AT79725B - Retaining strap for loads on impact airships. Retaining strap for loads on impact airships. - Google Patents

Retaining strap for loads on impact airships. Retaining strap for loads on impact airships.

Info

Publication number
AT79725B
AT79725B AT79725DA AT79725B AT 79725 B AT79725 B AT 79725B AT 79725D A AT79725D A AT 79725DA AT 79725 B AT79725 B AT 79725B
Authority
AT
Austria
Prior art keywords
loads
retaining strap
airships
impact
impact airships
Prior art date
Application number
Other languages
German (de)
Original Assignee
Luft Fahrzeug Ges M B H Luft F
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 Luft Fahrzeug Ges M B H Luft F filed Critical Luft Fahrzeug Ges M B H Luft F
Application granted granted Critical
Publication of AT79725B publication Critical patent/AT79725B/en

Links

Landscapes

  • Emergency Lowering Means (AREA)

Description

  

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 Wechsel der Richtung des Seiles. f zu rechnen, so kann, wie bei Fig. 2 punktiert gezeigt, die Anzahl der Seilschlingen vergrössert werden, ohne dass der Traggurt an der Hülle der Breite nach einen   grösseren   Raum beansprucht. Bei solchen Lasten, wo mit einem merklichen Wechsel der Seilrichtung nicht gerechnet zu werden braucht, würde eine Ausführungsform des Gurtes als einfache   bogenförmige   Führung für nur eine einzige Seilschlinge (nach Fig. i) genügen. 



   PATENT-ANSPRÜCHE   :     I.   Haltegurt für Lasten an Pralluftschiffen, dadurch gekennzeichnet, dass vom Knotenpunkt des Lastseiles eine Seilschlinge lose geführt durch den in Form einer Schlauchhülle in einem Kreisbogen am Tragkörper befestigten Gurt   verläuft, derart,   dass die Last in zwei gleich grosse Kräfte zerlegt wird, die ihrerseits am Bogenumfang eine kontinuierliche Belastung der Hülle   hervorrufen.  



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 Change the direction of the rope. f, then, as shown in dotted lines in FIG. 2, the number of rope loops can be increased without the carrying strap taking up a larger space on the casing width. In the case of loads where there is no need to reckon with a noticeable change in the direction of the rope, an embodiment of the belt as a simple curved guide would suffice for only a single rope loop (according to FIG. I).



   PATENT CLAIMS: I. Tether for loads on impact airships, characterized in that from the junction of the load rope a rope loop is loosely guided through the strap attached in the form of a hose sleeve in a circular arc to the supporting body, in such a way that the load is split into two equal forces which in turn cause a continuous load on the envelope at the arc circumference.

 

Claims (1)

2. Haltegurt nach Anspruch i, dadurch gekennzeichnet, dass sich das Lastseil im Knotenpunkt in zwei oder mehr Schlingen gabelt, die fächerförmig auseinandergehend in Kreisbögen am Gurtsaume verlaufen. 2. Retaining strap according to claim i, characterized in that the load rope forks at the junction into two or more loops which diverge in a fan shape in circular arcs on the belt hem.
AT79725D 1915-04-13 1916-04-08 Retaining strap for loads on impact airships. Retaining strap for loads on impact airships. AT79725B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE79725X 1915-04-13

Publications (1)

Publication Number Publication Date
AT79725B true AT79725B (en) 1920-01-10

Family

ID=5638777

Family Applications (1)

Application Number Title Priority Date Filing Date
AT79725D AT79725B (en) 1915-04-13 1916-04-08 Retaining strap for loads on impact airships. Retaining strap for loads on impact airships.

Country Status (1)

Country Link
AT (1) AT79725B (en)

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