BR112015015613A2 - sistema de potência elétrica para uma aeronave e método para produzir potência elétrica em uma aeronave - Google Patents

sistema de potência elétrica para uma aeronave e método para produzir potência elétrica em uma aeronave

Info

Publication number
BR112015015613A2
BR112015015613A2 BR112015015613A BR112015015613A BR112015015613A2 BR 112015015613 A2 BR112015015613 A2 BR 112015015613A2 BR 112015015613 A BR112015015613 A BR 112015015613A BR 112015015613 A BR112015015613 A BR 112015015613A BR 112015015613 A2 BR112015015613 A2 BR 112015015613A2
Authority
BR
Brazil
Prior art keywords
aircraft
electrical power
power system
turbine
producing
Prior art date
Application number
BR112015015613A
Other languages
English (en)
Inventor
Delgado Adon Jr
Dale Mathias Christopher
James Buchholz Todd
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR112015015613A2 publication Critical patent/BR112015015613A2/pt

Links

Classifications

    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • 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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/30—Fuel systems for specific fuels
    • 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
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • 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
    • 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
    • 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
    • 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
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

resumo “sistema de potência elétrica para uma aeronave e método para produzir potência elétrica em uma aeronave” trata-se de um sistema de potência elétrica para uma aeronave que inclui um motor de turbina (101) acoplado à aeronave (5) e que fornece empuxo propulsor e que emite calor durante a operação para definir uma fonte de alta temperatura, um sistema de combustível criogênico (12) situado dentro da aeronave e que fornece combustível para a turbina (101) e que emite calor a uma temperatura inferior ao calor do motor de turbina para definir uma fonte de baixa temperatura e um gerador de potência elétrica situado na aeronave e que tem um gerador termodinâmico que usa a diferença de temperatura para gerar potência elétrica e um método para produzir potência elétrica.
BR112015015613A 2012-12-28 2013-11-26 sistema de potência elétrica para uma aeronave e método para produzir potência elétrica em uma aeronave BR112015015613A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261746731P 2012-12-28 2012-12-28
PCT/US2013/071831 WO2014105334A1 (en) 2012-12-28 2013-11-26 System and method for aviation electric power production

Publications (1)

Publication Number Publication Date
BR112015015613A2 true BR112015015613A2 (pt) 2017-07-11

Family

ID=49883211

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015015613A BR112015015613A2 (pt) 2012-12-28 2013-11-26 sistema de potência elétrica para uma aeronave e método para produzir potência elétrica em uma aeronave

Country Status (7)

Country Link
US (1) US10006363B2 (pt)
EP (1) EP2938543A1 (pt)
JP (1) JP2016509549A (pt)
CN (1) CN104870312B (pt)
BR (1) BR112015015613A2 (pt)
CA (1) CA2895738A1 (pt)
WO (1) WO2014105334A1 (pt)

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DE102017217425A1 (de) * 2017-09-29 2019-04-04 Siemens Aktiengesellschaft Verfahren zum Antrieb eines Flugzeugs, Antriebssystem und Flugzeug
US20190145284A1 (en) * 2017-11-13 2019-05-16 National Chung Shan Institute Of Science And Technology Exhaust channel of microturbine engine
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US11465766B2 (en) * 2019-06-28 2022-10-11 The Boeing Company Systems and methods for cooling and generating power on high speed flight vehicles
US11506124B2 (en) * 2020-03-27 2022-11-22 Raytheon Technologies Corporation Supercritical CO2 cycle for gas turbine engines having supplemental cooling
EP4001599B8 (en) 2020-11-23 2023-04-12 The Boeing Company Methods and systems for generating power and thermal management having combined cycle architecture
CN113467271A (zh) * 2021-05-25 2021-10-01 中国航空工业集团公司沈阳飞机设计研究所 一种飞机电环控系统热仿真方法
US11731780B2 (en) * 2021-09-09 2023-08-22 Hamilton Sundstrand Corporation Aircraft system including a cryogenic fluid operated auxiliary power unit (APU)
CN117145633B (zh) * 2023-10-31 2024-01-19 中国航发四川燃气涡轮研究院 一种用于航空发动机的基于热电效应的余热回收系统

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Also Published As

Publication number Publication date
CA2895738A1 (en) 2014-07-03
CN104870312A (zh) 2015-08-26
JP2016509549A (ja) 2016-03-31
US10006363B2 (en) 2018-06-26
WO2014105334A1 (en) 2014-07-03
CN104870312B (zh) 2019-06-18
US20150330303A1 (en) 2015-11-19
EP2938543A1 (en) 2015-11-04

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 5A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2494 DE 23-10-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.