BR112013009247A2 - estrutura de biorda principal, particularmente para uma entrada de ar nacela de avião e nacela para um motor de avião - Google Patents

estrutura de biorda principal, particularmente para uma entrada de ar nacela de avião e nacela para um motor de avião

Info

Publication number
BR112013009247A2
BR112013009247A2 BR112013009247A BR112013009247A BR112013009247A2 BR 112013009247 A2 BR112013009247 A2 BR 112013009247A2 BR 112013009247 A BR112013009247 A BR 112013009247A BR 112013009247 A BR112013009247 A BR 112013009247A BR 112013009247 A2 BR112013009247 A2 BR 112013009247A2
Authority
BR
Brazil
Prior art keywords
airplane
nacelle
air intake
edge structure
main edge
Prior art date
Application number
BR112013009247A
Other languages
English (en)
Inventor
Coat Caroline
Florent Bouillon
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 BR112013009247A2 publication Critical patent/BR112013009247A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02—De-icing means for engines having icing phenomena
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0012—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular thermal properties
    • B29K2995/0013—Conductive
    • 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
    • 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
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • 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)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Textile Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Moulding By Coating Moulds (AREA)
  • Woven Fabrics (AREA)
  • Resistance Heating (AREA)

Abstract

estrutura de biorda pricinpal, particularmente para uma entrada de ar nacela de avião e nacela para um motor de avião. a invenção relata uma estrutura de borda principal (1), particularmente para uma entrada de ar de uma nacela de avião, incluindo uma borda principal (2) e uma participação interna (3) definindo um compartimento longitudinal (5), o qual está dentro da referida borda principal (2) e acomoda meios de degelo e/ou antigelo, em que a estrutura de borda principal é caracterizada pelo fato de que a referida borda principal (2) consiste de pelo menos uma estrutura composta multiaxial (23) posicionada no topo de um elemento de aquecimento (21) para degelo e/ou antigelo.
BR112013009247A 2010-10-29 2011-10-24 estrutura de biorda principal, particularmente para uma entrada de ar nacela de avião e nacela para um motor de avião BR112013009247A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1058931A FR2966801B1 (fr) 2010-10-29 2010-10-29 Structure de bord d'attaque notamment pour entree d'air de nacelle de moteur d'aeronef
PCT/FR2011/052475 WO2012056155A2 (fr) 2010-10-29 2011-10-24 Structure de bord d'attaque notamment pour entrée d'air de nacelle de moteur d'aéronef

Publications (1)

Publication Number Publication Date
BR112013009247A2 true BR112013009247A2 (pt) 2016-07-26

Family

ID=44169148

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013009247A BR112013009247A2 (pt) 2010-10-29 2011-10-24 estrutura de biorda principal, particularmente para uma entrada de ar nacela de avião e nacela para um motor de avião

Country Status (8)

Country Link
US (1) US20130230390A1 (pt)
EP (1) EP2632797B1 (pt)
CN (1) CN103648909A (pt)
BR (1) BR112013009247A2 (pt)
CA (1) CA2813925A1 (pt)
FR (1) FR2966801B1 (pt)
RU (1) RU2577975C2 (pt)
WO (1) WO2012056155A2 (pt)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10321519B2 (en) 2015-10-30 2019-06-11 Itt Manufacturing Enterprises Llc Metal and composite leading edge assemblies
US20200173363A1 (en) * 2018-12-04 2020-06-04 Rohr, Inc. Nacelle inlet structure

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4877689A (en) * 1988-09-30 1989-10-31 United States Of America As Represented By The Administrator, National Aeronautics And Space Administration High temperature insulation barrier composite
US5115962A (en) * 1988-12-20 1992-05-26 United Technologies Corporation Method of attaching ceramic fiber arrays to metallic substrates
US5654060A (en) * 1995-06-16 1997-08-05 The Boeing Company High temperature insulation system
FR2886674B1 (fr) * 2005-06-07 2007-08-03 Airbus France Sas Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur
DE102006031330B4 (de) * 2005-07-14 2014-03-20 Goodrich Corp. Für Eis empfänglicher Abschnitt eines Flugzeugs, insbesondere Flugtriebwerk- Zelleneinlasslippe, umfassend ein Eisschutzsystem, Flugtriebwerk mit einer solchen Einlasslippe sowie ein Verfahren zum Schutz einer solchen Einlasslippe vor Vereisung
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
FR2898867B1 (fr) * 2006-03-27 2008-12-19 Airbus France Sas Systeme pour le degivrage d'un capot d'entree d'air pour turbomoteur.
FR2912780B1 (fr) * 2007-02-20 2012-03-02 Airbus France Revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe
FR2930234B1 (fr) * 2008-04-21 2010-07-30 Aircelle Sa Systeme de degivrage et/ou d'antigivrage pour bord d'attaque de voilure d'aeronef.
EP2182269A1 (en) * 2008-10-31 2010-05-05 Rockwool International A/S Composite insulating product
DE102008063545C5 (de) * 2008-12-09 2015-04-30 Deutsches Zentrum für Luft- und Raumfahrt e.V. Multiaxialgelege, Verfahren zur Herstellung eines Faserverbundkunststoffs und Faserverbundkunststoff
US9004407B2 (en) * 2008-12-24 2015-04-14 Middle River Aircraft Systems Anti-icing system and method for preventing ice accumulation
JP5336225B2 (ja) * 2009-02-21 2013-11-06 東邦テナックス株式会社 多軸ステッチ基材とそれを用いたプリフォーム
US8549832B2 (en) * 2009-12-30 2013-10-08 MRA Systems Inc. Turbomachine nacelle and anti-icing system and method therefor
US8382039B2 (en) * 2009-12-30 2013-02-26 MRA Systems Inc. Turbomachine nacelle and anti-icing system and method therefor

Also Published As

Publication number Publication date
WO2012056155A3 (fr) 2014-01-09
WO2012056155A2 (fr) 2012-05-03
US20130230390A1 (en) 2013-09-05
CA2813925A1 (fr) 2012-05-03
CN103648909A (zh) 2014-03-19
RU2013123486A (ru) 2014-12-10
EP2632797B1 (fr) 2016-04-20
EP2632797A2 (fr) 2013-09-04
FR2966801B1 (fr) 2012-11-02
FR2966801A1 (fr) 2012-05-04
RU2577975C2 (ru) 2016-03-20

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]