公开(公告)号：US11802603B2

公开(公告)日：2023-10-31

申请号：US16896859

申请日：2020-06-09

Applicant: GOODRICH CORPORATION

Inventor： Jacob Allen Dickel

IPC: F16D65/847 ,  B64C25/36 ,  B64C25/42 ,  B64C25/44 ,  B60B3/00 ,  B60B21/00 ,  F16D65/78

CPC classification number: F16D65/847 ,  B64C25/36 ,  B64C25/42 ,  B64C25/44 ,  B60B3/00 ,  B60B21/00 ,  B60B2360/102 ,  B60B2360/104 ,  B60B2360/141 ,  B60B2900/212 ,  B60B2900/513 ,  F16D2065/785 ,  F16D2200/003 ,  F16D2200/0021

Abstract: A heat shield for an aircraft wheel assembly is made of a heat shield material evenly distributed across the heat shield along both the circumferential and the axial directions. The heat shield material has a high thermal conductivity greater than 30 W/mK. In various embodiments, the thermal conductivity is greater than 85 W/mK. In this manner, thermal flux is maximized throughout the heat shield to distribute heat evenly across the heat shield in both circumferential and axial directions.

公开(公告)号：US11946518B2

公开(公告)日：2024-04-02

申请号：US17719171

申请日：2022-04-12

Applicant: GOODRICH CORPORATION

Inventor： Nathaniel J. Herrmann ,  Robert L. French ,  Phillip E. Cooley ,  Jacob Allen Dickel

IPC: F16D65/095 ,  B64C25/44 ,  F16D55/36 ,  F16D65/847 ,  F16D55/00 ,  F16D65/02

CPC classification number: F16D65/095 ,  B64C25/44 ,  F16D55/36 ,  F16D65/847 ,  F16D2055/0008 ,  F16D2065/1364 ,  F16D2250/00

Abstract: A torque barrel for use with a brake system may comprise a torque barrel having a cylindrical structure including an inner surface, an outer surface, a first opening at a first end, and a second opening at an opposing second end; and a longitudinal hole disposed through the outer surface of the barrel between a first spline of the plurality of splines and a second spline of the plurality of splines.

公开(公告)号：US20230303240A1

公开(公告)日：2023-09-28

申请号：US18187130

申请日：2023-03-21

Applicant: GOODRICH CORPORATION

Inventor： KAROL STRAS ,  Adam Wyszowski ,  William P. May ,  Orly Leiva Lam ,  Michael Shu ,  Jacob Allen Dickel ,  Dominik Kosiba

IPC: B64C25/44 ,  F16D65/84

CPC classification number: B64C25/44 ,  F16D65/84 ,  F16D2065/781

Abstract: A wheel and brake assembly comprising: a stator; a rotating assembly mounted around and rotatable relative to the stator about an axis A; a torque tube in fixed engagement with the stator; a stack of brake disks mounted about the torque tube, the stack of brake disks comprising alternate rotor disks and stator disks, the stator disks attached to the torque tube and the rotor disks attached to the rotating assembly; a brake actuator configured to, in response to a brake command, apply a pressing force on the stack of brake disks to cause frictional engagement between the rotor disks and the stator disks such that the stator disks prevent the rotor disks and, hence the rotating assembly, from rotating relative to the torque tube.

公开(公告)号：US20210381567A1

公开(公告)日：2021-12-09

申请号：US16896859

申请日：2020-06-09

Applicant: GOODRICH CORPORATION

Inventor： Jacob Allen Dickel

IPC: F16D65/847 ,  B60B21/00 ,  B64C25/44

Abstract: A heat shield for an aircraft wheel assembly is made of a heat shield material evenly distributed across the heat shield along both the circumferential and the axial directions. The heat shield material has a high thermal conductivity greater than 30 W/mK. In various embodiments, the thermal conductivity is greater than 85 W/mK. In this manner, thermal flux is maximized throughout the heat shield to distribute heat evenly across the heat shield in both circumferential and axial directions.