公开(公告)号：US20200346737A1

公开(公告)日：2020-11-05

申请号：US16399936

申请日：2019-04-30

Applicant: Bell Helicopter Textron Inc.

Inventor： Eric Sinusas ,  Guillaume Noiseux-Boucher ,  Olivier Boisvert ,  Nicolas Doyon ,  Sebastien Duval

IPC: B64C5/02 ,  B64F5/10

Abstract: 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.

公开(公告)号：US20200346742A1

公开(公告)日：2020-11-05

申请号：US16399932

申请日：2019-04-30

Applicant: Bell Helicopter Textron Inc.

Inventor： Eric Sinusas ,  Guillaume Noiseux-Boucher ,  Olivier Boisvert ,  Nicolas Doyon ,  Sebastien Duval

IPC: B64C25/58

Abstract: 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.

公开(公告)号：US11518502B2

公开(公告)日：2022-12-06

申请号：US16399932

申请日：2019-04-30

Applicant: Bell Helicopter Textron Inc.

Inventor： Eric Sinusas ,  Guillaume Noiseux-Boucher ,  Olivier Boisvert ,  Nicolas Doyon ,  Sebastien Duval

IPC: B64C25/58

Abstract: 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.

公开(公告)号：US11459085B2

公开(公告)日：2022-10-04

申请号：US16399936

申请日：2019-04-30

Applicant: Bell Helicopter Textron Inc.

Inventor： Eric Sinusas ,  Guillaume Noiseux-Boucher ,  Olivier Boisvert ,  Nicolas Doyon ,  Sebastien Duval

IPC: B64C5/02 ,  B64F5/10

Abstract: 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.