Vorrichtung zum Prüfen der Dynamischen Belastung von Flugzeugstrukturen
Anmelder: Airbus Operations Limited 🇬🇧
Details
- Veröffentlichungs-Nr.
- EP4082919
- Aktenzeichen
- EP22169612
- Anmeldetag
- 25. April 2022
- Veröffentlichung
- 18. Februar 2026
- Erteilung
- 18. Februar 2026
- Rechtsraum
- EP
- IPC
- B64F5/60
Abstract
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.
Anmelder
- Firma
- Airbus Operations Limited
- Land
- 🇬🇧 Großbritannien
Deutsche Tochtergesellschaft des europäischen Luft- und Raumfahrtkonzerns Airbus mit Standorten wie Hamburg. Entwickelt und fertigt Flugzeugstrukturen und Komponenten für die zivile Luftfahrt.
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Fachgebiete
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Teesdale, Emily Catherine
Airbus Operations Limited · London