BR112015025526A2 - dispositivo de corte de energia dos alternadores de uma turbomáquina durante aceleração - Google Patents

dispositivo de corte de energia dos alternadores de uma turbomáquina durante aceleração

Info

Publication number
BR112015025526A2
BR112015025526A2 BR112015025526A BR112015025526A BR112015025526A2 BR 112015025526 A2 BR112015025526 A2 BR 112015025526A2 BR 112015025526 A BR112015025526 A BR 112015025526A BR 112015025526 A BR112015025526 A BR 112015025526A BR 112015025526 A2 BR112015025526 A2 BR 112015025526A2
Authority
BR
Brazil
Prior art keywords
current
turbomachine
power cut
generator
alternators
Prior art date
Application number
BR112015025526A
Other languages
English (en)
Other versions
BR112015025526B1 (pt
Inventor
lebrun Arnaud
Mcgrath Darragh
Lepage Thomas
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BR112015025526A2 publication Critical patent/BR112015025526A2/pt
Publication of BR112015025526B1 publication Critical patent/BR112015025526B1/pt

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
    • B64D41/00—Power installations for auxiliary purposes
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
    • H02J7/1415—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle with a generator driven by a prime mover other than the motor of a vehicle
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
    • H02J7/1423—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle with multiple batteries
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
    • H02J7/1446—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle in response to parameters of a vehicle
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/345—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering using capacitors as storage or buffering devices
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H02K7/1807—Rotary generators
    • H02K7/1823—Rotary generators structurally associated with turbines or similar engines
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output
    • H02P9/008—Arrangements for controlling electric generators for the purpose of obtaining a desired output wherein the generator is controlled by the requirements of the prime mover
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output
    • H02P9/48—Arrangements for obtaining a constant output value at varying speed of the generator, e.g. on vehicle
    • 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
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40—The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
    • H02J7/143—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle with multiple generators
    • 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
    • Y02T50/40—Weight reduction

Abstract

1/1 resumo “dispositivo de corte de energia dos alternadores de uma turbomáquina durante aceleração” a presente invenção tem como objetivo um sistema de geração elétrica contínuo para uma aeronave propulsada por uma turbomáquina, que compreende pelo menos uma capacidade de armazenamento elétrico (bat 1, bat 2), pelo menos um gerador de corrente (g1, g2) acionado mecanicamente por um eixo de rotação da turbomáquina e ligações elétricas entre a dita capacidade de armazenamento elétrico, o dito gerador e equipamentos da aeronave para alimentar os ditos equipamentos com corrente contínua, que compreendem pelo menos um meio alternativo de fornecimento de corrente contínua (sup 1, sup 2) aos ditos equipamentos, autônomo em relação a qualquer acionamento mecânico por um eixo de rotação da turbomáquina, e um dispositivo (cont) próprio para cortar a corrente do ou dos ditos geradores e para colocar simultaneamente em serviço o dito meio alternativo. o sistema é caracterizado pelo fato de que o dito dispositivo de corte de energia (cont) para ativar o dito corte de energia e colocar em serviço o meio alternativo de fornecimento da corrente, é comandado por um parâmetro de comando ou de funcionamento da turbomáquina. o meio alternativo de fornecimento de corrente é de preferência formado por um ou vários supercondensadores.
BR112015025526-4A 2013-04-22 2014-04-22 Sistema de geração elétrica para a alimentação com corrente de pelo menos um equipamento para uma aeronave propulsionada por uma turbomáquina, e, turbomáquina BR112015025526B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1353659A FR3004701B1 (fr) 2013-04-22 2013-04-22 Dispositif de delestage des alternateurs d'un turboreacteur pendant ses accelerations
FR1353659 2013-04-22
PCT/FR2014/050977 WO2014174207A1 (fr) 2013-04-22 2014-04-22 Dispositif de delestage des alternateurs d'une turbomachine pendant ses accelerations

Publications (2)

Publication Number Publication Date
BR112015025526A2 true BR112015025526A2 (pt) 2017-07-18
BR112015025526B1 BR112015025526B1 (pt) 2022-01-04

Family

ID=48656181

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015025526-4A BR112015025526B1 (pt) 2013-04-22 2014-04-22 Sistema de geração elétrica para a alimentação com corrente de pelo menos um equipamento para uma aeronave propulsionada por uma turbomáquina, e, turbomáquina

Country Status (8)

Country Link
US (1) US9988158B2 (pt)
EP (1) EP2989007B1 (pt)
CN (1) CN105143044B (pt)
BR (1) BR112015025526B1 (pt)
CA (1) CA2908858C (pt)
FR (1) FR3004701B1 (pt)
RU (1) RU2655183C2 (pt)
WO (1) WO2014174207A1 (pt)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3004701B1 (fr) * 2013-04-22 2015-04-03 Snecma Dispositif de delestage des alternateurs d'un turboreacteur pendant ses accelerations
EP2994386B1 (en) * 2013-05-06 2020-02-19 Sikorsky Aircraft Corporation Supplemental power for reduction of prime mover
US9981654B2 (en) * 2016-06-02 2018-05-29 Ford Global Technologies, Llc Methods and systems for surge control
US10211632B2 (en) 2016-08-05 2019-02-19 Hamilton Sundstrand Corporation Hybrid energy storage module arrangements
CN106786611B (zh) * 2016-12-12 2020-06-30 国网山东省电力公司青岛供电公司 一种电网电压控制方法及装置
FR3067874A1 (fr) * 2017-06-15 2018-12-21 Airbus Operations Systeme de controle d'alimentation electrique dans un aeronef
GB201807771D0 (en) * 2018-05-14 2018-06-27 Rolls Royce Plc Hybrid electric aircraft propulsion system
FR3086923B1 (fr) * 2018-10-04 2020-11-06 Safran Architecture electrique pour propulsion hybride
FR3095195B1 (fr) * 2019-04-17 2021-05-07 Safran Helicopter Engines Procéde de commande d’un réseau d’alimentation électrique d’un aéronef
US11591075B2 (en) * 2019-06-13 2023-02-28 Hamilton Sundstrand Corporation Intelligent engine offload of auxiliary loads for enhanced engine durability
FR3111333A1 (fr) * 2020-06-16 2021-12-17 Thales Architecture électrique d’un aéronef
US11682535B2 (en) 2021-03-12 2023-06-20 Essex Industries, Inc. Rocker switch
US11688568B2 (en) 2021-03-15 2023-06-27 Essex Industries, Inc. Five-position switch
FR3133643A1 (fr) 2022-03-15 2023-09-22 Safran Aircraft Engines Procédé et unité de commande d’ensemble moteur
FR3133642A1 (fr) 2022-03-15 2023-09-22 Safran Aircraft Engines Procédé et unité de commande d’ensemble moteur

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4058277A (en) * 1974-09-19 1977-11-15 Dornier Gmbh. Captive remote-controlled helicopter
US5977645A (en) * 1997-06-30 1999-11-02 Sundstrand Corporation Aircraft secondary power system
US6124646A (en) * 1998-02-11 2000-09-26 Alliedsignal Inc. Aircraft air conditioning system including electric generator for providing AC power having limited frequency range
US6606227B2 (en) * 2001-02-12 2003-08-12 Delphi Technologies, Inc. High voltage battery cutout circuit for a motor vehicle electrical system
US6968674B2 (en) * 2003-01-28 2005-11-29 General Electric Company Methods and apparatus for operating gas turbine engines
RU2232109C1 (ru) * 2003-09-22 2004-07-10 ОАО "ОКБ им. А.С.Яковлева" Способ электроснабжения бортовых систем летательного аппарата
FR2882200B1 (fr) * 2005-02-17 2015-05-01 Hispano Suiza Sa Alimentation electrique d'equipements d'un moteur d'avion a turbine a gaz
US7721554B2 (en) * 2006-02-02 2010-05-25 General Electric Company Aircraft auxiliary gas turbine engine and method for operating
US8164283B2 (en) 2008-11-04 2012-04-24 The Boeing Company System and method for energy capture and distribution
EP2216246A3 (en) * 2009-02-10 2014-04-23 Goodrich Corporation Aircraft electrical power system
FR2952672B1 (fr) * 2009-11-17 2011-12-09 Snecma Montage d'un boitier d'accessoires sur un carter intermediaire pour compartiment de soufflante de turboreacteur
WO2012012482A1 (en) * 2010-07-20 2012-01-26 Eaton Corporation Method of energy and power management in dynamic power systems with ultra-capacitors (super capacitors)
FR2979614B1 (fr) * 2011-09-04 2013-09-20 Eric Chantriaux Transmission electromagnetique de puissance pour aeronef a voilure tournante ou fixe.
US8820677B2 (en) * 2011-06-18 2014-09-02 Jason A. Houdek Aircraft power systems and methods
CA3114227C (en) * 2012-07-12 2023-09-19 Pratt & Whitney Canada Corp. Aircraft power outtake management
GB201219916D0 (en) * 2012-11-06 2012-12-19 Rolls Royce Plc An electrical generation arrangement for an aircraft
GB201219922D0 (en) * 2012-11-06 2012-12-19 Rolls Royce Plc Method of controlling an aircraft electrical power generation system
FR3004701B1 (fr) * 2013-04-22 2015-04-03 Snecma Dispositif de delestage des alternateurs d'un turboreacteur pendant ses accelerations
JP6170370B2 (ja) * 2013-08-07 2017-07-26 三菱航空機株式会社 航空機におけるロードシェッド方法および制御装置
GB2520024B (en) * 2013-11-06 2016-02-03 Ge Aviat Systems Ltd Electrical power system for an aircraft
EP2945244B1 (en) * 2014-05-15 2022-07-06 Airbus Operations GmbH Power and data distribution module and method for power and data distribution in an airborne vehicle

Also Published As

Publication number Publication date
EP2989007A1 (fr) 2016-03-02
WO2014174207A1 (fr) 2014-10-30
EP2989007B1 (fr) 2017-11-15
US9988158B2 (en) 2018-06-05
CA2908858A1 (fr) 2014-10-30
CN105143044B (zh) 2018-09-28
RU2015144334A3 (pt) 2018-03-30
RU2655183C2 (ru) 2018-05-24
CA2908858C (fr) 2021-02-16
RU2015144334A (ru) 2017-05-26
FR3004701A1 (fr) 2014-10-24
CN105143044A (zh) 2015-12-09
FR3004701B1 (fr) 2015-04-03
BR112015025526B1 (pt) 2022-01-04
US20160083106A1 (en) 2016-03-24

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 22/04/2014, OBSERVADAS AS CONDICOES LEGAIS.