Patent FR-1913-461752
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This is largely a biplane, with a small, but very interesting, helicopter-style rotating disk-blade enhancing sustentation while also aiding in stability. It is powered by an auxiliary motor.
- Inventor location: département Seine-et-Marne, France
Sources
- Original patent document and bibliography entry on espacenet
- on google patents
Year filed | 1913 |
---|---|
Year granted | 1913 |
Office | FR |
Patent number | 461752 |
Inventors | Anatole-Moise Bruneau |
Inventor country | FR |
Applicant person | Anatole-Moise Bruneau |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Stabilisateur-planeur-sustentateur pour aéroplanes |
English title | Stabilizer-glider-lift for airplanes |
Tech fields | stability, sustentation, HTA, hybrid, helicopter, biplane, motors, centrifuge |
Filing date | 1913/08/23 |
Full specification filed date | |
Application number | 461752D |
Grant date | 1913/11/06 |
Granted? | Yes |
Publication date | 1914/01/10 |
Supplementary to patent | |
Related to aircraft? | Yes |
Serial number | |
Patent agent | L. Chassevent |
Assigned to | |
National tech categories | FR 6.4 |
IPCs | IPC B64C1/00, IPC B64C17/06 |
CPCs | CPC B64C2700/6216, CPC B64C17/06 |
Family year | 1913 |
First filing? | Yes |
Cites these patents | |
Citations from after 1930 | |
Application ID | 19279727 |
INPADOC family ID | 5347456 |
Number of text pages | 2 |
Number of diagram pages | 1 |
Number of figures | 4 |
Number of claims | 1 |