Patent GB-1911-11229
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Tail arrangement ; "baffle flanges" ; stability
- Inventor location: No. 218, Bishop Street, Montreal ; Gentleman
- Dated May 9 and filed the same day
Patent family descending from Patent US-1911-994106
- Patent US-1911-994106 (English title: Aeroplane, National tech categories: USPC 244/45R)
- Patent GB-1911-11229 (English title: Improvements in Aeroplanes, Supplementary to patent: Patent US-1911-994106)
- Patent FR-1911-431358 (English title: Improvements brought to airplanes, Supplementary to patent: Patent US-1911-994106, National tech categories: FR 6.4)
- Patent CA-1912-142946 (English title: Aeroplane, Supplementary to patent: Patent US-1911-994106, National tech categories: CA 244/34)
Sources
- Original patent document and bibliography entry on espacenet
Year filed | 1911 |
---|---|
Year granted | 1911 |
Office | GB |
Patent number | 11229 |
Inventors | William Boyd Alexander |
Inventor country | CA |
Applicant person | William Boyd Alexander |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
Original title | Improvements in Aeroplanes |
English title | Improvements in Aeroplanes |
Tech fields | tail, stability |
Filing date | 1911-05-09 |
Full specification filed date | |
Application number | 191111229D |
Grant date | 1911-06-21 |
Granted? | 1 |
Publication date | |
Supplementary to patent | Patent US-1911-994106 |
Related to aircraft? | 1 |
Serial number | |
Patent agent | Johnsons & Willcox |
Assigned to | |
National tech categories | |
IPCs | IPC B64C39/00 |
CPCs | CPC B64C2700/6295, CPC B64C39/00 |
Family year | 1911 |
First filing? | 0 |
Cites these patents | |
Citations from after 1930 | |
Application ID | 23616444 |
INPADOC family ID | 11107085 |
Number of text pages | 3 |
Number of diagram pages | 1 |
Number of figures | 3 |
Number of claims | 5 |