FR3000018B1 - Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur - Google Patents

Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur

Info

Publication number
FR3000018B1
FR3000018B1 FR1262649A FR1262649A FR3000018B1 FR 3000018 B1 FR3000018 B1 FR 3000018B1 FR 1262649 A FR1262649 A FR 1262649A FR 1262649 A FR1262649 A FR 1262649A FR 3000018 B1 FR3000018 B1 FR 3000018B1
Authority
FR
France
Prior art keywords
stiffener
aircraft fuselage
manufacturing
aircraft
fuselage equipped
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
FR1262649A
Other languages
English (en)
Other versions
FR3000018A1 (fr
Inventor
Christophe Mialhe
Romain Delahaye
Philippe Rodrigo
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 SAS
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
Priority to FR1262649A priority Critical patent/FR3000018B1/fr
Priority to US14/652,118 priority patent/US9708050B2/en
Priority to PCT/FR2013/053232 priority patent/WO2014096741A1/fr
Priority to CN201380066896.7A priority patent/CN105073577B/zh
Publication of FR3000018A1 publication Critical patent/FR3000018A1/fr
Application granted granted Critical
Publication of FR3000018B1 publication Critical patent/FR3000018B1/fr
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
    • 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
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D5/00—Bending sheet metal along straight lines, e.g. to form simple curves
    • B21D5/16—Folding; Pleating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00—Making other particular articles
    • B21D53/92—Making other particular articles other parts for aircraft
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Connection Of Plates (AREA)
  • Body Structure For Vehicles (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
FR1262649A 2012-12-21 2012-12-21 Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur Expired - Fee Related FR3000018B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1262649A FR3000018B1 (fr) 2012-12-21 2012-12-21 Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur
US14/652,118 US9708050B2 (en) 2012-12-21 2013-12-20 Stiffener for an aircraft fuselage, method for manufacturing same, and aircraft fuselage equipped with such a stiffener
PCT/FR2013/053232 WO2014096741A1 (fr) 2012-12-21 2013-12-20 Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur
CN201380066896.7A CN105073577B (zh) 2012-12-21 2013-12-20 用于飞行器机身的加强件、用于制造飞行器机身的加强件的方法以及装有这种加强件的飞行器机身

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1262649A FR3000018B1 (fr) 2012-12-21 2012-12-21 Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur

Publications (2)

Publication Number Publication Date
FR3000018A1 FR3000018A1 (fr) 2014-06-27
FR3000018B1 true FR3000018B1 (fr) 2016-12-09

Family

ID=48289243

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1262649A Expired - Fee Related FR3000018B1 (fr) 2012-12-21 2012-12-21 Raidisseur de fuselage d'aeronef, son procede de fabrication, et fuselage d'aeronef equipe d'un tel raidisseur

Country Status (4)

Country Link
US (1) US9708050B2 (fr)
CN (1) CN105073577B (fr)
FR (1) FR3000018B1 (fr)
WO (1) WO2014096741A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD777014S1 (en) * 2014-08-12 2017-01-24 Servi-Sure, LLC Integrated stiffener
GB2571911A (en) * 2017-12-21 2019-09-18 Airbus Operations Gmbh A Stiffener for an Aircraft Assembly

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR531501A (fr) * 1916-08-31 1922-01-16 Zeppelin Werk Lindau G M B H élément portant de construction
US1357073A (en) * 1920-01-09 1920-10-26 Mooney Dermot Joseph Metal construction
US3698224A (en) * 1970-11-16 1972-10-17 Siderurgica Occidental C A Process for the production of steel structural shapes
US4635882A (en) * 1980-11-14 1987-01-13 The Boeing Company Method and apparatus for reducing low to mid frequency interior noise
DE3401189A1 (de) * 1983-01-25 1984-07-26 Westland PLC, Yeovil, Somerset Verbund-hubschrauberrumpf
US5307601A (en) * 1992-02-06 1994-05-03 Mccracken Robert G Beam member for use in concrete forming apparatus
US6458309B1 (en) * 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
JP4526698B2 (ja) * 2000-12-22 2010-08-18 富士重工業株式会社 複合材成形品及びその製造方法
US9359061B2 (en) * 2005-10-31 2016-06-07 The Boeing Company Compliant stiffener for aircraft fuselage
GB0611875D0 (en) * 2006-06-15 2006-07-26 Airbus Uk Ltd A stringer for an aircraft wing and a method of forming thereof
GB2441753B (en) * 2006-09-12 2009-02-11 Gkn Aerospace Services Ltd Rib post
NL2000232C2 (nl) * 2006-09-12 2008-03-13 Gtm Consulting B V Huidpaneel voor een vliegtuigromp.
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
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
ES2352941B1 (es) * 2008-05-16 2012-01-25 Airbus Operations, S.L. Estructura integrada de aeronave en material compuesto
US8074694B2 (en) * 2009-05-28 2011-12-13 The Boeing Company Stringer transition method
ES2382765B1 (es) * 2009-06-29 2013-05-03 Airbus Operations, S.L. Diseño de cuadernas de aeronave
EP2404824B1 (fr) * 2010-07-08 2015-09-09 Airbus Opérations SAS Structure d'aeronef et Procédé de réalisation d'une telle structure

Also Published As

Publication number Publication date
WO2014096741A1 (fr) 2014-06-26
FR3000018A1 (fr) 2014-06-27
CN105073577B (zh) 2017-12-26
US20150321742A1 (en) 2015-11-12
US9708050B2 (en) 2017-07-18
CN105073577A (zh) 2015-11-18

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