Difference between revisions of "Patent GB-1912-21604"
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| + | An aeroplane wing shaped by taut structural wires. | ||
| + | {{Patent family|Patent GB-1912-21604}} | ||
| + | === Sources === | ||
| + | * {{esp|GB|191221604A}} | ||
{{Patent | {{Patent | ||
|Year filed=1912 | |Year filed=1912 | ||
| Line 4: | Line 8: | ||
|Office=GB | |Office=GB | ||
|Patent number=21604 | |Patent number=21604 | ||
| − | |Inventors=Norman Arthur | + | |Inventors=Norman Arthur Thompson |
|Inventor country=GB | |Inventor country=GB | ||
| − | |Applicant person= | + | |Applicant person=Norman Arthur Thompson |
| + | |Applicant firm= | ||
|Applicant type=INDIV | |Applicant type=INDIV | ||
|Applicant is inventor=1 | |Applicant is inventor=1 | ||
| + | |Original title=Improvements in and relating to Aeroplane or like Structures | ||
| + | |English title=Improvements to aeroplanes and similar structures | ||
| + | |Tech field=aerofoil | ||
|Filing date=1912-09-23 | |Filing date=1912-09-23 | ||
| + | |Full specification filed date= | ||
|Application number=191221604D | |Application number=191221604D | ||
| − | |Granted= | + | |Grant date=1913-03-18 |
| + | |Granted=1 | ||
| + | |Publication date=1913-07-24 | ||
| + | |Supplementary to patent= | ||
| + | |Related to aircraft=1 | ||
| + | |Serial number= | ||
| + | |Patent agent=Marks & Clerk | ||
| + | |Assigned to= | ||
| + | |National tech categories=FR 6.4 | ||
| + | |IPCs=IPC B64C3/00 | ||
|CPCs=CPC B64C3/00; CPC B64C2700/6233 | |CPCs=CPC B64C3/00; CPC B64C2700/6233 | ||
|Family year=1912 | |Family year=1912 | ||
|First filing=1 | |First filing=1 | ||
| + | |Cites these patents= | ||
| + | |Citations from after 1930= | ||
|Application ID=23639594 | |Application ID=23639594 | ||
|INPADOC family ID=11127051 | |INPADOC family ID=11127051 | ||
| + | |Number of text pages=3 | ||
| + | |Number of diagram pages=1 | ||
| + | |Number of figures=5 | ||
| + | |Number of claims=4 | ||
}} | }} | ||
| − | |||
| − | |||
| − | |||
Latest revision as of 12:34, 20 October 2021
An aeroplane wing shaped by taut structural wires.
Patent family descending from Patent GB-1912-21604
- Patent GB-1912-21604 (English title: Improvements to aeroplanes and similar structures, National tech categories: FR 6.4)
- Patent FR-1914-462405 (English title: Improvements to aeroplanes and similar machines, Supplementary to patent: Patent GB-1912-21604, National tech categories: FR 6.4)
Sources
- Original patent document and bibliography entry on espacenet
| Year filed | 1912 |
|---|---|
| Year granted | 1912 |
| Office | GB |
| Patent number | 21604 |
| Inventors | Norman Arthur Thompson |
| Inventor country | GB |
| Applicant person | Norman Arthur Thompson |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Improvements in and relating to Aeroplane or like Structures |
| English title | Improvements to aeroplanes and similar structures |
| Tech fields | aerofoil |
| Filing date | 1912-09-23 |
| Full specification filed date | |
| Application number | 191221604D |
| Grant date | 1913-03-18 |
| Granted? | 1 |
| Publication date | 1913-07-24 |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | Marks & Clerk |
| Assigned to | |
| National tech categories | FR 6.4 |
| IPCs | IPC B64C3/00 |
| CPCs | CPC B64C3/00, CPC B64C2700/6233 |
| Family year | 1912 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 23639594 |
| INPADOC family ID | 11127051 |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 5 |
| Number of claims | 4 |
