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1.发明授权公开(公告)号：US08332114B2
公开(公告)日：2012-12-11
申请号：US12516829
申请日：2007-11-08
Applicant: Andrew Whittingham
Inventor： Andrew Whittingham
CPC classification number: B60T17/221 , B60T8/1703 , B60T8/885 , B60T2270/413
Abstract: A braking system (1) for an aircraft which includes a by-pass control system (9) for activation when undemanded braking or loss of braking is detected. The braking system (1) comprises: a brake pedal transducer (2) for generating a brake pedal actuation signal when a brake pedal (3) is applied; brake actuation means (5) for activating a brake (6) on receipt of a braking signal; braking pressure transducer means (7) for generating a braking output signal related to the braking force applied to the brake (6); primary processing means (4) in electrical communication with the brake pedal transducer (2) and the brake actuation means (5) and adapted to generate a braking signal on receipt of a brake pedal actuation signal; secondary processing means (8) adapted to receive the brake pedal actuation signal and braking output signal; and a bypass braking control system (9) adapted to receive the brake pedal actuation signal from the brake pedal transducer (2) and generate a braking signal in response to the brake pedal actuation signal. The secondary processing means (8) is adapted to disable the primary processing means (4) and enable the bypass braking control system (9) on detection of undemanded braking or loss of braking from the brake pedal actuation signal and braking output signal.
Abstract translation: 一种用于飞行器的制动系统（1），其包括旁路控制系统（9），用于当未检测到制动或制动失败时激活。 制动系统（1）包括：制动踏板传感器（2），用于在施加制动踏板（3）时产生制动踏板致动信号; 用于在接收到制动信号时启动制动器（6）的制动器致动装置（5） 制动压力传感器装置（7），用于产生与施加到制动器（6）的制动力相关的制动输出信号; 与制动踏板换能器（2）和制动器致动装置（5）电连通并且适于在接收到制动踏板致动信号时产生制动信号的主处理装置（4） 适于接收制动踏板致动信号和制动输出信号的二次处理装置（8）; 以及旁路制动控制系统（9），其适于从制动踏板换能器（2）接收制动踏板致动信号，并且响应于制动踏板致动信号产生制动信号。 第二处理装置（8）适于禁止主处理装置（4），并且能够在旁路制动控制系统（9）检测到制动踏板致动信号和制动输出信号的制动不合格或制动损失。
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Patent Agency Ranking
公开(公告)号：US20090084637A1
公开(公告)日：2009-04-02
申请号：US11577757
申请日：2006-01-09
Applicant: David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
Inventor： David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
CPC classification number: F16D66/021 , F16D2066/001 , F16D2121/24
Abstract: Method and apparatus for monitoring electrically-actuated aircraft brakes includes measuring the break heat pack thickness to determine wear of the brake discs and adjusting the measurement so as to give ongoing compensation for temperature variations and hence expansion of the heat pack.
Abstract translation: 用于监测电动飞机制动器的方法和装置包括测量断裂热包厚度以确定制动盘的磨损并调节测量值，以便对温度变化进行持续的补偿并因此给予热包的膨胀。
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公开(公告)号：US20090114488A1
公开(公告)日：2009-05-07
申请号：US11577767
申请日：2006-01-09
Applicant: David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
Inventor： David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
CPC classification number: F16D66/02 , B60T13/74 , F16D2066/001 , F16D2121/24
Abstract: An electrically actuated aircraft brake with a carbon-carbon composite heat pack and an electrical actuator for engaging the heat pack and operating the brake. When the brake is not being applied, the brake actuator is adjusted in dependence upon temperature, for example, by controlling the actuator to maintain a temperature regulated position.
Abstract translation: 具有碳 - 碳复合热封的电动飞机制动器和用于接合散热器并操作制动器的电致动器。 当不施加制动器时，例如通过控制致动器来维持温度调节位置，根据温度来调节制动致动器。
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公开(公告)号：US08230983B2
公开(公告)日：2012-07-31
申请号：US11577767
申请日：2006-01-09
Applicant: David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
Inventor： David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
IPC: F16D55/36
CPC classification number: F16D66/02 , B60T13/74 , F16D2066/001 , F16D2121/24
Abstract: An electrically actuated aircraft brake with a carbon-carbon composite heat pack and an electrical actuator for engaging the heat pack and operating the brake. When the brake is not being applied, the brake actuator is adjusted in dependence upon temperature, for example, by controlling the actuator to maintain a temperature regulated position.
Abstract translation: 具有碳 - 碳复合热封的电动飞机制动器和用于接合散热器并操作制动器的电致动器。 当不施加制动器时，例如通过控制致动器来维持温度调节位置，根据温度来调节制动致动器。
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公开(公告)号：US07673721B2
公开(公告)日：2010-03-09
申请号：US11577757
申请日：2006-01-09
Applicant: David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
Inventor： David Alexander Bailey , Jonathan Deric Lumb , Andrew Whittingham
IPC: F16D55/36
CPC classification number: F16D66/021 , F16D2066/001 , F16D2121/24
Abstract: Method and apparatus for monitoring electrically-actuated aircraft brakes includes measuring the break heat pack thickness to determine wear of the brake discs and adjusting the measurement so as to give ongoing compensation for temperature variations and hence expansion of the heat pack.
Abstract translation: 用于监测电动飞机制动器的方法和装置包括测量断裂热包厚度以确定制动盘的磨损并调节测量值，以便对温度变化进行持续的补偿并因此给予热包的膨胀。
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6.发明申请BRAKING SYSTEM FOR AN AIRCRAFT AND A METHOD OF MONITORING BRAKING FOR AN AIRCRAFT 有权用于飞机的制动系统和用于监视飞机制动器的方法公开(公告)号：US20100057320A1
公开(公告)日：2010-03-04
申请号：US12516829
申请日：2007-11-08
Applicant: Andrew Whittingham
Inventor： Andrew Whittingham
CPC classification number: B60T17/221 , B60T8/1703 , B60T8/885 , B60T2270/413
Abstract: A braking system (1) for an aircraft which includes a by-pass control system (9) for activation when undemanded braking or loss of braking is detected. The braking system (1) comprises: a brake pedal transducer (2) for generating a brake pedal actuation signal when a brake pedal (3) is applied; brake actuation means (5) for activating a brake (6) on receipt of a braking signal; braking pressure transducer means (7) for generating a braking output signal related to the braking force applied to the brake (6); primary processing means (4) in electrical communication with the brake pedal transducer (2) and the brake actuation means (5) and adapted to generate a braking signal on receipt of a brake pedal actuation signal; secondary processing means (8) adapted to receive the brake pedal actuation signal and braking output signal; and a bypass braking control system (9) adapted to receive the brake pedal actuation signal from the brake pedal transducer (2) and generate a braking signal in response to the brake pedal actuation signal. The secondary processing means (8) is adapted to disable the primary processing means (4) and enable the bypass braking control system (9) on detection of undemanded braking or loss of braking from the brake pedal actuation signal and braking output signal.
Abstract translation: 一种用于飞行器的制动系统（1），其包括旁路控制系统（9），用于当未检测到制动或制动失败时激活。 制动系统（1）包括：制动踏板传感器（2），用于在施加制动踏板（3）时产生制动踏板致动信号; 用于在接收到制动信号时启动制动器（6）的制动器致动装置（5） 制动压力传感器装置（7），用于产生与施加到制动器（6）的制动力相关的制动输出信号; 与制动踏板换能器（2）和制动器致动装置（5）电连通并且适于在接收到制动踏板致动信号时产生制动信号的主处理装置（4） 适于接收制动踏板致动信号和制动输出信号的二次处理装置（8）; 以及旁路制动控制系统（9），其适于从制动踏板换能器（2）接收制动踏板致动信号，并且响应于制动踏板致动信号产生制动信号。 第二处理装置（8）适于禁止主处理装置（4），并且能够在旁路制动控制系统（9）检测到制动踏板致动信号和制动输出信号的制动不合格或制动损失。
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