Patent US-1906-884432
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Airplane made from intersecting horizontal and vertical aeroplanes, plus motor and rudder; automatic stabilization system of compressed air which is released by tilt, acting to move the vessel back towards equilibrium
- Tech class CPC B64C3/14: Aerofoil profile
- Inventor location: a citizen of the USA resident in Genevilliers, France (USA)
- Witnesses (as shown on the final text page): Emile Leotret, likely more properly Émile Léotret, and H. C. Coxe, very likely the Hanson C. Coxe whom we have on hand
Sources
- Patent 884432 document and bibliographic info on espacenet
- Patent 884432 at google patents
- Short's DB
- PTO 244
- Neilson
| Year filed | 1906 |
|---|---|
| Year granted | 1908 |
| Office | US |
| Patent number | 884432 |
| Inventors | Melvin Vaniman |
| Inventor country | FR |
| Applicant person | Melvin Vaniman |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Aeroplane |
| English title | Aeroplane |
| Tech fields | airplane, frame, airfoil, texture, parachute, car, navigation, rudder, stability, takeoff, automatic stability |
| Filing date | 1906/11/27 |
| Full specification filed date | |
| Application number | 1906345394 |
| Grant date | 1908/04/14 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | 345394 |
| Patent agent | Richardson |
| Assigned to | |
| National tech categories | USPC 244/35R, USPC 244/89 |
| IPCs | IPC B64C3/14 |
| CPCs | CPC B64C3/14 |
| Family year | 1906 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | 1 |
| Application ID | 47095970 |
| INPADOC family ID | 43803995 |
| Number of text pages | 2 |
| Number of diagram pages | 2 |
| Number of figures | 5 |
| Number of claims | 1 |
