FR916967A - Device for connecting a sealed shell and components carried externally by the latter, in particular in an airplane - Google Patents
Device for connecting a sealed shell and components carried externally by the latter, in particular in an airplaneInfo
- Publication number
- FR916967A FR916967A FR916967DA FR916967A FR 916967 A FR916967 A FR 916967A FR 916967D A FR916967D A FR 916967DA FR 916967 A FR916967 A FR 916967A
- Authority
- FR
- France
- Prior art keywords
- airplane
- sealed shell
- components carried
- carried externally
- externally
- 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
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR916967T | 1945-07-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR916967A true FR916967A (en) | 1946-12-20 |
Family
ID=9423572
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR916967D Expired FR916967A (en) | 1945-07-03 | 1945-07-03 | Device for connecting a sealed shell and components carried externally by the latter, in particular in an airplane |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR916967A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2226510A1 (en) * | 2001-10-24 | 2005-03-16 | Gamesa Desarrollos Aeronauticos, S.A. | Method for bonding rear fuselage and vertical stabilizer, has connecting fasteners to longitudinal vertical stabilizer and joint surfaces of rear fuselage, where holes are formed on surfaces of rear fuselage |
EP2810869A1 (en) * | 2013-06-07 | 2014-12-10 | The Boeing Company | Lower joints between outboard wing boxes and center wing sections of aircraft wing assemblies |
US9475570B2 (en) | 2013-08-23 | 2016-10-25 | The Boeing Company | Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies |
-
1945
- 1945-07-03 FR FR916967D patent/FR916967A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2226510A1 (en) * | 2001-10-24 | 2005-03-16 | Gamesa Desarrollos Aeronauticos, S.A. | Method for bonding rear fuselage and vertical stabilizer, has connecting fasteners to longitudinal vertical stabilizer and joint surfaces of rear fuselage, where holes are formed on surfaces of rear fuselage |
EP2810869A1 (en) * | 2013-06-07 | 2014-12-10 | The Boeing Company | Lower joints between outboard wing boxes and center wing sections of aircraft wing assemblies |
US9227718B2 (en) | 2013-06-07 | 2016-01-05 | The Boeing Company | Lower joints between outboard wing boxes and center wing sections of aircraft wing assemblies |
US9475570B2 (en) | 2013-08-23 | 2016-10-25 | The Boeing Company | Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies |
US9731808B2 (en) | 2013-08-23 | 2017-08-15 | The Boeing Company | Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies |
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