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1. 发明授权

US08713987B2 On-board water spray system for aircraft 有权
标题翻译：机上喷水系统
公开(公告)号：US08713987B2
公开(公告)日：2014-05-06
申请号：US12760939
申请日：2010-04-15
申请人： Gary E. McKay
发明人： Gary E. McKay
IPC分类号： B64D47/00 , B64D43/00 , G01M17/06 , G01N19/02 , B60T8/56 , B60T17/22 , B64F5/00 , G01L5/28
CPC分类号： B05B12/126 , B60T8/56 , B60T17/221 , B60T2210/12 , B60T2210/13 , B60T2270/406 , B64C25/32 , B64D1/18 , B64F5/60 , G01N19/02 , Y10T137/6906
摘要： A system for simulating wet runway conditions by using a liquid container that is placed inside an aircraft. The liquid container is connected to a nozzle that sprays water in front of the wheels of the aircraft. A valve is used to control the flow of water from the nozzle. Systems, such as the braking system of the aircraft, can then be tested in wet runway conditions simulated by the system. The amount of water sprayed from the nozzle can also be electronically controlled in relation to the speed of the aircraft, such that the nozzle sprays a nearly uniform layer of liquid in front of the wheels. The system can also be modified to include two tanks to manipulate the center of gravity of the aircraft.
摘要翻译：一种用于通过使用放置在飞行器内的液体容器来模拟湿跑道状况的系统。液体容器连接到喷嘴，喷嘴在飞机的车轮前面。阀门用于控制来自喷嘴的水流。系统，例如飞机的制动系统，然后可以在由系统模拟的湿跑道条件下进行测试。从喷嘴喷射的水的量也可以相对于飞行器的速度进行电子控制，使得喷嘴在车轮前面喷射几乎均匀的液体层。该系统还可以修改为包括两个坦克来操纵飞机的重心。

2. 发明授权

US09315177B2 Antilock braking system with directional control 有权
标题翻译：防抱死制动系统带方向控制
公开(公告)号：US09315177B2
公开(公告)日：2016-04-19
申请号：US13419493
申请日：2012-03-14
申请人： Gary E. McKay
发明人： Gary E. McKay
IPC分类号： B60T8/17 , B64C25/46 , B64C25/48
CPC分类号： B60T8/1703 , B64C25/46 , B64C25/48
摘要： A system and method for adjusting a yaw of an aircraft having an antilock braking system is disclosed. The antilock braking system includes a controller configured to receive a directional input from a rudder. The controller is further configured to deliver a braking output to at least one of a left wheel brake and a right wheel brake. A position of the rudder indicates a pilot's desired steering response, and to allow for braking optimization by the antilock braking system, the pilot depresses fully the left wheel brake pedal and the right wheel brake pedal. The controller receives the directional input after both the right wheel brake pedal and the left wheel brake pedal have been fully depressed. The controller then delivers the braking output and a pressure on one of the left wheel brake and the right wheel brake is reduced in accordance with the directional input.
摘要翻译：公开了一种用于调整具有防抱死制动系统的飞行器的偏航的系统和方法。防抱死制动系统包括被配置为从方向舵接收定向输入的控制器。该控制器进一步构造成将制动输出传递给左轮制动器和右轮制动器中的至少一个。方向舵的位置表示飞行员所需的转向响应，并且为了允许防抱死制动系统进行制动优化，飞行员完全按下左轮制动踏板和右侧制动踏板。在右侧制动踏板和左侧制动踏板完全按下之后，控制器接收方向输入。然后，控制器输出制动输出，根据方向输入减小左侧制动器和右侧制动器之一上的压力。

3. 发明申请

US20130245907A1 Antilock Braking System With Directional Control 有权
标题翻译：具有定向控制的防抱死制动系统
公开(公告)号：US20130245907A1
公开(公告)日：2013-09-19
申请号：US13419493
申请日：2012-03-14
申请人： Gary E. McKay
发明人： Gary E. McKay
IPC分类号： B64C25/46 , B64C25/48 , B60T8/176
CPC分类号： B60T8/1703 , B64C25/46 , B64C25/48
摘要： A system and method for adjusting a yaw of an aircraft having an antilock braking system is disclosed. The antilock braking system includes a controller configured to receive a directional input from a rudder. The controller is further configured to deliver a braking output to at least one of a left wheel brake and a right wheel brake. A position of the rudder indicates a pilot's desired steering response, and to allow for braking optimization by the antilock braking system, the pilot depresses fully the left wheel brake pedal and the right wheel brake pedal. The controller receives the directional input after both the right wheel brake pedal and the left wheel brake pedal have been fully depressed. The controller then delivers the braking output and a pressure on one of the left wheel brake and the right wheel brake is reduced in accordance with the directional input.
摘要翻译：公开了一种用于调整具有防抱死制动系统的飞行器的偏航的系统和方法。防抱死制动系统包括被配置为从方向舵接收定向输入的控制器。该控制器进一步构造成将制动输出传递给左轮制动器和右轮制动器中的至少一个。方向舵的位置表示飞行员所需的转向响应，并且为了允许防抱死制动系统进行制动优化，飞行员完全按下左轮制动踏板和右侧制动踏板。在右侧制动踏板和左侧制动踏板完全按下之后，控制器接收方向输入。然后控制器输出制动输出，根据方向输入减小左轮制动器和右轮制动器之一上的压力。

4. 发明申请

US20110252863A1 On-Board Water Spray System For Aircraft 有权
标题翻译：机载喷水系统
公开(公告)号：US20110252863A1
公开(公告)日：2011-10-20
申请号：US12760939
申请日：2010-04-15
申请人： Gary E. McKay
发明人： Gary E. McKay
IPC分类号： G01N19/02
CPC分类号： B05B12/126 , B60T8/56 , B60T17/221 , B60T2210/12 , B60T2210/13 , B60T2270/406 , B64C25/32 , B64D1/18 , B64F5/60 , G01N19/02 , Y10T137/6906
摘要： A system for simulating wet runway conditions by using a liquid container that is placed inside an aircraft. The liquid container is connected to a nozzle that sprays water in front of the wheels of the aircraft. A valve is used to control the flow of water from the nozzle. Systems, such as the braking system of the aircraft, can then be tested in wet runway conditions simulated by the system. The amount of water sprayed from the nozzle can also be electronically controlled in relation to the speed of the aircraft, such that the nozzle sprays a nearly uniform layer of liquid in front of the wheels. The system can also be modified to include two tanks to manipulate the center of gravity of the aircraft.
摘要翻译：一种用于通过使用放置在飞行器内的液体容器来模拟湿跑道状况的系统。液体容器连接到喷嘴，喷嘴在飞机的车轮前面。阀门用于控制来自喷嘴的水流。系统，例如飞机的制动系统，然后可以在由系统模拟的湿跑道条件下进行测试。从喷嘴喷射的水的量也可以相对于飞行器的速度进行电子控制，使得喷嘴在车轮前面喷射几乎均匀的液体层。该系统还可以修改为包括两个坦克来操纵飞机的重心。

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