FR582680A - - Google Patents
Info
- Publication number
- FR582680A FR582680A FR582680DA FR582680A FR 582680 A FR582680 A FR 582680A FR 582680D A FR582680D A FR 582680DA FR 582680 A FR582680 A FR 582680A
- 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
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR582680A true FR582680A (en) | 1924-12-24 |
Family
ID=1539748
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR582680D Expired FR582680A (en) |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR582680A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2820600A (en) * | 1954-05-24 | 1958-01-21 | Northrop Aircraft Inc | Aircraft control surface assembly and actuating mechanism |
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0
- FR FR582680D patent/FR582680A/fr not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2820600A (en) * | 1954-05-24 | 1958-01-21 | Northrop Aircraft Inc | Aircraft control surface assembly and actuating mechanism |