Page values for "Patent AT-1911-59836"
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"Patents" values
1 row is stored for this pageField | Field type | Allowed values | Value |
---|---|---|---|
Year_filed | Date | 1911 | |
Year_granted | Date | 1913 | |
Office | Page | AT | |
Patent_number | String | 59836 | |
Inventors | List of Page, delimiter: ; | Carlo Navaro | |
Inventor_country | List of Page, delimiter: ; | IT | |
Applicant_person | List of Page, delimiter: ; | Carlo Navaro | |
Applicant_type | List of String, delimiter: ; | INDIV | |
Applicant_is_inventor | Boolean | Yes | |
Original_title | String | Gleichgewichtsregler für Flugzeuge | |
English_title | String | Airplane balance controller | |
Tech_fields | List of Page, delimiter: ; | Airplane • Equilibrium • Aerodynamics • Frame • Stability • Control • Piloting • Subsystem • Pendulum • Automatic stability | |
Filing_date | Date | 1911-10-12 | |
Grant_date | Date | 1913-02-15 | |
Granted | Boolean | Yes | |
Publication_date | Date | 1913-06-25 | |
Supplementary_to_patent | List of Page, delimiter: ; | Patent AT-1911-59835 • Patent IT-1911-06-09 Carlo Navaro • Patent IT-1910-10-17 Carlo Navaro | |
National_tech_categories | List of Page, delimiter: ; | AT 77d | |
IPCs | List of Page, delimiter: ; | IPC H04N1/40 • IPC H04N1/405 | |
CPCs | List of Page, delimiter: ; | CPC H04N1/40 | |
Family_year | Date | 1910 | |
First_filing | Boolean | No | |
Number_of_text_pages | Integer | 4 | |
Number_of_claims | Integer | 5 | |
Number_of_diagram_pages | Integer | 1 | |
Number_of_figures | Integer | 8 |