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
Authority: FR; France
Prior art keywords: turbomotors; aircraft; power balancing; balancing; power
Prior art date: 2006-06-19
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.)

2006-06-19

Filing date

2006-06-19

Publication date

2008-08-08

2006-06-19 Application filed by Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA

2006-06-19 Priority to FR0605477A priority Critical patent/FR2902408B1/fr

2007-06-07 Priority to CA2590991A priority patent/CA2590991C/fr

2007-06-15 Priority to IT000428A priority patent/ITTO20070428A1/it

2007-06-18 Priority to CNB2007101119785A priority patent/CN100540399C/zh

2007-06-19 Priority to US11/764,825 priority patent/US9346553B2/en

2007-12-21 Publication of FR2902408A1 publication Critical patent/FR2902408A1/fr

2008-08-08 Application granted granted Critical

2008-08-08 Publication of FR2902408B1 publication Critical patent/FR2902408B1/fr

Status Expired - Fee Related legal-status Critical Current

2026-06-19 Anticipated expiration legal-status Critical

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)
Combined Controls Of Internal Combustion Engines (AREA)
Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Testing Of Balance (AREA)
Retarders (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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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
US9593591B2 (en)	2013-03-13	2017-03-14	Rolls-Royce Corporation	Engine health monitoring and power allocation control for a turbine engine using electric generators
US9638101B1 (en)	2013-03-14	2017-05-02	Tucson Embedded Systems, Inc.	System and method for automatically controlling one or multiple turbogenerators
GB2515141B (en) *	2013-03-25	2015-10-21	Honeywell Int Inc	Multi-engine performance margin synchronization adaptive control system and method
US9458771B2 (en)	2013-03-25	2016-10-04	Honeywell International Inc.	Multi-engine performance margin synchronization adaptive control system and method
US9889944B2 (en) *	2013-08-28	2018-02-13	United Technologies Corporation	Multi-engine aircraft thrust balancing
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
US10723473B2 (en)	2015-12-03	2020-07-28	Honda Patents & Technologies North America, Llc	Method for dynamic command limiting in a distributed control system
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
EP3931096A4 (fr) *	2019-03-01	2022-11-23	Pratt & Whitney Canada Corp.	Équilibrage de couple pour systèmes de propulsion électrique hybrides et aéronef utilisant des systèmes de propulsion électrique hybrides
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

2006
- 2006-06-19 FR FR0605477A patent/FR2902408B1/fr not_active Expired - Fee Related
2007
- 2007-06-07 CA CA2590991A patent/CA2590991C/fr active Active
- 2007-06-15 IT IT000428A patent/ITTO20070428A1/it unknown
- 2007-06-18 CN CNB2007101119785A patent/CN100540399C/zh not_active Expired - Fee Related
- 2007-06-19 US US11/764,825 patent/US9346553B2/en not_active Expired - Fee Related

Also Published As

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

Publication	Publication Date	Title
FR2902408B1 (fr)	2008-08-08	Equilibrage en puissance de deux turbomoteurs d'un aeronef
NO20065943L (no)	2008-06-23	Kraftkabel/kraftumibilikal
FR2902933B1 (fr)	2008-09-05	Combineur/diviseur de puissance
DE602007010524D1 (de)	2010-12-30	Sekundärbatterie
FI20070841A (fi)	2007-11-07	Kondensaattorinvaraamismenetelmiä ja -laitteistoja
BR112013010226A2 (pt)	2016-09-13	"conversor eletrônico de potência "
HK1107729A1 (en)	2008-04-11	Three level power converter
EP1864844A4 (fr)	2011-04-27	Structure de refroidissement de batterie secondaire
IL195587A0 (en)	2009-09-01	Flashlight view of an anatomical structure
BRPI0404605B1 (pt)	2013-10-15	Formulação de gasolina de aviação
FI20060759A (fi)	2008-02-26	Rinnankytkettyjen taajuusmuuttajien tehotasapaino
GB0409859D0 (en)	2004-06-09	Measurement of laxity of human joints
FI20060868A0 (fi)	2006-09-29	Tehomuuttajan tehokomponenttien jäähdytys
EP1890761A4 (fr)	2010-08-11	Methodes permettant d'augmenter la lipolyse
NO20054115D0 (no)	2005-09-05	Kraftkabel
EP2018516A4 (fr)	2013-01-09	Demarreur de puissance de gyroscope
GB2426466B (en)	2009-12-02	Climbing aid
GB0421576D0 (en)	2004-10-27	Balancing assembly
GB2436074B (en)	2008-02-20	Balance assembly of an exercise auxiliary system
FR2890486B1 (fr)	2008-02-01	Condensateur de puissance
FR2879040B1 (fr)	2007-11-30	Coupleur de batteries
FR2870057B1 (fr)	2006-08-04	Convertisseur de puissance
ITPO20050002U1 (it)	2005-04-13	Apparecchiatura idroterapica multifunzionale
FR2868886B1 (fr)	2008-09-05	Bus de puissance
GB0607685D0 (en)	2006-05-31	Zero point power generator

Legal Events

Date	Code	Title	Description
2014-07-04	CD	Change of name or company name	Owner name: AIRBUS HELICOPTERS, FR Effective date: 20140602
2016-06-27	PLFP	Fee payment	Year of fee payment: 11
2017-06-21	PLFP	Fee payment	Year of fee payment: 12
2018-06-20	PLFP	Fee payment	Year of fee payment: 13
2020-06-19	PLFP	Fee payment	Year of fee payment: 15
2022-03-11	ST	Notification of lapse	Effective date: 20220205