Patent US-1916-1209426
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"This application is a continuation of my earlier application, Serial No. 692,269, filed April 22, 1912." Aeroplane constructors have concentrated the heavy parts (motor, fuel+tank, aviator) into a compact space in the fuselage. Concentrating the mass this way makes it easier for gusts to buffet the craft. For longitudinal stability, split the mass into three separate places in a triangle shape when viewed from front or back. Patent does not offer further specifics. (Apparent error: Family year says 1916 but other columns say this is supplementary to a 1912 patent)
- Tech classification CPC B64C39/08: Aircraft not otherwise provided for having multiple wings
- Inventor location: Chicago, Cook county, IL (FIPSloc=17031 imputed by HistPat)
Sources
- Patent 1209426 document and bibliographic info on espacenet
- Patent 1209426 at google patents
| Year filed | 1916 |
|---|---|
| Year granted | 1916 |
| Office | US |
| Patent number | 1209426 |
| Inventors | Hyman Eli Goldberg |
| Inventor country | US |
| Inventor location | |
| Applicant person | Hyman Eli Goldberg |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Aeroplane |
| English title | Aeroplane |
| Tech fields | stability |
| Filing date | 1916-04-15 |
| Full specification filed date | |
| Application number | 9128916 |
| Grant date | 1916-12-19 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | Patent US-1912-692269 |
| Related to aircraft? | 1 |
| Serial number | 91289 |
| Patent agent | Walter M. Huller |
| Assigned to | |
| National tech categories | USPC 244/45R |
| IPCs | IPC B64C39/00 |
| CPCs | CPC B64C 39/08, CPC B64C2700/6295 |
| Family year | 1916 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | 1 |
| Application ID | 47832664 |
| INPADOC family ID | 47273055 |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 1 |
| Number of claims | 8 |
