FR962428A - - Google Patents
Info
- Publication number
- FR962428A FR962428A FR962428DA FR962428A FR 962428 A FR962428 A FR 962428A FR 962428D A FR962428D A FR 962428DA FR 962428 A FR962428 A FR 962428A
- Authority
- FR
- France
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR962428A true FR962428A (de) | 1950-06-10 |
Family
ID=1563745
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR962428D Expired FR962428A (de) |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR962428A (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1985001489A1 (en) * | 1983-09-29 | 1985-04-11 | The Boeing Company | High strength to weight horizontal and vertical aircraft stabilizer |
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0
- FR FR962428D patent/FR962428A/fr not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1985001489A1 (en) * | 1983-09-29 | 1985-04-11 | The Boeing Company | High strength to weight horizontal and vertical aircraft stabilizer |
| US4667905A (en) * | 1983-09-29 | 1987-05-26 | The Boeing Company | High strength to weight horizontal and vertical aircraft stabilizer |