FR1345076A - Improvement to thin-skinned structures reinforced by longitudinal and transverse elements - Google Patents

Improvement to thin-skinned structures reinforced by longitudinal and transverse elements

Info

Publication number
FR1345076A
FR1345076A FR913215A FR913215A FR1345076A FR 1345076 A FR1345076 A FR 1345076A FR 913215 A FR913215 A FR 913215A FR 913215 A FR913215 A FR 913215A FR 1345076 A FR1345076 A FR 1345076A
Authority
FR
France
Prior art keywords
improvement
thin
longitudinal
transverse elements
structures reinforced
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
Application number
FR913215A
Other languages
French (fr)
Inventor
Jean Arsene Alphonse Farines
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.)
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Original Assignee
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
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 Sud Aviation Societe Nationale de Constructions Aerdnaettiques filed Critical Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Priority to FR913215A priority Critical patent/FR1345076A/en
Application granted granted Critical
Publication of FR1345076A publication Critical patent/FR1345076A/en
Expired 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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR913215A 1962-10-24 1962-10-24 Improvement to thin-skinned structures reinforced by longitudinal and transverse elements Expired FR1345076A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR913215A FR1345076A (en) 1962-10-24 1962-10-24 Improvement to thin-skinned structures reinforced by longitudinal and transverse elements

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR913215A FR1345076A (en) 1962-10-24 1962-10-24 Improvement to thin-skinned structures reinforced by longitudinal and transverse elements

Publications (1)

Publication Number Publication Date
FR1345076A true FR1345076A (en) 1963-12-06

Family

ID=8789345

Family Applications (1)

Application Number Title Priority Date Filing Date
FR913215A Expired FR1345076A (en) 1962-10-24 1962-10-24 Improvement to thin-skinned structures reinforced by longitudinal and transverse elements

Country Status (1)

Country Link
FR (1) FR1345076A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0142697A1 (en) * 1983-11-17 1985-05-29 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Shaped-surface structural elements, especially for aircraft, and device for manufacturing them
WO2007141268A1 (en) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Aircraft fuselage structure and method for producing it
WO2012131137A3 (en) * 2011-03-30 2012-12-06 Airbus Operations, S.L. Aircraft fuselage with highly resistant frames
US8651421B2 (en) 2006-06-06 2014-02-18 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
US8695922B2 (en) 2006-06-06 2014-04-15 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
FR3009274A1 (en) * 2013-08-01 2015-02-06 Airbus Operations Sas AIRCRAFT FUSELAGE FRAME ELEMENT INTEGRATING TABS FOR ATTACHING STIFFENERS
US9527606B2 (en) 2013-08-01 2016-12-27 Airbus Operations (S.A.S.) Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element
US9789948B2 (en) 2013-08-01 2017-10-17 Airbus Operations (S.A.S.) Tool for simultaneously holding several attachment clips in contact with an aircraft fuselage frame element
FR3105165A1 (en) * 2019-12-19 2021-06-25 Airbus Operations Frame element for an aircraft fuselage provided with openings suitable for mounting by threading a stiffener.

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0142697A1 (en) * 1983-11-17 1985-05-29 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Shaped-surface structural elements, especially for aircraft, and device for manufacturing them
US8695922B2 (en) 2006-06-06 2014-04-15 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
WO2007141268A1 (en) * 2006-06-06 2007-12-13 Airbus Deutschland Gmbh Aircraft fuselage structure and method for producing it
JP2009539673A (en) * 2006-06-06 2009-11-19 エアバス ドイッチュラント ゲゼルシャフト ミット ベシュレンクテル ハフツング Aircraft fuselage structure and manufacturing method thereof
CN101448697B (en) * 2006-06-06 2016-04-27 空中客车德国运营有限责任公司 Aircraft fuselage structure and manufacture method thereof
US8534605B2 (en) 2006-06-06 2013-09-17 Airbus Operations Gmbh Aircraft fuselage structure and method for producing it
US8651421B2 (en) 2006-06-06 2014-02-18 Airbus Operations Gmbh Aircraft fuselage structure and method for its production
US8899522B2 (en) 2011-03-30 2014-12-02 Airbus Operations, S.L. Aircraft fuselage with high strength frames
ES2400771A1 (en) * 2011-03-30 2013-04-12 Airbus Operations S.L. Aircraft fuselage comprising highly resistant ring frames
WO2012131137A3 (en) * 2011-03-30 2012-12-06 Airbus Operations, S.L. Aircraft fuselage with highly resistant frames
FR3009274A1 (en) * 2013-08-01 2015-02-06 Airbus Operations Sas AIRCRAFT FUSELAGE FRAME ELEMENT INTEGRATING TABS FOR ATTACHING STIFFENERS
EP2832634A3 (en) * 2013-08-01 2015-05-20 Airbus Operations (Sas) Frame element of an aircraft fuselage including tabs for attaching stiffeners
US9527606B2 (en) 2013-08-01 2016-12-27 Airbus Operations (S.A.S.) Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element
US9745043B2 (en) 2013-08-01 2017-08-29 Airbus Operations (S.A.S.) Aircraft fuselage frame element integrating tabs for the fastening of stiffeners
US9789948B2 (en) 2013-08-01 2017-10-17 Airbus Operations (S.A.S.) Tool for simultaneously holding several attachment clips in contact with an aircraft fuselage frame element
FR3105165A1 (en) * 2019-12-19 2021-06-25 Airbus Operations Frame element for an aircraft fuselage provided with openings suitable for mounting by threading a stiffener.

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