Difference between revisions of "Patent FR-1913-464351"
Jump to navigation
Jump to search
m (Text replacement - "|Number of citations=" to "|Citations from after 1930=") |
AvionHerbert (talk | contribs) m (Text replacement - "|Tech field=" to "|Tech fields=") |
||
| Line 16: | Line 16: | ||
|Original title=Dispositif amortisseur de chocs pour aéroplanes | |Original title=Dispositif amortisseur de chocs pour aéroplanes | ||
|English title=Airplane shock-absorber | |English title=Airplane shock-absorber | ||
| − | |Tech | + | |Tech fields=subsystem; shock-absorbers; airplane; landing |
|Filing date=1913-01-11 | |Filing date=1913-01-11 | ||
|Full specification filed date= | |Full specification filed date= | ||
Latest revision as of 18:22, 28 December 2024
Sources
- Original patent document and bibliography entry on espacenet
- Inventor location: France
| Year filed | 1913 |
|---|---|
| Year granted | 1914 |
| Office | FR |
| Patent number | 464351 |
| Inventors | Émile Latour, Henri Bouillon, Gustave Naudin |
| Inventor country | FR, FR, FR |
| Inventor location | |
| Applicant person | Émile Latour, Henri Bouillon, Gustave Naudin |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Dispositif amortisseur de chocs pour aéroplanes |
| English title | Airplane shock-absorber |
| Tech fields | subsystem, shock-absorbers, airplane, landing |
| Filing date | 1913-01-11 |
| Full specification filed date | |
| Application number | |
| Grant date | 1914-01-12 |
| Granted? | 1 |
| Publication date | 1914-03-19 |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | L. Chassevent |
| Assigned to | |
| National tech categories | FR 6.4 |
| IPCs | IPC B64D25/04 |
| CPCs | CPC B64D25/04 |
| Family year | 1913 |
| First filing? | |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | |
| INPADOC family ID | |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 6 |
| Number of claims | 2 |
