DE102004001078B8 - fuselage - Google Patents

fuselage Download PDF

Info

Publication number
DE102004001078B8
DE102004001078B8 DE200410001078 DE102004001078A DE102004001078B8 DE 102004001078 B8 DE102004001078 B8 DE 102004001078B8 DE 200410001078 DE200410001078 DE 200410001078 DE 102004001078 A DE102004001078 A DE 102004001078A DE 102004001078 B8 DE102004001078 B8 DE 102004001078B8
Authority
DE
Germany
Prior art keywords
fuselage
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
DE200410001078
Other languages
German (de)
Other versions
DE102004001078A1 (en
DE102004001078B4 (en
Inventor
Dipl.-Ing. Müller Rainer
Dipl.-Ing. Oestereich Wilko
Thorsten Reinelt
Peter Turanski
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
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
Priority to DE200410001078 priority Critical patent/DE102004001078B8/en
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Priority to BRPI0506667-0A priority patent/BRPI0506667A/en
Priority to US10/596,979 priority patent/US20070023572A1/en
Priority to EP05700701A priority patent/EP1701881B1/en
Priority to CNB2005800019492A priority patent/CN100418850C/en
Priority to DE602005013059T priority patent/DE602005013059D1/en
Priority to RU2006127021/11A priority patent/RU2384462C2/en
Priority to JP2006546190A priority patent/JP5021315B2/en
Priority to AT05700701T priority patent/ATE424346T1/en
Priority to CA002548369A priority patent/CA2548369A1/en
Priority to PCT/EP2005/000038 priority patent/WO2005068289A2/en
Publication of DE102004001078A1 publication Critical patent/DE102004001078A1/en
Application granted granted Critical
Publication of DE102004001078B4 publication Critical patent/DE102004001078B4/en
Publication of DE102004001078B8 publication Critical patent/DE102004001078B8/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • B64C1/12—Construction or attachment of skin panels
DE200410001078 2004-01-05 2004-01-05 fuselage Expired - Fee Related DE102004001078B8 (en)

Priority Applications (11)

Application Number Priority Date Filing Date Title
DE200410001078 DE102004001078B8 (en) 2004-01-05 2004-01-05 fuselage
AT05700701T ATE424346T1 (en) 2004-01-05 2005-01-05 AIRCRAFT FULL
EP05700701A EP1701881B1 (en) 2004-01-05 2005-01-05 Aircraft fuselage
CNB2005800019492A CN100418850C (en) 2004-01-05 2005-01-05 Aircraft fuselage
DE602005013059T DE602005013059D1 (en) 2004-01-05 2005-01-05 fuselage
RU2006127021/11A RU2384462C2 (en) 2004-01-05 2005-01-05 Hull
BRPI0506667-0A BRPI0506667A (en) 2004-01-05 2005-01-05 fuselage
US10/596,979 US20070023572A1 (en) 2004-01-05 2005-01-05 Fuselage
CA002548369A CA2548369A1 (en) 2004-01-05 2005-01-05 Fuselage
PCT/EP2005/000038 WO2005068289A2 (en) 2004-01-05 2005-01-05 Fuselage
JP2006546190A JP5021315B2 (en) 2004-01-05 2005-01-05 Aircraft fuselage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200410001078 DE102004001078B8 (en) 2004-01-05 2004-01-05 fuselage

Publications (3)

Publication Number Publication Date
DE102004001078A1 DE102004001078A1 (en) 2005-07-28
DE102004001078B4 DE102004001078B4 (en) 2013-02-14
DE102004001078B8 true DE102004001078B8 (en) 2013-06-13

Family

ID=34706778

Family Applications (1)

Application Number Title Priority Date Filing Date
DE200410001078 Expired - Fee Related DE102004001078B8 (en) 2004-01-05 2004-01-05 fuselage

Country Status (2)

Country Link
CN (1) CN100418850C (en)
DE (1) DE102004001078B8 (en)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005060958A1 (en) * 2005-12-20 2007-06-21 Airbus Deutschland Gmbh Aircraft structure protection, against damage from birds in flight, is an outer skin of glass fiber reinforced aluminum with a hollow zone to allow skin distortion through an impact
DE102007018753B4 (en) * 2007-04-20 2012-11-08 Airbus Operations Gmbh Fire protection room for aircraft passengers with the help of fuselage made of fiber-metal laminates
FR2921898B1 (en) * 2007-10-08 2009-12-11 Airbus France FUSELAGE STRUCTURE FOR AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL AND AIRCRAFT EQUIPPED WITH SUCH A FUSELAGE STRUCTURE
DE102008013365B4 (en) * 2008-03-10 2011-03-17 Airbus Operations Gmbh Transverse joint between two fuselage sections
ES2390318B1 (en) * 2009-03-10 2013-09-16 Airbus Operations, S.L. CLOSED STRUCTURE IN COMPOSITE MATERIAL.
DE102009015590A1 (en) * 2009-03-30 2010-10-07 Airbus Deutschland Gmbh Aircraft with an insulation system for heat and sound insulation
DE102010050740B4 (en) 2010-11-08 2012-12-06 Airbus Operations Gmbh Method and device for producing an aircraft structural component
DE102010053574B4 (en) 2010-12-06 2012-07-26 Airbus Operations Gmbh Method for repairing an aircraft structural component
DE102010053569B4 (en) 2010-12-06 2012-07-26 Airbus Operations Gmbh Method for repairing an aircraft structural component
DE102011101450B4 (en) 2011-05-13 2014-07-24 Airbus Operations Gmbh An aircraft subassembly and method for manufacturing an aircraft subassembly
DE102011101456A1 (en) 2011-05-13 2012-11-15 Airbus Operations Gmbh Connection device, assembly and method of manufacturing an assembly
EP2683043A1 (en) 2012-07-03 2014-01-08 Airbus Operations GmbH Cover sheath, fastening arrangement and method of fastening a conducting cable to a carrier component
DE102013008692A1 (en) 2013-05-22 2014-11-27 Airbus Operations Gmbh Method and device for deforming a component with a textile basic structure
EP2842711B1 (en) 2013-08-26 2018-10-10 Airbus Operations GmbH Apparatus and method for producing a composite material aircraft component
EP2871046A1 (en) 2013-11-06 2015-05-13 Airbus Operations GmbH Connecting port arrangement for use in an apparatus for producing a composite material component
DE102013226753A1 (en) 2013-12-19 2015-06-25 Airbus Operations Gmbh Apparatus and method for the continuous production of structural components made of fiber-reinforced composite materials and mold set
DE102013226730A1 (en) 2013-12-19 2015-07-09 Airbus Operations Gmbh Impregnating tool and method for continuously impregnating a reinforcing fiber material with a plastic material
DE102013226739A1 (en) 2013-12-19 2015-06-25 Airbus Operations Gmbh Forming tool, shaping device and method for deforming a semifinished fiber containing reinforcing fibers
DE102014215935A1 (en) 2014-08-12 2016-02-18 Airbus Operations Gmbh Apparatus and method for manufacturing components from a fiber reinforced composite material
DE102014221356B4 (en) 2014-10-21 2019-05-23 Airbus Operations Gmbh Assembly with individual components made of a fiber-reinforced composite material
EP3042747B1 (en) 2015-01-12 2018-03-14 Airbus Operations GmbH Forming apparatus and method for forming a semi-finished product comprising reinforcement fibres
DE102015211671A1 (en) 2015-06-24 2016-12-29 Airbus Operations Gmbh Method and device for producing a component using a vacuum film
DE102015211670A1 (en) 2015-06-24 2016-12-29 Airbus Operations Gmbh Method and device for mass production of components made of a fiber-reinforced composite material
EP3109152B1 (en) 2015-06-24 2019-08-07 Airbus Operations GmbH Stiffened fuselage component as well as method and apparatus for manufacturing a stiffened fuselage component
DE102016208232A1 (en) 2016-05-12 2017-11-16 Airbus Operations Gmbh Method and device for producing a semifinished product
US11248582B2 (en) * 2017-11-21 2022-02-15 General Electric Company Multiple material combinations for printed reinforcement structures of rotor blades

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3009183A1 (en) * 1979-07-19 1981-03-26 Société Européenne de Propulsion, Puteaux, Hauts-de-Seine THERMALLY INSULATING COMPOSITE MATERIAL BASED ON MINERAL FIBERS AND SYNTHETIC RESIN
DE3829712A1 (en) * 1988-09-01 1990-03-15 Basf Ag TEMPERATURE-RESISTANT THERMOPLASTIC MOLDS
EP0475677A1 (en) * 1990-09-08 1992-03-18 British Aerospace Public Limited Company Fire retarding means for aircraft
DE4420613C1 (en) * 1994-06-13 1995-08-10 Freudenberg Carl Fa Burn-through barrier for aircraft fuselages
WO2000032388A2 (en) * 1998-11-16 2000-06-08 Johns Manville International, Inc. Burn through resistant systems for transportation, especially aircraft
DE10010112A1 (en) * 2000-03-03 2001-09-06 Asglawo Gmbh Stoffe Zum Daemme Production of high temperature resistant thermal/acoustic insulating material for aircraft and space industry, comprises use of a powdered binding agent of silicon dioxide and a polymer resin

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1215912A (en) * 1958-11-22 1960-04-21 Bronzavia Sa Sheet material suitable for use as a protective shield against flame
US5154373A (en) * 1988-09-26 1992-10-13 Rockwell International Corporation Integral structure and thermal protection system
US5866272A (en) * 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
US6286785B1 (en) * 1999-03-11 2001-09-11 Nicholas Donald Kitchen Reinforcement system for aircraft fuselage frame and aluminum skin

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3009183A1 (en) * 1979-07-19 1981-03-26 Société Européenne de Propulsion, Puteaux, Hauts-de-Seine THERMALLY INSULATING COMPOSITE MATERIAL BASED ON MINERAL FIBERS AND SYNTHETIC RESIN
DE3829712A1 (en) * 1988-09-01 1990-03-15 Basf Ag TEMPERATURE-RESISTANT THERMOPLASTIC MOLDS
EP0475677A1 (en) * 1990-09-08 1992-03-18 British Aerospace Public Limited Company Fire retarding means for aircraft
DE4420613C1 (en) * 1994-06-13 1995-08-10 Freudenberg Carl Fa Burn-through barrier for aircraft fuselages
WO2000032388A2 (en) * 1998-11-16 2000-06-08 Johns Manville International, Inc. Burn through resistant systems for transportation, especially aircraft
US6322022B1 (en) * 1998-11-16 2001-11-27 Johns Manville International, Inc. Burn through resistant systems for transportation, especially aircraft
DE10010112A1 (en) * 2000-03-03 2001-09-06 Asglawo Gmbh Stoffe Zum Daemme Production of high temperature resistant thermal/acoustic insulating material for aircraft and space industry, comprises use of a powdered binding agent of silicon dioxide and a polymer resin

Also Published As

Publication number Publication date
DE102004001078A1 (en) 2005-07-28
CN1906084A (en) 2007-01-31
CN100418850C (en) 2008-09-17
DE102004001078B4 (en) 2013-02-14

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
8127 New person/name/address of the applicant

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE

R018 Grant decision by examination section/examining division
R020 Patent grant now final

Effective date: 20130515

R082 Change of representative

Representative=s name: KOPF WESTENBERGER WACHENHAUSEN PATENTANWAELTE , DE

Representative=s name: LKGLOBAL ] LORENZ & KOPF PARTG MBB PATENTANWAE, DE

R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee