ATE486779T1 - Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte - Google Patents

Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte

Info

Publication number
ATE486779T1
ATE486779T1 AT06778954T AT06778954T ATE486779T1 AT E486779 T1 ATE486779 T1 AT E486779T1 AT 06778954 T AT06778954 T AT 06778954T AT 06778954 T AT06778954 T AT 06778954T AT E486779 T1 ATE486779 T1 AT E486779T1
Authority
AT
Austria
Prior art keywords
icing
aircraft engine
air intake
engine casing
deicing
Prior art date
Application number
AT06778954T
Other languages
English (en)
Inventor
Gilles Chene
Alain Porte
Jacques Lalane
Original Assignee
Airbus Operations Sas
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
Priority claimed from FR0551713A external-priority patent/FR2887520B1/fr
Priority claimed from FR0551711A external-priority patent/FR2887518B1/fr
Priority claimed from FR0551712A external-priority patent/FR2887519B1/fr
Application filed by Airbus Operations Sas filed Critical Airbus Operations Sas
Application granted granted Critical
Publication of ATE486779T1 publication Critical patent/ATE486779T1/de

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
    • 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
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • 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
    • 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—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
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • 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—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/13—Two-dimensional trapezoidal
    • F05D2250/132—Two-dimensional trapezoidal hexagonal
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Resistance Heating (AREA)
  • Resistance Heating (AREA)
  • Measuring Volume Flow (AREA)
  • Catching Or Destruction (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
AT06778954T 2005-06-22 2006-06-19 Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte ATE486779T1 (de)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR0551713A FR2887520B1 (fr) 2005-06-22 2005-06-22 Systeme de degivrage a reseaux d'elements resistifs segregues
FR0551711A FR2887518B1 (fr) 2005-06-22 2005-06-22 Nacelle de moteur d'aeronef a dispositif de degivrage perfectionne et attenuation acoustique optimisee
FR0551712A FR2887519B1 (fr) 2005-06-22 2005-06-22 Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif
PCT/FR2006/050608 WO2006136748A2 (fr) 2005-06-22 2006-06-19 Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif

Publications (1)

Publication Number Publication Date
ATE486779T1 true ATE486779T1 (de) 2010-11-15

Family

ID=37570804

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06778954T ATE486779T1 (de) 2005-06-22 2006-06-19 Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte

Country Status (8)

Country Link
US (1) US20100199629A1 (de)
EP (1) EP1893484B1 (de)
JP (1) JP2008546945A (de)
AT (1) ATE486779T1 (de)
BR (1) BRPI0612110A2 (de)
CA (1) CA2611656C (de)
DE (1) DE602006018005D1 (de)
WO (1) WO2006136748A2 (de)

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FR3004165B1 (fr) * 2013-04-09 2015-03-27 Aircelle Sa Element d'aeronef necessitant un traitement contre le givre
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US9938852B2 (en) * 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly and methods of assembling the same
US9656761B2 (en) 2014-04-30 2017-05-23 The Boeing Company Lipskin for a nacelle and methods of making the same
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FR3060651B1 (fr) * 2016-12-20 2020-11-06 Airbus Operations Sas Structure d'entree d'air pour une nacelle d'aeronef
FR3061132B1 (fr) * 2016-12-27 2023-11-03 Airbus Operations Sas Structure pour ensemble propulsif d'aeronef, systeme et ensemble propulsif associes
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FR3120352B1 (fr) * 2021-03-03 2024-03-08 Airbus Operations Sas Entree d’air de nacelle munie d’un système de protection contre la glace mixte
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Also Published As

Publication number Publication date
BRPI0612110A2 (pt) 2010-10-19
CA2611656A1 (fr) 2006-12-28
US20100199629A1 (en) 2010-08-12
EP1893484A2 (de) 2008-03-05
CA2611656C (fr) 2014-01-07
DE602006018005D1 (de) 2010-12-16
WO2006136748A3 (fr) 2007-05-03
JP2008546945A (ja) 2008-12-25
EP1893484B1 (de) 2010-11-03
WO2006136748A2 (fr) 2006-12-28

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