BRPI1013593A2 - parte traseira de aeronave, compreendendo uma estrutura de suporte de motores montada oscilante sobre a fuselagem - Google Patents

parte traseira de aeronave, compreendendo uma estrutura de suporte de motores montada oscilante sobre a fuselagem

Info

Publication number
BRPI1013593A2
BRPI1013593A2 BRPI1013593A BRPI1013593A BRPI1013593A2 BR PI1013593 A2 BRPI1013593 A2 BR PI1013593A2 BR PI1013593 A BRPI1013593 A BR PI1013593A BR PI1013593 A BRPI1013593 A BR PI1013593A BR PI1013593 A2 BRPI1013593 A2 BR PI1013593A2
Authority
BR
Brazil
Prior art keywords
fuselage
support structure
engine support
mounted engine
aircraft rear
Prior art date
Application number
BRPI1013593A
Other languages
English (en)
Inventor
Esteban Quiroz-Hernandez
Frédéric Journade
Jean Michel Saucray
Jérôme Antypas
Laurent Lafont
Mathieu Bonnet
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
Application filed by Airbus Operations Sas filed Critical Airbus Operations Sas
Publication of BRPI1013593A2 publication Critical patent/BRPI1013593A2/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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/04—Power-plant nacelles, fairings or cowlings associated with fuselages
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
BRPI1013593A 2009-03-30 2010-03-29 parte traseira de aeronave, compreendendo uma estrutura de suporte de motores montada oscilante sobre a fuselagem BRPI1013593A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0951959A FR2943623B1 (fr) 2009-03-30 2009-03-30 Partie arriere d'aeronef comprenant une structure de support de moteurs montee oscillante sur le fuselage
PCT/FR2010/050566 WO2010112742A2 (fr) 2009-03-30 2010-03-29 Partie arriere d'aeronef comprenant une structure de support de moteurs montee oscillante sur le fuselage

Publications (1)

Publication Number Publication Date
BRPI1013593A2 true BRPI1013593A2 (pt) 2016-04-19

Family

ID=41396174

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1013593A BRPI1013593A2 (pt) 2009-03-30 2010-03-29 parte traseira de aeronave, compreendendo uma estrutura de suporte de motores montada oscilante sobre a fuselagem

Country Status (9)

Country Link
US (1) US8480025B2 (pt)
EP (1) EP2414228B1 (pt)
JP (1) JP5587973B2 (pt)
CN (1) CN102448815B (pt)
BR (1) BRPI1013593A2 (pt)
CA (1) CA2756345C (pt)
FR (1) FR2943623B1 (pt)
RU (1) RU2011143777A (pt)
WO (1) WO2010112742A2 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9067687B2 (en) * 2011-03-09 2015-06-30 Gunnar Rosenlund Propulsion system with movably mounted engines
EP2631180B1 (en) 2012-02-27 2014-04-02 Airbus Operations (S.A.S.) An engine attachment pylon
EP3024729B1 (en) 2013-07-26 2022-04-27 MRA Systems, LLC Aircraft engine pylon
ES2672528T3 (es) * 2014-11-27 2018-06-14 Airbus Operations S.L. Sección de fuselaje de aeronave
EP3181454A1 (en) * 2015-12-15 2017-06-21 Airbus Operations, S.L. Aircraft pylon assembly
FR3072947B1 (fr) * 2017-10-30 2021-12-17 Airbus Operations Sas Aeronef comprenant au moins un ensemble moteur relie au fuselage de l'aeronef par deux bielles de poussee positionnees au moins partiellement dans une entree d'air de l'ensemble moteur
KR20260057761A (ko) 2024-10-21 2026-04-28 주식회사 디에프씨 내수성 및 점착력이 우수한 수성 에멀젼 아크릴계 점착제, 및 이를 이용한 점착테이프

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR966757A (fr) * 1939-11-29 1950-10-18 Perfectionnements dans la propulsion et la construction des avions
US3490556A (en) * 1968-01-15 1970-01-20 Mc Donnell Douglas Corp Aircraft cabin noise reduction system with tuned vibration absorbers
US4492353A (en) * 1982-09-30 1985-01-08 Phillips Bryan D Aircraft capable of vertical short takeoff and landing
GB2129498B (en) * 1982-10-29 1986-04-03 Rolls Royce Mounting system for two coupled turboshaft gas turbine engines
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
US5065959A (en) * 1989-11-21 1991-11-19 The Boeing Company Vibration damping aircraft engine attachment
US5551650A (en) * 1994-06-16 1996-09-03 Lord Corporation Active mounts for aircraft engines
WO1998025821A1 (fr) * 1996-12-12 1998-06-18 Didier Delmotte Aeronefs equipes de motoreacteurs a pistons rotatifs et a helices contrarotatives
FR2826056B1 (fr) * 2001-06-14 2003-12-19 Snecma Moteurs Dispositif de propulsion a cycle variable par transmission mecanique pour avion supersonique
FR2891250B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
DE102006051572B4 (de) * 2006-11-02 2010-01-21 Airbus Deutschland Gmbh Flügel-Rumpf-Verbindung eines Flugzeugs
ES2341514B1 (es) * 2007-10-03 2011-04-18 Airbus España S.L. Configuracion estructural para el montaje de un motor sobre la estructura de una aeronave.
FR2931799B1 (fr) * 2008-05-30 2010-12-24 Airbus France Avion a reacteurs arrieres.
FR2935955B1 (fr) * 2008-09-18 2010-10-15 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs reliee au fuselage par au moins un element de blocage sollicite en compression.
FR2935953B1 (fr) * 2008-09-18 2010-10-29 Airbus France Partie arriere d'aeronef comprenant deux semi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef.
FR2935954B1 (fr) * 2008-09-18 2011-06-03 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs traversant le fuselage et reliee a celui-ci par au moins une bielle.
FR2939102B1 (fr) * 2008-12-01 2011-01-21 Airbus France Structure rigide de mat d'aeronef equipee d'une extension de nervure pour la reprise du moment selon la direction longitudinale
FR2939101B1 (fr) * 2008-12-01 2010-12-31 Airbus France Structure rigide de mat d'aeronef plaquee contre une extension laterale de fuselage pour sa fixation
ES2391967B1 (es) * 2010-01-14 2013-10-10 Airbus Operations, S.L. Pilón de soporte de motores de aeronaves.

Also Published As

Publication number Publication date
FR2943623A1 (fr) 2010-10-01
JP2012521928A (ja) 2012-09-20
CA2756345C (fr) 2016-11-15
WO2010112742A3 (fr) 2011-03-17
EP2414228B1 (fr) 2015-03-11
JP5587973B2 (ja) 2014-09-10
US8480025B2 (en) 2013-07-09
CN102448815B (zh) 2014-08-27
WO2010112742A2 (fr) 2010-10-07
CA2756345A1 (fr) 2010-10-07
CN102448815A (zh) 2012-05-09
US20120006937A1 (en) 2012-01-12
EP2414228A2 (fr) 2012-02-08
FR2943623B1 (fr) 2011-04-29
RU2011143777A (ru) 2013-05-10

Similar Documents

Publication Publication Date Title
BRPI0917143A2 (pt) avião equipado com motores de turboreator com fluxo duplo
BRPI0906953A2 (pt) Entrada de ar para nacela de aeronave, conjunto compreendendo entrada de ar, conjunto de propulsão para aeronave
BRPI0821504A2 (pt) nacela para motor de avião
IL224415A (en) An aircraft with integral aerodynamic configuration
BRPI0823241A2 (pt) Dispositivo aerodinâmico para um veículo
BRPI0912052A2 (pt) aeronave com alimentação por energia híbrida.
FR2915179B1 (fr) Aeronef a impact environnemental reduit.
PL2675712T3 (pl) Statek powietrzny o ulepszonych osiągach aerodynamicznych
BRPI0908079A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0820878A2 (pt) fuselagem com atenuação acústica para aeronave
BRPI0907771A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0821412A2 (pt) Configuração otimizada de motores para aeronave
BRPI0906171A2 (pt) Nacela de aeronave
BRPI0815499A2 (pt) Unidade de iluminação de aeronave
BRPI0918643A2 (pt) parte traseira de aeronave, compreendendo uma estrutura de suporte de motores atravessando a fuselagem e ligada a este por pelo menos uma biela.
EP2610173A4 (en) COAXIAL ROTATION HELICOPTER WITH SOLID ROTOR
FR2942453B1 (fr) Aeronef a structure de plancher renforcee.
PL2539548T3 (pl) Podatna obsada łożyska tylnego z ogranicznikiem do maszyny wirowej
FR2951434B1 (fr) Empennage horizontal d'aeronef muni d'un apex de bord d'attaque
FR2935349B1 (fr) Turbomachine a helices non carenees
BRPI0907959A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0917880A2 (pt) estrutura de entrada de ar para nacela de motor turbojato tencionada, nacela para um motor turbojato.
BRPI0914044A2 (pt) arranjo de entrada de ar para aeronave
BR112015011502A2 (pt) unidade de propulsão para uma aeronave compreendendo um motor turbojato de tipo de passagem, uma nacela circundando o motor turbojato e meios para deslocar pelo menos uma meia porção.
BRPI0816720A2 (pt) Estrutura aerodinâmica para veículo

Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]