WO2018026408A3 - Procédé et système pour turbine à gaz à deux bâtis - Google Patents
Procédé et système pour turbine à gaz à deux bâtis Download PDFInfo
- Publication number
- WO2018026408A3 WO2018026408A3 PCT/US2017/032319 US2017032319W WO2018026408A3 WO 2018026408 A3 WO2018026408 A3 WO 2018026408A3 US 2017032319 W US2017032319 W US 2017032319W WO 2018026408 A3 WO2018026408 A3 WO 2018026408A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- compressor
- turbine
- engine
- gas turbine
- positioned axially
- Prior art date
Links
Classifications
-
- 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
- F02K3/04—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 plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—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 plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
- F02C7/06—Arrangements of bearings; Lubricating
-
- 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
-
- 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)
Abstract
Selon l'invention, une turbine à gaz comprend un bloc réacteur comprenant un compresseur haute pression (HP), une chambre de combustion, et une turbine HP dans un agencement de flux en série. Une turbine basse pression (LP) est disposée axialement à l'arrière du bloc moteur et comprend une pluralité d'étages de pales de rotor. Un dernier étage de pales de rotor comprend un étage de pale de rotor à faible tourbillon. Un compresseur LP est positionné axialement à l'avant du bloc moteur et est accouplé à la turbine LP par une boîte de vitesses. Le compresseur LP est positionné radialement à l'extérieur en partant de la boîte de vitesses. Un ensemble ventilateur est directement accouplé au compresseur LP de telle manière que l'ensemble ventilateur et le compresseur LP tournent à la même vitesse. Un ensemble bâti-moteur comprend un élément de bâti de ventilateur avant disposé axialement entre le compresseur LP et le compresseur HP. L'ensemble bâti-moteur comprend également un élément de bâti central de turbine placé entre la turbine HP et la turbine LP.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17817936.2A EP3464833A2 (fr) | 2016-05-25 | 2017-05-12 | Procédé et système pour turbine à gaz à deux bâtis |
CN201780032101.9A CN109196187B (zh) | 2016-05-25 | 2017-05-12 | 用于两框架式燃气涡轮发动机的方法和系统 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201615164726A | 2016-05-25 | 2016-05-25 | |
US15/164,726 | 2016-05-25 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2018026408A2 WO2018026408A2 (fr) | 2018-02-08 |
WO2018026408A3 true WO2018026408A3 (fr) | 2018-04-26 |
Family
ID=60766124
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2017/032319 WO2018026408A2 (fr) | 2016-05-25 | 2017-05-12 | Procédé et système pour turbine à gaz à deux bâtis |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP3464833A2 (fr) |
CN (1) | CN109196187B (fr) |
WO (1) | WO2018026408A2 (fr) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102017211649A1 (de) * | 2017-07-07 | 2019-01-10 | MTU Aero Engines AG | Gasturbine mit einer schnelllaufenden Niederdruckturbine und einem Turbinengehäuse |
US11156097B2 (en) * | 2019-02-20 | 2021-10-26 | General Electric Company | Turbomachine having an airflow management assembly |
GB201903257D0 (en) * | 2019-03-11 | 2019-04-24 | Rolls Royce Plc | Efficient gas turbine engine installation and operation |
US11174916B2 (en) | 2019-03-21 | 2021-11-16 | Pratt & Whitney Canada Corp. | Aircraft engine reduction gearbox |
FR3097012B1 (fr) * | 2019-06-06 | 2022-01-21 | Safran Aircraft Engines | Procédé de régulation d’une accélération d’une turbomachine |
US11560840B2 (en) * | 2020-10-16 | 2023-01-24 | General Electric Company | Damper engine mount links |
US11268453B1 (en) | 2021-03-17 | 2022-03-08 | Pratt & Whitney Canada Corp. | Lubrication system for aircraft engine reduction gearbox |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130186058A1 (en) * | 2012-01-24 | 2013-07-25 | William G. Sheridan | Geared turbomachine fan and compressor rotation |
US20150143794A1 (en) * | 2013-11-22 | 2015-05-28 | United Technologies Corporation | Geared Turbofan Engine Gearbox Arrangement |
EP2975226A1 (fr) * | 2014-07-15 | 2016-01-20 | United Technologies Corporation | Support de section de turbine pour une turbine à gaz |
US20160084105A1 (en) * | 2014-09-24 | 2016-03-24 | United Technologies Corporation | Fan drive gear system |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7513102B2 (en) * | 2005-06-06 | 2009-04-07 | General Electric Company | Integrated counterrotating turbofan |
US7926259B2 (en) * | 2006-10-31 | 2011-04-19 | General Electric Company | Turbofan engine assembly and method of assembling same |
US8678743B1 (en) * | 2013-02-04 | 2014-03-25 | United Technologies Corporation | Method for setting a gear ratio of a fan drive gear system of a gas turbine engine |
-
2017
- 2017-05-12 WO PCT/US2017/032319 patent/WO2018026408A2/fr unknown
- 2017-05-12 CN CN201780032101.9A patent/CN109196187B/zh active Active
- 2017-05-12 EP EP17817936.2A patent/EP3464833A2/fr not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130186058A1 (en) * | 2012-01-24 | 2013-07-25 | William G. Sheridan | Geared turbomachine fan and compressor rotation |
US20150143794A1 (en) * | 2013-11-22 | 2015-05-28 | United Technologies Corporation | Geared Turbofan Engine Gearbox Arrangement |
EP2975226A1 (fr) * | 2014-07-15 | 2016-01-20 | United Technologies Corporation | Support de section de turbine pour une turbine à gaz |
US20160084105A1 (en) * | 2014-09-24 | 2016-03-24 | United Technologies Corporation | Fan drive gear system |
Also Published As
Publication number | Publication date |
---|---|
WO2018026408A2 (fr) | 2018-02-08 |
EP3464833A2 (fr) | 2019-04-10 |
CN109196187A (zh) | 2019-01-11 |
CN109196187B (zh) | 2021-12-07 |
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