公开(公告)号：US12017759B2

公开(公告)日：2024-06-25

申请号：US17386007

申请日：2021-07-27

Applicant: Goodrich Corporation

Inventor： Pawel Pacak ,  Karol Stras ,  Adam Wyszowski

IPC: F16D65/84 ,  B64C25/44 ,  F16D65/097 ,  F16D121/04 ,  F16D125/06

CPC classification number: B64C25/44 ,  F16D65/0971 ,  F16D2121/04 ,  F16D2125/06

Abstract: A piston engaging member of a piston assembly for engaging a pressure plate of an aircraft brake system, the engaging member comprising a body having a first side configured to selectably engage with the pressure plate, and a mount on a second side of the body configured to mount the piston engaging member with a piston of the piston assembly wherein the body comprises a cellular structure between the first and second sides.

公开(公告)号：US20170291696A1

公开(公告)日：2017-10-12

申请号：US15094127

申请日：2016-04-08

Applicant: Goodrich Corporation

Inventor： Adam Wyszowski

IPC: B64C25/36 ,  B64C25/42

CPC classification number: B64C25/36 ,  B60B3/02 ,  B60B21/12 ,  B60B2360/3416 ,  B60B2360/344 ,  B60B2360/36 ,  B60B2900/212 ,  B64C25/42

Abstract: Systems and methods for a heat-insulated wheel are disclosed herein. A wheel may comprise a wheel body comprising an outer diameter surface, an inner rim on an inboard side of the wheel body, an outer rim on an outboard side of the wheel body opposite the inner rim, and a heat insulator coupled to the outer diameter surface between the inner rim and the outer rim.

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：US11274716B2

公开(公告)日：2022-03-15

申请号：US16711188

申请日：2019-12-11

Applicant: Goodrich Corporation

Inventor： Karol Stras ,  Adam Wyszowski ,  Pawel Pacak

IPC: F16D65/84 ,  F16D55/36 ,  F16D65/78

Abstract: A braking system (4) for an aircraft wheel (2) comprises first and second brake rotor discs (20a, 20b) axially spaced along an axis (A) and rotationally coupled to the wheel (2), a stator disc (24) arranged axially between the first and second rotor discs (20a, 20b), and a heat shield (34) mounted to at least one of the first and second rotor discs (20a, 20b). Radially outer portions (30) of the first and second rotor discs (20a, 20b) extend radially outwardly of the stator disc (24) to define a gap (32) between the radially outer portions (30) of the first and second rotor discs (20a, 20b). The heat shield (34) extends at least partially over or into the gap (32).

公开(公告)号：US20230150303A1

公开(公告)日：2023-05-18

申请号：US17979599

申请日：2022-11-02

Applicant: Goodrich Corporation

Inventor： Karol Stras ,  Adam Wyszowski

IPC: B60B21/12 ,  B60B19/10

CPC classification number: B60B21/12 ,  B60B19/10 ,  B60B2360/10 ,  B60B2360/36 ,  B60B2360/70 ,  B60B2900/212 ,  B60B2900/513

Abstract: A chin ring heat shield for a wheel assembly arranged to provide a shield between convection and radiation heat from braking components and a tire of the wheel assembly, the chin ring comprising a first, radially extending, flat portion extending from a first chin ring end and a second, concave portion extending generally axially away from the first portion to a second chin ring end, wherein the axial length from the first chin ring end to the second chin ring end is sufficient to block a line of sight between the braking components and the tire when the chin ring is mounted between the braking components and the tire.

公开(公告)号：US20220033070A1

公开(公告)日：2022-02-03

申请号：US17386007

申请日：2021-07-27

Applicant: Goodrich Corporation

Inventor： Pawel Pacak ,  Karol Stras ,  Adam Wyszowski

IPC: B64C25/44 ,  F16D65/097

Abstract: A piston engaging member of a piston assembly for engaging a pressure plate of an aircraft brake system, the engaging member comprising a body having a first side configured to selectably engage with the pressure plate, and a mount on a second side of the body configured to mount the piston engaging member with a piston of the piston assembly wherein the body comprises a cellular structure between the first and second sides.