PL3123016T3 - Statek powietrzny z dwiema maszynami wirowymi z turbiną swobodną, zawierający urządzenie wspomagające - Google Patents
Statek powietrzny z dwiema maszynami wirowymi z turbiną swobodną, zawierający urządzenie wspomagająceInfo
- Publication number
- PL3123016T3 PL3123016T3 PL15725706T PL15725706T PL3123016T3 PL 3123016 T3 PL3123016 T3 PL 3123016T3 PL 15725706 T PL15725706 T PL 15725706T PL 15725706 T PL15725706 T PL 15725706T PL 3123016 T3 PL3123016 T3 PL 3123016T3
- Authority
- PL
- Poland
- Prior art keywords
- dual
- assistance device
- power assistance
- turboshaft
- aircraft
- Prior art date
Links
- 230000009977 dual effect Effects 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- 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
- B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
-
- 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
- B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
- B64D35/021—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants for electric power plants
- B64D35/022—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants for electric power plants of hybrid-electric type
- B64D35/025—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants for electric power plants of hybrid-electric type of parallel 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
- B64D35/08—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
-
- 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
- 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
- F02C7/26—Starting; Ignition
- F02C7/262—Restarting after flame-out
-
- 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
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical drives
-
- 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
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
- H02K7/1807—Rotary generators
- H02K7/1823—Rotary generators structurally associated with turbines or similar engines
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/20—Structural association with auxiliary dynamo-electric machines, e.g. with electric starter motors or exciters
-
- 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
- F05D2220/00—Application
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Control Of Eletrric Generators (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1400753A FR3019215B1 (fr) | 2014-03-27 | 2014-03-27 | Dispositif d'assistance pour une turbomachine a turbine libre d'un aeronef comprenant au moins deux turbomachines a turbine libre |
PCT/FR2015/050767 WO2015145077A1 (fr) | 2014-03-27 | 2015-03-26 | Dispositif d'assistance pour une turbomachine a turbine libre d'un aeronef comprenant au moins deux turbomachines a turbine libre |
EP15725706.4A EP3123016B1 (fr) | 2014-03-27 | 2015-03-26 | Aéronef comprenant au moins deux turbomachines à turbine libre avec dispositif d'assistance |
Publications (1)
Publication Number | Publication Date |
---|---|
PL3123016T3 true PL3123016T3 (pl) | 2018-07-31 |
Family
ID=51293010
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL15725706T PL3123016T3 (pl) | 2014-03-27 | 2015-03-26 | Statek powietrzny z dwiema maszynami wirowymi z turbiną swobodną, zawierający urządzenie wspomagające |
Country Status (11)
Country | Link |
---|---|
US (1) | US10151246B2 (pl) |
EP (1) | EP3123016B1 (pl) |
JP (1) | JP6557321B2 (pl) |
KR (1) | KR102285093B1 (pl) |
CN (1) | CN106536895B (pl) |
CA (1) | CA2943486C (pl) |
ES (1) | ES2664446T3 (pl) |
FR (1) | FR3019215B1 (pl) |
PL (1) | PL3123016T3 (pl) |
RU (1) | RU2686236C2 (pl) |
WO (1) | WO2015145077A1 (pl) |
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FR3029172B1 (fr) * | 2014-11-27 | 2018-05-25 | Safran Helicopter Engines | Groupe propulseur a moyens d'accouplement selectif |
WO2017015341A1 (en) * | 2015-07-20 | 2017-01-26 | Sikorsky Aircraft Corporation | Control system for rotorcraft in-flight engine restarting |
US11028812B2 (en) * | 2016-07-27 | 2021-06-08 | Astronics Advanced Electronic Systems Corp. | Integrated brushless starter generator |
US10654578B2 (en) | 2016-11-02 | 2020-05-19 | Rolls-Royce North American Technologies, Inc. | Combined AC and DC turboelectric distributed propulsion system |
US10934935B2 (en) * | 2017-01-30 | 2021-03-02 | Ge Aviation Systems Llc | Engine core assistance |
US10640225B2 (en) * | 2017-07-10 | 2020-05-05 | Rolls-Royce North American Technologies, Inc. | Selectively regulating current in distributed propulsion systems |
US10476417B2 (en) * | 2017-08-11 | 2019-11-12 | Rolls-Royce North American Technologies Inc. | Gas turbine generator torque DC to DC converter control system |
US10483887B2 (en) | 2017-08-11 | 2019-11-19 | Rolls-Royce North American Technologies, Inc. | Gas turbine generator temperature DC to DC converter control system |
US10491145B2 (en) | 2017-08-11 | 2019-11-26 | Rolls-Royce North American Technologies Inc. | Gas turbine generator speed DC to DC converter control system |
US10207592B1 (en) * | 2017-11-01 | 2019-02-19 | GM Global Technology Operations LLC | Autonomous hybrid power generation platform |
WO2019183427A1 (en) | 2018-03-22 | 2019-09-26 | Continental Motors, Inc. | Engine ignition timing and power supply system |
FR3079820B1 (fr) * | 2018-04-09 | 2020-04-17 | Safran Electrical & Power | Systeme et procede de demarrage/generation pour turbomachine d'aeronef |
FR3081150B1 (fr) * | 2018-05-18 | 2020-06-12 | Safran Helicopter Engines | Architecture de puissance d'un aeronef |
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 |
US10974844B2 (en) * | 2019-01-29 | 2021-04-13 | The Boeing Company | Aircraft auxiliary power unit (APU) control system having speed compensation |
US11718408B2 (en) | 2019-03-26 | 2023-08-08 | Pratt & Whitney Canada Corp. | Electric power system for powerplants of a multi-engine aircraft |
EP3725676B1 (en) * | 2019-04-16 | 2024-09-11 | Volocopter GmbH | Method of controlling an actuator system, emergency control system and aircraft equipped with such system |
FR3095806B1 (fr) | 2019-05-06 | 2021-08-20 | Safran Helicopter Engines | Système de propulsion hybride pour aéronef à décollage et atterrissage verticaux |
JP7252861B2 (ja) * | 2019-08-22 | 2023-04-05 | 三菱重工業株式会社 | ガスタービンの燃焼制御装置、燃焼制御方法及びプログラム |
GB201915310D0 (en) * | 2019-10-23 | 2019-12-04 | Rolls Royce Plc | Turboelectric generator system |
GB2589640A (en) * | 2019-12-06 | 2021-06-09 | Rolls Royce Plc | Gas turbine engine |
CA3116473A1 (en) * | 2020-06-08 | 2021-12-08 | Ty-Crop Manufacturing Ltd. | Methods and systems for reducing engine idling of fuel-driven equipment |
US20220063826A1 (en) * | 2020-08-31 | 2022-03-03 | General Electric Company | In-flight hybrid electric engine shutdown |
US12031479B2 (en) | 2020-08-31 | 2024-07-09 | General Electric Company | Hybrid electric propulsion system load share |
FR3117148A1 (fr) * | 2020-12-04 | 2022-06-10 | Safran | Procédé de mise à l’arrêt d’un moteur à turbine à gaz de turbogénérateur pour aéronef |
JP7365325B2 (ja) * | 2020-12-22 | 2023-10-19 | 本田技研工業株式会社 | ガスタービンシステム |
FR3118994B1 (fr) | 2021-01-15 | 2022-12-23 | Safran Helicopter Engines | Procede et dispositif d’allumage |
JP7535966B2 (ja) | 2021-03-17 | 2024-08-19 | 本田技研工業株式会社 | ガスタービン発電機 |
US11845388B2 (en) * | 2021-05-20 | 2023-12-19 | General Electric Company | AC electrical power system for a vehicle |
FR3126965A1 (fr) * | 2021-09-16 | 2023-03-17 | Safran Aircraft Engines | système d’alimentation électrique pour aéronef |
EP4174298B1 (en) * | 2021-10-29 | 2024-08-28 | RTX Corporation | Hybrid-electric single engine descent engine management |
US11939914B2 (en) * | 2021-12-02 | 2024-03-26 | Pratt & Whitney Canada Corp. | System and method of operating multi-engine system |
US11674456B1 (en) * | 2021-12-02 | 2023-06-13 | Pratt & Whitney Canada Corp. | System and method of operating multi-engine system |
US20230175437A1 (en) * | 2021-12-02 | 2023-06-08 | Pratt & Whitney Canada Corp. | System and method of operating multi-engine system |
US12077308B2 (en) | 2022-04-14 | 2024-09-03 | Textron Innovations Inc. | Supplemental engine transition control |
FR3137710B1 (fr) * | 2022-07-05 | 2024-06-07 | Safran Electrical & Power | Procédé de contrôle d’une turbomachine hybride |
US12054245B2 (en) * | 2022-07-18 | 2024-08-06 | Textron Innovations Inc. | Optimizing usage of supplemental engine power |
FR3138116A1 (fr) | 2022-07-20 | 2024-01-26 | Airbus Helicopters | Aéronef comportant au moins deux turbomoteurs et un dispositif configuré pour être relié à un des turbomoteurs et procédé de contrôle d’un tel aéronef |
FR3138827A1 (fr) * | 2022-08-12 | 2024-02-16 | Safran Helicopter Engines | Procédé de gestion de la sortie d’un mode de consommation spécifique d’un turbomoteur d’aéronef |
US12006880B2 (en) | 2022-09-12 | 2024-06-11 | General Electric Company | High bandwidth control of turbofan/turboprop thrust response using embedded electric machines |
FR3140866B1 (fr) | 2022-10-18 | 2024-08-30 | Airbus Helicopters | procédé et aéronef muni d’au moins un moteur à combustion et d’un système d’entraînement à au moins deux machines électriques |
FR3144977A1 (fr) * | 2023-01-18 | 2024-07-19 | Safran | Procédé de régulation de régime et dispositif de commande |
EP4417799A1 (en) * | 2023-02-14 | 2024-08-21 | Pratt & Whitney Canada Corp. | Sub-idle hybrid operation mode for hybrid electric propulsion system |
FR3147793A1 (fr) | 2023-04-13 | 2024-10-18 | Airbus Helicopters | procédé de pilotage d’un aéronef à voilure tournante multimoteur à consommation de carburant réduite au sol |
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FR2967132B1 (fr) * | 2010-11-04 | 2012-11-09 | Turbomeca | Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur dissymetrique a systeme de regulation pour sa mise en oeuvre |
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FR2990573B1 (fr) | 2012-05-11 | 2015-11-20 | Hispano Suiza Sa | Systeme de commande et d'alimentation en energie des turbomachines d'un helicoptere |
FR2993243B1 (fr) * | 2012-07-12 | 2014-07-11 | Eurocopter France | Architecture d'alimentation hybride en puissance mecanique d'un rotor, geree a partir du reseau de bord d'un giravion |
US9045996B2 (en) * | 2012-11-20 | 2015-06-02 | Honeywell International Inc. | Gas turbine engine optimization by electric power transfer |
CN103104342B (zh) * | 2013-01-29 | 2015-09-30 | 深圳智慧能源技术有限公司 | 涡轮发动机 |
GB201308292D0 (en) * | 2013-05-09 | 2013-06-12 | Rolls Royce Plc | Aircraft electrical system |
FR3011587B1 (fr) * | 2013-10-09 | 2015-11-06 | Turbomeca | Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur |
-
2014
- 2014-03-27 FR FR1400753A patent/FR3019215B1/fr active Active
-
2015
- 2015-03-26 KR KR1020167030206A patent/KR102285093B1/ko active IP Right Grant
- 2015-03-26 US US15/129,240 patent/US10151246B2/en active Active
- 2015-03-26 RU RU2016141965A patent/RU2686236C2/ru active
- 2015-03-26 CN CN201580016709.3A patent/CN106536895B/zh active Active
- 2015-03-26 ES ES15725706.4T patent/ES2664446T3/es active Active
- 2015-03-26 WO PCT/FR2015/050767 patent/WO2015145077A1/fr active Application Filing
- 2015-03-26 JP JP2017501506A patent/JP6557321B2/ja active Active
- 2015-03-26 CA CA2943486A patent/CA2943486C/fr active Active
- 2015-03-26 EP EP15725706.4A patent/EP3123016B1/fr active Active
- 2015-03-26 PL PL15725706T patent/PL3123016T3/pl unknown
Also Published As
Publication number | Publication date |
---|---|
CN106536895B (zh) | 2018-08-07 |
FR3019215B1 (fr) | 2019-05-31 |
CA2943486C (fr) | 2021-08-31 |
CA2943486A1 (fr) | 2015-10-01 |
RU2016141965A3 (pl) | 2018-09-11 |
KR102285093B1 (ko) | 2021-08-03 |
US10151246B2 (en) | 2018-12-11 |
JP6557321B2 (ja) | 2019-08-07 |
CN106536895A (zh) | 2017-03-22 |
RU2016141965A (ru) | 2018-04-27 |
KR20160140833A (ko) | 2016-12-07 |
US20180187604A1 (en) | 2018-07-05 |
ES2664446T3 (es) | 2018-04-19 |
JP2017512940A (ja) | 2017-05-25 |
FR3019215A1 (fr) | 2015-10-02 |
EP3123016A1 (fr) | 2017-02-01 |
RU2686236C2 (ru) | 2019-04-24 |
EP3123016B1 (fr) | 2018-03-07 |
WO2015145077A1 (fr) | 2015-10-01 |
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