DE102004058013B8 - Method for producing a structural structure with an integral profile-like stiffening element for an aircraft - Google Patents

Method for producing a structural structure with an integral profile-like stiffening element for an aircraft Download PDF

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Publication number
DE102004058013B8
DE102004058013B8 DE200410058013 DE102004058013A DE102004058013B8 DE 102004058013 B8 DE102004058013 B8 DE 102004058013B8 DE 200410058013 DE200410058013 DE 200410058013 DE 102004058013 A DE102004058013 A DE 102004058013A DE 102004058013 B8 DE102004058013 B8 DE 102004058013B8
Authority
DE
Germany
Prior art keywords
aircraft
producing
stiffening element
structural structure
integral profile
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
DE200410058013
Other languages
German (de)
Other versions
DE102004058013B3 (en
Inventor
Eckart Frankenberger
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
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Priority to DE200410058013 priority Critical patent/DE102004058013B8/en
Publication of DE102004058013B3 publication Critical patent/DE102004058013B3/en
Application granted granted Critical
Publication of DE102004058013B8 publication Critical patent/DE102004058013B8/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P13/00—Making metal objects by operations essentially involving machining but not covered by a single other subclass
    • B23P13/02—Making metal objects by operations essentially involving machining but not covered by a single other subclass in which only the machining operations are important
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—Stringers, longerons

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
DE200410058013 2004-12-01 2004-12-01 Method for producing a structural structure with an integral profile-like stiffening element for an aircraft Expired - Fee Related DE102004058013B8 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE200410058013 DE102004058013B8 (en) 2004-12-01 2004-12-01 Method for producing a structural structure with an integral profile-like stiffening element for an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200410058013 DE102004058013B8 (en) 2004-12-01 2004-12-01 Method for producing a structural structure with an integral profile-like stiffening element for an aircraft

Publications (2)

Publication Number Publication Date
DE102004058013B3 DE102004058013B3 (en) 2006-07-27
DE102004058013B8 true DE102004058013B8 (en) 2006-11-09

Family

ID=36650803

Family Applications (1)

Application Number Title Priority Date Filing Date
DE200410058013 Expired - Fee Related DE102004058013B8 (en) 2004-12-01 2004-12-01 Method for producing a structural structure with an integral profile-like stiffening element for an aircraft

Country Status (1)

Country Link
DE (1) DE102004058013B8 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9862478B2 (en) 2012-11-21 2018-01-09 Airbus Operations Limited Modular structural assembly

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7997529B2 (en) * 2006-01-19 2011-08-16 The Boeing Company Compliant panel for aircraft
US7766277B2 (en) * 2006-01-19 2010-08-03 The Boeing Company Deformable forward pressure bulkhead for an aircraft
FR2956597B1 (en) * 2010-02-23 2012-03-16 Airbus Operations Sas PROCESS FOR PRODUCING A REINFORCED CURVED METAL STRUCTURE AND CORRESPONDING STRUCTURE
DE202021106391U1 (en) * 2021-11-23 2021-11-29 Pilatus Flugzeugwerke Ag Aircraft component and aircraft

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19639667C1 (en) * 1996-09-27 1998-03-12 Daimler Benz Aerospace Airbus Process for welding profiles on large-format aluminum structural components using laser beams
DE19844035C1 (en) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Shell component for an aircraft, and method for its production
DE19960909A1 (en) * 1999-09-03 2001-06-21 Eads Airbus Gmbh Large-area structural component for an aircraft and method for producing the structural component
DE10007995C2 (en) * 2000-02-22 2002-03-07 Airbus Gmbh Structural component, in particular for an aircraft and method for producing a structural component

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19639667C1 (en) * 1996-09-27 1998-03-12 Daimler Benz Aerospace Airbus Process for welding profiles on large-format aluminum structural components using laser beams
DE19844035C1 (en) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Shell component for an aircraft, and method for its production
DE19960909A1 (en) * 1999-09-03 2001-06-21 Eads Airbus Gmbh Large-area structural component for an aircraft and method for producing the structural component
DE10007995C2 (en) * 2000-02-22 2002-03-07 Airbus Gmbh Structural component, in particular for an aircraft and method for producing a structural component

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
GROCHE, P. u.a.: Steifigkeitsoptimierter Leichtbau durch neue Umformverfahren für Blech, In: SIEGERT, K. - Neuere Entwicklungen in der Blechumformung - Frankfurt, MAT INFO Werkstoff - Informations- gesellschaft 05/2004, S. 201-222
GROCHE, P. u.a.: Steifigkeitsoptimierter Leichtbaudurch neue Umformverfahren für Blech, In: SIEGERT,K. - Neuere Entwicklungen in der Blechumformung - Frankfurt, MAT INFO Werkstoff - Informations- gesellschaft 05/2004, S. 201-222 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9862478B2 (en) 2012-11-21 2018-01-09 Airbus Operations Limited Modular structural assembly

Also Published As

Publication number Publication date
DE102004058013B3 (en) 2006-07-27

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Legal Events

Date Code Title Description
8100 Publication of the examined application without publication of unexamined application
8396 Reprint of erroneous front page
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE

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