A device for absorbing energy by compression including several first conduits spaced apart from one another and oriented in a compression direction and joining walls which are parallel to the compression direction and connect the first conduits so as to delimit, with the latter, at least one second conduit. This solution makes it possible to absorb a greater quantity of energy. An aircraft including at least one such device for absorbing energy is also disclosed.
DEVICE FOR ABSORBING ENERGY BY COMPRESSION, AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICE
2025-06-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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