Patent GB-1911-23194
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Double arrangement of gyroscopic pendula, mounted on an airplane frame, responding to centrifugal force created by the movement of a turning airplane.
- Inventor location: 37 rue Servient, Lyons
- Inventor occupation: Engineer
Sources
| Year filed | 1911 |
|---|---|
| Year granted | 1912 |
| Office | GB |
| Patent number | 23194 |
| Inventors | Louis Marmonier |
| Inventor country | FR |
| Applicant person | |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Improvements in Automatic Stabilizing Means for Aeroplanes and the like |
| English title | Automatic Stabilizing Means for Aeroplanes and the like |
| Tech fields | airplane, stability, gyroscope, pendulum, frame, subsystem |
| Filing date | 1911-10-20 |
| Full specification filed date | |
| Application number | 191123194D |
| Grant date | 1912-08-08 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | Patent FR-1910-433189 |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | Haseltine, Lake & Co. |
| Assigned to | |
| National tech categories | |
| IPCs | |
| CPCs | CPC B64C2700/6216, CPC B64C17/06 |
| Family year | |
| First filing? | 0 |
| Cites these patents | Patent GB-1909-978 |
| Citations from after 1930 | |
| Application ID | 23623349 |
| INPADOC family ID | 11113050 |
| Number of text pages | 3 |
| Number of diagram pages | 2 |
| Number of figures | 6 |
| Number of claims | 4 |
