PL3597885T3 - Architektura przekładni zębatej do silnika z wielowirnikową turbiną gazową - Google Patents
Architektura przekładni zębatej do silnika z wielowirnikową turbiną gazowąInfo
- Publication number
- PL3597885T3 PL3597885T3 PL19193921.4T PL19193921T PL3597885T3 PL 3597885 T3 PL3597885 T3 PL 3597885T3 PL 19193921 T PL19193921 T PL 19193921T PL 3597885 T3 PL3597885 T3 PL 3597885T3
- Authority
- PL
- Poland
- Prior art keywords
- gas turbine
- turbine engine
- gear train
- spool gas
- train architecture
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
- F02C3/145—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chamber being in the reverse flow-type
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
-
- 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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/12—Combinations with mechanical gearing
-
- 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
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/026—Shaft to shaft connections
-
- 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
- F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
-
- 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
- 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
- F02C3/113—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 with variable power transmission between rotors
-
- 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
- F02C7/06—Arrangements of bearings; Lubricating
-
- 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
- F02K3/04—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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/04—Features relating to lubrication or cooling or heating
- F16H57/048—Type of gearings to be lubricated, cooled or heated
- F16H57/0493—Gearings with spur or bevel gears
- F16H57/0495—Gearings with spur or bevel gears with fixed gear ratio
-
- 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
-
- 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
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- 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
- F05D2220/324—Application in turbines in gas turbines to drive unshrouded, 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/329—Application in turbines in gas turbines in helicopters
-
- 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
- F05D2230/00—Manufacture
- F05D2230/70—Disassembly methods
-
- 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
- F05D2230/00—Manufacture
- F05D2230/72—Maintenance
-
- 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
- F05D2240/00—Components
- F05D2240/60—Shafts
- F05D2240/61—Hollow
-
- 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
- F05D2250/36—Arrangement of components in inner-outer relationship, e.g. shaft-bearing arrangements
-
- 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
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
-
- 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
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
-
- 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
-
- 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
- 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
- F05D2260/98—Lubrication
-
- 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
- Y02T50/40—Weight reduction
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
- Supercharger (AREA)
Applications Claiming Priority (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201662363949P | 2016-07-19 | 2016-07-19 | |
US201662363956P | 2016-07-19 | 2016-07-19 | |
US201662363952P | 2016-07-19 | 2016-07-19 | |
US201662363947P | 2016-07-19 | 2016-07-19 | |
US201662363955P | 2016-07-19 | 2016-07-19 | |
US15/384,959 US10883424B2 (en) | 2016-07-19 | 2016-12-20 | Multi-spool gas turbine engine architecture |
US15/407,414 US10458340B2 (en) | 2016-07-19 | 2017-01-17 | Turbine shaft power take-off |
US15/407,445 US10767567B2 (en) | 2016-07-19 | 2017-01-17 | Multi-spool gas turbine engine architecture |
US15/407,439 US10690061B2 (en) | 2016-07-19 | 2017-01-17 | Gear train architecture for a multi-spool gas turbine engine |
US15/407,423 US10393027B2 (en) | 2016-07-19 | 2017-01-17 | Gas turbine engine shaft architecture and associated method of disassembly |
Publications (1)
Publication Number | Publication Date |
---|---|
PL3597885T3 true PL3597885T3 (pl) | 2022-07-18 |
Family
ID=59381171
Family Applications (7)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL19183868T PL3572638T3 (pl) | 2016-07-19 | 2017-07-19 | Silnik turbośmigłowy |
PL19193794.5T PL3597884T3 (pl) | 2016-07-19 | 2017-07-19 | Architektura silnika z wielowirnikową turbiną gazową |
PL19193921.4T PL3597885T3 (pl) | 2016-07-19 | 2017-07-19 | Architektura przekładni zębatej do silnika z wielowirnikową turbiną gazową |
PL17182096T PL3273033T3 (pl) | 2016-07-19 | 2017-07-19 | Przystawka odbioru mocy z wału turbiny |
PL17182087T PL3273032T3 (pl) | 2016-07-19 | 2017-07-19 | Budowa wielowałowego silnika turbospalinowego |
PL17182102T PL3273034T3 (pl) | 2016-07-19 | 2017-07-19 | Architektura wielowirnikowego silnika turbospalinowego |
PL17182076T PL3273031T3 (pl) | 2016-07-19 | 2017-07-19 | Architektura wału silnika turbogazowego i stosowana metoda demontażu |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL19183868T PL3572638T3 (pl) | 2016-07-19 | 2017-07-19 | Silnik turbośmigłowy |
PL19193794.5T PL3597884T3 (pl) | 2016-07-19 | 2017-07-19 | Architektura silnika z wielowirnikową turbiną gazową |
Family Applications After (4)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL17182096T PL3273033T3 (pl) | 2016-07-19 | 2017-07-19 | Przystawka odbioru mocy z wału turbiny |
PL17182087T PL3273032T3 (pl) | 2016-07-19 | 2017-07-19 | Budowa wielowałowego silnika turbospalinowego |
PL17182102T PL3273034T3 (pl) | 2016-07-19 | 2017-07-19 | Architektura wielowirnikowego silnika turbospalinowego |
PL17182076T PL3273031T3 (pl) | 2016-07-19 | 2017-07-19 | Architektura wału silnika turbogazowego i stosowana metoda demontażu |
Country Status (2)
Country | Link |
---|---|
EP (7) | EP3273032B1 (pl) |
PL (7) | PL3572638T3 (pl) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10883424B2 (en) | 2016-07-19 | 2021-01-05 | Pratt & Whitney Canada Corp. | Multi-spool gas turbine engine architecture |
US11415063B2 (en) | 2016-09-15 | 2022-08-16 | Pratt & Whitney Canada Corp. | Reverse-flow gas turbine engine |
US11035293B2 (en) | 2016-09-15 | 2021-06-15 | Pratt & Whitney Canada Corp. | Reverse flow gas turbine engine with offset RGB |
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 |
US10815899B2 (en) | 2016-11-15 | 2020-10-27 | Pratt & Whitney Canada Corp. | Gas turbine engine accessories arrangement |
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 |
CN110821677A (zh) | 2018-08-08 | 2020-02-21 | 普拉特 - 惠特尼加拿大公司 | 多发动机系统和方法 |
US11174916B2 (en) | 2019-03-21 | 2021-11-16 | Pratt & Whitney Canada Corp. | Aircraft engine reduction gearbox |
US11572838B2 (en) * | 2020-09-29 | 2023-02-07 | General Electric Company | Accessory gearbox for a turbine engine |
US11268453B1 (en) | 2021-03-17 | 2022-03-08 | Pratt & Whitney Canada Corp. | Lubrication system for aircraft engine reduction gearbox |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB603283A (en) * | 1946-06-27 | 1948-06-11 | Power Jets Res & Dev Ltd | Improvements in or relating to internal combustion turbine power plants |
US4611464A (en) * | 1984-05-02 | 1986-09-16 | United Technologies Corporation | Rotor assembly for a gas turbine engine and method of disassembly |
US7055303B2 (en) * | 2003-12-22 | 2006-06-06 | Pratt & Whitney Canada Corp. | Gas turbine engine architecture |
US20060137355A1 (en) * | 2004-12-27 | 2006-06-29 | Pratt & Whitney Canada Corp. | Fan driven emergency generator |
US20080075590A1 (en) * | 2006-09-27 | 2008-03-27 | Thomas Ory Moniz | Gas turbine engine assembly and method of assembling same |
EP2074288B1 (en) * | 2006-10-12 | 2014-06-25 | United Technologies Corporation | Turbofan engine with variable area fan nozzle and low spool generator for emergency power generation and method for providing emergency power. |
GB0903423D0 (en) * | 2009-03-02 | 2009-04-08 | Rolls Royce Plc | Variable drive gas turbine engine |
US8176725B2 (en) * | 2009-09-09 | 2012-05-15 | United Technologies Corporation | Reversed-flow core for a turbofan with a fan drive gear system |
JP5016706B2 (ja) * | 2009-11-04 | 2012-09-05 | 川崎重工業株式会社 | 航空機用始動発電装置 |
GB201219544D0 (en) * | 2012-10-31 | 2012-12-12 | Rolls Royce Deutschland | Geared compressor for gas turbine engine |
US20140252160A1 (en) * | 2013-03-07 | 2014-09-11 | United Technologies Corporation | Reverse flow gas turbine engine removable core |
IL228274A (en) * | 2013-09-03 | 2016-10-31 | Israel Aerospace Ind Ltd | Fan Turbo Engine and Method of Removing Fan Fan Turbo |
WO2015122948A2 (en) * | 2013-12-05 | 2015-08-20 | United Technologies Corporation | Gas turbine engines with intercoolers and recuperators |
US9890846B2 (en) * | 2014-12-08 | 2018-02-13 | General Electric Company | Gearbox with sealed accessory vent |
-
2017
- 2017-07-19 EP EP17182087.1A patent/EP3273032B1/en active Active
- 2017-07-19 EP EP19193921.4A patent/EP3597885B1/en active Active
- 2017-07-19 PL PL19183868T patent/PL3572638T3/pl unknown
- 2017-07-19 PL PL19193794.5T patent/PL3597884T3/pl unknown
- 2017-07-19 PL PL19193921.4T patent/PL3597885T3/pl unknown
- 2017-07-19 PL PL17182096T patent/PL3273033T3/pl unknown
- 2017-07-19 EP EP17182076.4A patent/EP3273031B1/en active Active
- 2017-07-19 PL PL17182087T patent/PL3273032T3/pl unknown
- 2017-07-19 PL PL17182102T patent/PL3273034T3/pl unknown
- 2017-07-19 EP EP17182096.2A patent/EP3273033B1/en active Active
- 2017-07-19 PL PL17182076T patent/PL3273031T3/pl unknown
- 2017-07-19 EP EP17182102.8A patent/EP3273034B1/en active Active
- 2017-07-19 EP EP19193794.5A patent/EP3597884B1/en active Active
- 2017-07-19 EP EP19183868.9A patent/EP3572638B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP3273031B1 (en) | 2019-07-03 |
EP3273034A1 (en) | 2018-01-24 |
EP3597885B1 (en) | 2022-04-20 |
PL3273034T3 (pl) | 2020-06-15 |
EP3273032A2 (en) | 2018-01-24 |
EP3273032A3 (en) | 2018-04-18 |
PL3273032T3 (pl) | 2020-04-30 |
PL3273031T3 (pl) | 2019-12-31 |
EP3273032B1 (en) | 2019-08-28 |
EP3572638A1 (en) | 2019-11-27 |
EP3273034B1 (en) | 2020-01-01 |
EP3572638B1 (en) | 2020-12-23 |
EP3597885A1 (en) | 2020-01-22 |
EP3597884B1 (en) | 2022-04-20 |
PL3572638T3 (pl) | 2021-07-05 |
EP3273031A1 (en) | 2018-01-24 |
EP3273033B1 (en) | 2020-12-02 |
PL3597884T3 (pl) | 2022-08-29 |
PL3273033T3 (pl) | 2021-06-28 |
EP3597884A1 (en) | 2020-01-22 |
EP3273033A1 (en) | 2018-01-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PL3309371T3 (pl) | Budowa przekładni zębatej dla wielowałowego silnika turbospalinowego | |
PL3597885T3 (pl) | Architektura przekładni zębatej do silnika z wielowirnikową turbiną gazową | |
PL3339610T3 (pl) | Architektura wielowirnikowego silnika turbospalinowego | |
PL3361073T3 (pl) | Silnik z wielowirnikową turbiną gazową | |
GB201518227D0 (en) | A geared gas turbine engine | |
PL3073103T3 (pl) | Przekładnia redukcyjna do silnika turbogazowego | |
GB201510050D0 (en) | A geared gas turbine engine | |
GB201412189D0 (en) | A nozzle arrangement for a gas turbine engine | |
PL3101258T5 (pl) | Budowa przekładniowa dla silnika turbospalinowego | |
GB201713259D0 (en) | A dual walled component for a gas turbine engine | |
GB201511841D0 (en) | Fuel spray nozel for a gas turbine engine | |
GB201518345D0 (en) | Combustor for a gas turbine engine | |
GB2545538B (en) | A gas turbine engine having sequential combustion | |
EP3279568B8 (en) | Combustor for a gas turbine engine | |
GB201707402D0 (en) | A Geared gas turbine engine | |
GB201720391D0 (en) | A gas turbine engine | |
GB201612099D0 (en) | A geared gas turbine engine | |
GB201419766D0 (en) | A sealing arrangement for a gas turbine engine | |
HK1247977A1 (zh) | 燃氣渦輪發動機 | |
EP3114328A4 (en) | Reduced stress boss geometry for a gas turbine engine | |
GB2558072B (en) | Turbine for a turbine engine | |
GB2553628B (en) | A gas turbine engine | |
GB201701630D0 (en) | A geared gas turbine engine | |
GB201612021D0 (en) | A method of operating a gas turbine engine | |
GB201513157D0 (en) | Combustor for a gas turbine engine |