Difference between revisions of "Patent AT-1911-59461"

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m (AvionHerbert moved page Patent AT-1913-59461 to 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-1913-59404]].
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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-1911-59404]].
  
 
Inventor location: Baden near Vienna
 
Inventor location: Baden near Vienna
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|Granted=1
 
|Granted=1
 
|Publication date=1913-06-10
 
|Publication date=1913-06-10
|Supplementary to patent=Patent AT-1913-59404
+
|Supplementary to patent=Patent AT-1911-59404
 
|Related to aircraft=1
 
|Related to aircraft=1
 
|Serial number=
 
|Serial number=

Revision as of 17:14, 2 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


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