WO2011080286A3 - Flugzeugrumpf und hautfeld - Google Patents

Flugzeugrumpf und hautfeld Download PDF

Info

Publication number
WO2011080286A3
WO2011080286A3 PCT/EP2010/070826 EP2010070826W WO2011080286A3 WO 2011080286 A3 WO2011080286 A3 WO 2011080286A3 EP 2010070826 W EP2010070826 W EP 2010070826W WO 2011080286 A3 WO2011080286 A3 WO 2011080286A3
Authority
WO
WIPO (PCT)
Prior art keywords
skin section
aircraft fuselage
fuselage
skin
aircraft
Prior art date
Application number
PCT/EP2010/070826
Other languages
English (en)
French (fr)
Other versions
WO2011080286A2 (de
Inventor
Torsten Noebel
Original Assignee
Airbus Operations Gmbh
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 Gmbh filed Critical Airbus Operations Gmbh
Priority to EP10803250A priority Critical patent/EP2519438A2/de
Priority to US13/519,327 priority patent/US9227717B2/en
Priority to CN201080060014.2A priority patent/CN102741119B/zh
Publication of WO2011080286A2 publication Critical patent/WO2011080286A2/de
Publication of WO2011080286A3 publication Critical patent/WO2011080286A3/de

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
    • 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
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/60—UAVs characterised by the material
    • B64U20/65—Composite materials
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials

Abstract

Offenbart ist ein Rumpf (2) aus einem faserverstärkten Verbundmaterial für ein Flugzeug mit einer Haut (4) und mit einer Vielzahl von Umfangsversteifungen (12) und nur einer geringen Anzahl von Längsversteifungen (10), wobei die Haut (4) eine Vielzahl von lokalen Verstärkungen (14) aufweist, sowie ein Hautfeld (6) zur Bildung eines derartigen Rumpfes.
PCT/EP2010/070826 2009-12-29 2010-12-29 Flugzeugrumpf und hautfeld WO2011080286A2 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP10803250A EP2519438A2 (de) 2009-12-29 2010-12-29 Flugzeugrumpf und hautfeld
US13/519,327 US9227717B2 (en) 2009-12-29 2010-12-29 Aircraft fuselage reinforcement system
CN201080060014.2A CN102741119B (zh) 2009-12-29 2010-12-29 飞行器机身及蒙皮区域

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US29051109P 2009-12-29 2009-12-29
DE102009060695.5 2009-12-29
US61/290,511 2009-12-29
DE102009060695A DE102009060695A1 (de) 2009-12-29 2009-12-29 Flugzeugrumpf und Hautfeld

Publications (2)

Publication Number Publication Date
WO2011080286A2 WO2011080286A2 (de) 2011-07-07
WO2011080286A3 true WO2011080286A3 (de) 2011-10-13

Family

ID=44226883

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2010/070826 WO2011080286A2 (de) 2009-12-29 2010-12-29 Flugzeugrumpf und hautfeld

Country Status (5)

Country Link
US (1) US9227717B2 (de)
EP (1) EP2519438A2 (de)
CN (1) CN102741119B (de)
DE (1) DE102009060695A1 (de)
WO (1) WO2011080286A2 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2730397B1 (de) 2012-11-07 2020-01-22 Airbus Operations GmbH Verfahren zum Herstellen eines Verbundstoffschalenelements
EP2842865B1 (de) * 2013-08-28 2019-12-18 Airbus Operations GmbH Fensterscheibe für ein flugwerk und verfahren zur herstellung davon
DE102014109362B4 (de) 2014-07-04 2016-03-03 Airbus Operation GmbH Luftfahrzeugstrukturkomponente
ES2662853T3 (es) * 2014-12-29 2018-04-10 Airbus Operations S.L. Cono de cola de una aeronave
EP3109152B1 (de) * 2015-06-24 2019-08-07 Airbus Operations GmbH Versteifte rumpfkomponente sowie verfahren und vorrichtung zur herstellung einer versteiften rumpfkomponente
CN106314753A (zh) * 2016-09-23 2017-01-11 江西洪都航空工业集团有限责任公司 一种高强度高刚度轻质整体机体结构
LU101288B1 (de) * 2019-06-26 2020-12-28 Airbus Operations Gmbh Verfahren zur herstellung von grossbauteilen aus thermoplastischen faserverbundwerkstoffen

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2766407A1 (fr) * 1997-07-22 1999-01-29 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
US20060226287A1 (en) * 2004-04-06 2006-10-12 Kent Grantham Structural panels for use in aircraft fuselages and other structures

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2412778A (en) * 1944-12-18 1946-12-17 Cons Vultee Aircraft Corp Suspension type flooring for aircraft
US4053667A (en) * 1974-09-09 1977-10-11 Lockheed Aircraft Corporation Stiffened structural laminate and method of molding laminate with stiffener beads
US5271986A (en) * 1991-04-19 1993-12-21 United Technologies Corporation Structural member having a stiffener bead therein and comprising plies of composite material extending for the full length and width of the structural member and continuously through the stiffener bead, and the article so made
FR2700407A1 (fr) 1993-01-14 1994-07-13 Sca Promotion France Panneau pour support d'informations.
US6187411B1 (en) * 1996-10-04 2001-02-13 The Boeing Company Stitch-reinforced sandwich panel and method of making same
US6648273B2 (en) 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7621482B2 (en) 2005-11-15 2009-11-24 The Boeing Company Weight optimized pressurizable aircraft fuselage structures having near elliptical cross sections
FI119726B (fi) 2006-09-26 2009-02-27 Patria Aerostructures Oy Ilma-aluksen kaarielementti, siipi, ohjainpinta sekä vakaaja
FR2911202B1 (fr) * 2007-01-05 2009-02-13 Airbus France Sas Procede d'optimisation de panneaux raidis sous contraintes '
FR2922516B1 (fr) * 2007-10-18 2010-04-16 Airbus France Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion
FR2922517B1 (fr) * 2007-10-18 2010-04-23 Airbus France Avion comportant des jonctions d'arrets de raidisseurs et procede de fabrication d'un tel avion
US8052826B2 (en) * 2009-03-24 2011-11-08 The Boeing Company Method of making bead-stiffened composite parts and parts made thereby
US8636252B2 (en) * 2010-06-25 2014-01-28 The Boeing Company Composite structures having integrated stiffeners with smooth runouts and method of making the same

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2766407A1 (fr) * 1997-07-22 1999-01-29 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
US20060226287A1 (en) * 2004-04-06 2006-10-12 Kent Grantham Structural panels for use in aircraft fuselages and other structures

Also Published As

Publication number Publication date
DE102009060695A1 (de) 2011-07-07
EP2519438A2 (de) 2012-11-07
CN102741119B (zh) 2016-03-23
CN102741119A (zh) 2012-10-17
US20120286093A1 (en) 2012-11-15
WO2011080286A2 (de) 2011-07-07
US9227717B2 (en) 2016-01-05

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