Difference between revisions of "Patent BE-1911-05-15 Georges de Bothezat"
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Revision as of 21:02, 19 February 2021
Automatic stability is achieved herein by way of aerodynamically dampening the effects longitudinal and transverse oscillations, while retaining indedependence in the forward thrust of the aircraft. It seems that a fraction of inventions geared towards automatic stabilty are less focused on the role played by aerodynamics.
Sources
- Direct and specific references to a specifically Belgian patent with this filing date are made in the originals of Patent GB-1912-11493 and Patent FR-1912-443330. Data provided around Patent HU-1912-64116 mention a predecssor with this filing date, without mentioning the nationality of said patent. Other descendants have been inferred by way of diagrams and so forth identical to those of the British and the French. This patent's original title is tentative though likely in that the French and francophone Swiss patents are consistent. Patent classification BE K is likewise a matter of likelihood. Access to the Belgian RdBdI volumes will help us ascertain all of these things more properly.
- Inventor location: St. Petersburg
Patent family descending from Patent BE-1911-05-15 Georges de Bothezat
- Patent BE-1911-05-15 Georges de Bothezat (English title: Airplane of automatic stability, National tech categories: BE K)
- Patent FR-1912-443330 (English title: Automatically stabilized aeroplane, Supplementary to patent: Patent BE-1911-05-15 Georges de Bothezat, National tech categories: FR 6.4)
- Patent CH-1912-63001 (English title: Aeroplane of automatic stability, Supplementary to patent: Patent BE-1911-05-15 Georges de Bothezat, National tech categories: CH 129b)
- Patent DK-1912-18402 (English title: Aeroplane that is automatically kept stable, Supplementary to patent: Patent BE-1911-05-15 Georges de Bothezat, National tech categories: DK 77)
- Patent ES-1912-53109 (English title: A, automatically stable airplane, Supplementary to patent: Patent BE-1911-05-15 Georges de Bothezat)
- Patent GB-1912-11493 (English title: Aeroplane having Automatic Stability, Supplementary to patent: Patent BE-1911-05-15 Georges de Bothezat)
- Patent HU-1912-64116 (English title: Self-stabiling aeroplane, Supplementary to patent: Patent BE-1911-05-15 Georges de Bothezat, National tech categories: HU V/h)
- Patent AU-1912-545612 (English title: Aeroplane having automatic stability, Supplementary to patent: Patent BE-1911-05-15 Georges de Bothezat, National tech categories: AU 90.3)
| Year filed | 1911 |
|---|---|
| Year granted | |
| Office | BE |
| Patent number | |
| Inventors | Georges de Bothezat |
| Inventor country | RU |
| Applicant person | Georges de Bothezat |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | |
| English title | Airplane of automatic stability |
| Tech fields | Airplane, Stability, Aerodynamics |
| Filing date | 1911-05-15 |
| Full specification filed date | |
| Application number | |
| Grant date | |
| Granted? | |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | |
| Serial number | |
| Patent agent | |
| Assigned to | |
| National tech categories | BE K |
| IPCs | |
| CPCs | |
| Family year | 1911 |
| First filing? | |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | |
| INPADOC family ID | |
| Number of text pages | |
| Number of diagram pages | |
| Number of figures | |
| Number of claims |
