BR112014006236A2 - montagem de aba de uma nacela de motor turbo equipada com pelo menos um sistema de degelo elétrico e nacela de motor turbo - Google Patents

montagem de aba de uma nacela de motor turbo equipada com pelo menos um sistema de degelo elétrico e nacela de motor turbo

Info

Publication number
BR112014006236A2
BR112014006236A2 BR112014006236A BR112014006236A BR112014006236A2 BR 112014006236 A2 BR112014006236 A2 BR 112014006236A2 BR 112014006236 A BR112014006236 A BR 112014006236A BR 112014006236 A BR112014006236 A BR 112014006236A BR 112014006236 A2 BR112014006236 A2 BR 112014006236A2
Authority
BR
Brazil
Prior art keywords
engine nacelle
turbo engine
flap assembly
defrost system
electric defrost
Prior art date
Application number
BR112014006236A
Other languages
English (en)
Inventor
Pereira David
Dunand Michel
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 BR112014006236A2 publication Critical patent/BR112014006236A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • H05B3/20—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2203/00—Aspects relating to Ohmic resistive heating covered by group H05B3/00
    • H05B2203/002—Heaters using a particular layout for the resistive material or resistive elements
    • H05B2203/003—Heaters using a particular layout for the resistive material or resistive elements using serpentine layout
BR112014006236A 2011-09-28 2012-09-07 montagem de aba de uma nacela de motor turbo equipada com pelo menos um sistema de degelo elétrico e nacela de motor turbo BR112014006236A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1158678A FR2980458B1 (fr) 2011-09-28 2011-09-28 Ensemble de levre pour nacelle de turboreacteur a degivrage electrique
PCT/FR2012/052006 WO2013045783A1 (fr) 2011-09-28 2012-09-07 Ensemble de lèvre pour nacelle de turboréacteur à dégivrage électrique

Publications (1)

Publication Number Publication Date
BR112014006236A2 true BR112014006236A2 (pt) 2017-04-04

Family

ID=46968275

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014006236A BR112014006236A2 (pt) 2011-09-28 2012-09-07 montagem de aba de uma nacela de motor turbo equipada com pelo menos um sistema de degelo elétrico e nacela de motor turbo

Country Status (8)

Country Link
US (1) US8975560B2 (pt)
EP (1) EP2760741B1 (pt)
CN (1) CN103826971A (pt)
BR (1) BR112014006236A2 (pt)
CA (1) CA2847806A1 (pt)
FR (1) FR2980458B1 (pt)
RU (1) RU2014115889A (pt)
WO (1) WO2013045783A1 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10399684B2 (en) * 2014-10-29 2019-09-03 The Boeing Company Induction heating coils with uniform heating
JP6549855B2 (ja) * 2015-02-17 2019-07-24 三菱航空機株式会社 航空機の風防
US10486821B2 (en) 2015-07-07 2019-11-26 The Boeing Company Jet engine anti-icing and noise-attenuating air inlets
CN108688824B (zh) * 2017-04-10 2020-07-14 清华大学 发动机进气口除冰系统、内燃发动机及航空器
CA3156694A1 (en) * 2019-11-01 2021-05-06 Ethan Dinauer Three phase medium voltage heater
CN113955124B (zh) * 2021-11-05 2024-02-13 天津航空机电有限公司 一种嵌入式进气道唇口防冰加热组件及制作方法
FR3130755A1 (fr) * 2021-12-20 2023-06-23 Airbus Operations Dispositif de chauffage à matelas chauffant pour un système de protection contre le givre d’un aéronef.

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699303A (en) * 1947-10-24 1955-01-11 Rotol Ltd Means for electrically heating the spinners of airscrews
US4688757A (en) 1986-08-11 1987-08-25 Dresser Industries, Inc. Soft seat Y pattern globe valve
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
US7469862B2 (en) * 2005-04-22 2008-12-30 Goodrich Corporation Aircraft engine nacelle inlet having access opening for electrical ice protection system
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
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
US7633450B2 (en) * 2005-11-18 2009-12-15 Goodrich Corporation Radar altering structure using specular patterns of conductive material
US7923668B2 (en) * 2006-02-24 2011-04-12 Rohr, Inc. Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
FR2898868B1 (fr) * 2006-03-24 2008-12-12 Aircelle Sa Structure pour levre d'entree d'air de nacelle a degivrage electrique
US7922120B2 (en) * 2006-11-15 2011-04-12 Honeywell International Inc. Wing ice protection heater element network
FR2908738B1 (fr) * 2006-11-16 2009-12-04 Airbus France Bord d'attaque d'aeronef.
US7922121B2 (en) * 2007-10-15 2011-04-12 Rosemount Aerospace Inc. Power distribution architecture for an ice protection system

Also Published As

Publication number Publication date
FR2980458B1 (fr) 2013-08-30
US8975560B2 (en) 2015-03-10
FR2980458A1 (fr) 2013-03-29
RU2014115889A (ru) 2015-11-10
WO2013045783A1 (fr) 2013-04-04
CA2847806A1 (fr) 2013-04-04
CN103826971A (zh) 2014-05-28
EP2760741A1 (fr) 2014-08-06
US20140209592A1 (en) 2014-07-31
EP2760741B1 (fr) 2016-11-16

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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 5A ANUIDADE.

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