Patent DE-1913-281533
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Aircraft whose wing halves can be adjusted about a common transverse axis and one longitudinal axis
- Tech classification: CPC B64C3/38 Adjustment of wings or parts of them
- Inventor location: Prag-Weinberge, a district in Prague, Czechia[1]
Sources
- Original patent document and Bibliographic info at DPMA
- Original patent document and bibliography entry at espacenet
- Archive record of this patent at Lilienthal museum patents
| Year filed | 1913 |
|---|---|
| Year granted | 1915 |
| Office | DE |
| Patent number | 281533 |
| Inventors | Adolf Linhart |
| Inventor country | CZ, AH |
| Applicant person | Adolf Linhart |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Flugzeug dessen Tragflächenhälften um eine gemeinsame Querachse und je eine Längsachse verstellt werden können |
| English title | Aircraft with wing panels around a common transverse axis and with adjustable longitudinal axis |
| Tech fields | wings, control |
| Filing date | March 21, 1913 |
| Full specification filed date | |
| Application number | |
| Grant date | January 13, 1915 |
| Granted? | Yes |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | Yes |
| Serial number | |
| Patent agent | |
| Assigned to | |
| National tech categories | DE 77h.5 |
| IPCs | IPC B64C3/38 |
| CPCs | CPC B64C3/38 |
| Family year | 1913 |
| First filing? | Yes |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | |
| INPADOC family ID | |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 6 |
| Number of claims | 2 |
