BR112015017917A2 - arquitetura para suprir potência elétrica de emergência para uma aeronave, aeronave e método para suprir potência elétrica de emergência em uma aeronave - Google Patents

arquitetura para suprir potência elétrica de emergência para uma aeronave, aeronave e método para suprir potência elétrica de emergência em uma aeronave

Info

Publication number
BR112015017917A2
BR112015017917A2 BR112015017917A BR112015017917A BR112015017917A2 BR 112015017917 A2 BR112015017917 A2 BR 112015017917A2 BR 112015017917 A BR112015017917 A BR 112015017917A BR 112015017917 A BR112015017917 A BR 112015017917A BR 112015017917 A2 BR112015017917 A2 BR 112015017917A2
Authority
BR
Brazil
Prior art keywords
aircraft
electrical power
emergency electrical
providing emergency
architecture
Prior art date
Application number
BR112015017917A
Other languages
English (en)
Inventor
Rideau Jean-François
Original Assignee
Microturbo
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 Microturbo filed Critical Microturbo
Publication of BR112015017917A2 publication Critical patent/BR112015017917A2/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
    • B64D41/00—Power installations for auxiliary purposes
    • B64D41/007—Ram air turbines
    • 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
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D15/00—Transmission of mechanical power
    • F03D15/10—Transmission of mechanical power using gearing not limited to rotary motion, e.g. with oscillating or reciprocating members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D7/00—Controlling wind motors 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20—Wind motors characterised by the driven apparatus
    • F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/30—Wind motors specially adapted for installation in particular locations
    • F03D9/32—Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/728—Onshore wind turbines
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Control Of Turbines (AREA)
  • Stand-By Power Supply Arrangements (AREA)

Abstract

resumo “arquitetura para suprir potência elétrica de emergência para uma aeronave, aeronave e método para suprir potência elétrica de emergência em uma aeronave” a invenção se refere a uma estrutura (3) para fornecer potência elétrica de emergência para uma aeronave (1) que compreende uma cabine pressurizada (10), pelo menos um motor principal e uma unidade de potência auxiliar (apu), sendo que a estrutura é projetada para fornecer potência elétrica para a aeronave no caso de falha do motor principal e da unidade auxiliar de emergência e que a estrutura compreende um circuito (30) para recuperar ar a partir da cabine (10) e um sistema gerador de eletricidade (32, 24, 34) que gera eletricidade pela despressurização do ar recuperado a partir da cabine (10).
BR112015017917A 2013-01-29 2014-01-23 arquitetura para suprir potência elétrica de emergência para uma aeronave, aeronave e método para suprir potência elétrica de emergência em uma aeronave BR112015017917A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1350727A FR3001442B1 (fr) 2013-01-29 2013-01-29 Architecture de fourniture de puissance electrique de secours amelioree dans un aeronef
PCT/FR2014/050135 WO2014118458A1 (fr) 2013-01-29 2014-01-23 Architecture de fourniture de puissance electrique de secours à un aeronef

Publications (1)

Publication Number Publication Date
BR112015017917A2 true BR112015017917A2 (pt) 2017-07-11

Family

ID=48407674

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015017917A BR112015017917A2 (pt) 2013-01-29 2014-01-23 arquitetura para suprir potência elétrica de emergência para uma aeronave, aeronave e método para suprir potência elétrica de emergência em uma aeronave

Country Status (9)

Country Link
US (1) US20160009409A1 (pt)
EP (1) EP2951093B1 (pt)
JP (1) JP2016508466A (pt)
CN (1) CN104955731A (pt)
BR (1) BR112015017917A2 (pt)
CA (1) CA2899510A1 (pt)
FR (1) FR3001442B1 (pt)
RU (1) RU2015136588A (pt)
WO (1) WO2014118458A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9617006B2 (en) * 2008-12-12 2017-04-11 Liebherr-Aerospace Lindenberg Gmbh Emergency power system for an aircraft
KR101546822B1 (ko) * 2015-07-06 2015-08-24 (주)누리일렉콤 풍력 발전기
US10919638B2 (en) 2016-05-31 2021-02-16 The Boeing Company Aircraft cabin pressurization energy harvesting
FR3072077B1 (fr) * 2017-10-05 2019-09-20 Liebherr-Aerospace Toulouse Module autonome de recuperation d'energie d'une cabine d'un aeronef et procede correspondant
US10988262B2 (en) 2018-03-14 2021-04-27 Honeywell International Inc. Cabin pressure control system architecture using cabin pressure air for inlet to APU core compressor
NL1042808B1 (en) * 2018-04-03 2019-10-10 Low Steven Airplane with improved safety
US11511865B2 (en) 2018-05-29 2022-11-29 Honeywell International Inc. Air supply management system for auxiliary power unit
US11273917B2 (en) 2018-05-29 2022-03-15 Honeywell International Inc. Cabin discharge air management system and method for auxiliary power unit
CA3116812A1 (en) * 2018-10-18 2020-04-23 Ihi Corporation Energy recovery device for aircraft
CN109728662A (zh) * 2018-11-23 2019-05-07 南京航空航天大学 飞机混合励磁应急发电机及其应用和控制方法
CN109936264A (zh) * 2018-11-23 2019-06-25 南京航空航天大学 飞机并列式混合励磁应急发电机及其应用、以及控制方法
CN109763897B (zh) * 2019-01-15 2021-04-20 三亚哈尔滨工程大学南海创新发展基地 一种基于金属纳米粉末燃烧的飞行器辅助发电机构

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1316275A (en) * 1969-10-02 1973-05-09 British Aircraft Corp Ltd Power supplies for aircraft services
US4864812A (en) * 1987-11-13 1989-09-12 Sundstrand Corporation Combined auxiliary and emergency power unit
DE4320302C2 (de) * 1993-06-18 1996-09-12 Daimler Benz Aerospace Airbus Anordnung zur Energiegewinnung an Bord eines Flugzeuges, insbesondere eines Passagierflugzeuges
US6283410B1 (en) * 1999-11-04 2001-09-04 Hamilton Sundstrand Corporation Secondary power integrated cabin energy system for a pressurized aircraft
US7721554B2 (en) * 2006-02-02 2010-05-25 General Electric Company Aircraft auxiliary gas turbine engine and method for operating
US20070220900A1 (en) * 2006-03-27 2007-09-27 General Electric Company Auxiliary gas turbine engine assembly, aircraft component and controller
US7707838B2 (en) * 2006-10-31 2010-05-04 General Electric Company Auxiliary power unit assembly
ES2363897B1 (es) * 2008-10-24 2012-07-04 Airbus Operations, S.L. Unidad de potencia auxiliar (apu) de una aeronave
FR2964086B1 (fr) * 2010-08-25 2013-06-14 Turbomeca Procede d'optimisation du rendement energetique global d'un aeronef et groupe de puissance principal de mise en oeuvre

Also Published As

Publication number Publication date
CN104955731A (zh) 2015-09-30
CA2899510A1 (fr) 2014-08-07
FR3001442B1 (fr) 2016-05-20
EP2951093A1 (fr) 2015-12-09
FR3001442A1 (fr) 2014-08-01
US20160009409A1 (en) 2016-01-14
EP2951093B1 (fr) 2016-06-08
JP2016508466A (ja) 2016-03-22
RU2015136588A (ru) 2017-03-07
WO2014118458A1 (fr) 2014-08-07

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Legal Events

Date Code Title Description
B08F Application fees: application dismissed [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]