FR2906785B1 - Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage - Google Patents

Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage

Info

Publication number
FR2906785B1
FR2906785B1 FR0654185A FR0654185A FR2906785B1 FR 2906785 B1 FR2906785 B1 FR 2906785B1 FR 0654185 A FR0654185 A FR 0654185A FR 0654185 A FR0654185 A FR 0654185A FR 2906785 B1 FR2906785 B1 FR 2906785B1
Authority
FR
France
Prior art keywords
fuselage
producing
longitudinal panels
aircraft
aircraft 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
FR0654185A
Other languages
English (en)
Other versions
FR2906785A1 (fr
Inventor
Guillaume Gallant
Philippe Bernadet
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
Priority to FR0654185A priority Critical patent/FR2906785B1/fr
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to EP07858512A priority patent/EP2076430A2/fr
Priority to CA002663415A priority patent/CA2663415A1/fr
Priority to JP2009531882A priority patent/JP2010505700A/ja
Priority to US12/444,972 priority patent/US20100032523A1/en
Priority to CN2007800347068A priority patent/CN101516723B/zh
Priority to RU2009117613/11A priority patent/RU2489312C2/ru
Priority to BRPI0717735-6A2A priority patent/BRPI0717735A2/pt
Priority to PCT/FR2007/052081 priority patent/WO2008043940A2/fr
Publication of FR2906785A1 publication Critical patent/FR2906785A1/fr
Application granted granted Critical
Publication of FR2906785B1 publication Critical patent/FR2906785B1/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
    • B64C1/068—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
    • B64C1/068—Fuselage sections
    • B64C1/0683—Nose cones
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2211/00—Modular constructions of airplanes or helicopters
FR0654185A 2006-10-10 2006-10-10 Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage Expired - Fee Related FR2906785B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0654185A FR2906785B1 (fr) 2006-10-10 2006-10-10 Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage
CA002663415A CA2663415A1 (fr) 2006-10-10 2007-10-04 Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage
JP2009531882A JP2010505700A (ja) 2006-10-10 2007-10-04 長手方向パネルから製作される航空機の胴体およびそのような胴体の製造方法
US12/444,972 US20100032523A1 (en) 2006-10-10 2007-10-04 Aircraft fuselage made from longitudinal panels and method of producing such a fuselage
EP07858512A EP2076430A2 (fr) 2006-10-10 2007-10-04 Fuselage d'aéronef réalisé a partir de panneaux longitudinaux et procédé de réalisation d'un tel fuselage
CN2007800347068A CN101516723B (zh) 2006-10-10 2007-10-04 基于纵向壁板实现的飞行器机身和实现该机身的方法
RU2009117613/11A RU2489312C2 (ru) 2006-10-10 2007-10-04 Фюзеляж летательного аппарата, выполненный из продольных панелей, и способ выполнения такого фюзеляжа
BRPI0717735-6A2A BRPI0717735A2 (pt) 2006-10-10 2007-10-04 Fuselagem de aeronave a partir de painéis longitudinais e processo de realização dessa fuselagem
PCT/FR2007/052081 WO2008043940A2 (fr) 2006-10-10 2007-10-04 Fuselage d'aéronef réalisé a partir de panneaux longitudinaux et procédé de réalisation d'un tel fuselage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0654185A FR2906785B1 (fr) 2006-10-10 2006-10-10 Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage

Publications (2)

Publication Number Publication Date
FR2906785A1 FR2906785A1 (fr) 2008-04-11
FR2906785B1 true FR2906785B1 (fr) 2009-12-04

Family

ID=38015384

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0654185A Expired - Fee Related FR2906785B1 (fr) 2006-10-10 2006-10-10 Fuselage d'aeronef realise a partir de panneaux longitudinaux et procede de realisation d'un tel fuselage

Country Status (9)

Country Link
US (1) US20100032523A1 (fr)
EP (1) EP2076430A2 (fr)
JP (1) JP2010505700A (fr)
CN (1) CN101516723B (fr)
BR (1) BRPI0717735A2 (fr)
CA (1) CA2663415A1 (fr)
FR (1) FR2906785B1 (fr)
RU (1) RU2489312C2 (fr)
WO (1) WO2008043940A2 (fr)

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US8752293B2 (en) * 2007-12-07 2014-06-17 The Boeing Company Method of fabricating structures using composite modules and structures made thereby
DE102008010197B4 (de) * 2008-02-20 2012-03-22 Airbus Operations Gmbh Verfahren zum Verbinden von zwei Rumpfsektionen unter Schaffung eines Querstoßes sowie Querstoßverbindung
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US9108718B2 (en) * 2009-10-08 2015-08-18 Mitsubishi Heavy Industries, Ltd. Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
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CN102126549A (zh) * 2010-01-20 2011-07-20 苏章仁 圆形截面飞行载体壳体顺航向非对称分离仿生结构
RU2553608C2 (ru) * 2011-02-04 2015-06-20 Мицубиси Хеви Индастрис, Лтд. Конструкция из композитного материала и оснащенные ей крыло и фюзеляж летательного аппарата
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Also Published As

Publication number Publication date
WO2008043940A3 (fr) 2008-06-12
CN101516723A (zh) 2009-08-26
JP2010505700A (ja) 2010-02-25
CN101516723B (zh) 2013-06-05
FR2906785A1 (fr) 2008-04-11
WO2008043940A2 (fr) 2008-04-17
RU2009117613A (ru) 2010-11-20
EP2076430A2 (fr) 2009-07-08
US20100032523A1 (en) 2010-02-11
BRPI0717735A2 (pt) 2013-10-22
RU2489312C2 (ru) 2013-08-10
CA2663415A1 (fr) 2008-04-17

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