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公开(公告)号：US20180105259A1
公开(公告)日：2018-04-19
申请号：US15295687
申请日：2016-10-17
Applicant: Goodrich Corporation
Inventor： Eric Cahill , Efrem E. Ayichew
CPC classification number: B64C25/42 , B60T8/1703 , B60T8/885 , B60T2220/04 , B60T2270/402 , B60T2270/413 , B64D45/00
Abstract: A brake system for an aircraft is provided according to various embodiments. The system may include a left pedal arrangement comprising a left pedal, a first left sensor to generate a first left signal in response to translation of the left pedal. The system also includes a right pedal arrangement comprising a right pedal, a first right sensor to generate a first right signal in response to translation of the right pedal. Normal brake control logic controls the brake system in response to a normal condition being set. The normal brake control logic commands a left brake based on the left signal, and a right brake based on the first right signal. Emergency brake control logic controls the brake system in response to an emergency condition being set. The emergency brake control logic commands a same force to the left and right brakes based the left and right signals.
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公开(公告)号：US09193475B2
公开(公告)日：2015-11-24
申请号：US13929389
申请日：2013-06-27
Applicant: Goodrich Corporation
Inventor： Eric Cahill
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。
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公开(公告)号：US20180105260A1
公开(公告)日：2018-04-19
申请号：US15296928
申请日：2016-10-18
Applicant: Goodrich Corporation
Inventor： Eric Cahill
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.
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公开(公告)号：US09272570B2
公开(公告)日：2016-03-01
申请号：US13952146
申请日：2013-07-26
Applicant: Goodrich Corporation
Inventor： Eric Cahill
CPC classification number: B60B7/10 , B60B7/0013 , B60B7/04 , B60B7/063 , B64C25/36
Abstract: A clamp-hubcap assembly is provided. The assembly may include a clamp, a hubcap, and a retaining device. The retaining device may be any suitable structure capable of coupling the clamp and the hubcap together.
Abstract translation: 提供一个夹紧毂盖组件。 组件可以包括夹具，轮毂盖和保持装置。 保持装置可以是能够将夹具和轮毂盖联接在一起的任何合适的结构。
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公开(公告)号：US20150028661A1
公开(公告)日：2015-01-29
申请号：US13952146
申请日：2013-07-26
Applicant: Goodrich Corporation
Inventor： Eric Cahill
CPC classification number: B60B7/10 , B60B7/0013 , B60B7/04 , B60B7/063 , B64C25/36
Abstract: A clamp-hubcap assembly is provided. The assembly may include a clamp, a hubcap, and a retaining device. The retaining device may be any suitable structure capable of coupling the clamp and the hubcap together.
Abstract translation: 提供一个夹紧毂盖组件。 组件可以包括夹具，轮毂盖和保持装置。 保持装置可以是能够将夹具和轮毂盖联接在一起的任何合适的结构。
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Patent Agency Ranking
公开(公告)号：US10053068B2
公开(公告)日：2018-08-21
申请号：US15221559
申请日：2016-07-27
Applicant: Goodrich Corporation
Inventor： Eric Cahill
CPC classification number: B60T8/1703 , B60T8/92 , B60T17/221 , B60T2270/404 , B60T2270/413 , B64C25/44
Abstract: A brake system comprises an inboard brake and an outboard brake. A primary control channel includes a primary outboard (POB) channel coupled to the outboard brake. The primary control channel includes a primary inboard (PIB) channel coupled to the inboard brake. A secondary control channel includes a secondary outboard (SOB) channel coupled to the outboard brake. The secondary control channel includes a secondary inboard (SIB) channel coupled to the inboard brake. The primary control channel is in communication with the secondary control channel.
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公开(公告)号：US20180029567A1
公开(公告)日：2018-02-01
申请号：US15221559
申请日：2016-07-27
Applicant: Goodrich Corporation
Inventor： Eric Cahill
CPC classification number: B60T8/1703 , B60T8/92 , B60T17/221 , B60T2270/404 , B60T2270/413 , B64C25/44
Abstract: A brake system may comprise an inboard brake and an outboard brake. A primary control channel may include a primary outboard (POB) channel coupled to the outboard brake. The primary control channel may include a primary inboard (PIB) channel coupled to the inboard brake. A secondary control channel may include a secondary outboard (SOB) channel coupled to the outboard brake. The secondary control channel may include a secondary inboard (SIB) channel coupled to the inboard brake. The primary control channel may be in communication with the secondary control channel.
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公开(公告)号：US09227617B2
公开(公告)日：2016-01-05
申请号：US14290521
申请日：2014-05-29
Applicant: Goodrich Corporation
Inventor： Eric Cahill , Marc Georgin
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.
Abstract translation: 用于测试飞行器制动系统的操作的方法利用以下步骤：将预定的电能水平施加到附接到制动组件的机电致动器，随后停止向机电致动器的电能。 在一些测试方法中，确定机电致动器的致动水平并用于评估制动性能。 在其他测试中，测量由致动器中的电动机产生的电压并用于评估制动性能。
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公开(公告)号：US20150344017A1
公开(公告)日：2015-12-03
申请号：US14290521
申请日：2014-05-29
Applicant: Goodrich Corporation
Inventor： Eric Cahill , Marc Georgin
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.
Abstract translation: 用于测试飞行器制动系统的操作的方法利用以下步骤：将预定的电能水平施加到附接到制动组件的机电致动器，随后停止向机电致动器的电能。 在一些测试方法中，确定机电致动器的致动水平并用于评估制动性能。 在其他测试中，测量由致动器中的电动机产生的电压并用于评估制动性能。
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公开(公告)号：US10259569B2
公开(公告)日：2019-04-16
申请号：US15295687
申请日：2016-10-17
Applicant: Goodrich Corporation
Inventor： Eric Cahill , Efrem E. Ayichew
Abstract: A brake system for an aircraft is provided according to various embodiments. The system may include a left pedal arrangement comprising a left pedal, a first left sensor to generate a first left signal in response to translation of the left pedal. The system also includes a right pedal arrangement comprising a right pedal, a first right sensor to generate a first right signal in response to translation of the right pedal. Normal brake control logic controls the brake system in response to a normal condition being set. The normal brake control logic commands a left brake based on the left signal, and a right brake based on the first right signal. Emergency brake control logic controls the brake system in response to an emergency condition being set. The emergency brake control logic commands a same force to the left and right brakes based the left and right signals.
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