Systems, devices, and methods including a wing panel; a spar disposed in the wing panel, where the spar comprises: an upper cap; a lower cap; a honeycomb core connected between at least a portion of the upper cap and the lower cap; an inner face sheet; and an outer face sheet, where at least a portion of the honeycomb core is disposed between the inner face sheet and the outer face sheet.
HONEYCOMB CORE FOR A SPAR OF AN UNMANNED AERIAL VEHICLE
WABENKERN FÜR EINEN HOLM EINES UNBEMANNTEN LUFTFAHRZEUGS
NOYAU EN NID D'ABEILLES POUR LONGERON D'UN VÉHICULE AÉRIEN SANS PILOTE
29.01.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
HONEYCOMB CORE FOR A SPAR OF AN UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2023
|Honeycomb core for a spar of an unmanned aerial vehicle
Europäisches Patentamt | 2023
|HONEYCOMB CORE FOR A SPAR OF AN UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2021
|Unmanned aerial vehicle deployment box and unmanned aerial vehicle honeycomb system
Europäisches Patentamt | 2024
|TRAILING EDGE SPAR CONNECTION FOR AN UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2021
|