A detachable connecting arrangement for fitting launchable external loads to an aircraft, having a hook-like connecting element fitted to the external load and a holding element fitted to the aircraft for the hook-like connecting element. The hook-like connecting element includes a lower supporting surface and an upper supporting surface. The holding element has a first opposing supporting surface that interacts with the lower supporting surface, and a second, upper opposing supporting surface that interacts with the upper supporting surface. The lower supporting surface and the first opposing supporting surface are designed to support mass forces of the external load directed away from the aircraft, and the upper supporting surface and the upper opposing supporting surface are designed to support mass forces of the external load directed towards the aircraft.
Detachable connecting arrangement for fitting launchable external loads to an aircraft
08.08.2017
Patent
Elektronische Ressource
Englisch
IPC: | F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16G Riemen, Kabel oder Seile, vorwiegend für Antriebszwecke , BELTS, CABLES, OR ROPES, PREDOMINANTLY USED FOR DRIVING PURPOSES |
Launchable and Retrievable Tetherobot
NTRS | 2010
|Launchable and retrievable tetherbot exploration system
SPIE | 2008
|Device for Handling a Water-Launchable Missile
NTIS | 1965
|