Difference between revisions of "Patent FR-1907-361723.8226"
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+ | This is the second addition to [[Patent FR-1905-361723]], which was filed 1905-08-26. | ||
+ | |||
+ | « Cette addition porte sur l’obtention par le basculateur de la sustentation supplémentaire nécessaire à un plan rester immobile dans l’air, ainsi que permettre, par le déplacement du centre de gravité, d’obtenir un glissement particulier du plan. » | ||
+ | |||
+ | That is, this addition works towards the establishment of a supplementary [[sustentation]] tilter necessary for a [[lift]] surface to remain steady in the air, so as to facilitate, via the displacement of the center of gravity, a sliding effect peculiar to the lift surface. | ||
+ | |||
+ | === Sources === | ||
+ | * {{esp|FR|8226E}} | ||
+ | * Inventor location: [[département]] [[Rhône]], France | ||
{{Patent | {{Patent | ||
+ | |Year filed=1907 | ||
|Year granted=1907 | |Year granted=1907 | ||
|Office=FR | |Office=FR | ||
Line 5: | Line 15: | ||
|Inventors=Jean Constantin | |Inventors=Jean Constantin | ||
|Inventor country=FR | |Inventor country=FR | ||
− | |Applicant person= | + | |Applicant person=Jean Constantin |
|Applicant type=INDIV | |Applicant type=INDIV | ||
− | |Applicant is inventor= | + | |Applicant is inventor=Yes |
− | |Filing date=1907 | + | |Original title=Aviateur équilibré |
+ | |English title=Balanced aircraft | ||
+ | |Tech field=equilibrium; lift; sustentation; airplane; subsystem; wings; aerodynamics | ||
+ | |Filing date=1907/09/23 | ||
|Application number=8226D | |Application number=8226D | ||
− | |Grant date=1908- | + | |Grant date=1907/12/03 |
− | | | + | |Granted=Yes |
+ | |Publication date=1908/02/08 | ||
+ | |Supplementary to patent=Patent FR-1905-361723 | ||
+ | |Related to aircraft=Yes | ||
+ | |Patent agent=J. Germain | ||
+ | |National tech categories=FR 6.4 | ||
+ | |IPCs=IPC B64C1/00 | ||
|CPCs=CPC B64C1/00; CPC B64C2700/6228 | |CPCs=CPC B64C1/00; CPC B64C2700/6228 | ||
|Family year=1905 | |Family year=1905 | ||
− | |First filing= | + | |First filing=No |
|Application ID=18678018 | |Application ID=18678018 | ||
|INPADOC family ID=5190171 | |INPADOC family ID=5190171 | ||
+ | |Number of text pages=2 | ||
+ | |Number of claims=1 | ||
}} | }} | ||
− | |||
− | |||
− |
Latest revision as of 12:09, 17 January 2022
This is the second addition to Patent FR-1905-361723, which was filed 1905-08-26.
« Cette addition porte sur l’obtention par le basculateur de la sustentation supplémentaire nécessaire à un plan rester immobile dans l’air, ainsi que permettre, par le déplacement du centre de gravité, d’obtenir un glissement particulier du plan. »
That is, this addition works towards the establishment of a supplementary sustentation tilter necessary for a lift surface to remain steady in the air, so as to facilitate, via the displacement of the center of gravity, a sliding effect peculiar to the lift surface.
Sources
- Original patent document and bibliography entry on espacenet
- Inventor location: département Rhône, France
Year filed | 1907 |
---|---|
Year granted | 1907 |
Office | FR |
Patent number | 8226 |
Inventors | Jean Constantin |
Inventor country | FR |
Applicant person | Jean Constantin |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Aviateur équilibré |
English title | Balanced aircraft |
Tech fields | equilibrium, lift, sustentation, airplane, subsystem, wings, aerodynamics |
Filing date | 1907/09/23 |
Full specification filed date | |
Application number | 8226D |
Grant date | 1907/12/03 |
Granted? | Yes |
Publication date | 1908/02/08 |
Supplementary to patent | Patent FR-1905-361723 |
Related to aircraft? | Yes |
Serial number | |
Patent agent | J. Germain |
Assigned to | |
National tech categories | FR 6.4 |
IPCs | IPC B64C1/00 |
CPCs | CPC B64C1/00, CPC B64C2700/6228 |
Family year | 1905 |
First filing? | No |
Cites these patents | |
Citations from after 1930 | |
Application ID | 18678018 |
INPADOC family ID | 5190171 |
Number of text pages | 2 |
Number of diagram pages | |
Number of figures | |
Number of claims | 1 |