Patent US-1910-989681
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Adjustable mast and aeroplanes; ball sockets for mast, planes & rudder; upper plane rotates at high speed, thus 'acting as a gyroscope'
- Tech class CPC B64C39/005 Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
- Inventor location: Smithville, Clay county, MO (FIPSloc=29047, imputed by HistPat)
Sources
- Patent 989681 document and bibliographic info on espacenet
- Patent 989681 at google patents
Year filed | 1910 |
---|---|
Year granted | 1911 |
Office | US |
Patent number | 989681 |
Inventors | Phineas S. Woods |
Inventor country | US |
Applicant person | Phineas S. Woods |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
Original title | Aeroplane |
English title | Aeroplane |
Tech fields | Airplane, frame, wheels, propeller, car, takeoff, landing, stability, parachute, rudder |
Filing date | 1910-04-11 |
Full specification filed date | |
Application number | 1910554619 |
Grant date | 1911-04-18 |
Granted? | 1 |
Publication date | |
Supplementary to patent | |
Related to aircraft? | 1 |
Serial number | 554619 |
Patent agent | Arthur Brown |
Assigned to | |
National tech categories | USPC 244/66 |
IPCs | |
CPCs | CPC B64C39/005 |
Family year | 1910 |
First filing? | 1 |
Cites these patents | |
Citations from after 1930 | 1 |
Application ID | |
INPADOC family ID | |
Number of text pages | 3 |
Number of diagram pages | 2 |
Number of figures | 5 |
Number of claims | 9 |