The invention provides an aircraft structure dynamic loading testing device, including a nozzle 141, 142, an attachment mechanism comprising a first portion 124 attached to the nozzle such that a nozzle force direction 141c is constrained at a set orientation and a second portion 125 for attaching to the aircraft structure 110 and configured to be constrained at a given orientation with respect to the aircraft structure, and a length of conduit 121, 123, wherein, in use, fluid is supplied along the length of conduit to the nozzle and ejected from the nozzle such that the nozzle exerts a dynamic force on the aircraft structure in the direction of the nozzle force direction. The invention also provides a dynamic loading testing device, a kit of parts and methods of dynamic load testing of a structure.
AN AIRCRAFT STRUCTURE DYNAMIC LOADING TESTING DEVICE
VORRICHTUNG ZUM PRÜFEN DER DYNAMISCHEN BELASTUNG VON FLUGZEUGSTRUKTUREN
DISPOSITIF DE TEST DE CHARGEMENT DYNAMIQUE DE STRUCTURE D'AÉRONEF
2022-11-02
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Loading systems for aircraft structural testing
Tema Archive | 1976
|Dynamic Loading of Aircraft Structures
British Library Conference Proceedings | 2013
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