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FR531501A - load-bearing construction element - Google Patents

load-bearing construction element

Info

Publication number
FR531501A
FR531501A FR531501DA FR531501A FR 531501 A FR531501 A FR 531501A FR 531501D A FR531501D A FR 531501DA FR 531501 A FR531501 A FR 531501A
Authority
FR
France
Prior art keywords
load
construction element
bearing construction
bearing
construction
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)
Inventor
Claudius Dornier
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.)
Zeppelin GmbH
Original Assignee
Zeppelinwerke GmbH
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 Zeppelinwerke GmbH filed Critical Zeppelinwerke GmbH
Application granted granted Critical
Publication of FR531501A publication Critical patent/FR531501A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR531501D 1916-08-31 1921-02-28 load-bearing construction element Expired FR531501A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE531501X 1916-08-31

Publications (1)

Publication Number Publication Date
FR531501A true FR531501A (en) 1922-01-16

Family

ID=6555005

Family Applications (1)

Application Number Title Priority Date Filing Date
FR531501D Expired FR531501A (en) 1916-08-31 1921-02-28 load-bearing construction element

Country Status (1)

Country Link
FR (1) FR531501A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3000018A1 (en) * 2012-12-21 2014-06-27 Airbus Operations Sas AIRCRAFT FUSELAGE STIFFENER, ITS MANUFACTURING METHOD, AND AIRCRAFT FUSELAGE EQUIPPED WITH SUCH STIFFENER

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3000018A1 (en) * 2012-12-21 2014-06-27 Airbus Operations Sas AIRCRAFT FUSELAGE STIFFENER, ITS MANUFACTURING METHOD, AND AIRCRAFT FUSELAGE EQUIPPED WITH SUCH STIFFENER
US9708050B2 (en) 2012-12-21 2017-07-18 Airbus Operations Sas Stiffener for an aircraft fuselage, method for manufacturing same, and aircraft fuselage equipped with such a stiffener

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