FR531501A - load-bearing construction element - Google Patents
load-bearing construction elementInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
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)
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 |
-
1921
- 1921-02-28 FR FR531501D patent/FR531501A/en not_active Expired
Cited By (2)
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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