公开(公告)号：US09975627B2

公开(公告)日：2018-05-22

申请号：US15296928

申请日：2016-10-18

Applicant: Goodrich Corporation

Inventor： Eric Cahill

IPC: B64C25/42 ,  B60T7/16

CPC classification number: B64C25/42 ,  B60T7/085 ,  B60T7/16 ,  B60T13/662 ,  B60T13/686 ,  B64C25/44

Abstract: A system for controlling a parking brake system on an aircraft is provided. The system includes a switch interface comprising an enable switch and an activate switch. The parking brake system is configured to switch the state of a parking brake in response to the enable switch and the activate switch being engaged at the same time. A second switch interface also includes an enable switch and an activate switch with the parking brake system configured to switch the state of the parking brake system in response to the second enable switch and the second activate switch being engaged at the same time. The system may also be controlled from a remote and/or virtual location.

公开(公告)号：US09714019B2

公开(公告)日：2017-07-25

申请号：US14929031

申请日：2015-10-30

Applicant: Goodrich Corporation

Inventor： Eric Cahill ,  Marc Georgin

IPC: B60T8/88 ,  B64C25/44 ,  B60T17/22 ,  B64C25/42 ,  B60T8/17

CPC classification number: B60T17/221 ,  B60T8/1703 ,  B60T8/885 ,  B60T2270/406 ,  B64C25/42 ,  B64C25/44

Abstract: Methods for testing the operation of an aircraft braking system utilize the steps of applying a predetermined electrical energy level to an electromechanical actuator attached to a brake assembly, followed by discontinuing electrical energy to the electromechanical actuator. In some test methods, an actuation level of the electromechanical actuator is determined and used to evaluate braking performance. In other tests, a voltage generated by an electric motor in an actuator is measured and used to evaluate braking performance.

公开(公告)号：US20160052502A1

公开(公告)日：2016-02-25

申请号：US14929031

申请日：2015-10-30

Applicant: Goodrich Corporation

Inventor： Eric Cahill ,  Marc Georgin

IPC: B60T17/22 ,  B64C25/44

CPC classification number: B60T17/221 ,  B60T8/1703 ,  B60T8/885 ,  B60T2270/406 ,  B64C25/42 ,  B64C25/44

Abstract: Methods for testing the operation of an aircraft braking system utilize the steps of applying a predetermined electrical energy level to an electromechanical actuator attached to a brake assembly, followed by discontinuing electrical energy to the electromechanical actuator. In some test methods, an actuation level of the electromechanical actuator is determined and used to evaluate braking performance. In other tests, a voltage generated by an electric motor in an actuator is measured and used to evaluate braking performance.

公开(公告)号：US20150002318A1

公开(公告)日：2015-01-01

申请号：US13929389

申请日：2013-06-27

Applicant: Goodrich Corporation

Inventor： Eric Cahill

IPC: B64D45/00

CPC classification number: B64D45/00 ,  B60C23/0474 ,  B60C2200/02

Abstract: Tire pressure monitoring systems and methods for detecting a tire burst are disclosed. The system may include a tire pressure sensor, a tire pressure monitor, and a tire burst indicator. The tire pressure sensor may measure tire pressure in an aircraft tire. The tire pressure monitor may analyze data from the tire pressure sensor to detect a tire burst. A tire burst may be detected in response to a rapid decrease in tire pressure. In response to detecting a tire burst, the tire pressure monitor may transmit a tire burst message to the tire burst indicator. The tire burst indicator may indicate to a pilot that a tire burst has been detected.

Abstract translation: 公开了用于检测轮胎爆裂的轮胎压力监测系统和方法。 该系统可以包括轮胎压力传感器，轮胎压力监视器和轮胎爆破指示器。 轮胎压力传感器可以测量飞机轮胎中的轮胎压力。 轮胎压力监视器可以分析来自轮胎压力传感器的数据以检测轮胎爆裂。 可以响应于轮胎压力的快速下降来检测轮胎爆裂。 响应于检测到轮胎爆裂，轮胎压力监视器可以将轮胎爆破消息传送到轮胎爆破指示符。 轮胎爆破指示器可以向飞行员指示已经检测到轮胎爆裂。