Difference between revisions of "Patent FR-1914-462405"
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| + | An aeroplane wing shaped by taut structural wires. | ||
| + | {{Patent family|Patent GB-1912-21604 }} | ||
| + | * Parent patent filing date: 1912-09-23 | ||
| + | * Inventor location: | ||
| + | === Sources === | ||
| + | * {{esp|FR|462405a}} | ||
{{Patent | {{Patent | ||
|Year filed=1913 | |Year filed=1913 | ||
| Line 7: | Line 13: | ||
|Inventor country=GB | |Inventor country=GB | ||
|Applicant person=Norman Arthur Thompson | |Applicant person=Norman Arthur Thompson | ||
| + | |Applicant firm= | ||
|Applicant type=INDIV | |Applicant type=INDIV | ||
|Applicant is inventor=1 | |Applicant is inventor=1 | ||
| − | |Original title= | + | |Original title=Perfectionnements aux aéroplanes et aux appareils similaires |
| − | |English title= | + | |English title=Improvements to aeroplanes and similar machines |
| − | |Tech field= | + | |Tech field=aerofoil |
|Filing date=1913-09-09 | |Filing date=1913-09-09 | ||
| + | |Full specification filed date= | ||
|Application number=462405D | |Application number=462405D | ||
| − | |Grant date= | + | |Grant date=1913-11-21 |
|Granted=1 | |Granted=1 | ||
| − | |Publication date= | + | |Publication date=1914-01-27 |
| − | |Supplementary to patent= | + | |Supplementary to patent=Patent GB-1912-21604 |
|Related to aircraft=1 | |Related to aircraft=1 | ||
|Serial number= | |Serial number= | ||
| − | |Patent agent= | + | |Patent agent=D. Casalonga |
|Assigned to= | |Assigned to= | ||
| − | |National tech categories= | + | |National tech categories=FR 6.4 |
| − | |IPCs= | + | |IPCs=IPC B64C3/00 |
|CPCs=CPC B64C2700/6233; CPC B64C3/00 | |CPCs=CPC B64C2700/6233; CPC B64C3/00 | ||
| − | |Family year= | + | |Family year=1912 |
|First filing=0 | |First filing=0 | ||
| + | |Cites these patents= | ||
| + | |Citations from after 1930= | ||
|Application ID=19280362 | |Application ID=19280362 | ||
|INPADOC family ID=5348008 | |INPADOC family ID=5348008 | ||
| + | |Number of text pages=3 | ||
| + | |Number of diagram pages=1 | ||
| + | |Number of figures=5 | ||
| + | |Number of claims=3 | ||
}} | }} | ||
| − | |||
| − | |||
| − | |||
Latest revision as of 12:34, 20 October 2021
An aeroplane wing shaped by taut structural wires.
- Parent patent filing date: 1912-09-23
- Inventor location:
Sources
- Original patent document and bibliography entry on espacenet
| Year filed | 1913 |
|---|---|
| Year granted | 1914 |
| Office | FR |
| Patent number | 462405 |
| Inventors | Norman Arthur Thompson |
| Inventor country | GB |
| Applicant person | Norman Arthur Thompson |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Perfectionnements aux aéroplanes et aux appareils similaires |
| English title | Improvements to aeroplanes and similar machines |
| Tech fields | aerofoil |
| Filing date | 1913-09-09 |
| Full specification filed date | |
| Application number | 462405D |
| Grant date | 1913-11-21 |
| Granted? | 1 |
| Publication date | 1914-01-27 |
| Supplementary to patent | Patent GB-1912-21604 |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | D. Casalonga |
| Assigned to | |
| National tech categories | FR 6.4 |
| IPCs | IPC B64C3/00 |
| CPCs | CPC B64C2700/6233, CPC B64C3/00 |
| Family year | 1912 |
| First filing? | 0 |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 19280362 |
| INPADOC family ID | 5348008 |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 5 |
| Number of claims | 3 |
