BRPI0403675A - Sistema de gerenciamento de energia de carga elétrica secundária para uma aeronave e método de controlar o consumo de energia de carga elétrica durante a operação de uma aeronave - Google Patents

Sistema de gerenciamento de energia de carga elétrica secundária para uma aeronave e método de controlar o consumo de energia de carga elétrica durante a operação de uma aeronave

Info

Publication number
BRPI0403675A
BRPI0403675A BR0403675-1A BRPI0403675A BRPI0403675A BR PI0403675 A BRPI0403675 A BR PI0403675A BR PI0403675 A BRPI0403675 A BR PI0403675A BR PI0403675 A BRPI0403675 A BR PI0403675A
Authority
BR
Brazil
Prior art keywords
aircraft
electrical charge
charge energy
management system
controlling
Prior art date
Application number
BR0403675-1A
Other languages
English (en)
Inventor
Michael D Bowman
Farhad Nozari
Thomas F Currier
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of BRPI0403675A publication Critical patent/BRPI0403675A/pt

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J1/00—Circuit arrangements for DC mains or DC distribution networks
    • H02J1/14—Balancing load and power generation in DC networks
    • 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
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2105/00—Networks for supplying or distributing electric power characterised by their spatial reach or by the load
    • H02J2105/30—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles
    • H02J2105/32—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles for aircrafts
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Multiple Motors (AREA)
  • Control Of Electric Motors In General (AREA)

Abstract

"SISTEMA DE GERENCIAMENTO DE ENERGIA DE CARGA ELéTRICA SECUNDáRIA PARA UMA AERONAVE E MéTODO DE CONTROLAR O CONSUMO DE ENERGIA DE CARGA ELéTRICA DURANTE A OPERAçãO DE UMA AERONAVE". Método de controlar o consumo da energia de carga elétrica durante a operação de uma aeronave (12) inclui a determinação das condições operacionais correntes da aeronave (12). Um limite de extração de energia motora secundária é determinado em resposta às condições operacionais correntes. A extração da energia motora secundária é determinada. Múltiplas cargas secundárias (18) são operadas em resposta ao limite de extração de energia motora secundária e à extração de energia motora secundária.
BR0403675-1A 2003-06-30 2004-06-30 Sistema de gerenciamento de energia de carga elétrica secundária para uma aeronave e método de controlar o consumo de energia de carga elétrica durante a operação de uma aeronave BRPI0403675A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/604,189 US20050006954A1 (en) 2003-06-30 2003-06-30 Aircraft secondary electric load controlling system

Publications (1)

Publication Number Publication Date
BRPI0403675A true BRPI0403675A (pt) 2005-04-05

Family

ID=33435342

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0403675-1A BRPI0403675A (pt) 2003-06-30 2004-06-30 Sistema de gerenciamento de energia de carga elétrica secundária para uma aeronave e método de controlar o consumo de energia de carga elétrica durante a operação de uma aeronave

Country Status (4)

Country Link
US (1) US20050006954A1 (pt)
EP (1) EP1494331A3 (pt)
BR (1) BRPI0403675A (pt)
CA (1) CA2472409C (pt)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0130530D0 (en) * 2001-12-20 2002-02-06 Bg Intellectual Pty Ltd A domestic combined heat and power unit
US8155876B2 (en) 2006-09-07 2012-04-10 The Boeing Company Systems and methods for controlling aircraft electrical power
US8237308B2 (en) * 2007-12-12 2012-08-07 The Boeing Company Dynamic electrical load management
DE102008048275B4 (de) 2008-09-22 2014-07-24 Airbus Operations Gmbh Treibstoffmanagement-System
US20110071706A1 (en) * 2009-09-23 2011-03-24 Adaptive Materials, Inc. Method for managing power and energy in a fuel cell powered aerial vehicle based on secondary operation priority
US20110189587A1 (en) * 2010-02-01 2011-08-04 Adaptive Materials, Inc. Interconnect Member for Fuel Cell
US8793026B2 (en) 2010-09-15 2014-07-29 The Boeing Company Electrical load management system
US9815564B2 (en) 2013-12-04 2017-11-14 The Boeing Company Non-propulsive utility power (NPUP) generation system for providing full-time secondary power during operation of an aircraft
US10227137B2 (en) * 2016-03-22 2019-03-12 Ge Aviation Systems Llc Hybrid power system for an aircraft
US11970062B2 (en) 2017-04-05 2024-04-30 Ge Aviation Systems Llc Systems and methods of power allocation for hybrid electric architecture
US20240327011A1 (en) * 2023-03-27 2024-10-03 Northrop Grumman Systems Corporation Adaptive aircraft power management system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4317177A (en) * 1980-01-14 1982-02-23 Martin P. Miller Power priority control system for aircraft and test apparatus therefor
GB9603350D0 (en) * 1995-04-05 1996-04-17 Oxley Dev Co Ltd Aircraft lighting system
US6510369B1 (en) * 1999-08-24 2003-01-21 Plug Power Inc. Residential load shedding
US6380639B1 (en) * 2000-05-11 2002-04-30 Bombardier Inc. System, method and apparatus for power regulation
FR2823027B1 (fr) * 2001-03-30 2003-07-25 Labinal Installation de gestion de puissance dans un avion

Also Published As

Publication number Publication date
CA2472409A1 (en) 2004-12-30
CA2472409C (en) 2008-06-10
EP1494331A3 (en) 2013-05-15
EP1494331A2 (en) 2005-01-05
US20050006954A1 (en) 2005-01-13

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Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]