Patent GB-1909-8118
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Rigid wings project backward, tips connected by lines, with wings having greater angle of incidence near fuselage and flatter at wingtips
- Tech class CPC B64C39/10: All-wing aircraft
- Inventor location: 16 Charing Cross, London, W.C.
- Inventor occupation: Gentleman
Sources
- Neilson, 1910, Aeroplane Patents, p60
- Original patent document and bibliography entry on espacenet
- Patent GB190908118A on google patents
Patent family descending from Patent GB-1909-8118
- Patent GB-1909-8118 (English title: design for automatically stable flying machine with reduced oscillation, Filing date: 1909-04-05)
- Patent US-1910-1003721 (English title: Aeroplane, Supplementary to patent: Patent GB-1909-8118, Filing date: 1910-04-01, National tech categories: USPC 244/45R)
- Patent FR-1910-414444 (English title: Improvements made to the construction of airplanes, Supplementary to patent: Patent GB-1909-8118, Filing date: 1910-04-04, National tech categories: FR 6.4)
Year filed | 1909 |
---|---|
Year granted | 1910 |
Office | GB |
Patent number | 8118 |
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 automatically stable flying machine with reduced oscillation |
Tech fields | airplane, stability, automatic stability |
Filing date | 1909/04/05 |
Full specification filed date | 1909/10/04 |
Application number | 190908118D |
Grant date | 1910/03/31 |
Granted? | Yes |
Publication date | |
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? | Yes |
Cites these patents | |
Citations from after 1930 | 0 |
Application ID | 23580387 |
INPADOC family ID | 11075760 |
Number of text pages | 7 |
Number of diagram pages | 3 |
Number of figures | 16 |
Number of claims | 6 |