Patent AT-1909-61611
Sources
- Espacenet bibliographic data for a quite likely candidate though the Austrian filing date is 5 September 1909
- Original via Espacenet of a quite likely candidate though the Austrian filing date is 5 September 1909
(The content fits quite well so as to designate this as Austrian 61611. We are currently fleshing out his other patents found via Espacenet, seeking among other things references to this Austrian parent patent. Being that we have found a very few typographical errors within RdBdI, relative to other data whether internal or external to the RdBdI, and given the wealth of virtually identical material filed by Sparmann in the other national offices, it seems overwhelmingly likely indeed that the RdBdI entry included here should refer to a patent filed in 5 September 1909.)
(Also, this patent, designated according to its year of granting, is the parent of a Belgian patent, dated according to the same criteria, at 1910. This has to do with a four-year delay between filing and granting, in the Austrian office, with Sparmann's reference made within the Belgian filing being based upon filing date. This patent seems also to be the unmentioned parent of at least one bloc within the other Sparmann patents we have on hand, all virtually identical and having to do with gyroscopically controlled stability.)
- Inventor location: 3 Landesgerichstrasse, Vienna, Austria
Patent family descending from Patent AT-1909-61611
- Patent AT-1909-61611 (English title: Gyro stabilizer for aircraft or other unstable body, National tech categories: AT 77d)
- Patent BE-1910-228539 (English title: Gyroscopic stabilizer pertinent to airplane wings, Supplementary to patent: Patent AT-1909-61611, National tech categories: BE K)
| Year filed | 1909 |
|---|---|
| Year granted | 1913 |
| Office | AT |
| Patent number | 61611 |
| Inventors | Edmund Sparmann |
| Inventor country | AT |
| Applicant person | Edmund Sparmann |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Kreisel-Stabilisator für Luftfahrzeuge oder andere unstabile Körper |
| English title | Gyro stabilizer for aircraft or other unstable body |
| Tech fields | stability, gyroscope, airplane, wings |
| Filing date | September 5, 1909 |
| Full specification filed date | |
| Application number | |
| Grant date | June 1, 1913 |
| Granted? | Yes |
| Publication date | October 10, 1913 |
| Supplementary to patent | |
| Related to aircraft? | Yes |
| Serial number | |
| Patent agent | |
| Assigned to | |
| National tech categories | AT 77d |
| IPCs | |
| CPCs | |
| Family year | 1909 |
| First filing? | No |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | |
| INPADOC family ID | |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 14 |
| Number of claims | 5 |
