Patent GB-1911-23271
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Use of gyroscope for stability; detail about the placement and alignment of the gyroscope, relative to other aircraft elements, to maximize its effect.
Sources
Original patent document and bibliography entry on espacenet
| Year filed | 1911 |
|---|---|
| Year granted | 1912 |
| Office | GB |
| Patent number | 23271 |
| Inventors | Frederick William Lanchester |
| Inventor country | GB |
| Applicant person | |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Improvements relating to the Stabilisation of Flying Machines |
| English title | Stabilisation of Flying Machines |
| Tech fields | stability, airplane, gyroscope, frame, design |
| Filing date | 1911-10-21 |
| Full specification filed date | 1912-05-21 |
| Application number | |
| Grant date | 1912-10-17 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | Marks & Clerk |
| Assigned to | |
| National tech categories | |
| IPCs | IPC B64D35/04 |
| CPCs | CPC B64D35/04 |
| Family year | |
| First filing? | |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | |
| INPADOC family ID | |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 3 |
| Number of claims | 3 |
