Difference between revisions of "Patent AT-1911-59461"
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| − | Adjustment of design (maybe using a supplementary duct) to control the effects of the explosion used in the parachute launcher described in [[Patent AT- | + | Adjustment of design (maybe using a supplementary duct) to control the effects of the explosion used in the parachute launcher described in [[Patent AT-1911-59404]]. |
Inventor location: Baden near Vienna | Inventor location: Baden near Vienna | ||
| Line 13: | Line 13: | ||
|Inventors=Adolf Freiherr Odkolek von Augezd | |Inventors=Adolf Freiherr Odkolek von Augezd | ||
|Inventor country=AT | |Inventor country=AT | ||
| − | |Applicant person= | + | |Applicant person=Adolf Freiherr Odkolek von Augezd |
|Applicant firm= | |Applicant firm= | ||
|Applicant type=INDIV | |Applicant type=INDIV | ||
| Line 19: | Line 19: | ||
|Original title=Vorrichtung zur Aufhebung des Rückstoßes bei Vorrichtung zum Abschleudern von Fallschirmen | |Original title=Vorrichtung zur Aufhebung des Rückstoßes bei Vorrichtung zum Abschleudern von Fallschirmen | ||
|English title=Neutralization recoil in the apparatus for launching parachutes | |English title=Neutralization recoil in the apparatus for launching parachutes | ||
| − | |Tech field= | + | |Tech field=parachutes; safety; stability |
| − | |Filing date= | + | |Filing date=1911-11-04 |
|Full specification filed date= | |Full specification filed date= | ||
|Application number= | |Application number= | ||
| − | |Grant date= | + | |Grant date=1913-01-15 |
|Granted=1 | |Granted=1 | ||
| − | |Publication date= | + | |Publication date=1913-06-10 |
| − | |Supplementary to patent=Patent AT- | + | |Supplementary to patent=Patent AT-1911-59404 |
|Related to aircraft=1 | |Related to aircraft=1 | ||
|Serial number= | |Serial number= | ||
| Line 34: | Line 34: | ||
|IPCs= | |IPCs= | ||
|CPCs= | |CPCs= | ||
| − | |Family year= | + | |Family year=1911 |
|First filing= | |First filing= | ||
| − | | | + | |Citations from after 1930= |
| − | | | + | |Cites these patents= |
|Application ID= | |Application ID= | ||
|INPADOC family ID= | |INPADOC family ID= | ||
Latest revision as of 21:02, 19 February 2021
Adjustment of design (maybe using a supplementary duct) to control the effects of the explosion used in the parachute launcher described in Patent AT-1911-59404.
Inventor location: Baden near Vienna
Sources
- Original patent document and Bibliographic info on this patent at DPMA
- Original patent document and bibliography entry on espacenet
| Year filed | 1911 |
|---|---|
| Year granted | 1913 |
| Office | AT |
| Patent number | 59461 |
| Inventors | Adolf Freiherr Odkolek von Augezd |
| Inventor country | AT |
| Applicant person | Adolf Freiherr Odkolek von Augezd |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Vorrichtung zur Aufhebung des Rückstoßes bei Vorrichtung zum Abschleudern von Fallschirmen |
| English title | Neutralization recoil in the apparatus for launching parachutes |
| Tech fields | parachutes, safety, stability |
| Filing date | 1911-11-04 |
| Full specification filed date | |
| Application number | |
| Grant date | 1913-01-15 |
| Granted? | 1 |
| Publication date | 1913-06-10 |
| Supplementary to patent | Patent AT-1911-59404 |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | |
| Assigned to | |
| National tech categories | AT 77d |
| IPCs | |
| CPCs | |
| Family year | 1911 |
| First filing? | |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | |
| INPADOC family ID | |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 1 |
| Number of claims | 3 |
