Patent US-1917-1431520
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"One of the many features of the complete system is that all the members which transmit stresses to a given point in each truss an integral at such a point, thus developing the full strength of the members with a minimum weight of metal."
Sources
- Patent 1431520 document and bibliographic info on espacenet
- Patent 1431520 at google patents
Year filed | 1917 |
---|---|
Year granted | 1922 |
Office | US |
Patent number | 1431520 |
Inventors | Charles Ward Hall |
Inventor country | US |
Inventor location | Larchmont, Larchmont, NY, Westchester county, New York state |
Applicant person | Charles Ward Hall |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
Original title | Aeroplane |
English title | Aeroplane |
Tech fields | airplane, design, metal, frame, fuselage, construction, stability |
Filing date | 1917-10-24 |
Full specification filed date | |
Application number | 19820917 |
Grant date | 1922-10-10 |
Granted? | 1 |
Publication date | |
Supplementary to patent | |
Related to aircraft? | 1 |
Serial number | 198209 |
Patent agent | William B. Whitney |
Assigned to | |
National tech categories | |
IPCs | |
CPCs | CPC B64C2700/6233, CPC B64C3/00 |
Family year | 1917 |
First filing? | 1 |
Cites these patents | |
Citations from after 1930 | |
Application ID | 48584273 |
INPADOC family ID | 44136857 |
Number of text pages | 11 |
Number of diagram pages | 5 |
Number of figures | 23 |
Number of claims | 77 |