FR1333200A - Improvements in the construction of aerodyne fuselages - Google Patents

Improvements in the construction of aerodyne fuselages

Info

Publication number
FR1333200A
FR1333200A FR900749A FR900749A FR1333200A FR 1333200 A FR1333200 A FR 1333200A FR 900749 A FR900749 A FR 900749A FR 900749 A FR900749 A FR 900749A FR 1333200 A FR1333200 A FR 1333200A
Authority
FR
France
Prior art keywords
aerodyne
fuselages
construction
aerodyne fuselages
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
FR900749A
Other languages
French (fr)
Inventor
Georges Ricard
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.)
Ateliers dAviation Louis Breguet SA
Original Assignee
Ateliers dAviation Louis Breguet SA
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 Ateliers dAviation Louis Breguet SA filed Critical Ateliers dAviation Louis Breguet SA
Priority to FR900749A priority Critical patent/FR1333200A/en
Priority to GB15161/63A priority patent/GB958883A/en
Application granted granted Critical
Publication of FR1333200A publication Critical patent/FR1333200A/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
    • B64C1/061—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
    • B64C1/068—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
    • 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)
  • Body Structure For Vehicles (AREA)
  • Laminated Bodies (AREA)
FR900749A 1962-06-14 1962-06-14 Improvements in the construction of aerodyne fuselages Expired FR1333200A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR900749A FR1333200A (en) 1962-06-14 1962-06-14 Improvements in the construction of aerodyne fuselages
GB15161/63A GB958883A (en) 1962-06-14 1963-04-17 Improvements in the construction of aircraft fuselages

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR900749A FR1333200A (en) 1962-06-14 1962-06-14 Improvements in the construction of aerodyne fuselages

Publications (1)

Publication Number Publication Date
FR1333200A true FR1333200A (en) 1963-07-26

Family

ID=8781029

Family Applications (1)

Application Number Title Priority Date Filing Date
FR900749A Expired FR1333200A (en) 1962-06-14 1962-06-14 Improvements in the construction of aerodyne fuselages

Country Status (2)

Country Link
FR (1) FR1333200A (en)
GB (1) GB958883A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006026170B4 (en) 2006-06-06 2012-06-21 Airbus Operations Gmbh Aircraft fuselage structure and method for its manufacture
DE102006026168A1 (en) * 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Aircraft fuselage structure and method for its manufacture
DE102006026169B4 (en) 2006-06-06 2012-06-21 Airbus Operations Gmbh Aircraft fuselage structure and method for its manufacture
FR2906785B1 (en) * 2006-10-10 2009-12-04 Airbus France AIRCRAFT FUSELAGE MADE FROM LONGITUDINAL PANELS AND METHOD FOR PRODUCING SUCH A FUSELAGE

Also Published As

Publication number Publication date
GB958883A (en) 1964-05-27

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