Patent US-1917-1290004
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Per Underwood's list of adjudicated patents (1922, p. 120) this patent was adjudicated with result "not infringed", (C.C.A. 2nd Cir., 266, F. 71) — this is Curtiss Aeroplane & Motor Corporation v. United Aircraft Engineering Corporation and covers a number of patents.
- Inventor location (imputed from HistPat): Buffalo, NY, USA
Sources
- Patent 1290004 document and bibliographic info on espacenet
- Patent 1290004 at google patents
- Original via Espacenet
Year filed | 1917 |
---|---|
Year granted | 1918 |
Office | US |
Patent number | 1290004 |
Inventors | Paul G. Zimmermann |
Inventor country | US |
Inventor location | |
Applicant person | Paul G. Zimmermann |
Applicant firm | Curtiss Aeroplane |
Applicant type | COMPANY + INDIV |
Applicant is inventor? | Yes |
Original title | Aeroplane-fitting |
English title | Aeroplane-fitting |
Tech fields | airplane, construction, fuselage, landing, adjudicated, Curtiss Aeroplane & Motor Corporation v. United Aircraft Engineering Corporation |
Filing date | May 14, 1917 |
Full specification filed date | |
Application number | 16858817 |
Grant date | December 31, 1918 |
Granted? | Yes |
Publication date | |
Supplementary to patent | |
Related to aircraft? | Yes |
Serial number | 168588 |
Patent agent | |
Assigned to | Curtiss Aeroplane |
National tech categories | |
IPCs | |
CPCs | CPC B64C1/26 |
Family year | 1917 |
First filing? | Yes |
Cites these patents | |
Citations from after 1930 | |
Application ID | 47975842 |
INPADOC family ID | 43430956 |
Number of text pages | 2 |
Number of diagram pages | 1 |
Number of figures | 4 |
Number of claims | 6 |