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公开(公告)号:US09503175B2
公开(公告)日:2016-11-22
申请号:US14299078
申请日:2014-06-09
Applicant: Honeywell International Inc.
Inventor: Thomas D. Judd , Sandra J. Howe-Ryberg , Darshan Gandhi
CPC classification number: H04B7/18506 , H04B7/18513
Abstract: An aerospace communication system comprises a communication management unit; a first communication device configured to transmit and receive data over a first communication network; and a second communication device configured to transmit and receive data over a second communication network. The first communication device is coupled to a corresponding interface of the communication management unit. The second communication device is communicatively separated from the communication management unit by the first communication device such that the communication management unit is unaware of the second communication device. The first communication device includes routing logic configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device for transmission over the second communication network.
Abstract translation: 航空航天通信系统包括通信管理单元; 配置为经由第一通信网络发送和接收数据的第一通信设备; 以及第二通信设备,被配置为通过第二通信网络发送和接收数据。 第一通信设备耦合到通信管理单元的相应接口。 第二通信设备由第一通信设备与通信管理单元通信地分离,使得通信管理单元不知道第二通信设备。 第一通信设备包括配置成确定是否通过第一通信网络发送从通信管理单元接收的每个消息或者通过第二通信网络发送的第二通信设备的路由逻辑。
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公开(公告)号:US10319239B2
公开(公告)日:2019-06-11
申请号:US14448923
申请日:2014-07-31
Applicant: Honeywell International Inc.
Inventor: Rakesh Kumar , Maria John Paul Dominic , Vivek Kumar Pandey , Siva Kommuri , Darshan Gandhi
Abstract: Systems and methods for context based controller pilot data link communication (CPDLC) are provided. In certain implementations, a method for CPDLC includes receiving data through the selection of a selectable item on a pilot interface, wherein the pilot interface is a non-CPDLC interface and communicating the data to a CPDLC application. Further, the method also includes constructing a CPDLC message based on the data; and transmitting the CPDLC message to an air traffic controller.
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公开(公告)号:US09420620B2
公开(公告)日:2016-08-16
申请号:US14501454
申请日:2014-09-30
Applicant: Honeywell International Inc.
Inventor: Sandra J. Howe-Ryberg , Darshan Gandhi
Abstract: Systems and methods for aircraft on-ground determination are provided. In one embodiment, an onboard motion controlled wireless avionics datalink gateway comprises: a wireless radio chipset module; and a velocity interlock coupled to an aircraft motion sensor and the wireless radio chipset module. The wireless radio chipset module is configured to establish one or more intra-aircraft radio communication links with one or more onboard avionics system, and wherein the wireless radio chipset module is configure to establish one or more external radio communication links with at least one ground-based wireless communication system. The aircraft motion sensor is configured to output to the velocity interlock an aircraft motion signal indicative of a velocity of an aircraft in which the gateway is installed. The velocity interlock enables and disables the one or more intra-aircraft radio communication links and the one or more external radio communication links based on the aircraft motion signal.
Abstract translation: 提供了飞机地面测定的系统和方法。 在一个实施例中,车载运动控制无线航空电子数据链路网关包括:无线无线电芯片组模块; 以及耦合到飞行器运动传感器和无线无线电芯片组模块的速度互锁。 无线无线芯片组模块被配置为与一个或多个机载航空电子系统建立一个或多个飞行中无线电通信链路,并且其中无线无线芯片组模块被配置为与至少一个地面无线电芯片组模块建立一个或多个外部无线电通信链路, 基于无线通信系统。 飞行器运动传感器被配置为输出速度互锁,指示其中安装有网关的飞行器的速度的飞行器运动信号。 速度联锁基于飞行器运动信号使一个或多个飞机内无线电通信链路和一个或多个外部无线电通信链路起作用和禁用。
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公开(公告)号:US20160095150A1
公开(公告)日:2016-03-31
申请号:US14501454
申请日:2014-09-30
Applicant: Honeywell International Inc.
Inventor: Sandra J. Howe-Ryberg , Darshan Gandhi
Abstract: Systems and methods for aircraft on-ground determination are provided. In one embodiment, an onboard motion controlled wireless avionics datalink gateway comprises: a wireless radio chipset module; and a velocity interlock coupled to an aircraft motion sensor and the wireless radio chipset module. The wireless radio chipset module is configured to establish one or more intra-aircraft radio communication links with one or more onboard avionics system, and wherein the wireless radio chipset module is configure to establish one or more external radio communication links with at least one ground-based wireless communication system. The aircraft motion sensor is configured to output to the velocity interlock an aircraft motion signal indicative of a velocity of an aircraft in which the gateway is installed. The velocity interlock enables and disables the one or more intra-aircraft radio communication links and the one or more external radio communication links based on the aircraft motion signal.
Abstract translation: 提供了飞机地面测定的系统和方法。 在一个实施例中,车载运动控制无线航空电子数据链路网关包括:无线无线电芯片组模块; 以及耦合到飞行器运动传感器和无线无线电芯片组模块的速度互锁。 无线无线芯片组模块被配置为与一个或多个机载航空电子系统建立一个或多个飞行中无线电通信链路,并且其中无线无线芯片组模块被配置为与至少一个地面无线电芯片组模块建立一个或多个外部无线电通信链路, 基于无线通信系统。 飞行器运动传感器被配置为输出速度互锁,指示其中安装有网关的飞行器的速度的飞行器运动信号。 速度联锁基于飞行器运动信号使一个或多个飞机内无线电通信链路和一个或多个外部无线电通信链路起作用和禁用。
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公开(公告)号:US20160035227A1
公开(公告)日:2016-02-04
申请号:US14448923
申请日:2014-07-31
Applicant: Honeywell International Inc.
Inventor: Rakesh Kumar , Maria John Paul Dominic , Vivek Kumar Pandey , Siva Kommuri , Darshan Gandhi
IPC: G08G5/00
CPC classification number: G08G5/0013 , G01C23/00 , G08G5/0021
Abstract: Systems and methods for context based controller pilot data link communication (CPDLC) are provided. In certain implementations, a method for CPDLC includes receiving data through the selection of a selectable item on a pilot interface, wherein the pilot interface is a non-CPDLC interface and communicating the data to a CPDLC application. Further, the method also includes constructing a CPDLC message based on the data; and transmitting the CPDLC message to an air traffic controller.
Abstract translation: 提供了基于上下文的控制器导频数据链路通信(CPDLC)的系统和方法。 在某些实施方式中,CPDLC的方法包括通过在导频接口上选择可选项目来接收数据,其中导频接口是非CPDLC接口并将数据传送到CPDLC应用。 此外,该方法还包括基于该数据构建CPDLC消息; 以及将CPDLC消息发送到空中交通管制员。
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公开(公告)号:US20150222351A1
公开(公告)日:2015-08-06
申请号:US14299078
申请日:2014-06-09
Applicant: Honeywell International Inc.
Inventor: Thomas D. Judd , Sandra J. Howe-Ryberg , Darshan Gandhi
IPC: H04B7/185
CPC classification number: H04B7/18506 , H04B7/18513
Abstract: An aerospace communication system comprises a communication management unit; a first communication device configured to transmit and receive data over a first communication network; and a second communication device configured to transmit and receive data over a second communication network. The first communication device is coupled to a corresponding interface of the communication management unit. The second communication device is communicatively separated from the communication management unit by the first communication device such that the communication management unit is unaware of the second communication device. The first communication device includes routing logic configured to determine whether to send each message received from the communication management unit over the first communication network or to the second communication device for transmission over the second communication network.
Abstract translation: 航空航天通信系统包括通信管理单元; 配置为经由第一通信网络发送和接收数据的第一通信设备; 以及第二通信设备,被配置为通过第二通信网络发送和接收数据。 第一通信设备耦合到通信管理单元的相应接口。 第二通信设备由第一通信设备与通信管理单元通信地分离,使得通信管理单元不知道第二通信设备。 第一通信设备包括配置成确定是否通过第一通信网络发送从通信管理单元接收的每个消息或者通过第二通信网络发送的第二通信设备的路由逻辑。
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