公开(公告)号：US12043240B2

公开(公告)日：2024-07-23

申请号：US17549498

申请日：2021-12-13

Applicant: GOODRICH CORPORATION

Inventor： Suk-Min Moon ,  Marc Georgin ,  Emad Al-Tabakha ,  Kaman Thapa Magar

IPC: B60T8/17 ,  B60T8/58 ,  B60T8/72 ,  B60T8/88 ,  B60T8/96 ,  B60T17/22 ,  B64C25/42 ,  G07C5/04 ,  B60T8/32

CPC classification number: B60T8/96 ,  B60T8/885 ,  B60T17/22 ,  B64C25/42 ,  G07C5/04 ,  B60T8/325 ,  B60T2250/04 ,  B60T2270/406

Abstract: A method for detecting an erroneous velocity data using a controller in communication with a velocity sensor onboard a vehicle includes receiving a time-series velocity data from the velocity sensor, calculating a time-series acceleration data using the time-series velocity data, calculating a time-series jerk data using the time-series acceleration data, calculating a saturated (numerically bounded) jerk data using the time-series jerk data, calculating an estimated acceleration data using the saturated jerk data, calculating a difference between the estimated acceleration data and the time-series acceleration data, and determining whether the difference is greater than a threshold value. The erroneous velocity data is detected in response to the difference being greater than the threshold value.

公开(公告)号：US11970263B2

公开(公告)日：2024-04-30

申请号：US17668647

申请日：2022-02-10

Applicant: GOODRICH CORPORATION

Inventor： Marc Georgin ,  Richard A. Poisson

IPC: B64C25/44 ,  B60T8/17 ,  B60T13/74 ,  B60T17/22

CPC classification number: B64C25/44 ,  B60T8/1703 ,  B60T17/221 ,  B60T13/741

Abstract: A braking system for an aircraft may comprise: a brake assembly; a hydraulic braking subsystem having a hydraulic brake actuator configured to operate the brake assembly; an electric braking subsystem having an electric brake actuator configured to operate the brake assembly and a load cell configured to measure a force supplied by the electric brake actuator; a hydraulic brake control unit configured to control the hydraulic braking subsystem; and an electric brake control unit configured to control the electric braking subsystem, the electric brake control unit in operable communication with the hydraulic brake control unit, the electric brake control unit configured to calibrate the load cell by a scale factor based on a measured force from the load cell, a measured hydraulic pressure used to exceed the measured force received from the hydraulic brake control unit, and a piston area of the hydraulic brake actuator.

公开(公告)号：US20210331786A1

公开(公告)日：2021-10-28

申请号：US17208938

申请日：2021-03-22

Applicant: GOODRICH CORPORATION

Inventor： Marc Georgin

IPC: B64C25/42 ,  B64D43/00

Abstract: An autobrake system includes a brake control unit (BCU), and a control knob in electronic communication with the BCU. The BCU is configured to receive a position signal from the control knob, the position signal corresponding a position of the control knob. The BCU is configured to select a braking deceleration based upon the position signal, wherein the braking deceleration continuously changes between a minimum braking deceleration and a maximum deceleration in response to the control knob moving between a first position and a second position for fine tuning of the braking deceleration.

公开(公告)号：US10830321B2

公开(公告)日：2020-11-10

申请号：US15047977

申请日：2016-02-19

Applicant: Goodrich Corporation

Inventor： David Drennen ,  Harald Klode ,  Kevin Rehfus ,  Satinder Mann ,  Marc Georgin ,  Robert French

IPC: F16H25/24 ,  F16D65/18 ,  F16H25/22 ,  F16D125/40 ,  F16D121/20 ,  F16D121/24 ,  F16H25/20

Abstract: The present disclosure provides an actuator assembly having a ball nut comprising a helical track and a ball screw. The ball screw of the actuator assembly includes a first translation bearing track having a first diameter, wherein the helical track and the first translation bearing track form a first translation bearing raceway in which a first translation bearing ball is disposed. The ball screw further includes a second translation bearing track having a second diameter, wherein the helical track and the second translation bearing track form a second translation bearing raceway in which a second translation bearing ball is disposed. The first diameter and the second diameter are not equal.

公开(公告)号：US10710561B2

公开(公告)日：2020-07-14

申请号：US16290420

申请日：2019-03-01

Applicant: GOODRICH CORPORATION

Inventor： Marc Georgin

IPC: B60T8/172 ,  B64C25/42 ,  B60T8/17 ,  B60T8/171 ,  B60T8/1761 ,  B60T7/04 ,  B60T8/32 ,  B60T8/176

Abstract: Systems and methods for aircraft braking are disclosed. The systems and methods may comprise a control mode executive configured to receive a pedal input and calculate a gear deceleration command comprising a desired deceleration rate based on the pedal input; a pedal deceleration controller in electronic communication with the control mode executive configured to receive the gear deceleration command from the control mode executive and calculate a gear pedal command based on at least one of the gear deceleration command and a deceleration feedback; and a pedal executive in electronic communication with the pedal deceleration controller configured to receive the gear pedal command, and generate a pedal braking command based on the gear pedal command.

公开(公告)号：US20200017202A1

公开(公告)日：2020-01-16

申请号：US16033967

申请日：2018-07-12

Applicant: GOODRICH CORPORATION

Inventor： Marc Georgin ,  Michael Kordik

IPC: B64C25/46 ,  B60T8/1761 ,  B60T8/17 ,  B60T8/32

Abstract: Braking control systems and methods, such as for an aircraft, use a dump valve to rapidly decrease hydraulic pressure applied to a brake actuator during a wheel skid condition. In response to the wheel speed recovering, the dump valve is commanded closed and the brake control system returns to normal braking. The dump valve and a servo-valve may work harmoniously for locked wheel brake control.

公开(公告)号：US20190232937A1

公开(公告)日：2019-08-01

申请号：US15884177

申请日：2018-01-30

Applicant: GOODRICH CORPORATION

Inventor： Marc Georgin ,  Michael Kordik

IPC: B60T17/22 ,  B60T8/17 ,  B60T8/172 ,  B60T15/02 ,  G07C5/00 ,  G07C5/08 ,  B64C25/42

Abstract: A method of performing prognostics on a hydraulic brake system of an aircraft may include determining, during primary braking mode and by a hydraulic brake controller, a first status of a first brake pressure sensor adjacent a brake assembly. The method may also include, in response to determining that the first status of the first brake pressure sensor is valid, determining, during park braking mode and by the hydraulic brake controller, a second status of a second brake pressure sensor adjacent a park valve assembly. In response to determining that the first status of the first brake pressure sensor is degraded, the method may include outputting, by the hydraulic brake controller, at least one of an inspection indicator and a maintenance indicator.

公开(公告)号：US20180326955A1

公开(公告)日：2018-11-15

申请号：US15595573

申请日：2017-05-15

Applicant: Goodrich Corporation

Inventor： Marc Georgin ,  Efrem E. Ayichew

IPC: B60T8/1761 ,  B60W10/188 ,  B64C25/42 ,  B60T8/17

CPC classification number: B60T8/1703 ,  B60T8/1701 ,  B60T8/1761 ,  B60T8/17613 ,  B60T8/24 ,  B60T2201/03 ,  B60T2230/02 ,  B60T2250/03 ,  B60W10/184 ,  B60W10/188 ,  B64C25/426 ,  B64C25/48 ,  G05D1/0816

Abstract: A method for controlling brakes may comprise receiving, by a controller, a yaw rate from an inertial sensor, calculating, by the controller, a force correction, calculating, by the controller, a pressure correction, and adjusting, by the controller, a pressure command for a brake control device.

公开(公告)号：US09981754B2

公开(公告)日：2018-05-29

申请号：US14940918

申请日：2015-11-13

Applicant: GOODRICH CORPORATION

Inventor： Marc Georgin

IPC: G08B21/00 ,  B64D45/00 ,  B64C25/42 ,  B60T8/17 ,  B60T8/171 ,  B60T8/172 ,  G08G5/00 ,  G08G5/06

CPC classification number: B64D45/00 ,  B60T8/1703 ,  B60T8/171 ,  B60T8/172 ,  B60T2210/14 ,  B60T2240/06 ,  B64C25/426 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/065

Abstract: Systems and methods for detecting runway conditions are disclosed. A weight on wheel system may determine that an aircraft is on the ground. Wheel speed sensors may measure the speed of the aircraft wheels. Axle reference speeds may be calculated for each landing gear based on the speed of the aircraft wheels. A weight on wheel time limit may be reached prior to the axle reference speeds reaching an on ground threshold. A brake control unit may determine that the runway is contaminated if the on ground threshold was not reached.

公开(公告)号：US09975628B2

公开(公告)日：2018-05-22

申请号：US14981235

申请日：2015-12-28

Applicant: GOODRICH CORPORATION

Inventor： Marc Georgin ,  Richard Paul Metzger, Jr.

IPC: B64C25/46 ,  B60T8/86 ,  B60T17/18 ,  B60T8/17

CPC classification number: B64C25/46 ,  B60T8/1703 ,  B60T8/86 ,  B60T17/18

Abstract: A method for controlling brakes is provided. The method comprises detecting an imminent skid by an anti-skid controller/deceleration controller (ASK/DK). The ASK/DK outputs at least one of a negative desired pressure command to a pressure control unit (PK) in response to detecting the imminent skid and causes a current command output from the PK to be reduced to release braking pressure if the negative desired pressure command minus a measured feedback pressure is greater than a deadband of the PK or outputs a negative desired force command to a force control unit (ForK) in response to detecting the imminent skid and causing a current command output from the ForK to be reduced to release braking force if the negative desired force command minus a measured feedback force is greater than a deadband of the Fork. A brake control system is also provided.