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公开(公告)号：US10176070B2
公开(公告)日：2019-01-08
申请号：US14716556
申请日：2015-05-19
Applicant: GOODRICH CORPORATION
Inventor： Eric D. Cahill , Paul R. Burte
Abstract: A system and method of identifying part failures is provided. The system may comprise monitoring a sensor, detecting a failure mode, selecting a row from a lookup table corresponding to the failure mode, looking up a line replaceable unit (LRU) failure probability for the detected failure mode, and reporting the LRU failure probability for the detected failure mode.
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公开(公告)号：US20190176973A1
公开(公告)日：2019-06-13
申请号：US16277407
申请日：2019-02-15
Applicant: GOODRICH CORPORATION
Inventor： Eric D. Cahill
Abstract: A system, apparatus and method provide emergency differential braking for effecting braked steering of an aircraft. A brake input device is provided that not only allows for emergency and parking brake functions, but also enables differential braking. The brake input device (e.g., a parking and/or emergency brake lever, pedal, handle, etc.) can be used in a brake system including a brake system control unit (BSCU), one or more electro-mechanical actuator controllers (EMACs) and a brake assembly including one or more electrical actuators. Each EMAC is electrically coupled to one or more of the actuators so as to provide electrical power for driving the actuators. Each EMAC is also communicatively coupled to the BSCU so as to receive braking data therefrom. In an emergency, the input device sends braking signals directly to the brake actuators.
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公开(公告)号：US20150217747A1
公开(公告)日：2015-08-06
申请号：US14527930
申请日：2014-10-30
Applicant: GOODRICH CORPORATION
Inventor： Eric D. Cahill , Paul R. Burte
CPC classification number: B60T17/221 , B60T13/14 , F15B1/24 , F15B19/005 , F15B2201/205 , F15B2201/31 , F15B2201/505 , F15B2201/51
Abstract: A method of detecting an accumulator failure is provided. The method may comprise measuring a first pressure on a gas-side of an accumulator, measuring a second pressure on a fluid-side of the accumulator, finding a difference between the first pressure and the second pressure, and comparing the difference to a predetermined threshold. A system for detecting an accumulator failure is also provided. The system may comprise a non-transitory memory communicating with a processor, the non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause the processor to perform operations. The operations may include receiving a first pressure measurement, receiving a second pressure measurement, determining a difference between the first pressure measurement and the second pressure measurement, and detecting the accumulator failure based on the difference.
Abstract translation: 提供了一种检测蓄电池故障的方法。 该方法可以包括测量蓄能器的气体侧上的第一压力，测量蓄能器的流体侧上的第二压力，找到第一压力和第二压力之间的差，并将差值与预定阈值进行比较 。 还提供了一种用于检测蓄电池故障的系统。 系统可以包括与处理器通信的非暂时性存储器，其中存储有指令的非瞬态存储器响应于处理器的执行使得处理器执行操作。 操作可以包括接收第一压力测量值，接收第二压力测量值，确定第一压力测量值和第二压力测量值之间的差值，以及基于该差值来检测累加器故障。
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公开(公告)号：US20130282251A1
公开(公告)日：2013-10-24
申请号：US13920992
申请日：2013-06-18
Applicant: Goodrich Corporation
Inventor： Eric D. Cahill
CPC classification number: B64C25/44 , B60T7/12 , B60T8/00 , B60T8/17 , B60T8/1703 , B60T13/741 , B60T2270/406 , B64C25/46
Abstract: Systems and methods tbr dynamically stable braking are disclosed. A first electromechanical brake actuator controller may be placed in communication with a second electromechanical brake actuator controller, wherein each of the first electromechanical brake actuator controller and second electromechanical brake actuator controller are in communication with electromechanical brake actuators that are associated with the same wheel. The first electromechanical brake actuator controller and second electromechanical brake actuator controllers may then communicate electromechanical brake actuator status information and take corrective measures in accordance with the status information.
Abstract translation: 公开了动态稳定制动的系统和方法。 第一机电制动致动器控制器可以放置成与第二机电制动致动器控制器连通，其中第一机电制动致动器控制器和第二机电制动致动器控制器中的每一个与与同一车轮相关联的机电制动致动器连通。 然后，第一机电制动执行器控制器和第二机电制动执行器控制器可以传达机电制动执行器状态信息，并根据状态信息采取纠正措施。
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公开(公告)号：US10737669B2
公开(公告)日：2020-08-11
申请号：US15945174
申请日：2018-04-04
Applicant: Goodrich Corporation
Inventor： Eric D. Cahill
Abstract: A brake control system for a landing gear of an aircraft is provided. The system includes a first control channel for providing brake control signals to one or more brakes on the landing gear, and a second control channel for providing brake control signals to another one or more brakes on the landing gear. At least one of the first control channel and the second control channel is configured to act as an executive in monitoring braking efforts applied by the one or more brakes as compared to braking efforts applied by the another one or more brake, and to cause the braking efforts of at least one of the one or more brakes or the another one or more brakes to be modified in an effort to equalize the braking efforts.
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Patent Agency Ranking
公开(公告)号：US20170261341A1
公开(公告)日：2017-09-14
申请号：US15603116
申请日：2017-05-23
Applicant: Goodrich Corporation
Inventor： Eric D. Cahill , Michael Shaw
IPC: G01D5/14 , H03K3/0232 , G01P3/44
CPC classification number: G01D5/14 , B64C25/00 , B64C25/46 , G01P3/44 , H03K3/0232
Abstract: Systems and methods disclosed herein may be useful for use in landing identification. In this regard, a method is provided comprising receiving pulse information over a first time period, wherein the pulse information is indicative of an angular distance traveled by a first wheel, comparing the pulse information to a threshold value, and determining a likelihood of a landing event based upon the comparison. In various embodiments, a system is provided comprising a monostable multivibrator in electrical communication with a metal-oxide-semiconductor field-effect transistor (MOSFET), a resistor-capacitor network in electrical communication with the MOSFET, and a comparator that receives a voltage from the resistor-capacitor network and a reference voltage.
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公开(公告)号：US09139292B2
公开(公告)日：2015-09-22
申请号：US13920992
申请日：2013-06-18
Applicant: Goodrich Corporation
Inventor： Eric D. Cahill
CPC classification number: B64C25/44 , B60T7/12 , B60T8/00 , B60T8/17 , B60T8/1703 , B60T13/741 , B60T2270/406 , B64C25/46
Abstract: Systems and methods for dynamically stable braking are disclosed. A first electromechanical brake actuator controller may be placed in communication with a second electromechanical brake actuator controller, wherein each of the first electromechanical brake actuator controller and second electromechanical brake actuator controller are in communication with electromechanical brake actuators that are associated with the same wheel. The first electromechanical brake actuator controller and second electromechanical brake actuator controllers may then communicate electromechanical brake actuator status information and take corrective measures in accordance with the status information.
Abstract translation: 公开了用于动态稳定制动的系统和方法。 第一机电制动致动器控制器可以放置成与第二机电制动致动器控制器连通，其中第一机电制动致动器控制器和第二机电制动致动器控制器中的每一个与与同一车轮相关联的机电制动致动器连通。 然后，第一机电制动执行器控制器和第二机电制动执行器控制器可以传达机电制动执行器状态信息，并根据状态信息采取纠正措施。
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公开(公告)号：US09533667B2
公开(公告)日：2017-01-03
申请号：US14527930
申请日：2014-10-30
Applicant: GOODRICH CORPORATION
Inventor： Eric D. Cahill , Paul R. Burte
CPC classification number: B60T17/221 , B60T13/14 , F15B1/24 , F15B19/005 , F15B2201/205 , F15B2201/31 , F15B2201/505 , F15B2201/51
Abstract: A method of detecting an accumulator failure is provided. The method may comprise measuring a first pressure on a gas-side of an accumulator, measuring a second pressure on a fluid-side of the accumulator, finding a difference between the first pressure and the second pressure, and comparing the difference to a predetermined threshold. A system for detecting an accumulator failure is also provided. The system may comprise a non-transitory memory communicating with a processor, the non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause the processor to perform operations. The operations may include receiving a first pressure measurement, receiving a second pressure measurement, determining a difference between the first pressure measurement and the second pressure measurement, and detecting the accumulator failure based on the difference.
Abstract translation: 提供了一种检测蓄电池故障的方法。 该方法可以包括测量蓄能器的气体侧上的第一压力，测量蓄能器的流体侧上的第二压力，找到第一压力和第二压力之间的差，并将差值与预定阈值进行比较 。 还提供了一种用于检测蓄电池故障的系统。 系统可以包括与处理器通信的非暂时性存储器，其中存储有指令的非瞬态存储器响应于处理器的执行使得处理器执行操作。 操作可以包括接收第一压力测量值，接收第二压力测量值，确定第一压力测量值和第二压力测量值之间的差值，以及基于该差值来检测累加器故障。
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公开(公告)号：US20160059956A1
公开(公告)日：2016-03-03
申请号：US14939663
申请日：2015-11-12
Applicant: Goodrich Corporation
Inventor： Eric D. Cahill
CPC classification number: B64C25/48 , B60T7/085 , B60T7/105 , B60T8/1703 , B60T8/885 , B60T2270/402
Abstract: A system, apparatus and method provide emergency differential braking for effecting braked steering of an aircraft. A brake input device is provided that not only allows for emergency and parking brake functions, but also enables differential braking. The brake input device (e.g., a parking and/or emergency brake lever, pedal, handle, etc.) can be used in a brake system including a brake system control unit (BSCU), one or more electro-mechanical actuator controllers (EMACs) and a brake assembly including one or more electrical actuators. Each EMAC is electrically coupled to one or more of the actuators so as to provide electrical power for driving the actuators. Each EMAC is also communicatively coupled to the BSCU so as to receive braking data therefrom. In an emergency, the input device sends braking signals directly to the brake actuators.
Abstract translation: 系统，装置和方法提供紧急差速制动以实现飞行器的制动转向。 提供了一种制动输入装置，不仅允许紧急和驻车制动功能，还可以实现差速制动。 制动输入装置（例如，停车和/或紧急制动杆，踏板，手柄等）可用于包括制动系统控制单元（BSCU），一个或多个机电致动器控制器（EMAC） ）和包括一个或多个电致动器的制动组件。 每个EMAC电耦合到一个或多个致动器，以便提供用于驱动致动器的电力。 每个EMAC也通信地耦合到BSCU，以便从其接收制动数据。 在紧急情况下，输入装置将制动信号直接发送到制动执行器。
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10.发明授权公开(公告)号：US08683857B2
公开(公告)日：2014-04-01
申请号：US13760836
申请日：2013-02-06
Applicant: Goodrich Corporation
Inventor： Eric D. Cahill
IPC: G01M17/00
CPC classification number: B60T17/221 , B64C25/42 , B64F5/60
Abstract: A method is disclosed that comprises severing an I/O channel between a brake system controller and an aircraft component; sending a test signal to the brake system controller; receiving, from the brake system controller, a feedback signal to the test signal; and determining an appropriateness of the feedback signal. A system is disclosed that comprises a brake system controller wrapped in a BITE region, wherein the BITE region comprises a testing module, a safety interlock region having an I/O channel between the brake system controller and another system, and a testing module capable of sending a test signal to the brake system controller.
Abstract translation: 公开了一种方法，其包括切断制动系统控制器和飞行器部件之间的I / O通道; 向制动系统控制器发送测试信号; 从制动系统控制器接收到测试信号的反馈信号; 并确定反馈信号的适当性。 公开了一种包括在BITE区域中的制动系统控制器的系统，其中BITE区域包括测试模块，具有在制动系统控制器和另一系统之间的I / O通道的安全互锁区域，以及能够 向制动系统控制器发送测试信号。
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