Patent US-1913-1065263
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Helicopter for aeroplanes ; adjustable blades ; wheel-rim which acts as gyroscope ; stabilizes the aeroplane and also as a fly-wheel for accumulating energy from the motor ; pilot can immediately jerk airplane up if needed ; VTOL
claims: hollow shaft with spokes radiating from it and blades rotating on all sides, rings or bearings and springs, sleeve on the shaft slides and is controlled by the pilot
Inventor location (imputed by HistPat): Dusseldorf, Germany ; citizen of German empire
Sources
- Patent 1065263 document and bibliographic info on espacenet
- Patent 1065263 at google patents
Year filed | 1910 |
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Year granted | 1913 |
Office | US |
Patent number | 1065263 |
Inventors | Gustav Mees |
Inventor country | DE |
Applicant person | Gustav Mees |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Aeroplane steering and stabilizing mechanism |
English title | Aeroplane steering and stabilizing mechanism |
Tech fields | propulsion, control, gyroscope, helicopter |
Filing date | January 18, 1910 |
Full specification filed date | |
Application number | 1910538686 |
Grant date | June 17, 1913 |
Granted? | Yes |
Publication date | |
Supplementary to patent | |
Related to aircraft? | Yes |
Serial number | 538686 |
Patent agent | |
Assigned to | |
National tech categories | USPC 416/136, USPC 416/195, USPC 416/164, USPC 244/79 |
IPCs | IPC B64C11/343 |
CPCs | CPC B64C11/343 |
Family year | 1910 |
First filing? | Yes |
Cites these patents | |
Citations from after 1930 | |
Application ID | 47583521 |
INPADOC family ID | 43917313 |
Number of text pages | |
Number of diagram pages | |
Number of figures | |
Number of claims |