PL2867122T3 - Sposób i konfiguracja dostarczania energii napędowej i/albo nienapędowej do architektury śmigłowca za pomocą pomocniczego silnia mocy - Google Patents

Sposób i konfiguracja dostarczania energii napędowej i/albo nienapędowej do architektury śmigłowca za pomocą pomocniczego silnia mocy

Info

Publication number
PL2867122T3
PL2867122T3 PL13733395T PL13733395T PL2867122T3 PL 2867122 T3 PL2867122 T3 PL 2867122T3 PL 13733395 T PL13733395 T PL 13733395T PL 13733395 T PL13733395 T PL 13733395T PL 2867122 T3 PL2867122 T3 PL 2867122T3
Authority
PL
Poland
Prior art keywords
propulsive
apu
helicopter
providing
energy
Prior art date
Application number
PL13733395T
Other languages
English (en)
Inventor
Olivier Bedrine
Christian SARRAT
Fabien Silet
Sébastien VIEILLARD
Original Assignee
Safran Helicopter Engines
Safran Power Units
Safran Electrical & Power
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, Safran Power Units, Safran Electrical & Power filed Critical Safran Helicopter Engines
Publication of PL2867122T3 publication Critical patent/PL2867122T3/pl

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
    • B64D35/08—Transmitting power from power plant 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/026—
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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)
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/19—Gearing
    • Y10T74/19014—Plural prime movers selectively coupled to common output
PL13733395T 2012-06-29 2013-06-12 Sposób i konfiguracja dostarczania energii napędowej i/albo nienapędowej do architektury śmigłowca za pomocą pomocniczego silnia mocy PL2867122T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1256246A FR2992630B1 (fr) 2012-06-29 2012-06-29 Procede et configuration d'apport d'energie propulsive et/ou non propulsive dans une architecture d'helicoptere par un moteur auxiliaire de puissance
EP13733395.1A EP2867122B1 (fr) 2012-06-29 2013-06-12 Procédé et configuration d'apport d'énergie propulsive et/ou non propulsive dans une architecture d'hélicoptère par un moteur auxiliaire de puissance
PCT/FR2013/051379 WO2014001683A1 (fr) 2012-06-29 2013-06-12 Procédé et configuration d'apport d'énergie propulsive et/ou non propulsive dans une architecture d'hélicoptère par un moteur auxiliaire de puissance

Publications (1)

Publication Number Publication Date
PL2867122T3 true PL2867122T3 (pl) 2020-11-02

Family

ID=46852228

Family Applications (1)

Application Number Title Priority Date Filing Date
PL13733395T PL2867122T3 (pl) 2012-06-29 2013-06-12 Sposób i konfiguracja dostarczania energii napędowej i/albo nienapędowej do architektury śmigłowca za pomocą pomocniczego silnia mocy

Country Status (10)

Country Link
US (1) US10301035B2 (pl)
EP (1) EP2867122B1 (pl)
JP (1) JP6320373B2 (pl)
KR (1) KR102097178B1 (pl)
CN (1) CN104487345B (pl)
CA (1) CA2876952C (pl)
FR (1) FR2992630B1 (pl)
PL (1) PL2867122T3 (pl)
RU (1) RU2639838C2 (pl)
WO (1) WO2014001683A1 (pl)

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US10569892B2 (en) * 2013-05-06 2020-02-25 Sikorsky Aircraft Corporation Supplemental power for reduction of prime mover
US10850863B2 (en) * 2014-03-04 2020-12-01 Pratt & Whitney Canada Corp. System and method for operating a multi-engine aircraft in an auxiliary power unit mode
FR3019219B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant
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
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
EP3197773A4 (en) * 2014-09-23 2018-02-21 Sikorsky Aircraft Corporation Hybrid electric power drive system for a rotorcraft
FR3027286B1 (fr) 2014-10-20 2018-01-05 Safran Helicopter Engines Systeme propulsif hybride d'un aeronef multi-moteur
US10220942B2 (en) 2016-08-19 2019-03-05 Bell Helicopter Textron Inc. Braking systems for rotorcraft
FR3055883B1 (fr) * 2016-09-09 2019-03-29 Airbus Helicopters Systeme mecanique de transmission d'un mouvement et aeronef equipe d'un systeme correspondant
JP6570095B2 (ja) * 2016-09-22 2019-09-04 トップ フライト テクノロジーズ， インコーポレイテッド 乗り物推進のための発電および分配
CN110023191B (zh) * 2017-01-10 2023-09-05 极光飞行科学公司 串联混合动力推进的垂直升降装置
US10934008B2 (en) 2017-02-10 2021-03-02 General Electric Company Dual function aircraft
FR3062882B1 (fr) 2017-02-15 2019-10-18 Safran Helicopter Engines Systeme propulsif d'un helicoptere monomoteur
FR3066444B1 (fr) * 2017-05-19 2021-04-16 Safran Architecture propulsive hybride d'aeronef comprenant un moteur avec une machine electrique reversible montee sur deux arbres
US11230385B2 (en) * 2017-06-08 2022-01-25 General Electric Company Hybrid-electric propulsion system for an aircraft
FR3069738B1 (fr) 2017-07-31 2019-08-16 Safran Electrical & Power Turbomachine a moteur de demarrage a ventilation reversible, procede de refroidissement associe
FR3078057B1 (fr) * 2018-02-19 2022-04-22 Safran Helicopter Engines Architecture de systeme propulsif d'un helicoptere bimoteurs
FR3079498B1 (fr) * 2018-03-30 2020-06-19 Airbus Operations Unite de propulsion a helice comprenant un moteur thermique et un moteur electrique et aeronef comportant une telle unite de propulsion a helice
FR3080835B1 (fr) * 2018-05-03 2021-04-09 Safran Helicopter Engines Systeme propulsif pour un helicoptere
FR3081150B1 (fr) * 2018-05-18 2020-06-12 Safran Helicopter Engines Architecture de puissance d'un aeronef
EP3578464A1 (en) * 2018-06-06 2019-12-11 Bombardier Inc. Electrical system for aircraft
FR3087421B1 (fr) * 2018-10-17 2022-03-04 Voltaero Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant
US11104430B2 (en) * 2019-09-27 2021-08-31 Textron Innovations Inc. Multimode powertrains for multi engine rotorcraft
CN111520234A (zh) * 2020-04-30 2020-08-11 中国直升机设计研究所 一种高原环境直升机发动机起动装置及方法
FR3116302B1 (fr) * 2020-11-13 2022-12-09 Safran Helicopter Engines Turbomachine à turbine libre comprenant des machines électriques assistant un générateur de gaz et une turbine libre

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FR2871138B1 (fr) * 2004-06-07 2006-08-04 Eurocopter France Mecanisme de transmission entre des accessoires et les organes moteurs d'entrainement du rotor d'un giravion, selectivement isolement ou conjointement
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FR2952907B1 (fr) * 2009-11-26 2011-12-09 Eurocopter France Installation motrice, helicoptere comportant une telle installation motrice, et procede mis en oeuvre par cette installation motrice
FR2962404B1 (fr) * 2010-07-08 2012-07-20 Eurocopter France Architecture electrique pour aeronef a voilure tournante a motorisation hybride
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FR2992024B1 (fr) * 2012-06-15 2017-07-21 Turbomeca Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere
FR2992686B1 (fr) * 2012-06-28 2016-05-06 Aircelle Sa Dispositif d’inversion de poussee pour un aeronef comprenant au moins deux inverseurs de poussee

Also Published As

Publication number Publication date
JP2015527519A (ja) 2015-09-17
US20150143950A1 (en) 2015-05-28
CN104487345B (zh) 2017-09-05
US10301035B2 (en) 2019-05-28
RU2639838C2 (ru) 2017-12-22
KR102097178B1 (ko) 2020-04-03
CA2876952C (fr) 2021-04-13
KR20150027142A (ko) 2015-03-11
EP2867122A1 (fr) 2015-05-06
WO2014001683A1 (fr) 2014-01-03
RU2014152025A (ru) 2016-08-20
FR2992630A1 (fr) 2014-01-03
JP6320373B2 (ja) 2018-05-09
EP2867122B1 (fr) 2020-04-15
CN104487345A (zh) 2015-04-01
FR2992630B1 (fr) 2015-02-20
CA2876952A1 (fr) 2014-01-03

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