FR2979896A1 - Element de cadre de fuselage d'aeronef - Google Patents

Element de cadre de fuselage d'aeronef Download PDF

Info

Publication number
FR2979896A1
FR2979896A1 FR1157971A FR1157971A FR2979896A1 FR 2979896 A1 FR2979896 A1 FR 2979896A1 FR 1157971 A FR1157971 A FR 1157971A FR 1157971 A FR1157971 A FR 1157971A FR 2979896 A1 FR2979896 A1 FR 2979896A1
Authority
FR
France
Prior art keywords
frame
aircraft fuselage
aircraft
cross
fuselage frame
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.)
Withdrawn
Application number
FR1157971A
Other languages
English (en)
French (fr)
Inventor
Christophe Mialhe
Patrick Lieven
Romain Delahaye
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 FR1157971A priority Critical patent/FR2979896A1/fr
Priority to ES12182730.7T priority patent/ES2473319T3/es
Priority to EP12182730.7A priority patent/EP2567890B1/fr
Priority to JP2012193366A priority patent/JP6054105B2/ja
Priority to CA2789142A priority patent/CA2789142C/fr
Priority to US13/607,096 priority patent/US8894010B2/en
Priority to CN201210460212.9A priority patent/CN102991665B/zh
Publication of FR2979896A1 publication Critical patent/FR2979896A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/10Bulkheads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/18Floors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Connection Of Plates (AREA)
FR1157971A 2011-09-08 2011-09-08 Element de cadre de fuselage d'aeronef Withdrawn FR2979896A1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR1157971A FR2979896A1 (fr) 2011-09-08 2011-09-08 Element de cadre de fuselage d'aeronef
ES12182730.7T ES2473319T3 (es) 2011-09-08 2012-09-03 Marco de fuselaje de aeronave
EP12182730.7A EP2567890B1 (fr) 2011-09-08 2012-09-03 Cadre de fuselage d'aéronef
JP2012193366A JP6054105B2 (ja) 2011-09-08 2012-09-03 航空機胴体のフレーム要素
CA2789142A CA2789142C (fr) 2011-09-08 2012-09-05 Element de cadre de fuselage d'aeronef
US13/607,096 US8894010B2 (en) 2011-09-08 2012-09-07 Aircraft fuselage frame element
CN201210460212.9A CN102991665B (zh) 2011-09-08 2012-09-07 飞行器机身框架件

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1157971A FR2979896A1 (fr) 2011-09-08 2011-09-08 Element de cadre de fuselage d'aeronef

Publications (1)

Publication Number Publication Date
FR2979896A1 true FR2979896A1 (fr) 2013-03-15

Family

ID=46750246

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1157971A Withdrawn FR2979896A1 (fr) 2011-09-08 2011-09-08 Element de cadre de fuselage d'aeronef

Country Status (7)

Country Link
US (1) US8894010B2 (enExample)
EP (1) EP2567890B1 (enExample)
JP (1) JP6054105B2 (enExample)
CN (1) CN102991665B (enExample)
CA (1) CA2789142C (enExample)
ES (1) ES2473319T3 (enExample)
FR (1) FR2979896A1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9505354B2 (en) * 2013-09-16 2016-11-29 The Boeing Company Carbon fiber reinforced polymer cargo beam with integrated cargo stanchions and c-splices
EP2889212B1 (en) * 2013-12-30 2016-01-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Subfloor structure with an integral hull for a rotary wing aircraft
US10625844B2 (en) * 2014-11-10 2020-04-21 The Boeing Company Fuselage with structural and non-structural stanchions
US10173765B2 (en) * 2016-04-07 2019-01-08 The Boeing Company Pressure bulkhead apparatus
ES1235737Y (es) * 2019-07-24 2020-01-02 Citd Engineering & Tech Sl Mamparo de presion
CN110498034B (zh) * 2019-08-26 2022-07-15 中国航空工业集团公司沈阳飞机设计研究所 一种开口处应力集中减缓结构
EP4420974A1 (de) * 2023-02-27 2024-08-28 Airbus Operations GmbH Verfahren zur herstellung eines rumpfstrukturbauteils für einen dreiecksbereich und einstückiges rumpfstrukturbauteil

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2877916A1 (fr) * 2004-11-15 2006-05-19 Airbus France Sas Cadre de structure de fuselage d'aeronef
DE102007030026A1 (de) * 2007-06-29 2009-01-02 Airbus Deutschland Gmbh Strukturbauteil mit Spant- und Querträgerelement
US20090321569A1 (en) * 2006-06-06 2009-12-31 Thorsten Schroeer Aircraft fuselage structure and method for its production

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2003433A (en) * 1932-07-01 1935-06-04 James B Ford Aircraft body
US3155348A (en) * 1962-06-14 1964-11-03 Aviation Louis Breguet Sa Aircraft fuselage
DE3141869C2 (de) * 1981-10-22 1984-02-02 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Fußbodenkonstruktion für den oberen Laderaum eines Luftfahrzeuges
ZA847393B (en) * 1983-09-21 1985-05-29 Tri Wall Pty Ltd Aircraft loading method and apparatus
US4648570A (en) * 1984-08-22 1987-03-10 The Boeing Company Method and apparatus for supporting interior aircraft elements
DE10145276B4 (de) * 2001-09-14 2008-04-10 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugzeug, insbesondere Passagierflugzeug, mit einem Rumpf, der eine tragende Primärstruktur und einen Frachtraum umfasst
JP2005171552A (ja) * 2003-12-09 2005-06-30 Grand Form:Kk 木造建築物の剛接合構造
FR2868039B1 (fr) * 2004-03-25 2007-06-08 Airbus France Sas Dispositif de renfort de structure creuse notamment de structure en caisson pour aeronef et structure creuse equipee d'un tel dispositif
US7455263B2 (en) * 2005-04-22 2008-11-25 The Boeing Company Airplane interior systems
US7861970B2 (en) * 2006-11-02 2011-01-04 The Boeing Company Fuselage structure including an integrated fuselage stanchion
DE102007011611B4 (de) * 2007-01-22 2010-12-09 Airbus Deutschland Gmbh Befestigungsanordnung für Verzurrbügel in einem Frachtraumboden eines Flugzeugs
US7721992B2 (en) * 2007-03-07 2010-05-25 The Boeing Company Aircraft floor to fuselage attachment
DE102008042036A1 (de) * 2008-09-12 2010-03-25 Airbus Deutschland Gmbh Stange zur Abstützung von Bauteilen innerhalb einer Rumpfzellenstruktur eines Flugzeugs
DE102009012426A1 (de) * 2009-03-10 2010-09-16 Telair International Gmbh Rollenbahn
FR2947525B1 (fr) * 2009-07-02 2011-09-02 Airbus Operations Sas Plancher d'aeronef a encombrement optimise
FR2947524B1 (fr) * 2009-07-02 2011-12-30 Airbus Operations Sas Procede de fabrication d'un aeronef comprenant un plancher
FR2954430B1 (fr) * 2009-12-18 2013-11-29 Eads Europ Aeronautic Defence Element structural d'absorption d'energie en materiau composite
DE102010014638B4 (de) * 2010-04-12 2019-08-01 Airbus Defence and Space GmbH Luftfahrzeug mit einer integrierten energieaufnehmenden Verformungsstruktur und Luftfahrzeug mit einem derartigen Rumpf
CN102139757A (zh) * 2010-07-28 2011-08-03 北京航空航天大学 一种适用于无人机和模型飞机的构架式前中机身

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2877916A1 (fr) * 2004-11-15 2006-05-19 Airbus France Sas Cadre de structure de fuselage d'aeronef
US20090321569A1 (en) * 2006-06-06 2009-12-31 Thorsten Schroeer Aircraft fuselage structure and method for its production
DE102007030026A1 (de) * 2007-06-29 2009-01-02 Airbus Deutschland Gmbh Strukturbauteil mit Spant- und Querträgerelement

Also Published As

Publication number Publication date
EP2567890B1 (fr) 2014-04-02
CA2789142C (fr) 2017-10-24
US20130306795A1 (en) 2013-11-21
CN102991665A (zh) 2013-03-27
CA2789142A1 (fr) 2013-03-08
EP2567890A1 (fr) 2013-03-13
JP6054105B2 (ja) 2016-12-27
JP2013056662A (ja) 2013-03-28
CN102991665B (zh) 2017-04-12
US8894010B2 (en) 2014-11-25
ES2473319T3 (es) 2014-07-04

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Effective date: 20150529