WO2013057355A3 - Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado - Google Patents

Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado Download PDF

Info

Publication number
WO2013057355A3
WO2013057355A3 PCT/ES2012/070731 ES2012070731W WO2013057355A3 WO 2013057355 A3 WO2013057355 A3 WO 2013057355A3 ES 2012070731 W ES2012070731 W ES 2012070731W WO 2013057355 A3 WO2013057355 A3 WO 2013057355A3
Authority
WO
WIPO (PCT)
Prior art keywords
damage
fuselage
resistant
skin
improved impact
Prior art date
Application number
PCT/ES2012/070731
Other languages
English (en)
French (fr)
Other versions
WO2013057355A2 (es
Inventor
Esteban MARTINO GONZÁLEZ
Eduardo VINUÉ SANTOLALLA
Diego FOLCH CORTÉS
Pablo GOYA ABAURREA
Enrique GUINALDO FERNÁNDEZ
Julien Guillemaut
Original Assignee
Airbus Operations S.L.
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 S.L., Airbus Operations Sas filed Critical Airbus Operations S.L.
Priority to ES12806063.9T priority Critical patent/ES2592633T3/es
Priority to EP12806063.9A priority patent/EP2774839B1/en
Priority to CN201280051361.8A priority patent/CN104066647B/zh
Publication of WO2013057355A2 publication Critical patent/WO2013057355A2/es
Publication of WO2013057355A3 publication Critical patent/WO2013057355A3/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B64C1/062—Frames specially adapted to absorb crash loads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/0685—Tail cones
    • 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
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Tires In General (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado. Se refiere a una sección (32) del fuselaje de una aeronave sometida a impactos de cuerpos externos, teniendo el fuselaje de la aeronave una forma curva con al menos un plano de simetría vertical (A-A) y un eje longitudinal central y comprendiendo un revestimiento (35) y una pluralidad de cuadernas (37) dispuestas perpendicularmente a dicho eje longitudinal, comprendiendo también dicha sección (32) del fuselaje al menos una estructura reticular interna (51, 53) montada sobre una estructura de soporte (41, 43) que incluye vigas longitudinales (39) unidas al revestimiento (35) e interconectadas con dichas cuadernas (37), estando dispuesta dicha estructura reticular interna (51, 53) para crear al menos una celda cerrada (75) con el revestimiento (45) para mejorar su resistencia y su tolerancia al daño respecto a dichos impactos.
PCT/ES2012/070731 2011-10-21 2012-10-19 Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado WO2013057355A2 (es)

Priority Applications (3)

Application Number Priority Date Filing Date Title
ES12806063.9T ES2592633T3 (es) 2011-10-21 2012-10-19 Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado
EP12806063.9A EP2774839B1 (en) 2011-10-21 2012-10-19 Improved impact resistant and damage tolerant aircraft fuselage
CN201280051361.8A CN104066647B (zh) 2011-10-21 2012-10-19 冲击抵抗和损坏容限改善的飞行器机身段

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ESP201131693 2011-10-21
ES201131693A ES2404946B1 (es) 2011-10-21 2011-10-21 Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado

Publications (2)

Publication Number Publication Date
WO2013057355A2 WO2013057355A2 (es) 2013-04-25
WO2013057355A3 true WO2013057355A3 (es) 2013-08-08

Family

ID=47429842

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2012/070731 WO2013057355A2 (es) 2011-10-21 2012-10-19 Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado

Country Status (5)

Country Link
US (1) US8678314B2 (es)
EP (1) EP2774839B1 (es)
CN (1) CN104066647B (es)
ES (2) ES2404946B1 (es)
WO (1) WO2013057355A2 (es)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2599711B1 (en) * 2011-12-01 2017-07-26 Airbus Operations S.L. Highly loaded frame of an aircraft fuselage with a lattice structured web
DE102014107404A1 (de) * 2014-05-26 2015-11-26 Airbus Operations Gmbh Druckschott für einen Flugzeugrumpf
CN104571125B (zh) * 2014-12-18 2016-01-27 北京控制工程研究所 一种利用一条标准弹道应对多种返回条件的控制方法
ES2661881T3 (es) * 2014-12-23 2018-04-04 Airbus Operations, S.L. Pala de hélice para motor de aeronave
US10358821B2 (en) * 2015-03-02 2019-07-23 The Boeing Company Thermoplastic truss structure for use in wing and rotor blade structures and methods for manufacture
EP3106381B1 (en) 2015-06-15 2018-10-24 Airbus Operations, S.L. Aircraft with a protective shield against an engine blade release
US9630702B2 (en) * 2015-06-30 2017-04-25 Rohr, Inc. Noise attenuation for an open rotor aircraft propulsion system
US9725155B2 (en) 2015-12-30 2017-08-08 General Electric Company Method and system for open rotor engine fuselage protection
JP6768348B2 (ja) 2016-05-26 2020-10-14 三菱重工業株式会社 胴体の断面形状設計方法、設計装置及び設計プログラム
EP3281861B1 (en) * 2016-08-11 2019-10-02 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A rotary wing aircraft with a fuselage that comprises at least one structural stiffened panel
EP3335982B1 (en) * 2016-12-16 2020-09-30 Airbus Operations, S.L. Aircraft having a rear section with a continuous skin for the fuselage and the vertical tail plane
EP3375706B1 (en) * 2017-03-15 2022-05-18 Airbus Operations S.L. Impact resistant fuselage
WO2019118908A1 (en) 2017-12-14 2019-06-20 Adaptive Global Solutions, LLC Fire resistant aerial vehicle for suppressing widespread fires
US11383817B2 (en) 2019-07-19 2022-07-12 The Boeing Company Modular fuselage assemblies for aircraft, aircraft including modular fuselage assemblies, and MEl'hods of assembling modular fuselage assemblies
EP3808650A1 (en) * 2019-10-17 2021-04-21 BAE SYSTEMS plc Packers for use in aircraft assembly
US20220306266A1 (en) * 2019-09-12 2022-09-29 Bae Systems Plc Packers for use in aircraft assembly
US20210339846A1 (en) * 2019-10-15 2021-11-04 General Electric Company Removeable fuselage shield for an aircraft
US20210221491A1 (en) * 2019-10-15 2021-07-22 General Electric Company Fuselage shield for an aircraft with an unducted engine
CN113200149B (zh) * 2021-05-18 2023-04-11 中国空气动力研究与发展中心空天技术研究所 一种基于进气道的固定翼无人机承力结构

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1108646A2 (de) * 1999-12-16 2001-06-20 EADS Airbus GmbH Strukturbauteil
US20090140096A1 (en) * 2007-11-30 2009-06-04 Airbus Espana, S.L. Impact resistant aircraft fuselage
DE102009056996A1 (de) * 2009-12-04 2011-06-09 Eads Deutschland Gmbh Versteifungsstruktur für Flächengebilde, Steife und Flugzeug

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6612217B1 (en) * 1998-06-02 2003-09-02 Sri International Penetration resistant fabric structures and materials
US6588705B1 (en) * 2001-11-21 2003-07-08 Skepsis Incorporated Security screen device for protecting persons and property
US7997529B2 (en) * 2006-01-19 2011-08-16 The Boeing Company Compliant panel for aircraft
DE102006026169B4 (de) * 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102007011627A1 (de) * 2007-01-23 2008-07-31 Airbus Deutschland Gmbh Innenverkleidung für ein Luftfahrzeug
US7866605B2 (en) * 2007-04-24 2011-01-11 The Boeing Company Energy absorbing impact band and method
US8490920B2 (en) * 2007-10-12 2013-07-23 Abe Karem Composite bulkhead and skin construction
US7926407B1 (en) * 2007-11-16 2011-04-19 Gerald Hallissy Armor shielding
FR2927606B1 (fr) * 2008-02-15 2010-07-30 Airbus France Fuselage d'aeronef en materiau composite a tenue au crash amelioree
DE102008002117B4 (de) * 2008-05-30 2013-10-31 Airbus Operations Gmbh Verbund und Struktur
ES2391967B1 (es) * 2010-01-14 2013-10-10 Airbus Operations, S.L. Pilón de soporte de motores de aeronaves.
ES2397875B1 (es) * 2010-03-15 2014-01-27 Airbus Operations, S.L. Método multi-daños para la optimización de un diseño estructural.
ES2398287B1 (es) * 2010-03-29 2014-01-29 Airbus Operations S.L. Fuselaje de aeronave resistente al impacto y tolerante al daño.
FR2960179A1 (fr) * 2010-05-20 2011-11-25 Airbus Operations Sas Piece structurale composite a rigidite evolutive
US8365803B2 (en) * 2010-10-20 2013-02-05 Schoenheit Ronald A Debris entrapment system
DE102011102364A1 (de) * 2011-05-24 2012-11-29 Airbus Operations Gmbh Freitragendes Kabinenstruktursegment

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1108646A2 (de) * 1999-12-16 2001-06-20 EADS Airbus GmbH Strukturbauteil
US20090140096A1 (en) * 2007-11-30 2009-06-04 Airbus Espana, S.L. Impact resistant aircraft fuselage
DE102009056996A1 (de) * 2009-12-04 2011-06-09 Eads Deutschland Gmbh Versteifungsstruktur für Flächengebilde, Steife und Flugzeug

Also Published As

Publication number Publication date
US20130099057A1 (en) 2013-04-25
ES2592633T3 (es) 2016-11-30
WO2013057355A2 (es) 2013-04-25
EP2774839A2 (en) 2014-09-10
ES2404946R1 (es) 2013-10-07
EP2774839B1 (en) 2016-06-15
CN104066647B (zh) 2016-09-21
US8678314B2 (en) 2014-03-25
CN104066647A (zh) 2014-09-24
ES2404946B1 (es) 2014-09-02
ES2404946A2 (es) 2013-05-29

Similar Documents

Publication Publication Date Title
WO2013057355A3 (es) Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado
CL2014001329A1 (es) Carenado de espacio, comprende: una pluralidad de paneles, los cuales se interconectan utilizando conectores para formar una aerodinamica que se extiende desde una parte frontal de un remolque y soportes conectados entre la pluralidad de paneles a traves de la estructura de soporte del remolque; un remolque.
WO2015047485A3 (en) Gas turbine engine cmc airfoil assembly
EP2772442A3 (en) Spacecraft with open sides
EP2703283A3 (en) Bonded composite aircraft wing
WO2011127899A3 (de) Luftfahrzeug mit einer integrierten energieaufnehmenden verformungsstruktur und luftfahrzeug mit einem derartigen rumpf
CL2014000120A1 (es) Amortiguador pasivo para amortiguar movimiento relativo entre miembros de una estructura, comprende al menos un primer y segundo conjunto de placas que se superponen entre si en un empalme giratorio que comprende un pasador o perno, un orificio de conexión en cada una de las placas del segundo conjunto, las cuales están dimensionadas para proporcionar una cantidad de holgura con el pasador de conexión, el que puede moverse dentro del orificio de conexion.
WO2012028467A8 (en) Air sucking vehicle fuselage component, method for producing an air sucking vehicle fuselage component and a vehicle, especially an aircraft, with an air sucking vehicle fuselage component
EP2487106A4 (en) Composite material structure, as well as aircraft wing and fuselage provided therewith
WO2012002769A3 (ko) 섬유상의 구조체들을 포함하는 전극 조립체
EP2671794A4 (en) Composite material structure, and aircraft wing and fuselage provided therewith
WO2010031958A3 (fr) Partie arriere d'aeronef comprenant deux demi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef
WO2011061260A3 (en) Cover for an aircraft structure
BR112012001965A2 (pt) viga para a suspensão de um turbomotor na estrutura de uma aeronave, utilização de uma viga, e, aeronave
BR112014029052A2 (pt) conjunto para conectar um assento de aeronave ao piso.
MX364103B (es) Estructura compuesta, por ejemplo una moneda.
ATE552168T1 (de) Anbindung einer tragfläche an eine rumpfzelle eines flugzeugs
EP2671792A4 (en) Composite material structure, and aircraft wing and fuselage provided therewith
WO2013056285A3 (de) Vorrichtung mit einer mehrzahl von energiewandlerelementen
EP2610179A3 (en) Aircraft air inlet diverter assemblies with improved aerodynamic characteristics
FR2978496B1 (fr) Ensemble propulsif d'aeronef comprenant au moins un turboreacteur et une nacelle
WO2013128054A3 (es) Estructura de refuerzo integrada en estructura interna de aeronave en material compuesto
EP2530021A3 (en) Assembling jig for at least one section of an aircraft fuselage
WO2012135876A3 (de) Neue art von zukünftigen luftschiffen
WO2011089580A3 (en) Side support arrangement

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 2012806063

Country of ref document: EP

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 12806063

Country of ref document: EP

Kind code of ref document: A2