FR2902408B1 - Equilibrage en puissance de deux turbomoteurs d'un aeronef - Google Patents

Equilibrage en puissance de deux turbomoteurs d'un aeronef

Info

Publication number
FR2902408B1
FR2902408B1 FR0605477A FR0605477A FR2902408B1 FR 2902408 B1 FR2902408 B1 FR 2902408B1 FR 0605477 A FR0605477 A FR 0605477A FR 0605477 A FR0605477 A FR 0605477A FR 2902408 B1 FR2902408 B1 FR 2902408B1
Authority
FR
France
Prior art keywords
turbomotors
aircraft
power balancing
balancing
power
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
FR0605477A
Other languages
English (en)
Other versions
FR2902408A1 (fr
Inventor
Francois Xavier Gaulmin
Lionel Iraudo
Daniel Chaniot
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0605477A priority Critical patent/FR2902408B1/fr
Priority to CA2590991A priority patent/CA2590991C/fr
Priority to IT000428A priority patent/ITTO20070428A1/it
Priority to CNB2007101119785A priority patent/CN100540399C/zh
Priority to US11/764,825 priority patent/US9346553B2/en
Publication of FR2902408A1 publication Critical patent/FR2902408A1/fr
Application granted granted Critical
Publication of FR2902408B1 publication Critical patent/FR2902408B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • B64D31/12—Initiating means actuated automatically for equalising or synchronising 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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Retarders (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Testing Of Balance (AREA)
FR0605477A 2006-06-19 2006-06-19 Equilibrage en puissance de deux turbomoteurs d'un aeronef Expired - Fee Related FR2902408B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0605477A FR2902408B1 (fr) 2006-06-19 2006-06-19 Equilibrage en puissance de deux turbomoteurs d'un aeronef
CA2590991A CA2590991C (fr) 2006-06-19 2007-06-07 Equilibrage en puissance de deux turbomoteurs d'un aeronef
IT000428A ITTO20070428A1 (it) 2006-06-19 2007-06-15 Equilibratura in potenza di due turbomotori di un aeromobile
CNB2007101119785A CN100540399C (zh) 2006-06-19 2007-06-18 平衡一架飞行器的两台涡轮轴发动机的功率的方法和系统
US11/764,825 US9346553B2 (en) 2006-06-19 2007-06-19 Balancing the power of two turboshaft engines of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0605477A FR2902408B1 (fr) 2006-06-19 2006-06-19 Equilibrage en puissance de deux turbomoteurs d'un aeronef

Publications (2)

Publication Number Publication Date
FR2902408A1 FR2902408A1 (fr) 2007-12-21
FR2902408B1 true FR2902408B1 (fr) 2008-08-08

Family

ID=37728267

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0605477A Expired - Fee Related FR2902408B1 (fr) 2006-06-19 2006-06-19 Equilibrage en puissance de deux turbomoteurs d'un aeronef

Country Status (5)

Country Link
US (1) US9346553B2 (fr)
CN (1) CN100540399C (fr)
CA (1) CA2590991C (fr)
FR (1) FR2902408B1 (fr)
IT (1) ITTO20070428A1 (fr)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2932919B1 (fr) 2008-06-24 2010-08-20 Eurocopter France Adaptation d'alertes de terrain selectives, en fonction la manoeuvrabilite instantanee d'un giravion
FR2946015B1 (fr) * 2009-06-02 2011-07-15 Airbus France Systeme de gestion automatique de modes de controle de moteurs d'un aeronef multimoteur.
FR2950324B1 (fr) * 2009-09-23 2011-08-26 Eurocopter France Procede et dispositif d'aide au pilotage d'un aeronef en cas de pannes d'un indicateur de premiere limitation
FR2967213B1 (fr) * 2010-11-10 2012-10-26 Eurocopter France Procede de commande pour systeme de securite survitesse de moteurs d'aeronef et circuit de commande pour mettre en oeuvre ledit procede
FR2973340B1 (fr) * 2011-03-30 2013-04-12 Eurocopter France Procede, dispositif d'aide au pilotage d'un aeronef, et aeronef
FR2985715B1 (fr) 2012-01-12 2013-12-27 Eurocopter France Installation motrice d'un aeronef, aeronef, et procede de pilotage dudit aeronef
FR2986506B1 (fr) 2012-02-06 2015-06-26 Eurocopter France Procede et dispositif pour realiser un controle de sante d'un turbomoteur d'un aeronef pourvu d'au moins un turbomoteur
FR2998058B1 (fr) * 2012-11-13 2016-02-05 Microturbo Dispositif et procede de protection d'un calculateur de turbo-machine d'aeronef contre les erreurs de mesure de vitesse
CA2896470C (fr) 2013-03-13 2020-09-22 Rolls-Royce North American Technologies, Inc. Controle de sante de moteur et commande d'attribution de puissance pour un moteur a turbine a l'aide de generateurs electriques
US9429078B1 (en) * 2013-03-14 2016-08-30 Tucson Embedded Systems, Inc. Multi-compatible digital engine controller
US9458771B2 (en) 2013-03-25 2016-10-04 Honeywell International Inc. Multi-engine performance margin synchronization adaptive control system and method
GB2515141B (en) * 2013-03-25 2015-10-21 Honeywell Int Inc Multi-engine performance margin synchronization adaptive control system and method
WO2015076888A2 (fr) * 2013-08-28 2015-05-28 United Technologies Corporation Équilibrage de poussée d'aéronef à multiples moteurs
GB2524775B (en) * 2014-04-02 2017-11-15 Rolls Royce Plc Aircraft vapour trail control system
FR3037923B1 (fr) 2015-06-23 2018-05-04 Airbus Helicopters Procede de regulation d'une installation motrice trimoteur pour un aeronef a voilure tournante
WO2017095992A1 (fr) 2015-12-03 2017-06-08 Honda Patents & Technologies North America, Llc Procédé permettant une limitation de commande dynamique dans un système de commande distribué
US10293951B2 (en) * 2016-03-17 2019-05-21 United Technologies Corporation Takeoff power management system and method for gas turbine engines
KR101866534B1 (ko) * 2016-04-26 2018-06-12 주식회사 엘에스엘시스템즈 하이브리드 드론과 그 제어 방법 및 이를 수행하기 위한 컴퓨팅 장치
GB201706269D0 (en) * 2017-04-20 2017-06-07 Rolls Royce Plc Fuel control system
US20200277073A1 (en) * 2019-03-01 2020-09-03 Pratt & Whitney Canada Corp. Torque balancing for hybrid electric propulsion systems and aircraft utilizing hybrid electric propulsion systems
US11753178B2 (en) 2019-11-12 2023-09-12 General Electric Company Systems and methods for removing heat from aircraft components
FR3104138B1 (fr) * 2019-12-09 2024-03-08 Safran Helicopter Engines Système et procédé d’équilibrage d’au moins un paramètre à équilibrer d’un moteur électrique d’un système propulsif
CN113404595A (zh) 2020-03-16 2021-09-17 通用电气公司 燃气涡轮发动机及其操作方法
CN112173169A (zh) * 2020-09-25 2021-01-05 中国直升机设计研究所 一种三发直升机发动机功率自动检查方法
JP7355726B2 (ja) * 2020-12-22 2023-10-03 本田技研工業株式会社 航空機用推進システム
CN113761719B (zh) * 2021-08-16 2024-01-23 中国航发湖南动力机械研究所 在地面试验中自动控制涡轴发动机t45温度的方法及系统、设备、存储介质

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE8107800L (sv) * 1981-03-30 1982-10-01 Avco Corp Temperaturregler-/synkroniseringssystem
US4644744A (en) * 1985-04-19 1987-02-24 Allied Corporation Control device for controlling an engine of a turbine power system having more than one engine
US4817046A (en) * 1986-04-10 1989-03-28 United Technologies Corporation Detection of engine failure in a multi-engine aircraft
DE4125372C1 (en) * 1991-07-31 1992-08-13 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Monitoring aircraft power unit esp. helicopter gas turbine drives - indicating only critical instantaneous parameters on display and warning of values outside set ranges
US5315819A (en) * 1991-09-17 1994-05-31 Allied-Signal Inc. Power management system for turbine engines
US5622045A (en) * 1995-06-07 1997-04-22 Allison Engine Company, Inc. System for detecting and accommodating gas turbine engine fan damage
FR2749545B1 (fr) * 1996-06-07 1998-08-07 Eurocopter France Indicateur de pilotage pour aeronef
ITTO20040050A1 (it) * 2004-02-03 2004-05-03 Agusta Spa Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli

Also Published As

Publication number Publication date
ITTO20070428A1 (it) 2007-12-20
US9346553B2 (en) 2016-05-24
FR2902408A1 (fr) 2007-12-21
CN100540399C (zh) 2009-09-16
CN101092170A (zh) 2007-12-26
CA2590991C (fr) 2014-04-15
US20080275597A1 (en) 2008-11-06
CA2590991A1 (fr) 2007-12-19

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Legal Events

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CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 15

ST Notification of lapse

Effective date: 20220205