PL3073103T3 - Przekładnia redukcyjna do silnika turbogazowego - Google Patents
Przekładnia redukcyjna do silnika turbogazowegoInfo
- Publication number
- PL3073103T3 PL3073103T3 PL16162598T PL16162598T PL3073103T3 PL 3073103 T3 PL3073103 T3 PL 3073103T3 PL 16162598 T PL16162598 T PL 16162598T PL 16162598 T PL16162598 T PL 16162598T PL 3073103 T3 PL3073103 T3 PL 3073103T3
- Authority
- PL
- Poland
- Prior art keywords
- gas turbine
- turbine engine
- reduction gearbox
- gearbox
- reduction
- Prior art date
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
- 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
- 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
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the 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
- 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
- F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
-
- 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
-
- 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
- F02K3/025—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 by-pass flow being at least partly used to create an independent thrust component
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
- F16H1/20—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members
- F16H1/22—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts
-
- 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
-
- 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
- F05D2220/326—Application in turbines in gas turbines to drive shrouded, low solidity propeller
-
- 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
- F05D2250/313—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being perpendicular 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
-
- 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
- F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H1/00—Toothed gearings for conveying rotary motion
- F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
- F16H1/20—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members
- F16H1/22—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts
- F16H1/222—Toothed gearings for conveying rotary motion without gears having orbital motion involving more than two intermeshing members with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts with non-parallel axes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H37/00—Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00
- F16H37/02—Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00 comprising essentially only toothed or friction gearings
- F16H37/04—Combinations of toothed gearings only
- F16H37/041—Combinations of toothed gearings only for conveying rotary motion with constant gear ratio
-
- 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)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Gear Transmission (AREA)
- Structure Of Transmissions (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/670,551 US9611789B2 (en) | 2015-03-27 | 2015-03-27 | Reduction gearbox for a gas turbine engine |
EP16162598.3A EP3073103B1 (en) | 2015-03-27 | 2016-03-29 | Reduction gearbox for a gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
PL3073103T3 true PL3073103T3 (pl) | 2019-04-30 |
Family
ID=55661254
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL16162598T PL3073103T3 (pl) | 2015-03-27 | 2016-03-29 | Przekładnia redukcyjna do silnika turbogazowego |
Country Status (6)
Country | Link |
---|---|
US (1) | US9611789B2 (pl) |
EP (1) | EP3073103B1 (pl) |
CN (1) | CN107614852B (pl) |
CA (1) | CA2924840C (pl) |
PL (1) | PL3073103T3 (pl) |
WO (1) | WO2016154737A1 (pl) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3042009B1 (fr) * | 2015-10-05 | 2018-07-13 | Safran Aircraft Engines | Turbo moteur a soufflantes deportees avec un systeme differentiel |
FR3044730B1 (fr) * | 2015-12-02 | 2017-12-22 | Hispano Suiza Sa | Reducteur de vitesse a deux lignes intermediaires pour turbopropulseur, turbopropulseur comportant ledit reducteur |
US11203949B2 (en) * | 2016-08-11 | 2021-12-21 | General Electric Company | Mechanically driven air vehicle thermal management device |
US20180087639A1 (en) | 2016-09-23 | 2018-03-29 | Bell Helicopter Textron Inc. | High Speed Engine Reduction Gearboxes |
CN108612588B (zh) * | 2018-04-18 | 2024-03-22 | 常州环能涡轮动力股份有限公司 | 微型航空涡轴驱动系统 |
CN108757876A (zh) * | 2018-07-20 | 2018-11-06 | 深圳市罗曼斯科技有限公司 | 一种后级变速齿轮以及一种变速箱 |
US11142330B2 (en) * | 2018-08-30 | 2021-10-12 | Aurora Flight Sciences Corporation | Mechanically-distributed propulsion drivetrain and architecture |
US11028778B2 (en) * | 2018-09-27 | 2021-06-08 | Pratt & Whitney Canada Corp. | Engine with start assist |
CN111022731B (zh) * | 2019-11-14 | 2024-06-14 | 慈溪凯业电器有限公司 | 一种智能型民用燃气表执行器 |
CN113294512B (zh) * | 2021-06-15 | 2022-08-19 | 中国航发沈阳发动机研究所 | 一种采用面齿轮进行功率分流的航空发动机中央传动结构 |
CN117570167B (zh) * | 2024-01-19 | 2024-03-19 | 江苏国茂减速机股份有限公司 | 一种多电机超大扭矩均衡输出减速器 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR543901A (fr) | 1921-11-25 | 1922-09-12 | Mecanique Rotative Soc D | Dispositif de transmission de puissance |
US2619797A (en) | 1948-01-28 | 1952-12-02 | Rolls Royce | Gas turbine engine driving a propeller |
US2613749A (en) | 1948-08-14 | 1952-10-14 | Lockheed Aircraft Corp | Gas turbine power plant having propeller drive |
FR1189941A (fr) | 1957-09-04 | 1959-10-08 | Aéronef | |
US4270408A (en) * | 1978-10-13 | 1981-06-02 | General Motors Corporation | Gear drive for gas turbine engine |
US6735954B2 (en) | 2001-12-21 | 2004-05-18 | Pratt & Whitney Canada Corp. | Offset drive for gas turbine engine |
US8015900B2 (en) | 2003-07-16 | 2011-09-13 | Sikorsky Aircraft Corporation | Split-torque gear box |
US6973783B1 (en) * | 2004-02-27 | 2005-12-13 | Hydro-Gear Limited Partnership | Zero turn drive apparatus |
US7144349B2 (en) | 2004-04-06 | 2006-12-05 | Pratt & Whitney Canada Corp. | Gas turbine gearbox |
US9010105B1 (en) * | 2007-08-01 | 2015-04-21 | Hydro-Gear Limited Partnership | Transmission and engine configuration |
US8191410B2 (en) * | 2009-08-28 | 2012-06-05 | General Electric Company | Mechanical drive train for testing full scale compressor rigs and gas turbines |
US8568089B2 (en) * | 2010-06-03 | 2013-10-29 | Hamilton Sundstrand Corporation | Gear arrangement |
US8490411B2 (en) * | 2010-11-17 | 2013-07-23 | United Technologies Corporation | Axial accessory gearbox |
US8973465B2 (en) | 2012-07-20 | 2015-03-10 | United Technologies Corporation | Gearbox for gas turbine engine |
RU2532089C1 (ru) | 2013-10-29 | 2014-10-27 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Дифференциальный редуктор турбовинтовного двигателя |
-
2015
- 2015-03-27 US US14/670,551 patent/US9611789B2/en active Active
-
2016
- 2016-03-22 CN CN201680030639.1A patent/CN107614852B/zh active Active
- 2016-03-22 WO PCT/CA2016/050329 patent/WO2016154737A1/en active Application Filing
- 2016-03-22 CA CA2924840A patent/CA2924840C/en active Active
- 2016-03-29 EP EP16162598.3A patent/EP3073103B1/en active Active
- 2016-03-29 PL PL16162598T patent/PL3073103T3/pl unknown
Also Published As
Publication number | Publication date |
---|---|
EP3073103B1 (en) | 2018-09-26 |
CN107614852B (zh) | 2019-08-23 |
EP3073103A1 (en) | 2016-09-28 |
CA2924840C (en) | 2023-03-07 |
CN107614852A (zh) | 2018-01-19 |
US9611789B2 (en) | 2017-04-04 |
US20160281609A1 (en) | 2016-09-29 |
CA2924840A1 (en) | 2016-09-27 |
WO2016154737A1 (en) | 2016-10-06 |
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