FR1462186A - Device for assembling parts subjected to stress - Google Patents

Device for assembling parts subjected to stress

Info

Publication number
FR1462186A
FR1462186A FR998763A FR998763A FR1462186A FR 1462186 A FR1462186 A FR 1462186A FR 998763 A FR998763 A FR 998763A FR 998763 A FR998763 A FR 998763A FR 1462186 A FR1462186 A FR 1462186A
Authority
FR
France
Prior art keywords
stress
assembling parts
parts subjected
subjected
assembling
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
FR998763A
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.)
CIE GENERALE D AERONAUTIQUE
Original Assignee
CIE GENERALE D AERONAUTIQUE
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 CIE GENERALE D AERONAUTIQUE filed Critical CIE GENERALE D AERONAUTIQUE
Priority to FR998763A priority Critical patent/FR1462186A/en
Application granted granted Critical
Publication of FR1462186A publication Critical patent/FR1462186A/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
    • 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)
FR998763A 1964-12-16 1964-12-16 Device for assembling parts subjected to stress Expired FR1462186A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR998763A FR1462186A (en) 1964-12-16 1964-12-16 Device for assembling parts subjected to stress

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR998763A FR1462186A (en) 1964-12-16 1964-12-16 Device for assembling parts subjected to stress

Publications (1)

Publication Number Publication Date
FR1462186A true FR1462186A (en) 1966-04-15

Family

ID=8844869

Family Applications (1)

Application Number Title Priority Date Filing Date
FR998763A Expired FR1462186A (en) 1964-12-16 1964-12-16 Device for assembling parts subjected to stress

Country Status (1)

Country Link
FR (1) FR1462186A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4830096A (en) * 1986-06-11 1989-05-16 Sundstrand Corporation Removable thermal control system
EP0637541A1 (en) * 1993-08-04 1995-02-08 Johannes Katz Decomposable wing and manufacturing system of a connecting element for thin walled shaped piece, in particular for the segments of such decomposable wing
WO2009056319A1 (en) * 2007-10-31 2009-05-07 Airbus Deutschland Gmbh Transversal butt strap and method for connecting two especially wound cfk fuselage sections in order to create a fuselage cell

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4830096A (en) * 1986-06-11 1989-05-16 Sundstrand Corporation Removable thermal control system
EP0637541A1 (en) * 1993-08-04 1995-02-08 Johannes Katz Decomposable wing and manufacturing system of a connecting element for thin walled shaped piece, in particular for the segments of such decomposable wing
WO2009056319A1 (en) * 2007-10-31 2009-05-07 Airbus Deutschland Gmbh Transversal butt strap and method for connecting two especially wound cfk fuselage sections in order to create a fuselage cell
US8783610B2 (en) 2007-10-31 2014-07-22 Airbus Operations Gmbh Transverse splicing plate for creating a fuselage, and a method for connecting two, in particular wound, CFP fuselage sections

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