Patent US-1912-1166488
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Streamlined body or nacelle ; undercarriage portion can move up or down ; lower section is attached to landing gear ; adjustments change aerodynamics ; can use lower section for hydroplaning ; may intend to use it for loading cargo or projectiles but I'm not seeing that.
- Inventor location: Washington, DC (FIPSloc=11001, imputed by HistPat)
- Tech class CPC B64C25/14 Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
- Witnesses as shown on the diagram pages: Louis R. Heinrichs and C. C. Hines
- Witnesses as shown on the final text page: C. C. Hines and Bennett Jones ; C. C. Hines appears on another occasion as a patent attorney for Smith.
Sources
- Patent 1166488 document and bibliographic info on espacenet
- Patent 1166488 at google patents
| Year filed | 1912 |
|---|---|
| Year granted | 1916 |
| Office | US |
| Patent number | 1166488 |
| Inventors | Rexford M. Smith |
| Inventor country | US |
| Inventor location | |
| Applicant person | Rexford M. Smith |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Aeroplane |
| English title | Aeroplane |
| Tech fields | fuselage, structure, nacelle, airplane, hydroplane, Hydro-aeroplane |
| Filing date | 1912/12/27 |
| Full specification filed date | |
| Application number | 1912738896 |
| Grant date | 1916/01/04 |
| Granted? | Yes |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | 738896 |
| Patent agent | |
| Assigned to | |
| National tech categories | USPC 244/102R, USPC 114/282 |
| IPCs | IPC B64C25/00 |
| CPCs | CPC B64C25/14 |
| Family year | 1912 |
| First filing? | Yes |
| Cites these patents | |
| Citations from after 1930 | 4 |
| Application ID | 47757597 |
| INPADOC family ID | 44023903 |
| Number of text pages | 4 |
| Number of diagram pages | 1 |
| Number of figures | 6 |
| Number of claims | 26 |
