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MX2008001442A - Circuito de suministro de energia electrica en una aeronave para equipo electrico que incluye un circuito de deshielo. - Google Patents

Circuito de suministro de energia electrica en una aeronave para equipo electrico que incluye un circuito de deshielo.

Info

Publication number
MX2008001442A
MX2008001442A MX2008001442A MX2008001442A MX2008001442A MX 2008001442 A MX2008001442 A MX 2008001442A MX 2008001442 A MX2008001442 A MX 2008001442A MX 2008001442 A MX2008001442 A MX 2008001442A MX 2008001442 A MX2008001442 A MX 2008001442A
Authority
MX
Mexico
Prior art keywords
circuit
electrical equipment
engine
icing
supplying electricity
Prior art date
Application number
MX2008001442A
Other languages
English (en)
Inventor
Rachid Boudyaf
Antoine Jean-Baptiste Stutz
Original Assignee
Hispano Suiza Sa
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 Hispano Suiza Sa filed Critical Hispano Suiza Sa
Publication of MX2008001442A publication Critical patent/MX2008001442A/es

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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Emergency Protection Circuit Devices (AREA)
  • Direct Current Feeding And Distribution (AREA)

Abstract

La presente invención se relaciona con circuito de suministro de energía eléctrica en una aeronave, el circuito comprende una red 17 de distribución de electricidad a bordo para distribuir equipo eléctrico 5b situado en un motor del aeroplano o en los alrededores del motor y un generador 27 de suministro de energía integrado en el motor de la aeronave para alimentar un circuito 5a de deshielo. El equipo eléctrico comprende cargas de góndola (5b) conectadas con un bus (35) de distribución de voltaje de CD, el mismo está conectado con un circuito (34) convertidor de voltaje energizado por la red (17) de distribución. El circuito (5a) de deshielo comprende al menos una resistencia eléctrica (61) para disipar electricidad posiblemente regresada al bus (35) de distribución de voltaje de CD por al menos algunas de las cargas de góndola. (Figura 2).
MX2008001442A 2007-01-31 2008-01-30 Circuito de suministro de energia electrica en una aeronave para equipo electrico que incluye un circuito de deshielo. MX2008001442A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0752986A FR2911848B1 (fr) 2007-01-31 2007-01-31 Circuit d'alimentation en energie electrique dans un aeronef pour des equipements electriques comprenant un circuit de degivrage

Publications (1)

Publication Number Publication Date
MX2008001442A true MX2008001442A (es) 2009-02-24

Family

ID=38330118

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2008001442A MX2008001442A (es) 2007-01-31 2008-01-30 Circuito de suministro de energia electrica en una aeronave para equipo electrico que incluye un circuito de deshielo.

Country Status (17)

Country Link
US (1) US7936082B2 (es)
EP (1) EP1953085B1 (es)
JP (1) JP5247168B2 (es)
CN (1) CN101234672B (es)
AT (1) ATE467559T1 (es)
BR (1) BRPI0800221B1 (es)
CA (1) CA2619541C (es)
DE (1) DE602008001166D1 (es)
ES (1) ES2346107T3 (es)
FR (1) FR2911848B1 (es)
IL (1) IL189114A (es)
MA (1) MA29728B1 (es)
MX (1) MX2008001442A (es)
RU (1) RU2450955C2 (es)
SG (2) SG144890A1 (es)
UA (1) UA94714C2 (es)
ZA (1) ZA200801001B (es)

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FR2948337B1 (fr) * 2009-07-24 2011-07-29 Aircelle Sa Circuit d'alimentation electrique pour nacelle de turboreacteur
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FR2967318B1 (fr) * 2010-11-10 2013-07-19 Hispano Suiza Sa Circuit d'alimentation pour un aeronef incluant une machine asynchrone
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FR2978878B1 (fr) * 2011-08-04 2013-08-09 Hispano Suiza Sa Dispositif d'alimentation electrique d'un aeronef au sol.
GB2495917B (en) * 2011-10-24 2014-10-22 Ge Aviat Systems Ltd Multiple source electrical power distribution in aircraft
FR2988694B1 (fr) * 2012-03-30 2014-03-28 Hispano Suiza Sa Dispositif d'alimentation electrique d'un aeronef au sol
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FR3000724B1 (fr) 2013-01-07 2015-01-02 Aircelle Sa Architecture degivrage electrique a haute disponibilite d'entree d'air de nacelle a etages commutes
FR3001443B1 (fr) * 2013-01-30 2016-05-27 Microturbo Procede et systeme d'alimentation en energie electrique d'un aeronef
RU2524776C1 (ru) * 2013-03-27 2014-08-10 Открытое акционерное общество "Электропривод" Способ запуска газотурбинного двигателя бесконтактным явнополюсным синхронным генератором с вращающимся выпрямителем
EP2949876B1 (en) 2014-05-29 2020-07-08 Rolls-Royce Corporation System and method to manage engine transients for rapid power demand changes
US10377498B2 (en) * 2016-01-21 2019-08-13 The Boeing Company Aircraft and associated method for providing electrical energy to an anti-icing system
US11473497B2 (en) * 2016-03-15 2022-10-18 Hamilton Sundstrand Corporation Engine bleed system with motorized compressor
US10794295B2 (en) 2016-03-15 2020-10-06 Hamilton Sunstrand Corporation Engine bleed system with multi-tap bleed array
US20170268430A1 (en) * 2016-03-15 2017-09-21 Hamilton Sundstrand Corporation Engine bleed system with turbo-compressor
CN108082496B (zh) * 2017-11-21 2020-03-24 武汉航空仪表有限责任公司 一种谐振式结冰探测器的驱动电路
FR3079820B1 (fr) * 2018-04-09 2020-04-17 Safran Electrical & Power Systeme et procede de demarrage/generation pour turbomachine d'aeronef
EP3578464A1 (en) * 2018-06-06 2019-12-11 Bombardier Inc. Electrical system for aircraft
US11465759B2 (en) * 2018-07-13 2022-10-11 The Boeing Company Multi-mode generator for ice protection on aircraft
US12499717B2 (en) * 2022-01-20 2025-12-16 Pratt & Whitney Canada Corp. Method and system for data transmission from an aircraft engine
US12365466B1 (en) * 2024-01-23 2025-07-22 General Electric Company Power switching system of an anti-ice system for use with a main power supply and an auxiliary power supply

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Also Published As

Publication number Publication date
RU2450955C2 (ru) 2012-05-20
IL189114A (en) 2011-10-31
CA2619541A1 (fr) 2008-07-31
ZA200801001B (en) 2008-11-26
ES2346107T3 (es) 2010-10-08
FR2911848A1 (fr) 2008-08-01
US20100283319A1 (en) 2010-11-11
CN101234672A (zh) 2008-08-06
EP1953085A1 (fr) 2008-08-06
JP2008207792A (ja) 2008-09-11
BRPI0800221A (pt) 2008-09-16
ATE467559T1 (de) 2010-05-15
US7936082B2 (en) 2011-05-03
BRPI0800221B1 (pt) 2020-02-11
JP5247168B2 (ja) 2013-07-24
EP1953085B1 (fr) 2010-05-12
CN101234672B (zh) 2013-12-18
UA94714C2 (ru) 2011-06-10
FR2911848B1 (fr) 2009-12-25
RU2008103650A (ru) 2009-08-10
MA29728B1 (fr) 2008-09-01
IL189114A0 (en) 2008-11-03
CA2619541C (fr) 2014-08-05
SG144890A1 (en) 2008-08-28
DE602008001166D1 (de) 2010-06-24
SG164372A1 (en) 2010-09-29

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