Patent GB-1909-11021
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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
- 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 |
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 |