Difference between revisions of "Patent FR-1911-426612"
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* Tech class: [[CPC B64C17/00]]: Aircraft stabilisation not otherwise provided for | * Tech class: [[CPC B64C17/00]]: Aircraft stabilisation not otherwise provided for | ||
* Inventor location: | * Inventor location: | ||
| + | {{Patent family|Patent FR-1911-426612}} | ||
=== Sources === | === Sources === | ||
* {{FRpatentsources|426612A}} | * {{FRpatentsources|426612A}} | ||
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|Full specification filed date= | |Full specification filed date= | ||
|Application number=426612D | |Application number=426612D | ||
| − | |Grant date=1911- | + | |Grant date=1911-05-09 |
|Granted=1 | |Granted=1 | ||
| − | |Publication date= | + | |Publication date=1911-07-11 |
|Supplementary to patent= | |Supplementary to patent= | ||
|Related to aircraft=1 | |Related to aircraft=1 | ||
|Serial number= | |Serial number= | ||
| − | |Patent agent= | + | |Patent agent=J. Rosen |
|Assigned to= | |Assigned to= | ||
| − | |National tech categories= | + | |National tech categories=FR 6.4 |
| − | |IPCs= | + | |IPCs=IPC B64C17/00 |
|CPCs=CPC B64C17/00; CPC B64C2700/6214 | |CPCs=CPC B64C17/00; CPC B64C2700/6214 | ||
|Family year=1911 | |Family year=1911 | ||
| Line 37: | Line 38: | ||
|Application ID=19245363 | |Application ID=19245363 | ||
|INPADOC family ID=5318086 | |INPADOC family ID=5318086 | ||
| − | |Number of text pages= | + | |Number of text pages=2 |
| − | |Number of diagram pages= | + | |Number of diagram pages=1 |
| − | |Number of figures= | + | |Number of figures=4 |
| − | |Number of claims= | + | |Number of claims=1 |
}} | }} | ||
Latest revision as of 01:08, 27 March 2024
- Tech class: CPC B64C17/00: Aircraft stabilisation not otherwise provided for
- Inventor location:
Patent family descending from Patent FR-1911-426612
- Patent FI-1911-4527 (English title: Apparatus for stabilizing the equilibrium position of an aeroplane, Supplementary to patent: Patent FR-1911-426612)
- Patent FR-1911-426612 (English title: Stabilization system for airplanes, National tech categories: FR 6.4)
- Patent GB-1912-2473 (English title: A system of flight stabilisation for aeroplanes, Supplementary to patent: Patent FR-1911-426612)
Sources
- Original patent document and bibliography entry on espacenet
- on google patents
| Year filed | 1911 |
|---|---|
| Year granted | 1911 |
| Office | FR |
| Patent number | 426612 |
| Inventors | Louis-Alphonse Canda |
| Inventor country | FR |
| Applicant person | Louis-Alphonse Canda |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Système de stabilisation de marche pour aéroplanes |
| English title | Stabilization system for airplanes |
| Tech fields | stability |
| Filing date | 1911-01-31 |
| Full specification filed date | |
| Application number | 426612D |
| Grant date | 1911-05-09 |
| Granted? | 1 |
| Publication date | 1911-07-11 |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | J. Rosen |
| Assigned to | |
| National tech categories | FR 6.4 |
| IPCs | IPC B64C17/00 |
| CPCs | CPC B64C17/00, CPC B64C2700/6214 |
| Family year | 1911 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | 0 |
| Application ID | 19245363 |
| INPADOC family ID | 5318086 |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 4 |
| Number of claims | 1 |
