Patent US-1910-1065263
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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
- Tech class: CPC B64C11/343: Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on the blades
- Inventor location: Dusseldorf, Germany ; citizen of German empire ; signed this document at Barmen
Inventor signed on 1910-01-03. 15 days later, this patent was recorded as filed at the patent office.
Sources
- Patent 1065263 document and bibliographic info on espacenet
- Patent 1065263 at google patents
Year filed | 1910 |
---|---|
Year granted | 1913 |
Office | US |
Patent number | 1065263 |
Inventors | Gustav Mees |
Inventor country | DE |
Inventor location | Düsseldorf |
Applicant person | Gustav Mees |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
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? | 1 |
Publication date | |
Supplementary to patent | |
Related to aircraft? | 1 |
Serial number | 538686 |
Patent agent | |
Assigned to | |
National tech categories | USPC 416/136, USPC 416/195, USPC 416/164, USPC 244/79 |
IPCs | |
CPCs | CPC B64C11/343 |
Family year | 1910 |
First filing? | 1 |
Cites these patents | |
Citations from after 1930 | 1 |
Application ID | 47583521 |
INPADOC family ID | 43917313 |
Number of text pages | 3 |
Number of diagram pages | 2 |
Number of figures | 7 |
Number of claims | 2 |