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公开(公告)号：US20150108283A1
公开(公告)日：2015-04-23
申请号：US14056475
申请日：2013-10-17
申请人： The Boeing Company
发明人： Adam Marshall Thoreen , Joshua Jay Baer , Joseph Adam Sikora , Matthew August Lassen , Michael Edwin Foster , Timothy P. Gallagher
CPC分类号： B64D45/0005 , B64C3/38 , B64C3/56 , B64C9/00 , B64C13/04 , B64C23/065 , B64C23/072 , B64C2009/005 , B64D45/00 , Y02T50/14 , Y02T50/145 , Y02T50/164
摘要： A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.
摘要翻译： 一种翼尖控制系统的方法和装置。 翼尖控制系统包括用于飞行器的驾驶舱和控制器的开关系统。 开关系统被配置成被置于无效状态并产生一个布防信号。 控制器与交换机系统通信。 控制器被配置为响应于在飞行器的操作期间发生的事件，从开关系统接收布防信号，在视觉上指示飞行器在开关系统中的翼尖的期望位置，并且产生移动指令以移动翼尖 。
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公开(公告)号：US20160280392A1
公开(公告)日：2016-09-29
申请号：US15080586
申请日：2016-03-25
申请人： The Boeing Company
发明人： Adam Marshall Thoreen , Joshua Jay Baer , Joseph Adam Sikora , Matthew August Lassen , Michael Edwin Foster , Timothy P. Gallagher
CPC分类号： B64D45/0005 , B64C3/38 , B64C3/56 , B64C9/00 , B64C13/04 , B64C23/065 , B64C23/072 , B64C2009/005 , B64D45/00 , Y02T50/14 , Y02T50/145 , Y02T50/164
摘要： A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.
摘要翻译： 一种翼尖控制系统的方法和装置。 翼尖控制系统包括用于飞行器的驾驶舱和控制器的开关系统。 开关系统被配置成被置于无效状态并产生一个布防信号。 控制器与交换机系统通信。 控制器被配置为响应于在飞行器的操作期间发生的事件，从开关系统接收布防信号，在视觉上指示飞行器在开关系统中的翼尖的期望位置，并且产生移动指令以移动翼尖 。
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公开(公告)号：US09950810B2
公开(公告)日：2018-04-24
申请号：US15080586
申请日：2016-03-25
申请人： The Boeing Company
发明人： Adam Marshall Thoreen , Joshua Jay Baer , Joseph Adam Sikora , Matthew August Lassen , Michael Edwin Foster , Timothy Patrick Gallagher, Jr.
CPC分类号： B64D45/0005 , B64C3/38 , B64C3/56 , B64C9/00 , B64C13/04 , B64C23/065 , B64C23/072 , B64C2009/005 , B64D45/00 , Y02T50/14 , Y02T50/145 , Y02T50/164
摘要： A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.
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公开(公告)号：US09296472B2
公开(公告)日：2016-03-29
申请号：US14056475
申请日：2013-10-17
申请人： The Boeing Company
发明人： Adam Marshall Thoreen , Joshua Jay Baer , Joseph Adam Sikora , Matthew August Lassen , Michael Edwin Foster , Timothy P. Gallagher
CPC分类号： B64D45/0005 , B64C3/38 , B64C3/56 , B64C9/00 , B64C13/04 , B64C23/065 , B64C23/072 , B64C2009/005 , B64D45/00 , Y02T50/14 , Y02T50/145 , Y02T50/164
摘要： A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.
摘要翻译： 一种翼尖控制系统的方法和装置。 翼尖控制系统包括用于飞行器的驾驶舱和控制器的开关系统。 开关系统被配置成被置于无效状态并产生一个布防信号。 控制器与交换机系统通信。 控制器被配置为响应于在飞行器的操作期间发生的事件，从开关系统接收布防信号，在视觉上指示飞行器在开关系统中的翼尖的期望位置，并且产生移动指令以移动翼尖 。
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