Patent US-1918-1589780
Jump to navigation
Jump to search
Compound wing for aircraft, with wing panels staggered to promote lift.
As in Wragg's previous patent family, he states here that the invention could apply to LTA as well as HTA (but it's a bit of a stretch, as the concept relates directly to aviation, airfoil, lift, etc.).
- Note that this patent was administratively delayed for an unusually long time.
- Inventor location (imputed from HistPat): Melbourne, Victoria, Australia
Sources
- Patent 1589780 document and bibliographic info on espacenet
- Patent 1589780 at google patents
Year filed | 1918 |
---|---|
Year granted | 1926 |
Office | US |
Patent number | 1589780 |
Inventors | Charles Arthur Wragg |
Inventor country | AU |
Applicant person | Charles Arthur Wragg |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | 1 |
Original title | Flying machine |
English title | Flying machine |
Tech fields | flying machine, aerodynamics, airfoil, camber, lift, wing, speed, stability |
Filing date | 1918-11-27 |
Full specification filed date | |
Application number | 26436518 |
Grant date | 1926-06-22 |
Granted? | 1 |
Publication date | |
Supplementary to patent | |
Related to aircraft? | 1 |
Serial number | 264365 |
Patent agent | Davis & Davis |
Assigned to | |
National tech categories | |
IPCs | |
CPCs | CPC B64C21/08, CPC Y02T50/166 |
Family year | |
First filing? | |
Cites these patents | |
Citations from after 1930 | |
Application ID | 49125409 |
INPADOC family ID | 44658041 |
Number of text pages | 2 |
Number of diagram pages | 2 |
Number of figures | 8 |
Number of claims | 9 |