A honeycomb structure including a first external side, a second external side, and an anti-friction agent buffer for receiving an anti-friction agent. An opening to an anti-friction agent inlet and an opening to an air outlet are present on the first external side. This honeycomb structure may be useful in an aircraft as part of a belly-landing system for the aircraft.
AIRCRAFT WITH BELLY-LANDING PROTECTION
2024-01-04
Patent
Electronic Resource
English
REMOTELY CONTROLLABLE AIRPLANE ADAPTED FOR BELLY-LANDING
European Patent Office | 2017
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