Energy absorption stabilizers and methods

According to one implementation of the present disclosure, a stabilizer of an aircraft includes an energy absorbing assembly. The energy absorbing assembly includes first and second portions and a retractable section. The retractable section may be at least partially affixed to the first portion and...

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Bibliographische Detailangaben
Hauptverfasser: Doyon, Nicolas, Duval, Sebastien, Sinusas, Eric, Noiseux-Boucher, Guillaume, Boisvert, Olivier
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:According to one implementation of the present disclosure, a stabilizer of an aircraft includes an energy absorbing assembly. The energy absorbing assembly includes first and second portions and a retractable section. The retractable section may be at least partially affixed to the first portion and is configured to enable displacement of the second portion of the stabilizer with respect to the first portion.