Patent US-1916-1222140
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- Tech class CPC B64C1/06: Frames; Stringers; Longerons ; Fuselage sections ; CPC B64C2001/0081: Fuselage structures substantially made from particular materials from metallic materials
- Inventor location: Grinnell, Iowa
Sources
- Patent 1222140 document and bibliographic info on espacenet
- Patent 1222140 at google patents
| Year filed | 1916 |
|---|---|
| Year granted | 1917 |
| Office | US |
| Patent number | 1222140 |
| Inventors | William C. Robinson |
| Inventor country | US |
| Inventor location | Iowa |
| Applicant person | William C. Robinson |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Aeroplane-fuselage structure |
| English title | Aeroplane-fuselage structure |
| Tech fields | fuselage |
| Filing date | 1916-03-27 |
| Full specification filed date | |
| Application number | 8711516 |
| Grant date | 1917-04-10 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | 87115 |
| Patent agent | Orvig & Bair |
| Assigned to | |
| National tech categories | |
| IPCs | |
| CPCs | CPC B64C2001/0081, CPC B64C1/06 |
| Family year | 1916 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | 3 |
| Application ID | 47855075 |
| INPADOC family ID | 47202426 |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 5 |
| Number of claims | 3 |
