Difference between revisions of "Patent GB-1908-15637"
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| + | Wing warping, integrated with propulsion and traction, playing into overall precision of control. | ||
| + | * Inventor location: 149 rue de Silly, Boulogne-sur-Seine, France | ||
| + | === Sources === | ||
| + | * {{esp|gb|190915637a}} | ||
| + | * {{Neilson1910|77|p77}} | ||
{{Patent | {{Patent | ||
|Year filed=1908 | |Year filed=1908 | ||
| Line 7: | Line 12: | ||
|Inventor country=FR | |Inventor country=FR | ||
|Applicant person=Robert Esnault-Pelterie | |Applicant person=Robert Esnault-Pelterie | ||
| + | |Applicant firm= | ||
|Applicant type=INDIV | |Applicant type=INDIV | ||
|Applicant is inventor=1 | |Applicant is inventor=1 | ||
|Original title=Improvements in Aeroplanes | |Original title=Improvements in Aeroplanes | ||
| + | |English title=Improvements in variably controlled monoplane wing warping having to do with lift per se | ||
| + | |Tech fields=airplane; monoplane; wing warping; lift | ||
|Filing date=1908-07-16 | |Filing date=1908-07-16 | ||
| + | |Full specification filed date= | ||
|Application number=190915637D | |Application number=190915637D | ||
| + | |Grant date= | ||
|Granted=1 | |Granted=1 | ||
| − | |Related to aircraft= | + | |Publication date= |
| − | |CPCs=CPC B64C2700/6245 | + | |Supplementary to patent=Patent FR-1908-392672 |
| − | |Family year= | + | |Related to aircraft=1 |
| − | |First filing= | + | |Serial number= |
| − | | | + | |Patent agent=Abel & Imray |
| − | |INPADOC family ID= | + | |Assigned to= |
| − | |Number of text pages= | + | |National tech categories= |
| + | |IPCs= | ||
| + | |CPCs=CPC B64C2700/6245; CPC B64C3/52 | ||
| + | |Family year=1908 | ||
| + | |First filing=1 | ||
| + | |Cites these patents= | ||
| + | |Citations from after 1930= | ||
| + | |Application ID=23584609 | ||
| + | |INPADOC family ID=5906502 | ||
| + | |Number of text pages=3 | ||
| + | |Number of diagram pages=1 | ||
| + | |Number of figures=8 | ||
| + | |Number of claims=7 | ||
}} | }} | ||
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Latest revision as of 07:24, 17 October 2021
Wing warping, integrated with propulsion and traction, playing into overall precision of control.
- Inventor location: 149 rue de Silly, Boulogne-sur-Seine, France
Sources
- Original patent document and bibliography entry on espacenet
- Neilson, 1910, Aeroplane Patents, p77
| Year filed | 1908 |
|---|---|
| Year granted | 1909 |
| Office | GB |
| Patent number | 15637 |
| Inventors | Robert Esnault-Pelterie |
| Inventor country | FR |
| Applicant person | Robert Esnault-Pelterie |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Improvements in Aeroplanes |
| English title | Improvements in variably controlled monoplane wing warping having to do with lift per se |
| Tech fields | |
| Filing date | 1908-07-16 |
| Full specification filed date | |
| Application number | 190915637D |
| Grant date | |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | Patent FR-1908-392672 |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | Abel & Imray |
| Assigned to | |
| National tech categories | |
| IPCs | |
| CPCs | CPC B64C2700/6245, CPC B64C3/52 |
| Family year | 1908 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 23584609 |
| INPADOC family ID | 5906502 |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 8 |
| Number of claims | 7 |
