公开(公告)号：US12179913B2

公开(公告)日：2024-12-31

申请号：US16111352

申请日：2018-08-24

Applicant: Hamilton Sundstrand Corporation

Inventor： Mark R. Gurvich ,  Georgios S. Zafiris ,  Edward P. Marron ,  Brayton Reed ,  Joyel M. Schaefer ,  Michael King

IPC: B64C27/14 ,  B29C70/30 ,  B64D35/00 ,  F16C3/02

Abstract: A drive shaft for an aircraft according to an example of the present disclosure includes, among other things, an elongated core extending between a pair of opposed couplings, an energy absorption layer made of a composite comprising metal, the energy absorption layer disposed on the core, and a first composite ballistic layer disposed along a length of the core.

公开(公告)号：US20200063788A1

公开(公告)日：2020-02-27

申请号：US16111352

申请日：2018-08-24

Applicant: Hamilton Sundstrand Corporation

Inventor： Mark R. Gurvich ,  Georgios S. Zafiris ,  Edward P. Marron ,  Brayton Reed ,  Joyel M. Schaefer ,  Michael King

IPC: F16C3/02 ,  B64D35/00 ,  B64D45/02 ,  B29C70/30

Abstract: A drive shaft for an aircraft according to an example of the present disclosure includes, among other things, an elongated core extending between a pair of opposed couplings, an energy absorption layer made of a composite comprising metal, the energy absorption layer disposed on the core, and a first composite ballistic layer disposed along a length of the core.