Patent US-1910-1171075
Jump to navigation
Jump to search
This invention relates to flying machines with aeroplanes.
Objectives of this invention:
- to Construct a flying machine which will have maximum strength and stability with minimum weight of material, and which will have a low wind resistance with maximum lifting power.
- to so construct and position the parts as to prevent interference of the moving parts of the machine, that is the propeller-and controlling devices, with each other and with the frame.
- to so distribute the component parts and the power plant that the center of gravity will be near the drivers seat.
- to arrange the driving means and the power plant in a novel manner and to construct a novel form of power plant.
- to provide balancing means which will be automatic in its operation . . . compensating means which will compensate against lateral wind pressure.
- to provide the rudder or controlling plane or planes with a novel form of controlling or operating means and to make the connection in such a . . . .
- Taylor's location: Farmingdale, Long Island, New York, US, and US citizen
- Neuberger's location: New York, New York, US
- Witnesses: J. H. Bruninga and J. A. Watson
Regarding administrative culture, and American particularities, and our own fields of data entry, Taylor, is the "assignor to" Neuberger (which isn't identical to "assigned to"), on the original document. It is the bibliographic data which gives us Taylor, definitely, as the inventor, with Neuberger, definitely, as the applicant.
Sources
- Patent 1171075 document and bibliographic info on espacenet
- Patent 1171075 at google patents
| Year filed | 1910 |
|---|---|
| Year granted | 1916 |
| Office | US |
| Patent number | 1171075 |
| Inventors | Edwin Taylor |
| Inventor country | US |
| Applicant person | David M. Neuberger |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | No |
| Original title | Flying-Machine |
| English title | Flying-Machine |
| Tech fields | Airplane, Wings, Incidence, Stability, Automatic stability, Hybrid, Helicopter, Frame, Propellers |
| Filing date | 1910/08/22 |
| Full specification filed date | |
| Application number | 1910578324 |
| Grant date | 1916/02/08 |
| Granted? | Yes |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | Yes |
| Serial number | 578324 |
| Patent agent | |
| Assigned to | |
| National tech categories | USPC 244/226 |
| IPCs | |
| CPCs | CPC B64C13/00 |
| Family year | 1910 |
| First filing? | Yes |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 47765584 |
| INPADOC family ID | 43938407 |
| Number of text pages | 7 |
| Number of diagram pages | 4 |
| Number of figures | 6 |
| Number of claims |
