Patent CA-1911-136795
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File:CA 136795 figs.png
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Hybrid airplane-LTA design intended to improve stability and safety against disturbances, comprising
a longitudinal fuselage or frame work having a series of circular hoops connected thereto, a gas bag contained within the said fuselage, a frame work below the same, super-posed main planes connected to the said framework, a further supplemental frame work below the aforesaid frame work designed to contain the operator and provided with suitable running wheels and chassis, an elevating plane at the forward end of the fuselage and a suitable tail at the rear of the same composed of superposed planes and a vertical rudder
Inventor location: Toronto, Ontario, Canada
Sources
- Bibliographic info on this patent at CIPO
- Original patent document and bibliography entry on espacenet
- Patent CA136795 on google patents
| Year filed | 1911 |
|---|---|
| Year granted | 1911 |
| Office | CA |
| Patent number | 136795 |
| Inventors | Edwin Fisher |
| Inventor country | CA |
| Inventor location | Toronto, Ontario |
| Applicant person | |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Aeroplane; Aeroplane |
| English title | Aeroplane |
| Tech fields | hybrid, airplane, LTA, safety, stability, rudder, frame, wheels, passenger, chassis, balloon |
| Filing date | 1911-03-06 |
| Full specification filed date | |
| Application number | |
| Grant date | 1911-11-14 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | |
| Assigned to | |
| National tech categories | CA 244/4 |
| IPCs | |
| CPCs | |
| Family year | |
| First filing? | |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | |
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| Number of text pages | 5 |
| Number of diagram pages | 1 |
| Number of figures | 2 |
| Number of claims | 4 |
