Patent GB-1913-10605
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Reference is made on this original to German filing priority date 1912-05-04.
This seems to be in keeping with this inventor's manner of achieving automatic airplane stability by way of using aerodynamic principles, more particularly the play and pressure of wind resistance on wing-like surfaces at the front of the aircraft, to engage immediately with springs which pull cables ultimately also involving pulleys, pistons; and gaskets. This all affects a rudder of stability.
Sources
- Original patent document and bibliography entry on espacenet
- on google patents
- Inventor location: Burgdorf, self-described as having no fixed abode. He is a book-binder, turned aviator.
Year filed | 1913 |
---|---|
Year granted | 1913 |
Office | GB |
Patent number | 10605 |
Inventors | Otto Albin Budig |
Inventor country | DE |
Applicant person | Otto Albin Budig |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Improvements in Stabilizing Apparatus for Aeroplanes |
English title | Automatic airplane stability achieved by way of wind resistance on a proper surface ultimately effecting the operation of a rudder of stability |
Tech fields | stability, airplane, biplane, frame, construction, design, aerodynamics, springs, equilibrium, rudder, cables, automatic stability, pulleys, pistons |
Filing date | 1913/05/05 |
Full specification filed date | 1913/05/05 |
Application number | 191310605D |
Grant date | 1913/06/05 |
Granted? | Yes |
Publication date | |
Supplementary to patent | Patent DE-1912-05-04 Otto Albin Budig |
Related to aircraft? | Yes |
Serial number | |
Patent agent | Herbert Haddan & Co. |
Assigned to | |
National tech categories | |
IPCs | IPC B64C1/00, IPC B64C17/00 |
CPCs | CPC B64C2700/6218, CPC B64C17/00 |
Family year | 1912 |
First filing? | No |
Cites these patents | |
Citations from after 1930 | |
Application ID | 23650767 |
INPADOC family ID | 11136594 |
Number of text pages | 2 |
Number of diagram pages | 1 |
Number of figures | 2 |
Number of claims | 2 |