011-10-26 | 2016-03-04 | Snecma | Boitier d'entrainement d'accessoires pour turboreacteur |
US9068515B2 (en) * | 2011-12-07 | 2015-06-30 | United Technologies Corporation | Accessory gearbox with tower shaft removal capability |
FR2998498B1 (fr) * | 2012-11-27 | 2014-11-14 | Hispano Suiza Sa | Procede de realisation d'un carter de transmission de puissance |
WO2014130239A2 (en) | 2013-02-25 | 2014-08-28 | United Technologies Corporation | Auxiliary lubricant supply pump stage integral with main lubricant pump stage |
FR3007462B1 (fr) * | 2013-06-21 | 2017-11-24 | Hispano-Suiza | Boitier d'accessoires de turbomachine equipe d'une pompe centrifuge |
FR3016408B1 (fr) * | 2014-01-16 | 2019-05-31 | Safran Transmission Systems | Ensemble d'entrainement d'accessoires pour turbomachine d'aeronef |
FR3021358B1 (fr) | 2014-05-23 | 2018-07-20 | Safran Aircraft Engines | Boite d'engrenages de turbomachine d'aeronef |
FR3027367B1 (fr) * | 2014-10-17 | 2018-02-09 | Safran Transmission Systems | Support d'equipement d'une turbomachine comprenant un reducteur magnetique |
US9917490B2 (en) * | 2014-11-21 | 2018-03-13 | Hamilton Sundstrand Corporation | Tail cone generator with integral speed increasing gearbox |
FR3041052B1 (fr) | 2015-09-14 | 2018-07-27 | Safran Transmission Systems | Boitier d'entrainement d'equipements dans une turbomachine |
US10072582B2 (en) * | 2016-04-28 | 2018-09-11 | General Electric Company | Integral offset oil tank for inline accessory gearbox |
US11415063B2 (en) | 2016-09-15 | 2022-08-16 | Pratt & Whitney Canada Corp. | Reverse-flow gas turbine engine |
US10883424B2 (en) | 2016-07-19 | 2021-01-05 | Pratt & Whitney Canada Corp. | Multi-spool gas turbine engine architecture |
US10676205B2 (en) * | 2016-08-19 | 2020-06-09 | General Electric Company | Propulsion engine for an aircraft |
US10465611B2 (en) | 2016-09-15 | 2019-11-05 | Pratt & Whitney Canada Corp. | Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool |
US11035293B2 (en) | 2016-09-15 | 2021-06-15 | Pratt & Whitney Canada Corp. | Reverse flow gas turbine engine with offset RGB |
US10815899B2 (en) | 2016-11-15 | 2020-10-27 | Pratt & Whitney Canada Corp. | Gas turbine engine accessories arrangement |
FR3059361B1 (fr) * | 2016-11-28 | 2018-12-07 | Safran Aircraft Engines | Reservoir d'huile comprenant un dispositif de controle du niveau d'huile |
US10808624B2 (en) | 2017-02-09 | 2020-10-20 | Pratt & Whitney Canada Corp. | Turbine rotor with low over-speed requirements |
US10746188B2 (en) | 2017-03-14 | 2020-08-18 | Pratt & Whitney Canada Corp. | Inter-shaft bearing connected to a compressor boost system |
FR3070726B1 (fr) * | 2017-09-07 | 2019-08-23 | Safran Transmission Systems | Boitier d'accessoires pour turbomachine |
RU186180U1 (ru) * | 2018-06-06 | 2019-01-11 | Публичное акционерное общество "МОТОР СИЧ" | Узел соединения входного устройства и коробки приводов турбовинтового двигателя |
GB201811219D0 (en) * | 2018-07-09 | 2018-08-29 | Rolls Royce Plc | Apparatus for gas turbine engines |
US11536153B2 (en) | 2018-08-08 | 2022-12-27 | Pratt & Whitney Canada Corp. | Turboshaft gas turbine engine |
FR3086974B1 (fr) | 2018-10-04 | 2021-01-08 | Safran Trans Systems | Boitier d'engrenages de turbomachine |
US11261795B2 (en) | 2018-10-18 | 2022-03-01 | Rolls-Royce North American Technologies, Inc. | Dual mode starter generator |
US11008945B2 (en) | 2018-10-18 | 2021-05-18 | Rolls-Royce North American Technologies, Inc. | Accessory gearbox with oppositely disposed starter/generator and air turbine starter |
CA3053117A1 (en) * | 2018-10-18 | 2020-04-18 | Rolls-Royce North American Technologies Inc. | Dual mode starter generator |
FR3095832B1 (fr) | 2019-05-10 | 2021-05-21 | Safran Aircraft Engines | Système huile pour turbomachine |
FR3104640B1 (fr) * | 2019-12-13 | 2021-12-10 | Safran Aircraft Engines | Platine d’équipements hydrauliques de turbomachine aéronautique |
FR3106155B1 (fr) | 2020-01-09 | 2022-07-15 | Safran Aircraft Engines | Système de lubrification d’engrenages pour une turbomachine d’aéronef |
US11572838B2 (en) * | 2020-09-29 | 2023-02-07 | General Electric Company | Accessory gearbox for a turbine engine |
FR3139864A1 (fr) * | 2022-09-20 | 2024-03-22 | Safran Transmission Systems | Boitier d’accessoires compact comportant une machine electrique integree |
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US3152443A (en) * | 1959-07-17 | 1964-10-13 | United Aircraft Canada | Gas turbine powerplant |
JPS52129805U (ja) * | 1976-03-31 | 1977-10-03 | ||
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US20050279102A1 (en) * | 2004-06-17 | 2005-12-22 | Pratt & Whitney Canada Corp. | Modulated current gas turbine engine starting system |
JP2008185033A (ja) * | 2007-01-30 | 2008-08-14 | Hispano Suiza | ギアボックスに取り付けられた始動装置を組み込んだガスタービンエンジン |
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-
2009
- 2009-01-30 FR FR0950617A patent/FR2941744B1/fr active Active
-
2010
- 2010-01-29 RU RU2011135971/06A patent/RU2538373C2/ru active
- 2010-01-29 US US13/146,944 patent/US8905191B2/en active Active
- 2010-01-29 JP JP2011546860A patent/JP5479495B2/ja not_active Expired - Fee Related
- 2010-01-29 PL PL10701690T patent/PL2391803T3/pl unknown
- 2010-01-29 BR BRPI1007421-0A patent/BRPI1007421B1/pt not_active IP Right Cessation
- 2010-01-29 WO PCT/EP2010/051122 patent/WO2010086422A1/fr active Application Filing
- 2010-01-29 ES ES10701690.9T patent/ES2600517T3/es active Active
- 2010-01-29 CN CN201080005718.XA patent/CN102301097B/zh active Active
- 2010-01-29 EP EP10701690.9A patent/EP2391803B1/fr active Active
- 2010-01-29 CA CA2750490A patent/CA2750490C/fr not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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US3152443A (en) * | 1959-07-17 | 1964-10-13 | United Aircraft Canada | Gas turbine powerplant |
JPS52129805U (ja) * | 1976-03-31 | 1977-10-03 | ||
US4779413A (en) * | 1986-11-20 | 1988-10-25 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Starter lubrication system for a turbine plant |
US20030059295A1 (en) * | 2001-09-26 | 2003-03-27 | Olsen Andrew J. | Interchangeable power turbine cartridge assembly |
US20050279102A1 (en) * | 2004-06-17 | 2005-12-22 | Pratt & Whitney Canada Corp. | Modulated current gas turbine engine starting system |
JP2008185033A (ja) * | 2007-01-30 | 2008-08-14 | Hispano Suiza | ギアボックスに取り付けられた始動装置を組み込んだガスタービンエンジン |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2017503964A (ja) * | 2014-01-16 | 2017-02-02 | イスパノ スイザ | アクセサリ・ギアボックス |
JP2017508915A (ja) * | 2014-02-18 | 2017-03-30 | サフラン・トランスミッション・システムズ | タービンエンジン用装置を駆動するための筐体 |
Also Published As
Publication number | Publication date |
---|---|
BRPI1007421B1 (pt) | 2020-10-27 |
CA2750490A1 (fr) | 2010-08-05 |
BRPI1007421A2 (pt) | 2016-02-16 |
ES2600517T3 (es) | 2017-02-09 |
RU2011135971A (ru) | 2013-03-10 |
US8905191B2 (en) | 2014-12-09 |
EP2391803B1 (fr) | 2016-07-27 |
RU2538373C2 (ru) | 2015-01-10 |
JP5479495B2 (ja) | 2014-04-23 |
CA2750490C (fr) | 2016-11-08 |
US20110284328A1 (en) | 2011-11-24 |
CN102301097A (zh) | 2011-12-28 |
FR2941744A1 (fr) | 2010-08-06 |
EP2391803A1 (fr) | 2011-12-07 |
PL2391803T3 (pl) | 2017-01-31 |
CN102301097B (zh) | 2015-07-01 |
FR2941744B1 (fr) | 2011-09-16 |
WO2010086422A1 (fr) | 2010-08-05 |
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