Patent GB-1911-23194
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This British patent makes reference to the French priority date 1910-10-20.
This is a double arrangement of gyroscopic pendula, mounted on an airplane frame, responding to centrifugal force created by the movement of a turning airplane.
Sources
- Original patent document and bibliography entry on espacenet
- Patent GB191123194A on google patents
- Inventor location: 37 rue Servient, Lyons
- Inventor occupation: Engineer
Year filed | 1911 |
---|---|
Year granted | 1912 |
Office | GB |
Patent number | 23194 |
Inventors | Louis Marmonier |
Inventor country | FR |
Inventor location | |
Applicant person | Louis Marmonier |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
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, automatic stability |
Filing date | 1911/10/20 |
Full specification filed date | |
Application number | 191123194D |
Grant date | 1912/08/08 |
Granted? | Yes |
Publication date | |
Supplementary to patent | Patent FR-1910-433189 |
Related to aircraft? | Yes |
Serial number | |
Patent agent | Haseltine, Lake & Co. |
Assigned to | |
National tech categories | |
IPCs | IPC B64C1/00, IPC B64C17/06 |
CPCs | CPC B64C2700/6216, CPC B64C17/06 |
Family year | 1910 |
First filing? | No |
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 |