Patent US-1911-1039181
Jump to navigation
Jump to search
- Tech class: CPC B64C1/00: Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like; CPC G05D1/0061: Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
- Inventor location: Washington, DC (FIPSloc=11001) (imputed by HistPat)
Sources
- Patent 1039181 document and bibliographic info on espacenet
- Patent 1039181 at google patents
Year filed | 1911 |
---|---|
Year granted | 1912 |
Office | US |
Patent number | 1039181 |
Inventors | Roy M. Palmer |
Inventor country | US |
Inventor location | Washington DC |
Applicant person | Roy M. Palmer |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
Original title | Aerostructural balance |
English title | Aerostructural balance |
Tech fields | balance |
Filing date | 1911-06-16 |
Full specification filed date | |
Application number | 1911633468 |
Grant date | 1912-09-24 |
Granted? | 1 |
Publication date | |
Supplementary to patent | |
Related to aircraft? | 1 |
Serial number | 633468 |
Patent agent | Harry Ellis Chandler |
Assigned to | |
National tech categories | USPC 244/177 |
IPCs | |
CPCs | CPC B64C1/00, CPC G05D1/0061 |
Family year | 1911 |
First filing? | 1 |
Cites these patents | |
Citations from after 1930 | 0 |
Application ID | 47538844 |
INPADOC family ID | 43968063 |
Number of text pages | 2 |
Number of diagram pages | 2 |
Number of figures | 5 |
Number of claims | 4 |