Patent FR-1911-434281
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- Inventor location: rue Coypel, 7, Paris, Seine; France
Sources
- Original patent document and bibliography entry on espacenet
- Patent FR434281A on google patents
Patent family descending from Patent FR-1911-434281
- Patent FR-1911-434281 (English title: Bird's body fuselage which aims to increase the speed of the airplanes by its very tapered shape at the front, by the arrangement of the propeller at the rear and by a very special device of the head forming a rudder, Filing date: 1911-09-16, National tech categories: FR 6.4)
- Patent GB-1912-21051 (English title: Improvements relating to flying machines with boat-shaped or bird-shaped bodies, Supplementary to patent: Patent FR-1911-434281, Filing date: 1912-09-16)
- Patent FR-1913-434281.17328 (English title: Bird's body fuselage which aims to increase the speed of the airplanes by its very tapered shape at the front, by the arrangement of the propeller at the rear and by a very special device of the head forming a rudder, Supplementary to patent: Patent FR-1911-434281, Filing date: 1913-02-27, National tech categories: FR 6.4)
| Year filed | 1911 |
|---|---|
| Year granted | 1912 |
| Office | FR |
| Patent number | 434281 |
| Inventors | Jean-Baptiste-Eugène Gangler |
| Inventor country | FR |
| Inventor location | |
| Applicant person | Jean-Baptiste-Eugène Gangler |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Fuselage corps d'oiseau qui a pour but d'augmenter la vitesse des aéroplanes par sa forme très effilée à l'avant, par la disposition de l'hélice à l'arrière et par un dispositif tout spécial de la tete formant gouvernail de direction |
| English title | Bird's body fuselage which aims to increase the speed of the airplanes by its very tapered shape at the front, by the arrangement of the propeller at the rear and by a very special device of the head forming a rudder |
| Tech fields | Airplane, Fuselage, Aerodynamics, Frame, Construction, Design, Rudder |
| Filing date | 1911/09/16 |
| Full specification filed date | |
| Application number | 434281D |
| Grant date | 1911/11/21 |
| Granted? | Yes |
| Publication date | 1912/01/30 |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | None |
| Assigned to | |
| National tech categories | FR 6.4 |
| IPCs | IPC B64C39/00 |
| CPCs | CPC B64C39/00, CPC B64C2700/6295 |
| Family year | 1911 |
| First filing? | No |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 19252874 |
| INPADOC family ID | 5200684 |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 5 |
| Number of claims | 2 |
