Patent FR-1913-451312.18613
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This is an addition to Patent FR-1912-451312, which brevet was filed 1912-12-03, an airplane design, envisioning ailerons on the wings, adjustable by the pilot.
Sources
- Original patent document and bibliography entry on espacenet
- Inventor location: département Seine, France
This location represents a change, the parent patent giving the location département Nord, France.
Patent family descending from Patent FR-1913-451312.18613
- Patent FR-1913-451312.18613 (English title: Method of stabilizing and steering airplanes flying slowly, Supplementary to patent: Patent FR-1912-451312, National tech categories: FR 6.4)
- Patent GB-1914-867 (English title: Stabilizing and Steering Airplanes Flying at Low Speeds, Supplementary to patent: Patent FR-1912-451312 • Patent FR-1913-451312.18613)
| Year filed | 1913 |
|---|---|
| Year granted | 1914 |
| Office | FR |
| Patent number | 18613 |
| Inventors | |
| Inventor country | FR |
| Applicant person | |
| Applicant firm | Ateliers d'aviation Louis Bréguet |
| Applicant type | COMPANY |
| Applicant is inventor? | No |
| Original title | Mode de stabilisation et de direction des aéroplanes en marche ralentie |
| English title | Method of stabilizing and steering airplanes flying slowly |
| Tech fields | airplane, stability, navigation, aileron |
| Filing date | 1913/12/15 |
| Full specification filed date | |
| Application number | 18613D |
| Grant date | 1914/03/02 |
| Granted? | Yes |
| Publication date | 1914/05/27 |
| Supplementary to patent | Patent FR-1912-451312 |
| Related to aircraft? | Yes |
| Serial number | |
| Patent agent | Armengaud jeune |
| Assigned to | |
| National tech categories | FR 6.4 |
| IPCs | IPC CPC B64C13/00 |
| CPCs | CPC B64C13/00, CPC B64C2700/6256 |
| Family year | 1912 |
| First filing? | No |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 18729724 |
| INPADOC family ID | 5201499 |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 8 |
| Number of claims | 2 |
