FR543443A - Method of assembling the spars in the airplanes - Google Patents
Method of assembling the spars in the airplanesInfo
- Publication number
- FR543443A FR543443A FR543443DA FR543443A FR 543443 A FR543443 A FR 543443A FR 543443D A FR543443D A FR 543443DA FR 543443 A FR543443 A FR 543443A
- Authority
- FR
- France
- Prior art keywords
- spars
- airplanes
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/185—Spars
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR543443T | 1921-11-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR543443A true FR543443A (en) | 1922-09-02 |
Family
ID=8931609
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR543443D Expired FR543443A (en) | 1921-11-10 | 1921-11-10 | Method of assembling the spars in the airplanes |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR543443A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007020049A1 (en) * | 2005-08-17 | 2007-02-22 | Airbus Deutschland Gmbh | Continuous fuselage connection |
EP3998192A1 (en) * | 2021-02-19 | 2022-05-18 | Lilium eAircraft GmbH | Wing spar structure |
-
1921
- 1921-11-10 FR FR543443D patent/FR543443A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007020049A1 (en) * | 2005-08-17 | 2007-02-22 | Airbus Deutschland Gmbh | Continuous fuselage connection |
US7931234B2 (en) | 2005-08-17 | 2011-04-26 | Airbus Deutschland Gmbh | Continuous fuselage connection |
EP3998192A1 (en) * | 2021-02-19 | 2022-05-18 | Lilium eAircraft GmbH | Wing spar structure |
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