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公开(公告)号：US10017164B2
公开(公告)日：2018-07-10
申请号：US15870665
申请日：2018-01-12
Applicant: The Boeing Company
Inventor： Scott Brandon Kanemori , Bruce Lam , David T. Yamamoto , Thomas Todd Griffith
CPC classification number: B60T8/1703 , B60T8/00 , B60T8/325 , B60T2201/03 , B64C25/42 , B64C25/426
Abstract: A system, method, and apparatus for brake load alleviation amongst at least one first brake and at least one second brake is disclosed. The method involves sensing an amount of brake pedal application in response to engagement of at least brake pedal. The method further involves determining whether the amount of brake pedal application is greater than a brake pedal application threshold value. Also, the method involves generating a brake application profile, when it is determined that the amount of brake pedal application is greater than the brake pedal application threshold value. The brake application profile indicates that actuation of at least one first brake is delayed by a first time delay, and that actuation of at least one second brake is delayed by a second time delay. Further, the method involves actuating at least one first brake and at least one second brake according to the brake application profile.
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公开(公告)号：US20150120098A1
公开(公告)日：2015-04-30
申请号：US14064804
申请日：2013-10-28
Applicant: The Boeing Company
Inventor： Michael Gian Catalfamo , Jean Marie Crane , Marisa R. Jenkins , John David Anderson , Thomas Todd Griffith , Bechara J. Mallouk
IPC: G08G5/02
CPC classification number: G08G5/02 , G08G5/0021 , G08G5/025
Abstract: A system and method for determining a predicted stopping performance of an aircraft moving on a runway. A predicted stopping force acting on the aircraft to stop the aircraft is determined by a processor unit as the aircraft is moving on the runway. A predicted deceleration of the aircraft moving on the runway is determined by the processor unit using the predicted stopping force acting on the aircraft to stop the aircraft. The predicted stopping performance of the aircraft on the runway is determined by the processor unit using the predicted deceleration of the aircraft.
Abstract translation: 一种用于确定在跑道上移动的飞行器的预测停止性能的系统和方法。 当飞机在跑道上移动时，作用在飞机上以阻止飞行器的预测的停止力由处理器单元确定。 在跑道上移动的飞行器的预测减速度由处理器单元使用预测的作用在飞行器上的停止力来确定，以停止飞行器。 飞机在跑道上的预测的停止性能由处理器单元使用飞机预测的减速度来确定。
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3.发明申请公开(公告)号：US20150203194A1
公开(公告)日：2015-07-23
申请号：US14161492
申请日：2014-01-22
Applicant: THE BOEING COMPANY
Inventor： Thomas Todd Griffith
CPC classification number: B64C25/46 , B60T8/1703 , B60T8/172 , B60T8/176 , B60T8/17616 , B60T8/325
Abstract: Systems, methods, and apparatus for optimizing real-time antiskid control initialization for a vehicle on a travel surface are disclosed. In one or more embodiments, a method involves determining when at least one wheel of the vehicle touches ground. The method further involves calculating a rate of wheel spin up for at least one wheel. Also, the method involves determining whether the rate of wheel spin up exceeds a wheel spin up rate threshold. In addition, the method involves applying a high level of brake force when the rate of wheel spin up exceeds the wheel spin up rate threshold, and applying a low level of brake force when the rate of wheel spin up does not exceed the wheel spin up rate threshold.
Abstract translation: 公开了用于优化行驶表面上的车辆的实时防滑控制初始化的系统，方法和装置。 在一个或多个实施例中，一种方法包括确定车辆的至少一个车轮何时接地。 该方法还包括计算至少一个车轮的车轮旋转速率。 此外，该方法涉及确定车轮旋转速率是否超过车轮旋转速率阈值。 此外，该方法包括当车轮旋转速度超过车轮旋转速率阈值时施加高水平的制动力，并且当车轮旋转速度不超过车轮旋转时施加低水平的制动力 速率阈值。
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公开(公告)号：US09082301B2
公开(公告)日：2015-07-14
申请号：US14064804
申请日：2013-10-28
Applicant: The Boeing Company
Inventor： Michael Gian Catalfamo , Jean Marie Crane , Marisa R. Jenkins , John David Anderson , Thomas Todd Griffith , Bechara J. Mallouk
CPC classification number: G08G5/02 , G08G5/0021 , G08G5/025
Abstract: A system and method for determining a predicted stopping performance of an aircraft moving on a runway. A predicted stopping force acting on the aircraft to stop the aircraft is determined by a processor unit as the aircraft is moving on the runway. A predicted deceleration of the aircraft moving on the runway is determined by the processor unit using the predicted stopping force acting on the aircraft to stop the aircraft. The predicted stopping performance of the aircraft on the runway is determined by the processor unit using the predicted deceleration of the aircraft.
Abstract translation: 一种用于确定在跑道上移动的飞行器的预测停止性能的系统和方法。 当飞机在跑道上移动时，作用在飞机上以阻止飞行器的预测的停止力由处理器单元确定。 在跑道上移动的飞行器的预测减速度由处理器单元使用预测的作用在飞行器上的停止力来确定，以停止飞行器。 飞机在跑道上的预测的停止性能由处理器单元使用飞机预测的减速度来确定。
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公开(公告)号：US20180134265A1
公开(公告)日：2018-05-17
申请号：US15870665
申请日：2018-01-12
Applicant: The Boeing Company
Inventor： Scott Brandon Kanemori , Bruce Lam , David T. Yamamoto , Thomas Todd Griffith
CPC classification number: B60T8/1703 , B60T8/00 , B60T8/325 , B60T2201/03 , B64C25/42 , B64C25/426
Abstract: A system, method, and apparatus for brake load alleviation amongst at least one first brake and at least one second brake is disclosed. The method involves sensing an amount of brake pedal application in response to engagement of at least brake pedal. The method further involves determining whether the amount of brake pedal application is greater than a brake pedal application threshold value. Also, the method involves generating a brake application profile, when it is determined that the amount of brake pedal application is greater than the brake pedal application threshold value. The brake application profile indicates that actuation of at least one first brake is delayed by a first time delay, and that actuation of at least one second brake is delayed by a second time delay. Further, the method involves actuating at least one first brake and at least one second brake according to the brake application profile.
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Patent Agency Ranking
公开(公告)号：US09950699B2
公开(公告)日：2018-04-24
申请号：US14038504
申请日：2013-09-26
Applicant: THE BOEING COMPANY
Inventor： Scott Brandon Kanemori , Bruce Lam , David T. Yamamoto , Thomas Todd Griffith
CPC classification number: B60T8/1703 , B60T8/00 , B60T8/325 , B60T2201/03 , B64C25/42 , B64C25/426
Abstract: A system, method, and apparatus for brake load alleviation amongst at least one first brake and at least one second brake is disclosed. The method involves sensing an amount of brake pedal application in response to engagement of at least brake pedal. The method further involves determining whether the amount of brake pedal application is greater than a brake pedal application threshold value. Also, the method involves generating a brake application profile, when it is determined that the amount of brake pedal application is greater than the brake pedal application threshold value. The brake application profile indicates that actuation of at least one first brake is delayed by a first time delay, and that actuation of at least one second brake is delayed by a second time delay. Further, the method involves actuating at least one first brake and at least one second brake according to the brake application profile.
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公开(公告)号：US20150088371A1
公开(公告)日：2015-03-26
申请号：US14038504
申请日：2013-09-26
Applicant: THE BOEING COMPANY
Inventor： Scott Brandon Kanemori , Bruce Lam , David T. Yamamoto , Thomas Todd Griffith
CPC classification number: B60T8/1703 , B60T8/00 , B60T8/325 , B60T2201/03 , B64C25/42 , B64C25/426
Abstract: A system, method, and apparatus for brake load alleviation amongst at least one first brake and at least one second brake is disclosed. The method involves sensing an amount of brake pedal application in response to engagement of at least brake pedal. The method further involves determining whether the amount of brake pedal application is greater than a brake pedal application threshold value. Also, the method involves generating a brake application profile, when it is determined that the amount of brake pedal application is greater than the brake pedal application threshold value. The brake application profile indicates that actuation of at least one first brake is delayed by a first time delay, and that actuation of at least one second brake is delayed by a second time delay. Further, the method involves actuating at least one first brake and at least one second brake according to the brake application profile.
Abstract translation: 公开了一种在至少一个第一制动器和至少一个第二制动器之间用于制动负载减轻的系统，方法和装置。 该方法包括响应于至少制动踏板的接合来感测制动踏板施加量。 该方法还包括确定制动踏板应用的量是否大于制动踏板应用阈值。 此外，当确定制动踏板应用的量大于制动踏板应用阈值时，该方法涉及产生制动施加轮廓。 制动应用轮廓指示至少一个第一制动器的致动被延迟第一时间延迟，并且至少一个第二制动器的致动被延迟第二时间延迟。 此外，该方法包括根据制动应用轮廓来致动至少一个第一制动器和至少一个第二制动器。
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公开(公告)号：US11037454B2
公开(公告)日：2021-06-15
申请号：US15343164
申请日：2016-11-03
Applicant: The Boeing Company
Inventor： Joseph Michael Wapenski , Nima Forghani , Thomas Todd Griffith
Abstract: An automatic braking system controller automatically decelerates an aircraft on a runway according to a brake-to-exit or a constant deceleration function. The automatic braking system controller determines whether the aircraft can decelerate to a selected velocity prior to reaching a target location along the runway. In response to determining that the aircraft can decelerate to the selected velocity prior to reaching the target location, the automatic braking system controller automatically decelerates the aircraft with a comfortable deceleration profile such that the aircraft reaches the selected velocity at the target location.
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公开(公告)号：US20180122250A1
公开(公告)日：2018-05-03
申请号：US15343164
申请日：2016-11-03
Applicant: The Boeing Company
Inventor： Joseph Michael Wapenski , Nima Forghani , Thomas Todd Griffith
IPC: G08G5/06
CPC classification number: G08G5/06 , B60T8/1703 , B64C25/426
Abstract: An automatic braking system controller automatically decelerates an aircraft on a runway according to a brake-to-exit or a constant deceleration function. The automatic braking system controller determines whether the aircraft can decelerate to a selected velocity prior to reaching a target location along the runway. In response to determining that the aircraft can decelerate to the selected velocity prior to reaching the target location, the automatic braking system controller automatically decelerates the aircraft with a comfortable deceleration profile such that the aircraft reaches the selected velocity at the target location.
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10.发明授权公开(公告)号：US09139293B2
公开(公告)日：2015-09-22
申请号：US14161492
申请日：2014-01-22
Applicant: THE BOEING COMPANY
Inventor： Thomas Todd Griffith
CPC classification number: B64C25/46 , B60T8/1703 , B60T8/172 , B60T8/176 , B60T8/17616 , B60T8/325
Abstract: Systems, methods, and apparatus for optimizing real-time antiskid control initialization for a vehicle on a travel surface are disclosed. In one or more embodiments, a method involves determining when at least one wheel of the vehicle touches ground. The method further involves calculating a rate of wheel spin up for at least one wheel. Also, the method involves determining whether the rate of wheel spin up exceeds a wheel spin up rate threshold. In addition, the method involves applying a high level of brake force when the rate of wheel spin up exceeds the wheel spin up rate threshold, and applying a low level of brake force when the rate of wheel spin up does not exceed the wheel spin up rate threshold.
Abstract translation: 公开了用于优化行驶表面上的车辆的实时防滑控制初始化的系统，方法和装置。 在一个或多个实施例中，一种方法包括确定车辆的至少一个车轮何时接地。 该方法还包括计算至少一个车轮的车轮旋转速率。 此外，该方法涉及确定车轮旋转速率是否超过车轮旋转速率阈值。 此外，该方法包括当车轮旋转速度超过车轮旋转速率阈值时施加高水平的制动力，并且当车轮旋转速度不超过车轮旋转时施加低水平的制动力 速率阈值。
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