Difference between revisions of "Patent GB-1911-3882"
Jump to navigation
Jump to search
m (Text replacement - "/06 B64" to "/06; CPC B64") |
AvionHerbert (talk | contribs) |
||
(5 intermediate revisions by one other user not shown) | |||
Line 1: | Line 1: | ||
+ | This original makes reference to an a priori German filing date 1910-03-05. | ||
+ | |||
+ | This original, within the text, associates these innovations with those earlier described in [[Patent GB-1910-25749]]. | ||
+ | |||
+ | === Sources === | ||
+ | * {{esp|GB|191103882A}} | ||
+ | * Inventor location: Wilhelmstrasse 20, Ronsdorf, Empire of Germany, formerly 143 Kantstrasse, Charlottenburg, Empire of Germany | ||
+ | * Inventor occupation: Engineer | ||
{{Patent | {{Patent | ||
|Year filed=1911 | |Year filed=1911 | ||
Line 4: | Line 12: | ||
|Office=GB | |Office=GB | ||
|Patent number=3882 | |Patent number=3882 | ||
− | |Inventors=Gustav | + | |Inventors=Gustav Mees |
|Inventor country=DE | |Inventor country=DE | ||
− | |Applicant person= | + | |Applicant person=Gustav Mees |
|Applicant type=INDIV | |Applicant type=INDIV | ||
− | |Applicant is inventor= | + | |Applicant is inventor=Yes |
− | |Filing date=1911 | + | |Original title=A Method of and Means for Automatically Stabilizing Flying Machines in the Event of Failure of the Motor |
+ | |English title=A Method of and Means for Automatically Stabilizing Flying Machines in the Event of Failure of the Motor | ||
+ | |Tech field=stability; equilibrium | ||
+ | |Filing date=1911/02/15 | ||
+ | |Full specification filed date=1911/02/15 | ||
|Application number=191103882D | |Application number=191103882D | ||
− | |Granted= | + | |Grant date=1911/08/10 |
+ | |Granted=Yes | ||
+ | |Publication date=1911/08/10 | ||
+ | |Supplementary to patent=Patent DE-1910-03-05 Gustav Mees; Patent GB-1910-25749 | ||
+ | |Related to aircraft=Yes | ||
+ | |Patent agent=Herbert Haddan & Co. | ||
+ | |IPCs=IPC B64C1/00; IPC B64C17/06 | ||
|CPCs=CPC B64C17/06; CPC B64C2700/6216 | |CPCs=CPC B64C17/06; CPC B64C2700/6216 | ||
|Family year=1909 | |Family year=1909 | ||
− | |First filing= | + | |First filing=Yes |
|Application ID=23612331 | |Application ID=23612331 | ||
|INPADOC family ID=5907232 | |INPADOC family ID=5907232 | ||
+ | |Number of text pages=3 | ||
+ | |Number of diagram pages=1 | ||
+ | |Number of figures=1 | ||
+ | |Number of claims=2 | ||
}} | }} | ||
− | |||
− |
Latest revision as of 11:09, 25 November 2022
This original makes reference to an a priori German filing date 1910-03-05.
This original, within the text, associates these innovations with those earlier described in Patent GB-1910-25749.
Sources
- Original patent document and bibliography entry on espacenet
- Inventor location: Wilhelmstrasse 20, Ronsdorf, Empire of Germany, formerly 143 Kantstrasse, Charlottenburg, Empire of Germany
- Inventor occupation: Engineer
Year filed | 1911 |
---|---|
Year granted | 1911 |
Office | GB |
Patent number | 3882 |
Inventors | Gustav Mees |
Inventor country | DE |
Applicant person | Gustav Mees |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | A Method of and Means for Automatically Stabilizing Flying Machines in the Event of Failure of the Motor |
English title | A Method of and Means for Automatically Stabilizing Flying Machines in the Event of Failure of the Motor |
Tech fields | stability, equilibrium |
Filing date | 1911/02/15 |
Full specification filed date | 1911/02/15 |
Application number | 191103882D |
Grant date | 1911/08/10 |
Granted? | Yes |
Publication date | 1911/08/10 |
Supplementary to patent | Patent DE-1910-03-05 Gustav Mees, Patent GB-1910-25749 |
Related to aircraft? | Yes |
Serial number | |
Patent agent | Herbert Haddan & Co. |
Assigned to | |
National tech categories | |
IPCs | IPC B64C1/00, IPC B64C17/06 |
CPCs | CPC B64C17/06, CPC B64C2700/6216 |
Family year | 1909 |
First filing? | Yes |
Cites these patents | |
Citations from after 1930 | |
Application ID | 23612331 |
INPADOC family ID | 5907232 |
Number of text pages | 3 |
Number of diagram pages | 1 |
Number of figures | 1 |
Number of claims | 2 |