PL3401530T3 - Sposób i system ustawiania harmonogramu przyspieszenia do rozruchu silnika - Google Patents

Sposób i system ustawiania harmonogramu przyspieszenia do rozruchu silnika

Info

Publication number
PL3401530T3
PL3401530T3 PL18171688T PL18171688T PL3401530T3 PL 3401530 T3 PL3401530 T3 PL 3401530T3 PL 18171688 T PL18171688 T PL 18171688T PL 18171688 T PL18171688 T PL 18171688T PL 3401530 T3 PL3401530 T3 PL 3401530T3
Authority
PL
Poland
Prior art keywords
setting
engine start
acceleration schedule
schedule
acceleration
Prior art date
Application number
PL18171688T
Other languages
English (en)
Inventor
Sylvain Lamarre
Pierre Alexandre
Original Assignee
Pratt & Whitney Canada Corp.
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 Pratt & Whitney Canada Corp. filed Critical Pratt & Whitney Canada Corp.
Publication of PL3401530T3 publication Critical patent/PL3401530T3/pl

Links

Classifications

    • 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
    • F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
    • 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
    • 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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F05D2260/00—Function
    • F05D2260/85—Starting
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/04—Purpose of the control system to control acceleration (u)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
PL18171688T 2017-05-10 2018-05-10 Sposób i system ustawiania harmonogramu przyspieszenia do rozruchu silnika PL3401530T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/591,696 US10352189B2 (en) 2017-05-10 2017-05-10 Method and system for setting an acceleration schedule for engine start
EP18171688.7A EP3401530B1 (en) 2017-05-10 2018-05-10 Method and system for setting an acceleration schedule for engine start

Publications (1)

Publication Number Publication Date
PL3401530T3 true PL3401530T3 (pl) 2022-01-10

Family

ID=62165362

Family Applications (1)

Application Number Title Priority Date Filing Date
PL18171688T PL3401530T3 (pl) 2017-05-10 2018-05-10 Sposób i system ustawiania harmonogramu przyspieszenia do rozruchu silnika

Country Status (4)

Country Link
US (2) US10352189B2 (pl)
EP (1) EP3401530B1 (pl)
CA (1) CA3002390A1 (pl)
PL (1) PL3401530T3 (pl)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10352189B2 (en) * 2017-05-10 2019-07-16 Pratt & Whitney Canada Corp. Method and system for setting an acceleration schedule for engine start
CN109896022B (zh) * 2019-03-28 2023-12-08 河南机电职业学院 一种轻型无人机高压气动助推起飞装置
CN112731055B (zh) * 2020-12-21 2023-01-06 潍柴动力股份有限公司 起动机线路故障检测方法、装置及发动机电控设备、介质
US12571350B2 (en) 2023-07-28 2026-03-10 Rolls-Royce Corporation Multi-modal gas-turbine engine starting
US12529340B2 (en) 2023-07-28 2026-01-20 Rolls-Royce Corporation Emergency start of a gas turbine engine
US12398678B2 (en) 2023-07-28 2025-08-26 Rolls-Royce Corporation Motor and motor controller thermal management features
US12535016B2 (en) 2023-08-11 2026-01-27 Pratt & Whitney Canada Corp. Systems and methods for identifying insufficient starter acceleration for an aircraft engine

Family Cites Families (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4321791A (en) 1979-12-26 1982-03-30 Eaton Corporation Electronic fuel control system for a gas turbine engine
US4593523A (en) * 1980-12-17 1986-06-10 Allied Corporation Method and apparatus for acceleration limiting a gas turbine engine
US4648797A (en) * 1983-12-19 1987-03-10 United Technologies Corporation Torque control system
GB8911806D0 (en) 1989-05-23 1989-07-12 Rolls Royce Plc Gas turbine engine fuel control system with enhanced relight capability
US5907949A (en) 1997-02-03 1999-06-01 United Technologies Corporation Starting fuel control method for a turbine engine
US6810676B2 (en) 2001-12-14 2004-11-02 Pratt & Whitney Canada Corp. Method of engine starting in a gas turbine engine
AU2003249698A1 (en) * 2002-07-12 2004-02-02 Cummins Inc. Start -up control of internal combustion engines
US7506517B2 (en) * 2004-11-23 2009-03-24 Honeywell International, Inc. System and method for turbine engine startup profile characterization
US20060129301A1 (en) * 2004-12-14 2006-06-15 General Electric Company Method and apparatus for assessing gas turbine acceleration capability
US7448220B2 (en) * 2005-10-19 2008-11-11 Hamilton Sundstrand Corporation Torque control for starting system
WO2007102763A1 (en) * 2006-03-09 2007-09-13 Volvo Technology Corporation Hybrid powertrain
US7854582B2 (en) * 2007-05-08 2010-12-21 Pratt & Whitney Canada Corp. Operation of an aircraft engine after emergency shutdown
US7926287B2 (en) * 2007-05-08 2011-04-19 Pratt & Whitney Canada Corp. Method of operating a gas turbine engine
US20100083632A1 (en) * 2008-10-08 2010-04-08 Searete Llc, A Limited Liability Corporation Of The State Of Delaware Hybrid propulsive engine including at least one independently rotatable compressor rotor
US8109073B2 (en) * 2008-10-08 2012-02-07 The Invention Science Fund I, Llc Hybrid propulsive engine including at least one independently rotatable compressor stator
US8954228B2 (en) * 2008-12-30 2015-02-10 Rolls-Royce Corporation Gas turbine engine failure detection
JP2011043136A (ja) 2009-08-24 2011-03-03 Honda Motor Co Ltd ガスタービン・エンジンの始動時燃料制御装置
US20110146292A1 (en) 2009-12-23 2011-06-23 General Electric Company Method for starting a turbomachine
US8566000B2 (en) * 2010-02-23 2013-10-22 Williams International Co., L.L.C. System and method for controlling a single-spool turboshaft engine
FR2968716B1 (fr) * 2010-12-13 2012-12-28 Turbomeca Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et turbomoteur mettant en oeuvre un tel procede
US8626372B2 (en) * 2011-09-15 2014-01-07 General Electric Company Systems and methods for diagnosing an engine
FR2986571B1 (fr) * 2012-02-06 2014-02-21 Eurocopter France Dispositif et procede de regulation d'un turbomoteur, et aeronef
US9447747B2 (en) * 2012-05-04 2016-09-20 Ford Global Technologies, Llc Methods and systems for stopping an engine
FR2995345B1 (fr) 2012-09-10 2018-06-15 Safran Helicopter Engines Procede et systeme de demarrage d'un turbomoteur d'aeronef
CN105408151A (zh) * 2013-03-15 2016-03-16 储存能源解决方案公司 液压混合系统
US9035478B2 (en) * 2013-08-26 2015-05-19 Ge Aviation Systems, Llc Aircraft engine constant frequency starter/generator
US9126591B2 (en) * 2013-10-18 2015-09-08 Ford Global Technologies, Llc Hybrid vehicle powertrain management system and method
EP2878795B8 (en) * 2013-11-27 2016-10-12 Airbus Operations GmbH Engine for propelling an aircraft and aircraft having at least one engine and at least one hydrogen tank
FR3015571B1 (fr) * 2013-12-23 2018-11-23 Safran Helicopter Engines Procede et systeme de demarrage fiabilise de turbomachine
US9604628B2 (en) * 2014-01-17 2017-03-28 Ford Global Technologies, Llc Powertrain control of a hybrid vehicle in park or neutral
GB201403178D0 (en) * 2014-02-24 2014-04-09 Rolls Royce Plc Electrical power generator for a gas turbine engine
US10309304B2 (en) * 2014-03-04 2019-06-04 Sikorsky Aircraft Corporation Electrical augmentation of a gas turbine engine
FR3025252B1 (fr) * 2014-08-29 2021-10-29 Microturbo Dispositif et procede de demarrage d'une turbine a gaz, procede de regulation de la vitesse de rotation d'une turbine a gaz, et turbine a gaz et turbomoteur associes
US10233838B2 (en) * 2014-09-09 2019-03-19 The United States Of America, As Represented By The Secretary Of The Navy Recuperated gas turbine engine
EP2995798A1 (en) * 2014-09-11 2016-03-16 Toyota Jidosha Kabushiki Kaisha Control apparatus for internal combustion engine
US10703215B2 (en) * 2014-10-20 2020-07-07 Ford Global Technologies, Llc Hybrid powertrain speed control
US9988038B2 (en) * 2015-04-09 2018-06-05 Ford Global Technologies, Llc Methods and system for controlling torque flow through a torque converter
US20170158324A1 (en) * 2015-12-07 2017-06-08 Daniel Keith Schlak Vertical takeoff and landing aircraft and gas turbine engine with fan thrust and exhaust thrust delivered downwardly
US10508601B2 (en) * 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
CN108883824A (zh) * 2016-03-23 2018-11-23 冯春魁 飞行器的数据的获取、处理及飞行状况监控的方法及系统
US10815824B2 (en) * 2017-04-04 2020-10-27 General Electric Method and system for rotor overspeed protection
US10352189B2 (en) * 2017-05-10 2019-07-16 Pratt & Whitney Canada Corp. Method and system for setting an acceleration schedule for engine start
US10633104B2 (en) * 2017-05-17 2020-04-28 General Electric Company Hybrid-electric propulsion system for an aircraft
US10676199B2 (en) * 2017-06-12 2020-06-09 General Electric Company Propulsion system for an aircraft
US10483887B2 (en) * 2017-08-11 2019-11-19 Rolls-Royce North American Technologies, Inc. Gas turbine generator temperature DC to DC converter control system
US10476417B2 (en) * 2017-08-11 2019-11-12 Rolls-Royce North American Technologies Inc. Gas turbine generator torque 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
US10378452B1 (en) * 2018-02-26 2019-08-13 The Boeing Company Hybrid turbine jet engines and methods of operating the same
EP3543504B1 (en) * 2018-03-23 2022-10-19 Ge Avio S.r.l. Control system and method for propeller-speed overshoot limitation in a turbopropeller engine
US20190323426A1 (en) * 2018-04-19 2019-10-24 The Boeing Company Supercharging systems for aircraft engines
US10981660B2 (en) * 2018-04-19 2021-04-20 The Boeing Company Hybrid propulsion engines for aircraft
US10968825B2 (en) * 2018-04-19 2021-04-06 The Boeing Company Flow multiplier systems for aircraft
US11565821B2 (en) * 2018-07-30 2023-01-31 Raytheon Technologies Corporation Hybrid energy storage system control for an aircraft engine
US20200056551A1 (en) * 2018-08-20 2020-02-20 United Technologies Corporation Aircraft engine idle suppressor and method
CN110886656B (zh) * 2018-09-11 2024-06-18 普拉特-惠特尼加拿大公司 用于为发动机启动设定加速度计划的方法与系统
US11319880B2 (en) * 2018-10-26 2022-05-03 Rolls-Royce North American Technologies, Inc. Electrical controller for engine-driven electric machine
GB201819694D0 (en) * 2018-12-03 2019-01-16 Rolls Royce Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine
GB201819696D0 (en) * 2018-12-03 2019-01-16 Rolls Royce Plc Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine
GB201819695D0 (en) * 2018-12-03 2019-01-16 Rolls Royce Plc Methods and apparatus for controlling at least part of a start-up or re-light process of a gas turbine engine
GB201906526D0 (en) * 2019-05-09 2019-06-26 Rolls Royce Plc Hybrid electric aircraft propulsion system
EP3772148A1 (en) * 2019-07-29 2021-02-03 Raytheon Technologies Corporation Hybrid electric power distribution and control for an aircraft
EP3798119B1 (en) * 2019-09-30 2023-02-22 Ratier-Figeac SAS Drive system for counter-rotating parts

Also Published As

Publication number Publication date
EP3401530A1 (en) 2018-11-14
CA3002390A1 (en) 2018-11-10
US10352189B2 (en) 2019-07-16
US20190284953A1 (en) 2019-09-19
EP3401530B1 (en) 2021-10-06
US20180328220A1 (en) 2018-11-15
US11131211B2 (en) 2021-09-28

Similar Documents

Publication Publication Date Title
PL3401530T3 (pl) Sposób i system ustawiania harmonogramu przyspieszenia do rozruchu silnika
IL259219B (en) Laser system with color spots and method for aircraft
IL263796A (en) Manipulation system and method for an airplane
SG11202007258SA (en) Blockchain ledger-based evidence acquisition method and system
HUE072459T2 (hu) Jármû, valamint jármûindítás-vezérlési eljárás és rendszer
GB2566523B (en) System and method for vehicle convoys
GB201717182D0 (en) System and method for scheduling vehicles
PL3276148T3 (pl) Układ i sposób sterowania silnikiem turbospalinowym
SG10202108617XA (en) Method and system for starting application
GB201818436D0 (en) an advanced automobile engine device and using method thereof
PL3279450T3 (pl) System i metoda dla sterownika silnika oparte na mocy przyspieszania
GB201603443D0 (en) Method and apparatus to control an ignition system
KR20180084848A (ko) 점화 시스템을 제어하는 방법 및 장치
GB2537598B (en) Method of controlling an engine system
HUE059817T2 (hu) Rendszer és eljárás dízelgenerátor összeállítás integrált vezérlõrendszeréhez
GB201819438D0 (en) Method and system for monitoring the mass of an object
GB2600350B (en) System and method for controlling engine
EP4061763C0 (en) ENGINE SUPPORT SYSTEM AND METHOD
ZA201905146B (en) System, method and apparatus for solid fuel ignition
KR20180084850A (ko) 점화 시스템을 제어하는 방법 및 장치
EP3314208A4 (en) System and method for real time scheduling
HUE054817T2 (hu) Rendszer és eljárás egy jármû régiók közötti üzemeltetéséhez
PT3404570T (pt) Procedimento e sistema para autenticação baseada em comportamento
GB2535852B (en) Engine intake system and method for operating same
GB2527103B (en) A method and system for a spark ignition engine