Patent GB-1909-11021
Revision as of 18:34, 28 December 2024 by AvionHerbert (talk | contribs) (Text replacement - "|Tech field=" to "|Tech fields=")
Rigid wings project backward, the tips connected by lines, with the wings having greater angle of incidence near the fuselage and flatter at the wingtips.
Sources
- Neilson, 1910, p. 60
- Original patent document and bibliography entry on espacenet
- Patent GB190911021A on google patents
- Inventor location: 16, Charing Cross, London, W.C.
- Inventor occupation: Gentleman
| Year filed | 1909 |
|---|---|
| Year granted | 1910 |
| Office | GB |
| Patent number | 11021 |
| Inventors | John William Dunne |
| Inventor country | GB |
| Inventor location | |
| Applicant person | John William Dunne |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Improvements relating to Aeroplanes |
| English title | design for flying machine with automatic stability and freedom from oscillation |
| Tech fields | airplane, aerodynamics, design, incidence, stability, automatic stability |
| Filing date | 1909/05/10 |
| Full specification filed date | 1909/11/09 |
| Application number | |
| Grant date | 1910/05/05 |
| Granted? | Yes |
| Publication date | 1910/05/05 |
| Supplementary to patent | |
| Related to aircraft? | Yes |
| Serial number | |
| Patent agent | Marks & Clerk |
| Assigned to | |
| National tech categories | |
| IPCs | IPC B64C39/10 |
| CPCs | CPC B64C39/10 |
| Family year | 1909 |
| First filing? | No |
| Cites these patents | |
| Citations from after 1930 | 1 |
| Application ID | 23581989 |
| INPADOC family ID | 11077150 |
| Number of text pages | 5 |
| Number of diagram pages | 1 |
| Number of figures | 9 |
| Number of claims | 4 |
