FR1150797A - Improvements to structural elements of aircraft - Google Patents

Improvements to structural elements of aircraft

Info

Publication number
FR1150797A
FR1150797A FR1150797DA FR1150797A FR 1150797 A FR1150797 A FR 1150797A FR 1150797D A FR1150797D A FR 1150797DA FR 1150797 A FR1150797 A FR 1150797A
Authority
FR
France
Prior art keywords
aircraft
structural elements
structural
elements
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
Other languages
French (fr)
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.)
Columbia Products Co
Original Assignee
Columbia Products Co
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 Columbia Products Co filed Critical Columbia Products Co
Application granted granted Critical
Publication of FR1150797A publication Critical patent/FR1150797A/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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR1150797D 1956-04-16 1956-04-16 Improvements to structural elements of aircraft Expired FR1150797A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1150797T 1956-04-16

Publications (1)

Publication Number Publication Date
FR1150797A true FR1150797A (en) 1958-01-17

Family

ID=9647546

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1150797D Expired FR1150797A (en) 1956-04-16 1956-04-16 Improvements to structural elements of aircraft

Country Status (1)

Country Link
FR (1) FR1150797A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463055A1 (en) * 1979-08-09 1981-02-20 Alkan R & Cie STRUCTURE OF MATS FOR ATTACHING LOADS UNDER AIRPLANE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463055A1 (en) * 1979-08-09 1981-02-20 Alkan R & Cie STRUCTURE OF MATS FOR ATTACHING LOADS UNDER AIRPLANE

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