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    • 2. 发明授权
    • Systems and methods for enhancing situational awareness of an aircraft on the ground
    • 增强地面飞机情境意识的系统和方法
    • US08242950B2
    • 2012-08-14
    • US11451648
    • 2006-06-12
    • Cyro A. StoneGregory T. StaytonCharles C. Manberg
    • Cyro A. StoneGregory T. StaytonCharles C. Manberg
    • G01S13/00
    • G08G5/0078G01S7/04G01S13/74G01S13/931G01S2013/9335G01S2013/9339G01S2013/9353G08G5/0008G08G5/0021G08G5/0065
    • A delineated collision avoidance system may comprise a processor for executing one or more instructions that implement one or more functions of the collision avoidance system, a transceiver for transmitting information from and receiving information for the host aircraft, and memory for storing the one or more instructions for execution by the processor to implement the one or more functions of the collision avoidance system to: receive from the transceiver information from another aircraft, generate from the received information a track for the other aircraft, and determine whether the track will intersect within a predefined period of time a region of interest around the host aircraft. In a variation, the system may include a display and the memory may include instructions to: determine whether a predefined condition is satisfied and change an appearance of a symbol shown on the display to indicate that the predefined condition is satisfied.
    • 描绘的防撞系统可以包括用于执行实现冲突避免系统的一个或多个功能的一个或多个指令的处理器,用于从主机飞行器发送信息并且接收主机的信息的收发器,以及用于存储一个或多个指令的存储器 用于由处理器执行以实现冲突避免系统的一个或多个功能:从来自另一飞行器的收发器信息接收从所接收的信息生成另一飞行器的轨道,并且确定轨道是否将在预定义的范围内相交 时间段是主机周围的一个感兴趣的区域。 在一个变型中,系统可以包括显示器,并且存储器可以包括以下指令:确定是否满足预定义条件,并且改变显示器上所示的符号的外观以指示满足预定条件。
    • 5. 发明申请
    • Integrated avionics system
    • 综合航电系统
    • US20080174472A1
    • 2008-07-24
    • US11786988
    • 2007-04-10
    • Cyro A. StoneJames R. TroxelGregory T. Stayton
    • Cyro A. StoneJames R. TroxelGregory T. Stayton
    • G01S13/93
    • G08G5/04G08G5/0021G08G5/0086
    • There is provided an avionics system that provides several avionics functions within a single LRU. In one embodiment, the system comprises a software-configurable RF assembly, one or more processor assemblies that are configured to provide multiple TAWS/TCAS/Mode S/ADS-B/ATC functions, interfaces to allow connections to aircraft electronics and data loaders, and multipurpose antennas. In one embodiment, a common processor architecture allows generic avionics processors to be configured to operate a number of TAWS/TCAS/Mode S/ADS-B/ATC functions without the need for multiple LRUs, and software-defined RF functions allow RF circuitry that interfaces to the processors to handle current and future communication needs.
    • 提供了一个航空电子系统,可在单个LRU内提供多种航空电子设备功能。 在一个实施例中,系统包括可配置软件的RF组件,被配置为提供多个TAWS / TCAS /模式S / ADS-B / ATC功能的一个或多个处理器组件,允许连接到飞行器电子设备和数据加载器的接口, 和多功能天线。 在一个实施例中,通用处理器架构允许通用航空电子设备处理器被配置为操作多个TAWS / TCAS /模式S / ADS-B / ATC功能,而不需要多个LRU,并且软件定义的RF功能允许RF电路 与处理器的接口,以处理当前和未来的通信需求。
    • 6. 发明申请
    • INTEGRATED AVIONICS SYSTEM
    • 综合航空系统
    • US20150248838A1
    • 2015-09-03
    • US14320182
    • 2014-06-30
    • Cyro A. StoneJames R. TroxelGregory T. Stayton
    • Cyro A. StoneJames R. TroxelGregory T. Stayton
    • G08G5/04G08G5/00
    • G08G5/04G08G5/0021G08G5/0086
    • There is provided an avionics system that provides several avionics functions within a single LRU. In one embodiment, the system comprises a software-configurable RF assembly, one or more processor assemblies that are configured to provide multiple TAWS/TCAS/Mode S/ADS-B/ATC functions, interfaces to allow connections to aircraft electronics and data loaders, and multipurpose antennas. In one embodiment, a common processor architecture allows generic avionics processors to be configured to operate a number of TAWS/TCAS/Mode S/ADS-B/ATC functions without the need for multiple LRUs, and software-defined RF functions allow RF circuitry that interfaces to the processors to handle current and future communication needs.
    • 提供了一个航空电子系统,可在单个LRU内提供多种航空电子设备功能。 在一个实施例中,系统包括可配置软件的RF组件,被配置为提供多个TAWS / TCAS /模式S / ADS-B / ATC功能的一个或多个处理器组件,允许连接到飞行器电子设备和数据加载器的接口, 和多功能天线。 在一个实施例中,通用处理器架构允许通用航空电子设备处理器被配置为操作多个TAWS / TCAS /模式S / ADS-B / ATC功能,而不需要多个LRU,并且软件定义的RF功能允许RF电路 与处理器的接口,以处理当前和未来的通信需求。
    • 7. 发明授权
    • Integrated avionics system
    • 综合航电系统
    • US08768540B2
    • 2014-07-01
    • US11786988
    • 2007-04-10
    • Cyro A. StoneJames R. TroxelGregory T. Stayton
    • Cyro A. StoneJames R. TroxelGregory T. Stayton
    • G01C23/00
    • G08G5/04G08G5/0021G08G5/0086
    • There is provided an avionics system that provides several avionics functions within a single LRU. In one embodiment, the system comprises a software-configurable RF assembly, one or more processor assemblies that are configured to provide multiple TAWS/TCAS/Mode S/ADS-B/ATC functions, interfaces to allow connections to aircraft electronics and data loaders, and multipurpose antennas. In one embodiment, a common processor architecture allows generic avionics processors to be configured to operate a number of TAWS/TCAS/Mode S/ADS-B/ATC functions without the need for multiple LRUs, and software-defined RF functions allow RF circuitry that interfaces to the processors to handle current and future communication needs.
    • 提供了一个航空电子系统,可在单个LRU内提供多种航空电子设备功能。 在一个实施例中,系统包括可配置软件的RF组件,被配置为提供多个TAWS / TCAS /模式S / ADS-B / ATC功能的一个或多个处理器组件,允许连接到飞行器电子设备和数据加载器的接口, 和多功能天线。 在一个实施例中,通用处理器架构允许通用航空电子设备处理器被配置为操作多个TAWS / TCAS /模式S / ADS-B / ATC功能,而不需要多个LRU,并且软件定义的RF功能允许RF电路 与处理器的接口,以处理当前和未来的通信需求。