AT68947B - Sighting device for projectile launching devices in aircraft (in particular aircraft). - Google Patents

Sighting device for projectile launching devices in aircraft (in particular aircraft).

Info

Publication number
AT68947B
AT68947B AT68947DA AT68947B AT 68947 B AT68947 B AT 68947B AT 68947D A AT68947D A AT 68947DA AT 68947 B AT68947 B AT 68947B
Authority
AT
Austria
Prior art keywords
aircraft
sighting device
projectile launching
launching devices
flight altitude
Prior art date
Application number
Other languages
German (de)
Original Assignee
Krupp Ag
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Krupp Ag filed Critical Krupp Ag
Application granted granted Critical
Publication of AT68947B publication Critical patent/AT68947B/en

Links

Landscapes

  • Traffic Control Systems (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

  

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Ohne dass am Wesen der Erfindung etwas geändert würde, könnte die Kurvenschar i1 auch durch eine   Xurvensebar   ersetzt werden, bei der jeder einzelnen Kurve eine konstante Flughöhe   eNtspricht nod   von den beiden Koordinaten eines Kurvenpunktes die in   ac¯ler Richtung   
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**WARNUNG** Ende DESC Feld kannt Anfang CLMS uberlappen**.



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Without changing anything in the essence of the invention, the family of curves i1 could also be replaced by a Xurvensebar, in which each individual curve corresponds to a constant flight altitude, nod of the two coordinates of a curve point, the one in the ac¯ler direction
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** WARNING ** End of DESC field may overlap beginning of CLMS **.

Claims (1)

scharen bilden, von denen die eine (i1) die Beziehungen zwischen der Flughöhe, der Zeit, die zum Durchfahren einer der Flughöhe proportionalen wagerechten Strecke erforderlich ist, und dem Wurfwinkel in der Weise graphisch darstellt, dass jeder Kurve ein konstanter Wert einer der beiden erstgenannten Grössen entspricht und die Koordinaten jeder Kurve den Wurfwmkel EMI4.3 **WARNUNG** Ende CLMS Feld Kannt Anfang DESC uberlappen**. form groups, of which one (i1) shows the relationships between the flight altitude, the time required to travel a horizontal distance proportional to the flight altitude, and the throwing angle in such a way that each curve has a constant value of one of the first two Sizes and the coordinates of each curve correspond to the throwing angle EMI4.3 ** WARNING ** End of CLMS field may overlap beginning of DESC **.
AT68947D 1912-12-23 1913-11-26 Sighting device for projectile launching devices in aircraft (in particular aircraft). AT68947B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE68947X 1912-12-23

Publications (1)

Publication Number Publication Date
AT68947B true AT68947B (en) 1915-06-10

Family

ID=5634681

Family Applications (1)

Application Number Title Priority Date Filing Date
AT68947D AT68947B (en) 1912-12-23 1913-11-26 Sighting device for projectile launching devices in aircraft (in particular aircraft).

Country Status (1)

Country Link
AT (1) AT68947B (en)

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