公开(公告)号：US20190023253A1

公开(公告)日：2019-01-24

申请号：US15808376

申请日：2017-11-09

Applicant: Goodrich Corporation

Inventor： Eric Daniel Cahill ,  Paul R. Burte ,  Efrem E. Ayichew ,  Lane B. Robbins ,  Marc Georgin

IPC: B60T17/22 ,  B64C25/44 ,  B60T7/12 ,  B60T8/17 ,  B60T8/171 ,  B60T11/28

Abstract: A brake control system (BCS) may comprise a first controller, a second controller in electronic communication with the first controller, and a valve comprising a first coil and a second coil. The first controller may be configured to actuate the valve via the first coil. The second controller may be configured to actuate the valve via the second coil. The first controller may be configured to disable the second controller to take over control of the valve.

公开(公告)号：US20230415714A1

公开(公告)日：2023-12-28

申请号：US17848251

申请日：2022-06-23

Applicant: Goodrich Corporation

Inventor： Marc J. Georgin ,  Paul R. Burte ,  Lane B. Robbins ,  Richard A. Poisson

IPC: B60T8/17 ,  B60T7/04 ,  B60T17/22 ,  B60T13/68 ,  B64C25/44

CPC classification number: B60T8/1703 ,  B60T7/042 ,  B60T17/22 ,  B60T13/686 ,  B64C25/44 ,  B60T2270/82 ,  B60T2270/413 ,  B60T2270/404 ,  B60T2220/04

Abstract: An aircraft braking system is disclosed that includes a first pedal, first and second pedal sensors for the first pedal, a first brake control unit (e.g., primary), and a separate second brake control unit (e.g., secondary). The first pedal position sensor is operatively interconnected with one of the first brake control unit and the second brake control unit, while the second pedal position sensor is operatively interconnected with the other of the first brake control unit and the second brake control unit. Outputs from these pedal sensors may be used to control operation of the aircraft braking system in at least some fashion.

公开(公告)号：US09950701B2

公开(公告)日：2018-04-24

申请号：US14531746

申请日：2014-11-03

Applicant: GOODRICH CORPORATION

Inventor： Steven Keller ,  Paul L. Summers ,  Lane B. Robbins ,  Scott Streng

IPC: G01F3/02 ,  B60T8/172 ,  B60T8/17 ,  G01M17/02 ,  G01P3/44 ,  B60C23/00 ,  B60C23/04

CPC classification number: B60T8/1725 ,  B60C23/00 ,  B60C23/0408 ,  B60C23/0488 ,  B60C2200/02 ,  B60T8/1703 ,  G01M17/02 ,  G01P3/44

Abstract: What is described is a tire pressure sensor for use in a wheel of aircraft landing gear. The tire pressure sensor includes a position sensor configured to detect a movement of the wheel and generate a wheel movement signal based on the movement. The tire pressure sensor also includes a processor coupled to the position sensor. The processor is configured to receive the wheel movement signal, determine a wheel rotational speed of the wheel based on the wheel movement signal and generate a wheel rotational speed signal based on the wheel rotational speed.

公开(公告)号：US10723342B2

公开(公告)日：2020-07-28

申请号：US15808376

申请日：2017-11-09

Applicant: Goodrich Corporation

Inventor： Eric Daniel Cahill ,  Paul R. Burte ,  Efrem E. Ayichew ,  Lane B. Robbins ,  Marc Georgin

IPC: B60T17/18 ,  B60T17/22 ,  B60T8/17 ,  B60T7/12 ,  B60T8/171 ,  B60T11/28 ,  B64C25/44 ,  B64C25/34

Abstract: A brake control system (BCS) may comprise a first controller, a second controller in electronic communication with the first controller, and a valve comprising a first coil and a second coil. The first controller may be configured to actuate the valve via the first coil. The second controller may be configured to actuate the valve via the second coil. The first controller may be configured to disable the second controller to take over control of the valve.

公开(公告)号：US20160214585A1

公开(公告)日：2016-07-28

申请号：US14531746

申请日：2014-11-03

Applicant: GOODRICH CORPORATION

Inventor： STEVEN KELLER ,  Paul L. Summers, JR. ,  Lane B. Robbins ,  Scott Streng

IPC: B60T8/172 ,  G01M17/02 ,  G01P3/44 ,  B60T8/17

CPC classification number: B60T8/1725 ,  B60C23/00 ,  B60C23/0408 ,  B60C23/0488 ,  B60C2200/02 ,  B60T8/1703 ,  G01M17/02 ,  G01P3/44

Abstract: What is described is a tire pressure sensor for use in a wheel of aircraft landing gear. The tire pressure sensor includes a position sensor configured to detect a movement of the wheel and generate a wheel movement signal based on the movement. The tire pressure sensor also includes a processor coupled to the position sensor. The processor is configured to receive the wheel movement signal, determine a wheel rotational speed of the wheel based on the wheel movement signal and generate a wheel rotational speed signal based on the wheel rotational speed.

Abstract translation: 描述的是用于飞机起落架的车轮的轮胎压力传感器。 轮胎压力传感器包括位置传感器，其被配置为检测车轮的运动并基于该运动产生车轮运动信号。 轮胎压力传感器还包括耦合到位置传感器的处理器。 处理器被配置为接收车轮移动信号，基于车轮移动信号确定车轮的车轮转速，并且基于车轮转速产生车轮转速信号。