Patent US-1917-1355738
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- Tech class: CPC B64C3/00 Wings ; CPC Y10T403/29: Rotarily connected, differentially translatable members, e.g., turn-buckle, etc.
- Inventor location: Buffalo, NY
Sources
- Patent 1355738 document and bibliographic info on espacenet
- Patent 1355738 at google patents
| Year filed | 1917 |
|---|---|
| Year granted | 1920 |
| Office | US |
| Patent number | 1355738 |
| Inventors | Nelson W. Dalton |
| Inventor country | US |
| Inventor location | |
| Applicant person | Nelson W. Dalton |
| Applicant firm | Curtiss Aeroplane |
| Applicant type | COMPANY+INDIV |
| Applicant is inventor? | 0 |
| Original title | Aeroplane-wing structure |
| English title | Aeroplane-wing structure |
| Tech fields | |
| Filing date | 1917-11-10 |
| Full specification filed date | |
| Application number | 20136217 |
| Grant date | 1920-10-12 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | 201362 |
| Patent agent | John P. Tarbox |
| Assigned to | |
| National tech categories | |
| IPCs | IPC B64C3/00 |
| CPCs | CPC B64C2700/6235, CPC B64C3/00, CPC Y10T403/29 |
| Family year | 1917 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | 0 |
| Application ID | 48609743 |
| INPADOC family ID | 44303974 |
| Number of text pages | 5 |
| Number of diagram pages | 3 |
| Number of figures | 16 |
| Number of claims | 16 |
