CA2874962C - Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere - Google Patents

Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere Download PDF

Info

Publication number
CA2874962C
CA2874962C CA2874962A CA2874962A CA2874962C CA 2874962 C CA2874962 C CA 2874962C CA 2874962 A CA2874962 A CA 2874962A CA 2874962 A CA2874962 A CA 2874962A CA 2874962 C CA2874962 C CA 2874962C
Authority
CA
Canada
Prior art keywords
power
main
engine
auxiliary
engines
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
CA2874962A
Other languages
English (en)
French (fr)
Other versions
CA2874962A1 (fr
Inventor
Pascal Dauriac
Olivier Bedrine
Patrick Marconi
Jean-Francois Rideau
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.)
Safran Helicopter Engines SAS
Safran Power Units SAS
Original Assignee
Safran Power Units SAS
Turbomeca 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 Safran Power Units SAS, Turbomeca SA filed Critical Safran Power Units SAS
Publication of CA2874962A1 publication Critical patent/CA2874962A1/fr
Application granted granted Critical
Publication of CA2874962C publication Critical patent/CA2874962C/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
    • 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
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/02—Plural gas-turbine plants having a common power output
    • 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
    • F02C7/277—Mechanical drives the starter being a separate turbine
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
    • 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
    • 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
    • Y02T50/50—On board measures aiming to increase energy efficiency
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)
  • Hybrid Electric Vehicles (AREA)
CA2874962A 2012-06-15 2013-06-12 Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere Expired - Fee Related CA2874962C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1255599 2012-06-15
FR1255599A FR2992024B1 (fr) 2012-06-15 2012-06-15 Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere
PCT/FR2013/051376 WO2014009620A1 (fr) 2012-06-15 2013-06-12 Procédé et architecture de transfert d'énergie optimisé entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere

Publications (2)

Publication Number Publication Date
CA2874962A1 CA2874962A1 (fr) 2014-01-16
CA2874962C true CA2874962C (fr) 2021-03-30

Family

ID=47049238

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2874962A Expired - Fee Related CA2874962C (fr) 2012-06-15 2013-06-12 Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere

Country Status (12)

Country Link
US (1) US10059460B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EP (1) EP2861493B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JP6313756B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
KR (1) KR102097841B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CN (1) CN104379450B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA2874962C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
ES (1) ES2698953T3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2992024B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IN (1) IN2014DN10616A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
PL (1) PL2861493T3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
RU (1) RU2629621C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
WO (1) WO2014009620A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2986780B1 (fr) * 2012-02-13 2014-11-14 Motorisations Aeronautiques Dispositif d’alimentation en air d’un groupe auxiliaire de puissance d’un aeronef, aeronef
FR2992630B1 (fr) * 2012-06-29 2015-02-20 Turbomeca Procede et configuration d'apport d'energie propulsive et/ou non propulsive dans une architecture d'helicoptere par un moteur auxiliaire de puissance
US8939399B2 (en) 2012-07-31 2015-01-27 Textron Innovations Inc. System and method of augmenting power in a rotorcraft
US10569892B2 (en) 2013-05-06 2020-02-25 Sikorsky Aircraft Corporation Supplemental power for reduction of prime mover
FR3008679B1 (fr) * 2013-07-16 2015-08-14 Eurocopter France Installation motrice modulaire et aeronef muni d'un rotor de sustentation
FR3019220A1 (fr) * 2014-03-27 2015-10-02 Turbomeca Procede de redemarrage alternatif d'un turbomoteur en veille d'un helicoptere et architecture multi-moteur permettant la mise en œuvre d'un tel procede
FR3019219B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant
FR3019224B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Procede d'assistance d'un turbomoteur en veille d'un helicoptere multi-moteur et architecture d'un systeme propulsif d'un helicoptere comprenant au moins un turbomoteur pouvant etre en veille
FR3019358B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Procede de gestion globale optimisee d'un reseau energetique d'un aeronef et dispositif correspondant
FR3019218B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant
FR3019588B1 (fr) * 2014-04-08 2019-06-14 Safran Helicopter Engines Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif et procede correspondant
US10066547B2 (en) 2014-07-01 2018-09-04 United Technologies Corporation Combined two engine cycle with at least one recuperated cycle engine for rotor drive
FR3024180B1 (fr) * 2014-07-28 2016-07-22 Turbomeca Dispositif pneumatique de reactivation rapide d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel dispositif et helicoptere correspondant
FR3026435B1 (fr) * 2014-09-29 2016-10-21 Turbomeca Dispositif et procede de test d'integrite d'un systeme de reactivation rapide d'un turbomoteur d'un helicoptere
FR3031500B1 (fr) 2015-01-12 2017-01-13 Turbomeca Dispositif et procede de regulation d'un moteur auxiliaire adapte pour fournir une puissance propulsive au rotor d'un helicoptere
FR3036235B1 (fr) 2015-05-15 2018-06-01 Airbus Helicopters Procede pour activer un moteur electrique d'une installation hybride d'un aeronef multimoteur et un aeronef
FR3043724A1 (fr) * 2015-11-16 2017-05-19 Snecma Procede de dimensionnement d'un ensemble propulsif comprenant un moteur principal et un moteur auxiliaire
US10723452B2 (en) * 2017-02-15 2020-07-28 Sikorsky Aircraft Corporation Engine systems for rotorcraft
US10393017B2 (en) * 2017-03-07 2019-08-27 Rolls-Royce Corporation System and method for reducing specific fuel consumption (SFC) in a turbine powered aircraft
FR3078057B1 (fr) * 2018-02-19 2022-04-22 Safran Helicopter Engines Architecture de systeme propulsif d'un helicoptere bimoteurs
US11415044B2 (en) * 2018-06-19 2022-08-16 Raytheon Technologies Corporation Multi-engine architecture with linkages to multiple spools
CN109339952B (zh) * 2018-09-29 2020-01-21 北京航空航天大学 一种直升机的发动机启动系统和机载能量管理系统
US10954863B2 (en) 2019-04-09 2021-03-23 General Electric Company Phasing gearbox
US11663863B2 (en) 2019-06-07 2023-05-30 Pratt & Whitney Canada Corp. Methods and systems for operating a rotorcraft
US11479348B2 (en) 2019-08-31 2022-10-25 Textron Innovations Inc. Power management systems for multi engine rotorcraft
RU2729311C1 (ru) * 2020-01-29 2020-08-05 Борис Яппарович Альмухаметов Гибридная турбовентиляторная установка со встроенным роторным ДВС
EP3904217B1 (en) 2020-04-27 2022-09-28 LEONARDO S.p.A. Aircraft capable of hovering
US11608189B2 (en) * 2020-08-11 2023-03-21 Textron Innovations Inc Multistage infrared suppression exhaust system
US11434824B2 (en) 2021-02-03 2022-09-06 General Electric Company Fuel heater and energy conversion system
CN113323757B (zh) * 2021-06-01 2022-12-20 北京清软创想信息技术有限责任公司 一种分离式气压型辅助动力空气管路系统
IT202200006545A1 (it) 2022-04-01 2023-10-01 Ge Avio Srl Metodo ed apparecchiatura per calibrare un sensore di coppia di un motore aeronautico
US12385434B2 (en) * 2022-06-26 2025-08-12 Rtx Corporation Aircraft powerplant with boosted gas turbine engine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3455182A (en) * 1967-04-12 1969-07-15 Garrett Corp Helicopter lift augmentation means
US3963372A (en) * 1975-01-17 1976-06-15 General Motors Corporation Helicopter power plant control
US5054716A (en) * 1989-10-16 1991-10-08 Bell Helicopter Textron Inc. Drive system for tiltrotor aircraft
FR2670553B1 (fr) * 1990-12-12 1993-04-02 Aerospatiale Mecanisme de transmission de puissance entre un arbre moteur et deux ensembles a entrainer, utilisable notamment sur les giravions.
US5239830A (en) * 1992-03-05 1993-08-31 Avco Corporation Plural engine power producing system
US6098921A (en) * 1999-05-06 2000-08-08 Piasecki Aircraft Corp. Rotary wing aircraft supplementary power drive system
RU2224686C1 (ru) * 2003-04-07 2004-02-27 Открытое акционерное общество "Казанский вертолетный завод" Вертолёт
DE102005046729B4 (de) * 2005-09-29 2012-01-05 Airbus Operations Gmbh Energieversorgungssystem für die Versorgung von Luftfahrzeugsystemen
GB0714924D0 (en) * 2007-08-01 2007-09-12 Rolls Royce Plc An engine arrangement
GB2460246B (en) * 2008-05-21 2012-09-19 Matthew P Wood Helicopter with auxiliary power unit for emergency rotor power
FR2962488B1 (fr) * 2010-07-06 2014-05-02 Turbomeca Procede et architecture de recombinaison de puissance de turbomachine
US8845898B2 (en) * 2010-07-07 2014-09-30 Hamilton Sundstrand Corporation APU fuel filter housing scupper
US8684304B2 (en) 2010-11-16 2014-04-01 Rolls-Royce Corporation Aircraft, propulsion system, and system for taxiing an aircraft

Also Published As

Publication number Publication date
JP2015525321A (ja) 2015-09-03
JP6313756B2 (ja) 2018-04-18
IN2014DN10616A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 2015-09-11
US10059460B2 (en) 2018-08-28
CN104379450B (zh) 2017-05-31
FR2992024A1 (fr) 2013-12-20
ES2698953T3 (es) 2019-02-06
KR102097841B1 (ko) 2020-04-06
EP2861493A1 (fr) 2015-04-22
RU2014150999A (ru) 2016-08-10
PL2861493T3 (pl) 2019-03-29
CA2874962A1 (fr) 2014-01-16
KR20150030203A (ko) 2015-03-19
WO2014009620A1 (fr) 2014-01-16
US20150122944A1 (en) 2015-05-07
FR2992024B1 (fr) 2017-07-21
EP2861493B1 (fr) 2018-10-17
RU2629621C2 (ru) 2017-08-30
CN104379450A (zh) 2015-02-25

Similar Documents

Publication Publication Date Title
CA2874962C (fr) Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere
CA2876952C (fr) Procede et configuration d'apport d'energie propulsive et/ou non propulsive dans une architecture d'helicoptere par un moteur auxiliaire de puissance
EP2591219B1 (fr) Procédé et architecture de recombinaison de puissance de turbomachine
US11084591B2 (en) Aircraft cabin blower system having a transmission receiving mechanical power from a first and seccond input wherein the first input is configured to receive mechanical power from a turbine engine and a first electrical machine to configured to receive mechanical power from the turbine engine independent of the transmission
CA2843802C (fr) Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie
FR2964087A1 (fr) Procede d'optimisation de l'operabilite de motorisation d'un aeronef et groupe de puissance autonome de mise en oeuvre
FR3033830B1 (fr) Groupe de puissance pour aeronefs
WO2025012539A1 (fr) Ensemble propulsif d'aeronef et procede de gestion thermique
FR2944260A1 (fr) Systeme de generation de puissance electrique pour aeronef a propulsion arriere
FR3150183A1 (fr) Turbomachine à hybridation électrique parallèle
FR3033831A1 (fr) Moteur pour aeronefs
WO2024023413A1 (fr) Ensemble propulsif amélioré pour aéronef hybridé multimoteurs
EP4562285A1 (fr) Ensemble propulsif ameliore pour aeronef hybride multi moteurs
WO2016146939A1 (fr) Perfectionnements aux groupes de puissance pour aéronefs
FR2944261A1 (fr) Systeme de generation de puissance electrique pour aeronef a propulsion arriere

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20180516

MKLA Lapsed

Effective date: 20220613