Patent US-1913-1054989
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Airplane with internal oscillating elements
- Tech class CPC B64C21/02: Influencing air-flow over aircraft surfaces by affecting boundary-layer flow by use of slot, ducts, porous areas, or the like
- Inventor location: Los Angeles, Los Angeles county, CA (FIPSloc=6037, imputed by HistPat)
- Schneider was a subject of Austria-Hungary, and Kurrell a subject of Germany
- inventors signed off on April 27 ; it's filed at USPO on May 4
Sources
- Patent 1054989 document and bibliographic info on espacenet
- Patent 1054989 at google patents
Year filed | 1912 |
---|---|
Year granted | 1913 |
Office | US |
Patent number | 1054989 |
Inventors | Heinrich Schneider, Theodor Kurrell |
Inventor country | US |
Applicant person | Heinrich Schneider, Theodor Kurrell |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
Original title | Aerial navigation |
English title | Aerial navigation |
Tech fields | airplane, frame, stability, airfoil, takeoff |
Filing date | 1912-05-04 |
Full specification filed date | |
Application number | 1912695294 |
Grant date | 1913-03-04 |
Granted? | 1 |
Publication date | |
Supplementary to patent | |
Related to aircraft? | 1 |
Serial number | 695294 |
Patent agent | Alex H. Lidders |
Assigned to | |
National tech categories | USPC 244/203 |
IPCs | |
CPCs | CPC B64C21/02 |
Family year | 1912 |
First filing? | 1 |
Cites these patents | |
Citations from after 1930 | 0 |
Application ID | |
INPADOC family ID | |
Number of text pages | 3 |
Number of diagram pages | 2 |
Number of figures | 6 |
Number of claims | 8 |