Difference between revisions of "Patent FR-1910-417723"
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| + | « RÉSUMÉ » (that is, summary) : | ||
| + | |||
| + | "The present invention has for its object an apparatus of automatic stability, with lateral action, for flying machines, composing wings linked rigidly to one another, with elastic extremities, the apparatus in question being characterized by the fact that the wings are established in such a manner as to be able to turn around and axis disposed in the longitudinal vertical median plane of the aircraft’s frame, and that the said lower exterior surfaces are constituted of elastic parts, the rigid parts of these wings carrying supports directed downwardly, and receiving, at their free extremity, guided [[rollers]], over which pass cables, which end at a fixed point on the frame of the aircraft, on the axis of wing rotation, in such a manner as to automatically assure, during the rotation or the displacement of the wings, a corresponding displacement of the elastic extremities of these latter (wings)." | ||
| + | |||
| + | (These elaborate means of combining the virtues of [[elasticity]] and [[rigidity]] are somewhat novel. Of precise interest also are [[rollers]], or [[bearings]], operating in conjunction with [[cables]].) | ||
| + | |||
| + | This must be related in its conception to [[Patent FR-1910-417722]], filed by the same pair of inventors, using an identical French invention title, filed in fact of the very same day. Here again we have Hungarian interest in [[stability]] of [[airplane]]s, achieved automatically, said achievement being arrived at through an always distinct and varied number of different principles and means. In the case of these two patents relative to one another, the inventors must have been going over principles, as consciously varied, and distinguishing them, separately, rather than forcing them into one "system". | ||
| + | === Sources === | ||
| + | {{FRpatentsources|417723A}} | ||
| + | * Inventor location: Hungary | ||
{{Patent | {{Patent | ||
|Year filed=1910 | |Year filed=1910 | ||
| Line 4: | Line 14: | ||
|Office=FR | |Office=FR | ||
|Patent number=417723 | |Patent number=417723 | ||
| − | |Inventors=Josef | + | |Inventors=Josef Marek; Alexandre Temesvary |
|Inventor country=HU | |Inventor country=HU | ||
| − | |Applicant person= | + | |Applicant person=József Marek; Sándor Temesváry |
|Applicant type=INDIV | |Applicant type=INDIV | ||
| − | |Applicant is inventor= | + | |Applicant is inventor=Yes |
| − | |Filing date=1910 | + | |Original title=Dispositif de stabilisateur automatique à action latérale, pour machines volantes |
| + | |English title=Automatic stability apparatus, with lateral action, for flying machines | ||
| + | |Tech fields=airplane; stability; wings; aerodynamics; cables; elasticity; automatic stability | ||
| + | |Filing date=1910/05/12 | ||
|Application number=417723D | |Application number=417723D | ||
| − | |Grant date=1910- | + | |Grant date=1910/07/08 |
| − | | | + | |Granted=Yes |
| − | |CPCs=CPC B64C2700/6218 | + | |Publication date=1910/11/21 |
| − | |Family year= | + | |Supplementary to patent=Patent HU-1910-51215 |
| − | |First filing= | + | |Related to aircraft=Yes |
| − | | | + | |Patent agent=J. Fayollet |
| − | |INPADOC family ID= | + | |National tech categories=FR 6.4 |
| − | |Number of text pages= | + | |IPCs=IPC B64C1/00; IPC B64C17/00 |
| + | |CPCs=CPC B64C2700/6218; CPC B64C17/00 | ||
| + | |Family year=1910 | ||
| + | |First filing=No | ||
| + | |Application ID=19236672 | ||
| + | |INPADOC family ID=5310632 | ||
| + | |Number of text pages=2 | ||
| + | |Number of diagram pages=1 | ||
| + | |Number of figures=1 | ||
| + | |Number of claims=1 | ||
}} | }} | ||
| − | |||
| − | |||
| − | |||
Latest revision as of 17:49, 28 December 2024
« RÉSUMÉ » (that is, summary) :
"The present invention has for its object an apparatus of automatic stability, with lateral action, for flying machines, composing wings linked rigidly to one another, with elastic extremities, the apparatus in question being characterized by the fact that the wings are established in such a manner as to be able to turn around and axis disposed in the longitudinal vertical median plane of the aircraft’s frame, and that the said lower exterior surfaces are constituted of elastic parts, the rigid parts of these wings carrying supports directed downwardly, and receiving, at their free extremity, guided rollers, over which pass cables, which end at a fixed point on the frame of the aircraft, on the axis of wing rotation, in such a manner as to automatically assure, during the rotation or the displacement of the wings, a corresponding displacement of the elastic extremities of these latter (wings)."
(These elaborate means of combining the virtues of elasticity and rigidity are somewhat novel. Of precise interest also are rollers, or bearings, operating in conjunction with cables.)
This must be related in its conception to Patent FR-1910-417722, filed by the same pair of inventors, using an identical French invention title, filed in fact of the very same day. Here again we have Hungarian interest in stability of airplanes, achieved automatically, said achievement being arrived at through an always distinct and varied number of different principles and means. In the case of these two patents relative to one another, the inventors must have been going over principles, as consciously varied, and distinguishing them, separately, rather than forcing them into one "system".
Sources
- Original patent document and bibliography entry on espacenet
- Patent FR417723A on google patents
- Inventor location: Hungary
| Year filed | 1910 |
|---|---|
| Year granted | 1910 |
| Office | FR |
| Patent number | 417723 |
| Inventors | Josef Marek, Alexandre Temesvary |
| Inventor country | HU |
| Inventor location | |
| Applicant person | József Marek, Sándor Temesváry |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Dispositif de stabilisateur automatique à action latérale, pour machines volantes |
| English title | Automatic stability apparatus, with lateral action, for flying machines |
| Tech fields | airplane, stability, wings, aerodynamics, cables, elasticity, automatic stability |
| Filing date | 1910/05/12 |
| Full specification filed date | |
| Application number | 417723D |
| Grant date | 1910/07/08 |
| Granted? | Yes |
| Publication date | 1910/11/21 |
| Supplementary to patent | Patent HU-1910-51215 |
| Related to aircraft? | Yes |
| Serial number | |
| Patent agent | J. Fayollet |
| Assigned to | |
| National tech categories | FR 6.4 |
| IPCs | IPC B64C1/00, IPC B64C17/00 |
| CPCs | CPC B64C2700/6218, CPC B64C17/00 |
| Family year | 1910 |
| First filing? | No |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 19236672 |
| INPADOC family ID | 5310632 |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 1 |
| Number of claims | 1 |
