[go: up one dir, main page]

PL2652269T3 - Sposób sterowania wytwarzaniem energii elektrycznej wykorzystywanej w turbinie gazowej statku powietrznego i urządzenie do wdrażania takiego sposobu - Google Patents

Sposób sterowania wytwarzaniem energii elektrycznej wykorzystywanej w turbinie gazowej statku powietrznego i urządzenie do wdrażania takiego sposobu

Info

Publication number
PL2652269T3
PL2652269T3 PL11813545T PL11813545T PL2652269T3 PL 2652269 T3 PL2652269 T3 PL 2652269T3 PL 11813545 T PL11813545 T PL 11813545T PL 11813545 T PL11813545 T PL 11813545T PL 2652269 T3 PL2652269 T3 PL 2652269T3
Authority
PL
Poland
Prior art keywords
generation
controlling
gas turbine
device implementing
aircraft gas
Prior art date
Application number
PL11813545T
Other languages
English (en)
Inventor
Stephen Langford
Pierre Harriet
Original Assignee
Safran Helicopter Engines
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL2652269T3 publication Critical patent/PL2652269T3/pl

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R16/00Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
    • B60R16/02Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements
    • B60R16/03Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements for supply of electrical power to vehicle subsystems or for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/32Arrangement, mounting, or driving, of auxiliaries
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10Adaptations for driving, or combinations with, electric generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10Gas-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275Mechanical drives
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/329Application in turbines in gas turbines in helicopters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/70Application in combination with
    • F05D2220/76Application in combination with an electrical generator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/85Starting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/10Purpose of the control system to cope with, or avoid, compressor flow instabilities
    • F05D2270/101Compressor surge or stall

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Eletrric Generators (AREA)
PL11813545T 2010-12-13 2011-12-12 Sposób sterowania wytwarzaniem energii elektrycznej wykorzystywanej w turbinie gazowej statku powietrznego i urządzenie do wdrażania takiego sposobu PL2652269T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1060419A FR2968716B1 (fr) 2010-12-13 2010-12-13 Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et turbomoteur mettant en oeuvre un tel procede
PCT/FR2011/052935 WO2012080633A1 (fr) 2010-12-13 2011-12-12 Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et dispositif mettant en oeuvre un tel procede
EP11813545.8A EP2652269B1 (fr) 2010-12-13 2011-12-12 Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et dispositif mettant en oeuvre un tel procede

Publications (1)

Publication Number Publication Date
PL2652269T3 true PL2652269T3 (pl) 2018-06-29

Family

ID=44170226

Family Applications (1)

Application Number Title Priority Date Filing Date
PL11813545T PL2652269T3 (pl) 2010-12-13 2011-12-12 Sposób sterowania wytwarzaniem energii elektrycznej wykorzystywanej w turbinie gazowej statku powietrznego i urządzenie do wdrażania takiego sposobu

Country Status (11)

Country Link
US (1) US8866318B2 (pl)
EP (1) EP2652269B1 (pl)
JP (1) JP5923515B2 (pl)
KR (1) KR101914313B1 (pl)
CN (1) CN103228872B (pl)
CA (1) CA2816512C (pl)
ES (1) ES2664773T3 (pl)
FR (1) FR2968716B1 (pl)
PL (1) PL2652269T3 (pl)
RU (1) RU2598476C2 (pl)
WO (1) WO2012080633A1 (pl)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2986570B1 (fr) 2012-02-06 2014-02-28 Eurocopter France Dispositif et procede de regulation d'une installation motrice comportant au moins un turbomoteur, et aeronef
FR2986571B1 (fr) 2012-02-06 2014-02-21 Eurocopter France Dispositif et procede de regulation d'un turbomoteur, et aeronef
CA2804462C (en) 2012-07-12 2021-05-25 Pratt & Whitney Canada Corp. Aircraft power outtake management
FR2994939B1 (fr) * 2012-09-05 2014-08-22 Turbomeca Boitier a accessoires pour la commande de volets d'un aeronef
EP3004564A4 (en) * 2013-06-07 2016-11-23 Ge Aviat Systems Llc TURBO FAN MOTOR WITH GENERATOR
FR3011144B1 (fr) 2013-09-26 2018-06-15 Dassault Aviation Procede et module de protection contre les pics de couple entre moteur et une machine electrique
CN103552690B (zh) * 2013-10-29 2016-04-20 中国南方航空工业(集团)有限公司 螺旋桨发动机的负拉力保护方法
US9944400B2 (en) 2014-02-11 2018-04-17 Sikorsky Aircraft Corporation Adaptive engine acceleration for accessory loads
FR3019218B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant
FR3019219B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant
US10087902B2 (en) 2015-05-11 2018-10-02 Sikorsky Aircraft Corporation Power limiting generator control unit (GCU)
US20170044989A1 (en) * 2015-08-14 2017-02-16 General Electric Company Gas turbine engine stall margin management
US10352189B2 (en) * 2017-05-10 2019-07-16 Pratt & Whitney Canada Corp. Method and system for setting an acceleration schedule for engine start
EP3769394A1 (en) * 2018-03-20 2021-01-27 Nexus Technologies, Inc. Regulating the operating point of a power inverter
FR3079820B1 (fr) * 2018-04-09 2020-04-17 Safran Electrical & Power Systeme et procede de demarrage/generation pour turbomachine d'aeronef
US11097849B2 (en) 2018-09-10 2021-08-24 General Electric Company Aircraft having an aft engine
JP7049234B2 (ja) * 2018-11-15 2022-04-06 本田技研工業株式会社 ハイブリッド飛行体
JP7471776B2 (ja) * 2019-02-18 2024-04-22 三菱重工業株式会社 ジェットエンジン
US11428171B2 (en) 2019-12-06 2022-08-30 General Electric Company Electric machine assistance for multi-spool turbomachine operation and control
US11725594B2 (en) 2020-08-31 2023-08-15 General Electric Company Hybrid electric engine speed regulation
US12031479B2 (en) * 2020-08-31 2024-07-09 General Electric Company Hybrid electric propulsion system load share
CN113191643B (zh) * 2021-05-06 2022-04-01 四川大学 电-气互联系统脆弱线路辨识方法
CN114483323B (zh) * 2022-01-27 2023-08-22 中国航发沈阳发动机研究所 具备通断功能的航空发动机功率提取系统及其调试方法
US12459659B2 (en) 2022-03-07 2025-11-04 General Electric Company Method and apparatus for controlling electrical machines operating with a turbine engine
FR3137416B1 (fr) * 2022-06-30 2025-05-02 Safran Aircraft Engines Système de propulsion pour aéronef avec turbomoteur couplé à un générateur électrique à puissance bridée en fonction du régime moteur
US12480449B2 (en) 2022-08-22 2025-11-25 General Electric Company Propulsion system including an electric machine for starting a gas turbine engine
US12006880B2 (en) 2022-09-12 2024-06-11 General Electric Company High bandwidth control of turbofan/turboprop thrust response using embedded electric machines
CN115839277B (zh) * 2022-12-20 2025-06-06 中国航发控制系统研究所 一种航空发动机及其功率提取与分配方法
CN116291961A (zh) * 2023-03-22 2023-06-23 北京航空航天大学 一种电涡轮增压的固液火箭发动机输送系统及其控制方法

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4456830A (en) * 1982-04-22 1984-06-26 Lockheed Corporation AC Motor-starting for aircraft engines using APU free turbine driven generators
FR2608854B1 (fr) * 1986-12-19 1989-03-31 Thomson Csf Dispositif anti-transitoires pour l'alimentation electrique de materiel embarque
US5583420A (en) * 1993-10-01 1996-12-10 Lucas Aerospace Power Equipment Corporation Microprocessor controller for starter/generator
DE19739917A1 (de) * 1997-09-11 1999-03-18 Siemens Ag System zur Versorgung elektromotorischer Verbraucher mit elektrischer Energie
US7210653B2 (en) * 2002-10-22 2007-05-01 The Boeing Company Electric-based secondary power system architectures for aircraft
US6777822B1 (en) * 2003-04-01 2004-08-17 Hamilton Sundstrand Corporation Control system for an auxiliary power unit
US6931856B2 (en) * 2003-09-12 2005-08-23 Mes International, Inc. Multi-spool turbogenerator system and control method
JP4092728B2 (ja) * 2005-01-25 2008-05-28 独立行政法人 宇宙航空研究開発機構 航空機用推進システム
FR2882200B1 (fr) * 2005-02-17 2015-05-01 Hispano Suiza Sa Alimentation electrique d'equipements d'un moteur d'avion a turbine a gaz
US7513120B2 (en) 2005-04-08 2009-04-07 United Technologies Corporation Electrically coupled supercharger for a gas turbine engine
FR2900636B1 (fr) 2006-05-05 2009-03-06 Hispano Suiza Sa Circuit d'alimentation en energie electrique pour des equipements electriques d'un moteur d'aeronef ou de son environnement
FR2902759B1 (fr) * 2006-06-27 2008-10-24 Turbomeca Systeme de generation de puissance pour aeronef utilisant une pile a combustible
RU2338907C1 (ru) * 2007-01-30 2008-11-20 Дмитрий Александрович Новосельцев Газотурбинная установка для производства электроэнергии, сжатого воздуха и механического привода оборудования
FR2914697B1 (fr) 2007-04-06 2012-11-30 Turbomeca Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration
FR2929324B1 (fr) 2008-03-25 2012-10-12 Turbomeca Turbomoteur comportant une machine electrique reversible
JP4459280B2 (ja) * 2008-05-13 2010-04-28 川崎重工業株式会社 エンジンの発電・スタータ装置
GB2466871A (en) * 2009-01-07 2010-07-14 Champion Aerospace Inc DC aircraft power supply having voltage modulation attenuator
US7869234B2 (en) * 2009-03-25 2011-01-11 Ametek, Inc. Poly-phase AC/DC active power converter
US8148834B2 (en) * 2009-05-19 2012-04-03 General Electric Company Aircraft engine starting/generating system and method of control
FR2972711B1 (fr) * 2011-03-17 2013-04-19 Hispano Suiza Sa Alimentation en energie electrique d'un aeronef
DE102011119644B4 (de) * 2011-11-28 2017-11-16 Airbus Operations Gmbh Steuern eines elektrischen Verbrauchers eines Luftfahrzeugs
DE102011121707A1 (de) * 2011-12-20 2013-07-04 Airbus Operations Gmbh Elektrisches System für ein Luftfahrzeug

Also Published As

Publication number Publication date
RU2598476C2 (ru) 2016-09-27
EP2652269A1 (fr) 2013-10-23
CA2816512A1 (fr) 2012-06-21
EP2652269B1 (fr) 2018-03-07
CN103228872A (zh) 2013-07-31
JP2014501875A (ja) 2014-01-23
FR2968716B1 (fr) 2012-12-28
KR101914313B1 (ko) 2018-11-01
WO2012080633A1 (fr) 2012-06-21
FR2968716A1 (fr) 2012-06-15
CN103228872B (zh) 2015-07-01
US20130234506A1 (en) 2013-09-12
JP5923515B2 (ja) 2016-05-24
CA2816512C (fr) 2018-12-04
KR20130140023A (ko) 2013-12-23
US8866318B2 (en) 2014-10-21
RU2013123511A (ru) 2015-01-20
ES2664773T3 (es) 2018-04-23

Similar Documents

Publication Publication Date Title
PL2652269T3 (pl) Sposób sterowania wytwarzaniem energii elektrycznej wykorzystywanej w turbinie gazowej statku powietrznego i urządzenie do wdrażania takiego sposobu
EP3075982A4 (en) Gas turbine suitable for renewable energy and control method thereof
LT2694808T (lt) Vėjo jėgainė ir vėjo jėgainės eksploatavimo būdas
GB2543622B (en) A Method of Operating a Hybrid Combustion Turbine Power Generation System
EP2672089A4 (en) Control device for gas turbine power generation plant
EP2590304A3 (en) Wind turbine generator and wind turbine
PL2469084T3 (pl) Sposób i układ sterowania mocą wyjściową turbiny wiatrowej
ZA201207580B (en) Method for the operation of a wind turbine
ZA201102950B (en) Concentrated solar power gas turbine and concentrated-solar-power-gas turbine power generating equipment
GB2498458B (en) Method for operating a wind turbine generator
SG11201403015WA (en) Geared turbofan gas turbine engine architecture
SG11201402667QA (en) Geared turbofan gas turbine engine architecture
SG11201403012PA (en) Geared turbofan gas turbine engine architecture
SG11201402823TA (en) Geared turbofan gas turbine engine architecture
EP2540993A4 (en) Aircraft gas turbine
SG11201402824RA (en) Geared turbofan gas turbine engine architecture
SG11201403011RA (en) Geared turbofan gas turbine engine architecture
EP2407646B8 (de) Verfahren und Vorrichtung zur Einstellung der Rotorlage bei einer Gasturbine oder Dampfturbine
EP2375062A4 (en) WIND TURBINE GENERATOR DEVICE AND METHOD FOR CONTROLLING THE WIND TURBINE GENERATOR DEVICE
PT2617993T (pt) Gerador de turbina eólica e procedimento operativo para o mesmo
PL2609313T3 (pl) Sposób optymalizowania regulacji zespołu mocy z turbiną swobodną do statku powietrznego oraz jednostka sterująca do wdrożenia tego sposobu
EP2844869A4 (en) WIND TURBINE SYSTEM AND METHOD OF OPERATING A WIND TURBINE SYSTEM
EP2776711A4 (en) METHOD FOR OPERATING A WIND TURBINE AND CONTROLLING THEREOF
EP2682586A3 (en) Gas turbine combustor and operating method for gas turbine combustor
EP2620605A4 (en) METHOD AND CONTROL DEVICE FOR TURBINE GENERATOR