公开(公告)号：US20180016001A1

公开(公告)日：2018-01-18

申请号：US15643283

申请日：2017-07-06

Applicant: Goodrich Corporation

Inventor： Rony Giovanni Ganis ,  James Bernard

IPC: B64C25/42 ,  B64C25/34

CPC classification number: B64C25/42 ,  B64C25/34

Abstract: An arrangement for landing gear comprises a piston, a bogie beam and forward and rear brake rods. The piston has an attachment portion with a pivot connection for the bogie beam at its lower end. The bogie beam is mounted to the attachment portion at the pivot connection. The bogie beam supports forward and rear brake assemblies on forward and rear sides of the piston. The forward brake rod is connected to the forward brake assembly at a location for acting under tension during braking and the rear brake rod is connected to the rear brake assembly at a location for acting under tension during braking. The rear end of the forward brake rod is connected to the attachment portion forward of the pivot connection of the bogie beam, and a forward end of the rear brake rod is connected to the attachment portion.

公开(公告)号：US20170369158A1

公开(公告)日：2017-12-28

申请号：US15193968

申请日：2016-06-27

Applicant: Goodrich Corporation

Inventor： Mark R. Gurvich ,  Georgios S. Zafiris ,  Rony Giovanni Ganis

IPC: B64C25/34

Abstract: Systems and methods for landing gear arrangements are provided. In various embodiments, a landing gear arrangement may comprise a first composite layer, the first composite layer having a cylindrical geometry, a metallic ring comprising an inner surface and an outer surface, the metallic ring perimetrically surrounding at least a portion of the first composite layer, the inner surface being in contact with the first composite layer, a metallic connecting tab extending away from the outer surface, and a second composite layer at least partially perimetrically surrounding the metallic ring and at least partially perimetrically surrounding the first composite layer, the outer surface being in contact with the second composite layer.

公开(公告)号：US09796467B2

公开(公告)日：2017-10-24

申请号：US14048914

申请日：2013-10-08

Applicant: Goodrich Corporation

Inventor： Rony Giovanni Ganis

IPC: B64C25/26 ,  B64C25/16 ,  B64C25/00 ,  B64C7/00

CPC classification number: B64C25/16 ,  B64C7/00 ,  B64C25/001 ,  B64C2025/003

Abstract: A noise abatement system for an aircraft landing gear is provided. The system may have a retention member and a covering member. In this regard, the system may be configured to block the airflow through a structural void to abate noise. Moreover, the system may be shaped to diminish aerodynamic drag.

公开(公告)号：US09726325B2

公开(公告)日：2017-08-08

申请号：US14267720

申请日：2014-05-01

Applicant: Goodrich Corporation

Inventor： Rony Giovanni Ganis ,  Peter F. Giddings

IPC: F16S3/04 ,  B32B37/18 ,  B32B37/14 ,  F16C7/02

CPC classification number: F16S3/04 ,  B32B37/142 ,  B32B37/18 ,  B32B2597/00 ,  B32B2605/08 ,  B32B2605/18 ,  F16C7/026 ,  Y10T428/13 ,  Y10T428/1372

Abstract: Composite tubes comprising a compression sleeve coupled to an inner surface of a composite tube, a carbon extrusion member disposed within the composite tube, and an end fitting comprising a locking feature, wherein the end fitting is coupled to an inner surface of the compression sleeve and the locking feature is configured to engage the carbon extrusion member are disclosed. Methods comprising coupling a compression sleeve to an inner surface of a distal end of a composite tube, placing a carbon extrusion member inside the compression sleeve and the composite tube, and disposing an end fitting on the distal end of the composite tube, wherein the end fitting comprises a locking feature configured to interact with the carbon extrusion member are also disclosed.

公开(公告)号：US20160375990A1

公开(公告)日：2016-12-29

申请号：US14048914

申请日：2013-10-08

Applicant: Goodrich Corporation

Inventor： Rony Giovanni Ganis

IPC: B64C25/16 ,  B64C7/00

CPC classification number: B64C25/16 ,  B64C7/00 ,  B64C25/001 ,  B64C2025/003

Abstract: A noise abatement system for an aircraft landing gear is provided. The system may have a retention member and a covering member. In this regard, the system may be configured to block the airflow through a structural void to abate noise. Moreover, the system may be shaped to diminish aerodynamic drag.

Abstract translation: 提供一种用于飞机起落架的噪声消除系统。 系统可以具有保持构件和覆盖构件。 在这方面，该系统可被配置为阻挡通过结构空隙的气流以消除噪音。 此外，该系统可以被成形为减小空气动力学阻力。

公开(公告)号：US11260966B2

公开(公告)日：2022-03-01

申请号：US16828042

申请日：2020-03-24

Applicant: GOODRICH CORPORATION

Inventor： Scott Alan Eastman ,  Mark R. Gurvich ,  Paul Papas ,  Steven W. Gronda ,  Rony Giovanni Ganis

IPC: B64C25/10 ,  B05D1/28 ,  B05D1/18 ,  B05D1/02 ,  B32B5/02 ,  B32B27/30 ,  B32B27/08 ,  B32B5/24 ,  B32B27/28 ,  B32B27/40 ,  B32B27/36

Abstract: A composite structure may comprise a composite core comprising a composite material, and a heat resistant system coupled to the composite core comprising a binder and/or at least one of a heat dissipation material or a thermal barrier material. The heat dissipation material may comprise boron nitride, graphene, graphite, carbon fiber, carbon nanotubes, aluminum foil, and/or copper foil, and the thermal barrier material may comprise montmorillonite, aluminum hydroxide, magnesium hydroxide, silicate glass, mica powder or flake, aluminum oxide powder, titanium dioxide powder, and/or zirconium oxide powder. The binder may comprise at least one of polyvinyl alcohol, polyvinyl alcohol copolyacetate, polyacrylamide, polyethylene glycol, polyethylenimine, polyurethane, polyester, or latex.

公开(公告)号：US11230370B2

公开(公告)日：2022-01-25

申请号：US16255483

申请日：2019-01-23

Applicant: GOODRICH CORPORATION

Inventor： Eric Goldring ,  Rony Giovanni Ganis

IPC: B64C25/26 ,  B64C25/20 ,  B64C25/34 ,  B64C25/10 ,  B64C25/22

Abstract: An upper side brace for use in landing gear includes a main body having a mounting end configured to be proximal to an aircraft and a lower end configured to be proximal to a lower side brace. The upper side brace further includes an unlock actuator cylinder formed monolithic with the main body and configured to house a piston to form an unlock actuator.

公开(公告)号：US11105389B2

公开(公告)日：2021-08-31

申请号：US16277729

申请日：2019-02-15

Applicant: GOODRICH CORPORATION

Inventor： Eric Goldring ,  Rony Giovanni Ganis

IPC: F16F9/32 ,  B60G13/06

Abstract: A metallic liner includes a cylindrical body defining a wear resilient surface, and a bearing carrier extending radially inward from the wear resilient surface, wherein the wear resilient surface and the cylindrical body are formed as a monolithic piece.

公开(公告)号：US11085465B2

公开(公告)日：2021-08-10

申请号：US16298928

申请日：2019-03-11

Applicant: GOODRICH CORPORATION

Inventor： Eric Goldring ,  Rony Giovanni Ganis

IPC: B64C25/62 ,  F15B15/14

Abstract: Retention systems for retaining a gland is provided. A hydraulic actuator may comprise a cylinder closed at an end by a gland, wherein the gland comprises a gland body having a bearing flange disposed within an interior volume of the cylinder, a lock ring retainer disposed between the gland body and the cylinder and contacted with the bearing flange, and a lock ring coupled between the lock ring retainer and a lock ring channel of the cylinder.

公开(公告)号：US10823213B2

公开(公告)日：2020-11-03

申请号：US16003865

申请日：2018-06-08

Applicant: GOODRICH CORPORATION

Inventor： Mark R. Gurvich ,  Georgios S. Zafiris ,  Rony Giovanni Ganis

IPC: F16B7/04 ,  B64C25/00

Abstract: A composite tube may include a body having a longitudinal centerline axis and an end portion having a tapered section and an end rim. At least one of a radially outward edge and a radially inward edge of the end rim may be non-circular. The end rim may be circumferentially continuous, and the tapered section may diverge radially outward in a direction from the body to the end rim. A joint assembly may include a support wedge that at least partially engages at least one of a radially inward surface of the end portion and a radially outward surface of the end portion of the composite tube.