Patent US-1910-982402
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Front of projectile has conical concavity; spiral within; cutting edge
- Inventor location: Dayton, Hamilton county, OH (FIPSloc=39061), Montgomery county, OH (FIPSloc=39113), (imputed by HistPat)
- Tech class: CPC F42B10/30 Stabilising arrangements using spin induced by gas action using rocket motor nozzles
- Witnesses as shown on the diagram pages W. A. W. Williams and K. E. Klein
- Witnesses as shown on the final text page: Mason Crable and Wellmore B. Turner
Sources
- Patent 982402 document and bibliographic info on espacenet
- Patent 982402 at google patents
Year filed | 1910 |
---|---|
Year granted | 1911 |
Office | US |
Patent number | 982402 |
Inventors | George E. Wells |
Inventor country | US |
Inventor location | |
Applicant person | George E. Wells |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Projectile |
English title | Projectile |
Tech fields | military, projectile |
Filing date | 1910/05/28 |
Full specification filed date | |
Application number | |
Grant date | 1911/01/24 |
Granted? | Yes |
Publication date | |
Supplementary to patent | |
Related to aircraft? | 0.5 |
Serial number | 563949 |
Patent agent | Dudley Browne & Phelps |
Assigned to | |
National tech categories | USPC 244/3.23 |
IPCs | |
CPCs | CPC F42B10/30 |
Family year | 1910 |
First filing? | Yes |
Cites these patents | |
Citations from after 1930 | 3 |
Application ID | |
INPADOC family ID | |
Number of text pages | 2 |
Number of diagram pages | 1 |
Number of figures | 2 |
Number of claims | 7 |