Patent GB-1910-10816
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This was a heavier-than-air craft with innovation pertinent to lift, with wings improved by way of electrification. It had to do with efficiency, and greater lifting power.
- "Applicant has discovered that by electrifying the planes of an aeroplane it is possible to sustain a heavier weight other conditions being equal.
- "The theory of this is not known definitely but application is of the opinion that it may be due to a local increase in the density or the viscosity of the air produced by the electrification . . . "
- Inventor location: Brant Rock, Massachusetts
- Still to identify: which one is the parent of this particular patent
- Note extraordinarily brief period between filing and grant ; possibly this was an established inventor and it had been accepted already in the U.S. so they just scooted it through.
Sources
- Original patent document and bibliography entry on espacenet
- Neilson, 1910, Aeroplane Patents, p79
Year filed | 1909 |
---|---|
Year granted | 1910 |
Office | GB |
Patent number | 10816 |
Inventors | Reginald Aubrey Fessenden |
Inventor country | US |
Applicant person | Reginald Aubrey Fessenden |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
Original title | Improvements in Flying Machines |
English title | Electric-powered wings for flying machines |
Tech fields | wings, airplane |
Filing date | May 2, 1910 |
Full specification filed date | |
Application number | 191010816D |
Grant date | May 19, 1910 |
Granted? | 1 |
Publication date | |
Supplementary to patent | Patent US-1909-11-01 |
Related to aircraft? | 1 |
Serial number | |
Patent agent | |
Assigned to | |
National tech categories | |
IPCs | IPC B64C21/10, IPC B64C23/00 |
CPCs | CPC B64C23/00, CPC B64C23/005, CPC B64C21/10, CPC Y02T50/166 |
Family year | 1909 |
First filing? | 1 |
Cites these patents | |
Citations from after 1930 | |
Application ID | 23599007 |
INPADOC family ID | 11091949 |
Number of text pages | 1 |
Number of diagram pages | 1 |
Number of figures | 1 |
Number of claims | 1 |