Textron Innovations Inc.

Nicolas Doyon

Eric Albert Sinusas

Sebastien Duval

Guillaume Noiseux-Boucher

Olivier Andre Boisvert

According to one implementation of the present disclosure, a stabilizer of an aircraft includes an energy attenuating portion. The energy attenuating portion includes first and second edge sections separated by an adaptable section. The adaptable section may be rigid in a first range of directions and compressible in a second range of directions.

Energy attenuation 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 is configured to enable displacement of the second portion of the stabilizer with respect to the first portion.

Growing community of inventors

Montreal, Canada

Nicolas Doyon