BRPI0921661A2 - método para comendar e controlar pelo menos um elemento de aquecimento resistivo pertencente a um conjunto de degelo de nacela de motor turbojato de avião e dispositivo para a implementação do método - Google Patents

método para comendar e controlar pelo menos um elemento de aquecimento resistivo pertencente a um conjunto de degelo de nacela de motor turbojato de avião e dispositivo para a implementação do método

Info

Publication number
BRPI0921661A2
BRPI0921661A2 BRPI0921661A BRPI0921661A BRPI0921661A2 BR PI0921661 A2 BRPI0921661 A2 BR PI0921661A2 BR PI0921661 A BRPI0921661 A BR PI0921661A BR PI0921661 A BRPI0921661 A BR PI0921661A BR PI0921661 A2 BRPI0921661 A2 BR PI0921661A2
Authority
BR
Brazil
Prior art keywords
mending
implementing
controlling
heating element
resistive heating
Prior art date
Application number
BRPI0921661A
Other languages
English (en)
Inventor
David Pereira
Laurence Lemais
Original Assignee
Aircelle 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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI0921661A2 publication Critical patent/BRPI0921661A2/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
    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/20—Means for detecting icing or initiating de-icing
    • B64D15/22—Automatic initiation by icing detector
    • 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
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Resistance Heating (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI0921661A 2008-11-17 2009-08-26 método para comendar e controlar pelo menos um elemento de aquecimento resistivo pertencente a um conjunto de degelo de nacela de motor turbojato de avião e dispositivo para a implementação do método BRPI0921661A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0806416A FR2938503A1 (fr) 2008-11-17 2008-11-17 Procede de controle d'un systeme de degivrage electrique
PCT/FR2009/001032 WO2010055215A1 (fr) 2008-11-17 2009-08-26 Procédé de contrôle d'un système de dégivrage électrique

Publications (1)

Publication Number Publication Date
BRPI0921661A2 true BRPI0921661A2 (pt) 2016-02-16

Family

ID=40790675

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0921661A BRPI0921661A2 (pt) 2008-11-17 2009-08-26 método para comendar e controlar pelo menos um elemento de aquecimento resistivo pertencente a um conjunto de degelo de nacela de motor turbojato de avião e dispositivo para a implementação do método

Country Status (9)

Country Link
US (1) US9102411B2 (pt)
EP (1) EP2352672B1 (pt)
CN (1) CN102209666B (pt)
BR (1) BRPI0921661A2 (pt)
CA (1) CA2741457A1 (pt)
ES (1) ES2403049T3 (pt)
FR (1) FR2938503A1 (pt)
RU (1) RU2501717C2 (pt)
WO (1) WO2010055215A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
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US8517601B2 (en) * 2010-09-10 2013-08-27 Ultra Electronics Limited Ice detection system and method
CN102522026B (zh) * 2011-11-29 2013-09-18 天津空中代码工程应用软件开发有限公司 飞行结冰模拟器
CN102897324B (zh) * 2012-07-13 2015-06-10 中国商用飞机有限责任公司 一种飞机防冰装置
RU2558408C2 (ru) * 2013-12-30 2015-08-10 Федеральное государственное унитарное предприятие "Крыловский государственный научный центр" Электроимпульсное противообледенительное устройство
US10179654B2 (en) * 2015-10-20 2019-01-15 Honeywell International Inc. Architecture for air data probe power supply control
US10392117B2 (en) * 2016-09-23 2019-08-27 General Electric Company Icing condition detection using instantaneous humidity sensing
RU2666886C1 (ru) * 2017-11-14 2018-09-12 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Способ управления противообледенительной системой воздухозаборника газотурбинного двигателя самолета
FR3079818A1 (fr) 2018-04-10 2019-10-11 Airbus Operations (S.A.S.) Nacelle de moteur d'aeronef munie d'un systeme de protection contre le givre et procede de protection associe
US10822999B2 (en) * 2018-07-24 2020-11-03 Raytheon Technologies Corporation Systems and methods for fan blade de-icing
CN114476079B (zh) * 2021-12-27 2023-10-20 武汉航空仪表有限责任公司 一种基于结冰条件判断的传感器及方法
CN114313272B (zh) * 2022-02-07 2024-09-27 中国商用飞机有限责任公司 结冰探测器、电子设备和结冰探测方法
CN117284470A (zh) * 2022-06-20 2023-12-26 海鹰航空通用装备有限责任公司 一种电加热防除冰机翼蒙皮结构及其成型方法
FR3163924A1 (fr) * 2024-06-26 2026-01-02 Safran Electrical & Power Procédé de degivrage pour un turbopropulseur

Family Cites Families (22)

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GB772188A (en) * 1953-09-11 1957-04-10 Honeywell Regulator Co A new or improved icing indicator for aircraft
GB1082707A (en) * 1966-07-27 1967-09-13 Rosemount Eng Co Ltd Improvements in or relating to ice detection apparatus
US3596264A (en) * 1969-03-13 1971-07-27 Holley Carburetor Co Multichannel frost ice and snow detecting device
US4688757A (en) * 1986-08-11 1987-08-25 Dresser Industries, Inc. Soft seat Y pattern globe valve
US4831819A (en) * 1987-07-02 1989-05-23 Avco Corporation Anti-icing valve
US5412181A (en) * 1993-12-27 1995-05-02 The B. F. Goodrich Company Variable power density heating using stranded resistance wire
US6151567A (en) * 1994-05-27 2000-11-21 Hamilton Sundstrand Corporation Data communication analysis and simulation tool
US6227492B1 (en) * 1999-08-06 2001-05-08 Bell Helicopter Textron Inc. Redundant ice management system for aircraft
US6593547B1 (en) * 2000-11-30 2003-07-15 Pacific Scientific Electro Kinetics Division Air gap deicing device
US7588212B2 (en) * 2003-07-08 2009-09-15 Rohr Inc. Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
FR2863586B1 (fr) * 2003-12-12 2007-01-19 Eurocopter France Dispositif de degivrage/antigivrage modulaire d'une surface aerodynamique.
FR2875542B1 (fr) * 2004-09-21 2009-02-13 Airbus France Sas Dispositif de protection contre le givrage pour moteurs d'aeronefs et procedes de degivrage associe
EP1893484B1 (fr) * 2005-06-22 2010-11-03 Airbus Operations (S.A.S) Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif
FR2887519B1 (fr) * 2005-06-22 2008-10-10 Airbus France Sas Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif
RU2411161C2 (ru) * 2005-06-22 2011-02-10 Эрбюс Франс Система защиты от обледенения и борьбы с обледенением гондолы двигателя летательного аппарата, содержащая резистивный слой
US7708227B2 (en) * 2006-01-06 2010-05-04 Cox & Company, Inc. Energy-efficient electro-thermal ice-protection system
US7564373B2 (en) * 2006-11-30 2009-07-21 Safe Flight Instrument Corporation System and method for detecting ice formation on an aircraft
GB0722398D0 (en) * 2007-11-15 2007-12-27 Rolls Royce Plc A method of monitoring a gas turbine engine
US8049147B2 (en) * 2008-03-28 2011-11-01 United Technologies Corporation Engine inlet ice protection system with power control by zone
US7938368B2 (en) * 2008-04-07 2011-05-10 United Technologies Corporation Nosecone ice protection system for a gas turbine engine
FR2941439B1 (fr) * 2009-01-28 2011-01-14 Aircelle Sa Dispositif de degivrage electrique et systeme de controle associe
CN102522026B (zh) * 2011-11-29 2013-09-18 天津空中代码工程应用软件开发有限公司 飞行结冰模拟器

Also Published As

Publication number Publication date
CN102209666A (zh) 2011-10-05
EP2352672A1 (fr) 2011-08-10
WO2010055215A1 (fr) 2010-05-20
FR2938503A1 (fr) 2010-05-21
US20110225975A1 (en) 2011-09-22
ES2403049T3 (es) 2013-05-13
EP2352672B1 (fr) 2013-01-16
US9102411B2 (en) 2015-08-11
CN102209666B (zh) 2015-08-05
RU2501717C2 (ru) 2013-12-20
CA2741457A1 (fr) 2010-05-20
RU2011124179A (ru) 2012-12-27

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Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law

Free format text: REFERENTE A 7A ANUIDADE.

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 2385 DE 20-09-2016 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.