BR112015015576A2 - aeronave e método de gerenciamento de combustível criogênico evaporado - Google Patents

aeronave e método de gerenciamento de combustível criogênico evaporado

Info

Publication number
BR112015015576A2
BR112015015576A2 BR112015015576A BR112015015576A BR112015015576A2 BR 112015015576 A2 BR112015015576 A2 BR 112015015576A2 BR 112015015576 A BR112015015576 A BR 112015015576A BR 112015015576 A BR112015015576 A BR 112015015576A BR 112015015576 A2 BR112015015576 A2 BR 112015015576A2
Authority
BR
Brazil
Prior art keywords
cryogenic fuel
aircraft
evaporated
management method
storage tank
Prior art date
Application number
BR112015015576A
Other languages
English (en)
Inventor
Delgado Adon Jr
Jay Epstein Michael
Harold Weisgerber Robert
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 BR112015015576A2 publication Critical patent/BR112015015576A2/pt

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
    • 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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/02—Tanks
    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

resumo “aeronave e método de gerenciamento de combustível criogênico evaporado” trata-se de um método de gerenciamento de combustível criogênico evaporado em um tanque de armazenamento de um sistema de combustível criogênico de uma aeronave e de uma aeronave que tem pelo menos um motor de turbina que proporciona força propulsiva para a aeronave, e um sistema de combustível criogênico que inclui um tanque de armazenagem de combustível criogênico resfriado passivamente, localizado dentro da aeronave, uma abertura de pressão (501) acoplada fluidamente ao tanque de armazenagem de combustível criogênico e gás evaporado de exaustão a partir do combustível criogênico, para definir uma corrente de abertura de gás natural, e um conversor catalítico (508) acoplado fluidamente à abertura de pressão.
BR112015015576A 2012-12-28 2013-11-26 aeronave e método de gerenciamento de combustível criogênico evaporado BR112015015576A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201261746953P 2012-12-28 2012-12-28
PCT/US2013/071806 WO2014105333A1 (en) 2012-12-28 2013-11-26 Aircraft and method of managing evaporated cryogenic fuel

Publications (1)

Publication Number Publication Date
BR112015015576A2 true BR112015015576A2 (pt) 2017-07-11

Family

ID=50023834

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015015576A BR112015015576A2 (pt) 2012-12-28 2013-11-26 aeronave e método de gerenciamento de combustível criogênico evaporado

Country Status (7)

Country Link
US (1) US9676491B2 (pt)
EP (1) EP2938542A1 (pt)
JP (1) JP2016510278A (pt)
CN (1) CN104870311B (pt)
BR (1) BR112015015576A2 (pt)
CA (1) CA2895784A1 (pt)
WO (1) WO2014105333A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160023336A1 (en) * 2014-07-24 2016-01-28 Taizhou Dajiang Ind. Co., Ltd. Phase transition heat storage device
US11555473B2 (en) 2018-05-29 2023-01-17 Kontak LLC Dual bladder fuel tank
US11638331B2 (en) 2018-05-29 2023-04-25 Kontak LLC Multi-frequency controllers for inductive heating and associated systems and methods
GB2587558B (en) * 2018-10-15 2021-12-01 Gkn Aerospace Services Ltd Apparatus
JPWO2020115822A1 (ja) * 2018-12-04 2021-02-15 中国電力株式会社 アンモニア気化器
US11267580B2 (en) * 2018-12-19 2022-03-08 Hamilton Sundstrand Corporation Fuel systems for aircraft and methods of pressurizing fuel
US11753178B2 (en) * 2019-11-12 2023-09-12 General Electric Company Systems and methods for removing heat from aircraft components
US11674442B2 (en) * 2020-03-16 2023-06-13 General Electric Company Gas turbine engine and method of operating
US11668243B2 (en) 2021-05-25 2023-06-06 Raytheon Technologies Corporation Methods and systems for starting hydrogen powered gas generators
EP4261452A1 (de) * 2022-04-13 2023-10-18 MAGNA Energy Storage Systems GesmbH Boil-off-managementsystem
EP4265897A1 (en) * 2022-04-22 2023-10-25 Eaton Intelligent Power Limited Hydrogen fuel system for aircraft
US20230348090A1 (en) * 2022-04-28 2023-11-02 Blended Wing Aircraft, Inc. Aircraft with fuel tanks stored aft of a cabin in a main body and a method for manufacturing
US20230406526A1 (en) * 2022-06-15 2023-12-21 Blended Wing Aircraft, Inc. Method for fueling an aircraft

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3157147A (en) * 1963-05-09 1964-11-17 California Research Corp Vessel for liquefied gas
US3768982A (en) * 1971-06-22 1973-10-30 Ford Motor Co Catalytic converter with electrically preheated catalyst
US3979005A (en) * 1974-05-13 1976-09-07 The Boeing Company Cryogenic tank and aircraft structural interface
EP0670264A1 (de) 1994-03-02 1995-09-06 Daimler-Benz Aerospace Aktiengesellschaft Treibstoffversorgungssystem
US6393821B1 (en) * 1998-08-21 2002-05-28 Edan Prabhu Method for collection and use of low-level methane emissions
JP2002106798A (ja) * 2000-09-29 2002-04-10 Honda Motor Co Ltd 液体水素貯蔵装置
JP2003014214A (ja) * 2001-06-29 2003-01-15 Matsushita Electric Ind Co Ltd 焼却装置
CN1259219C (zh) 2003-12-30 2006-06-14 上海交通大学 燃氢高速飞机的液氢燃料携带和换热系统
US7806365B2 (en) * 2006-07-05 2010-10-05 The Boeing Company Long endurance hydrogen powered vehicle
US7837764B2 (en) * 2008-06-06 2010-11-23 The Boeing Company Oxygen exchange manifold, systems and methods for inerting a volatile environment
GB201004837D0 (en) * 2010-03-23 2010-05-05 Airbus Uk Ltd Fuel system and method
JP2013542874A (ja) 2010-09-30 2013-11-28 ゼネラル・エレクトリック・カンパニイ 燃料貯蔵システム

Also Published As

Publication number Publication date
CN104870311B (zh) 2017-03-15
US9676491B2 (en) 2017-06-13
WO2014105333A1 (en) 2014-07-03
EP2938542A1 (en) 2015-11-04
CN104870311A (zh) 2015-08-26
CA2895784A1 (en) 2014-07-03
JP2016510278A (ja) 2016-04-07
US20150344143A1 (en) 2015-12-03

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Legal Events

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B08F Application fees: dismissal - article 86 of industrial property law

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B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)

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.