公开(公告)号：US20230392657A1

公开(公告)日：2023-12-07

申请号：US17833308

申请日：2022-06-06

Applicant: GOODRICH CORPORATION

Inventor： Nathaniel J. Herrmann ,  Wenping Zhao

IPC: F16D65/12 ,  F16D65/095 ,  F16D65/78 ,  B64C25/42 ,  B32B3/26 ,  B32B7/05 ,  B32B15/08 ,  B32B9/04 ,  B32B9/00

CPC classification number: F16D65/128 ,  F16D65/095 ,  F16D65/78 ,  B64C25/42 ,  B32B3/266 ,  B32B7/05 ,  B32B15/08 ,  B32B9/041 ,  B32B9/005 ,  F16D2065/785 ,  B32B2307/304 ,  B32B2605/18

Abstract: An aircraft brake insulator assembly for a brake mechanism of an aircraft includes a torque barrel assembly and a multi-layer insulator. The torque barrel assembly includes a torque plate and a torque barrel coupled to the torque plate. The multi-layer insulator is configured to be located between a piston housing of the brake mechanism and the torque plate. The multi-layer insulator includes a first insulator layer and a second insulator layer contacting the first insulator layer.