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1.发明授权Locating parts with electromagnetic identification (EMID) tags for contextual visualization 有权使用电磁识别（EMID）标签定位用于上下文可视化的部件公开(公告)号：US09576167B2
公开(公告)日：2017-02-21
申请号：US14303440
申请日：2014-06-12
Applicant: THE BOEING COMPANY
Inventor： Anil Kumar , Winfeng Li , Arun Ayyagari , Kevin Y. Ung , Sudhakar S. Shetty
CPC classification number: G06K7/10366 , G01S13/75 , G06K7/10099 , G06K7/10386
Abstract: In one or more embodiments, a disclosed method involves transmitting a first transmit signal(s) having a first signal strength and/or a first field of view (FOV), thereby establishing a first radiation region. The method further involves receiving a first receive signal(s) radiated from an EMID tag(s). Also, the method involves transmitting a second transmit signal(s) having a second signal strength and/or a second field of view (FOV), thereby establishing a second radiation region. In addition, the method involves receiving a second receive signal(s) radiated from an EMID tag(s). Additionally, the method involves subtracting the second radiation region from the first radiation region to determine a difference region. Also, the method involves determining which of the EMID tags are located within the difference region by using the first receive signal(s) and the second receive signal(s). Further, the method involves determining a location of the EMID tag(s) located within the difference region.
Abstract translation: 在一个或多个实施例中，所公开的方法包括发送具有第一信号强度和/或第一视场（FOV）的第一发射信号，由此建立第一辐射区域。 该方法还包括接收从一个或多个EMID标签辐射的第一接收信号。 此外，该方法涉及发送具有第二信号强度和/或第二视场（FOV）的第二发射信号，由此建立第二辐射区域。 另外，该方法包括接收从一个或多个EMID标签辐射的第二接收信号。 另外，该方法包括从第一辐射区域减去第二辐射区域以确定差分区域。 此外，该方法涉及通过使用第一接收信号和第二接收信号来确定哪个EMID标签位于差分区域内。 此外，该方法涉及确定位于差异区域内的EMID标签的位置。
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2.发明授权Methods and systems for use in analyzing cyber-security threats in an aviation platform 有权用于分析航空平台中网络安全威胁的方法和系统公开(公告)号：US09171167B2
公开(公告)日：2015-10-27
申请号：US13922825
申请日：2013-06-20
Applicant: The Boeing Company
Inventor： Arun Ayyagari , Winfeng Li , John Eric Bush , Sudhakar S. Shetty , Brian C. Grubel , Dion S. Reid
CPC classification number: G06F21/577 , H04B7/18506 , H04L63/1433
Abstract: Methods and systems for use in in analyzing cyber-security threats for an aircraft are described herein. One example method includes generating an interconnection graph for a plurality of interconnected aircraft systems. The interconnection graph includes a plurality of nodes and a plurality of links. The method also includes defining a cost function for a cyber-security threat to traverse each link and defining a requirements function for a cyber-security threat to exploit each node. The method further includes generating a set of threat traversal graphs for each cyber-security threat of a plurality of cyber-security threats.
Abstract translation: 本文描述了用于分析飞机的网络安全威胁的方法和系统。 一个示例性方法包括生成多个互连飞行器系统的互连图。 互连图包括多个节点和多个链路。 该方法还包括定义用于网络安全威胁的成本函数，以遍历每个链接，并为网络安全威胁定义需求函数以利用每个节点。 该方法还包括为多个网络安全威胁的每个网络安全威胁生成一组威胁遍历图。
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公开(公告)号：US20140341309A1
公开(公告)日：2014-11-20
申请号：US13897243
申请日：2013-05-17
Applicant: The Boeing Company
Inventor： Nha Thanh Nguyen , Anil Kumar , Timothy M. Mitchell , Radhakrishna G. Sampigethaya , Arun Ayyagari , Sudhakar S. Shetty
IPC: H04B3/54
CPC classification number: H04B3/54 , H04B2203/5408 , H04B2203/5466
Abstract: Provided are methods and systems for terrestrial data transmission between aircrafts and external networks connected to gates at airports. This type of data transmission is performed through an electrical power cable that includes multiple conductors interconnecting electrical components of an aircraft and a gate. Each conductor may be used to establish a separate broadband over power line (BPL) communication channel using its own frequency range that does not overlap with frequency ranges of other channels. As such, no radio frequency (RF) shielding is needed in the cable and any standard multi-conductor cable may be used. A channel management unit is used to control allocation of data domains among different communication channels depending on characteristics of the data domains, characteristics of the channels, and other factors. For example, one channel may be designated for secure data transfer of specific data domains, such as aircraft control data.
Abstract translation: 提供了飞机与外部网络之间的地面数据传输的方法和系统，这些网络连接到机场的大门。 这种类型的数据传输通过电力电缆进行，该电力电缆包括互连飞行器和门的电气部件的多个导体。 每个导体可以用于使用其与其它信道的频率范围不重叠的其自身频率范围来建立单独的宽带电力线（BPL）通信信道。 因此，在电缆中不需要射频（RF）屏蔽，并且可以使用任何标准的多导体电缆。 信道管理单元用于根据数据域的特性，信道的特性以及其他因素来控制不同通信信道中的数据域的分配。 例如，可以指定一个信道用于特定数据域的安全数据传输，例如飞行器控制数据。
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公开(公告)号：US09667316B2
公开(公告)日：2017-05-30
申请号：US13897243
申请日：2013-05-17
Applicant: The Boeing Company
Inventor： Nha Thanh Nguyen , Anil Kumar , Timothy M. Mitchell , Radhakrishna G. Sampigethaya , Arun Ayyagari , Sudhakar S. Shetty
IPC: H04B3/54
CPC classification number: H04B3/54 , H04B2203/5408 , H04B2203/5466
Abstract: Provided are methods and systems for terrestrial data transmission between aircrafts and external networks connected to gates at airports. This type of data transmission is performed through an electrical power cable that includes multiple conductors interconnecting electrical components of an aircraft and a gate. Each conductor may be used to establish a separate broadband over power line (BPL) communication channel using its own frequency range that does not overlap with frequency ranges of other channels. As such, no radio frequency (RF) shielding is needed in the cable and any standard multi-conductor cable may be used. A channel management unit is used to control allocation of data domains among different communication channels depending on characteristics of the data domains, characteristics of the channels, and other factors. For example, one channel may be designated for secure data transfer of specific data domains, such as aircraft control data.
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5.发明申请ENERGY-HARVESTING-BASED CONTROL AND COMMUNICATION FOR A CABIN SERVICES SYSTEM 有权基于能量收集的控制和通信为客舱服务系统公开(公告)号：US20160347453A1
公开(公告)日：2016-12-01
申请号：US14721787
申请日：2015-05-26
Applicant: THE BOEING COMPANY
Inventor： Arun Ayyagari , Sudhakar S. Shetty , Scott Edward Marston , Venkata Prabhakar
CPC classification number: B64D11/0015 , B64D11/00155 , B64D45/00 , B64D2011/0053 , H04L67/12
Abstract: A passenger control unit is provided that may include a push-button, power assembly, and control and communication circuitry. The push-button may be for control of a passenger service unit (PSU) onboard a passenger vehicle, and may also generate mechanical energy when pushed. The power assembly may convert the mechanical energy to electrical energy, and store the electrical energy, solely from which the control and communication circuitry may be powered. The control and communication circuitry may include a microprocessor and a communications interface. The microprocessor may receive an indication when the push-button is pushed, and generate an instruction to control the PSU in response thereto. And the communications interface wirelessly transmit the instruction to a control unit configured to effect control of the PSU based thereon.
Abstract translation: 提供了一个乘客控制单元，其可以包括按钮，电源组件以及控制和通信电路。 按钮可以用于控制乘客车辆上的乘客服务单元（PSU），并且还可以在推动时产生机械能量。 功率组件可以将机械能转换成电能，并存储电能，仅由控制和通信电路供电。 控制和通信电路可以包括微处理器和通信接口。 当按下按钮时，微处理器可以接收指示，并响应于此产生一个控制PSU的指令。 并且通信接口将指令无线地发送到配置为基于其实现对PSU的控制的控制单元。
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Patent Agency Ranking
6.发明申请LOCATING PARTS WITH ELECTROMAGNETIC IDENTIFICATION (EMID) TAGS FOR CONTEXTUAL VISUALIZATION 有权具有电磁识别（EMID）标签的定位部件，用于实现可视化公开(公告)号：US20150363616A1
公开(公告)日：2015-12-17
申请号：US14303440
申请日：2014-06-12
Applicant: THE BOEING COMPANY
Inventor： Anil Kumar , Winfeng Li , Arun Ayyagari , Kevin Y. Ung , Sudhakar S. Shetty
IPC: G06K7/10
CPC classification number: G06K7/10366 , G01S13/75 , G06K7/10099 , G06K7/10386
Abstract: In one or more embodiments, a disclosed method involves transmitting a first transmit signal(s) having a first signal strength and/or a first field of view (FOV), thereby establishing a first radiation region. The method further involves receiving a first receive signal(s) radiated from an EMID tag(s). Also, the method involves transmitting a second transmit signal(s) having a second signal strength and/or a second field of view (FOV), thereby establishing a second radiation region. In addition, the method involves receiving a second receive signal(s) radiated from an EMID tag(s). Additionally, the method involves subtracting the second radiation region from the first radiation region to determine a difference region. Also, the method involves determining which of the EMID tags are located within the difference region by using the first receive signal(s) and the second receive signal(s). Further, the method involves determining a location of the EMID tag(s) located within the difference region.
Abstract translation: 在一个或多个实施例中，所公开的方法包括发送具有第一信号强度和/或第一视场（FOV）的第一发射信号，由此建立第一辐射区域。 该方法还包括接收从一个或多个EMID标签辐射的第一接收信号。 此外，该方法涉及发送具有第二信号强度和/或第二视场（FOV）的第二发射信号，由此建立第二辐射区域。 另外，该方法包括接收从一个或多个EMID标签辐射的第二接收信号。 另外，该方法包括从第一辐射区域减去第二辐射区域以确定差分区域。 此外，该方法涉及通过使用第一接收信号和第二接收信号来确定哪个EMID标签位于差分区域内。 此外，该方法涉及确定位于差异区域内的EMID标签的位置。
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7.发明授权Energy-harvesting-based control and communication for a cabin services system 有权基于能量收集的控制和通信为客舱服务系统公开(公告)号：US09533762B2
公开(公告)日：2017-01-03
申请号：US14721787
申请日：2015-05-26
Applicant: THE BOEING COMPANY
Inventor： Arun Ayyagari , Sudhakar S. Shetty , Scott Edward Marston , Venkata Prabhakar
CPC classification number: B64D11/0015 , B64D11/00155 , B64D45/00 , B64D2011/0053 , H04L67/12
Abstract: A passenger control unit is provided that may include a push-button, power assembly, and control and communication circuitry. The push-button may be for control of a passenger service unit (PSU) onboard a passenger vehicle, and may also generate mechanical energy when pushed. The power assembly may convert the mechanical energy to electrical energy, and store the electrical energy, solely from which the control and communication circuitry may be powered. The control and communication circuitry may include a microprocessor and a communications interface. The microprocessor may receive an indication when the push-button is pushed, and generate an instruction to control the PSU in response thereto. And the communications interface wirelessly transmit the instruction to a control unit configured to effect control of the PSU based thereon.
Abstract translation: 提供了一个乘客控制单元，其可以包括按钮，电源组件以及控制和通信电路。 按钮可以用于控制乘客车辆上的乘客服务单元（PSU），并且还可以在推动时产生机械能量。 功率组件可以将机械能转换成电能，并存储电能，仅由控制和通信电路供电。 控制和通信电路可以包括微处理器和通信接口。 当按下按钮时，微处理器可以接收指示，并响应于此产生一个控制PSU的指令。 并且通信接口将指令无线地发送到配置为基于其实现对PSU的控制的控制单元。
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8.发明授权Systems and methods for physical security of information flows over a power cable connection 有权通过电力电缆连接的信息物理安全的系统和方法公开(公告)号：US09100104B2
公开(公告)日：2015-08-04
申请号：US13888008
申请日：2013-05-06
Applicant: The Boeing Company
Inventor： Nha Thanh Nguyen , Timothy M. Mitchell , Anil Kumar , Radhakrishna G. Sampigethaya , Arun Ayyagari , Sudhakar S. Shetty
CPC classification number: H04B3/56 , H04B3/54 , H04B3/542 , H04B7/18506 , H04B2203/5445 , H04B2203/5487 , H04L12/10 , H04L67/12
Abstract: An aircraft includes a first electrical connector configured to couple with a first power cable, a first data communication network and a first modem coupled to first electrical connector and first data communication network and is configured to transmit data received at first electrical connector through first power cable to first data communication network and to transmit data from first data communication network to first power cable through first electrical connector. The aircraft additionally includes a second electrical connector configured to couple with a second power cable, a second data communication network and a second modem coupled to second electrical connector and to second data communication network and is configured to transmit data received at second electrical connector through second power cable to second data communication network and to transmit data from second data communication network to second power cable through second electrical connector.
Abstract translation: 飞机包括第一电连接器，其被配置为与第一电力电缆，第一数据通信网络和耦合到第一电连接器和第一数据通信网络的第一调制解调器耦合，并且被配置为通过第一电力电缆 到第一数据通信网络并且通过第一电连接器将数据从第一数据通信网络传输到第一电力电缆。 飞机还包括第二电连接器，其被配置为与第二电力电缆，第二数据通信网络和耦合到第二电连接器的第二调制解调器和第二数据通信网络耦合，并且被配置为通过第二电缆将第二电连接器上接收的数据 电力电缆连接到第二数据通信网络，并通过第二电连接器将数据从第二数据通信网络传输到第二电力电缆。
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9.发明申请SYSTEMS AND METHODS FOR PHYSICAL SECURITY OF INFORMATION FLOWS OVER A POWER CABLE CONNECTION 有权通过电力电缆连接进行信息流的物理安全的系统和方法公开(公告)号：US20150023437A1
公开(公告)日：2015-01-22
申请号：US13888008
申请日：2013-05-06
Applicant: The Boeing Company
Inventor： Nha Thanh Nguyen , Timothy M. Mitchell , Anil Kumar , Radhakrishna G. Sampigethaya , Arun Ayyagari , Sudhakar S. Shetty
CPC classification number: H04B3/56 , H04B3/54 , H04B3/542 , H04B7/18506 , H04B2203/5445 , H04B2203/5487 , H04L12/10 , H04L67/12
Abstract: An aircraft includes a first electrical connector configured to couple with a first power cable, a first data communication network and a first modem coupled to first electrical connector and first data communication network and is configured to transmit data received at first electrical connector through first power cable to first data communication network and to transmit data from first data communication network to first power cable through first electrical connector. The aircraft additionally includes a second electrical connector configured to couple with a second power cable, a second data communication network and a second modem coupled to second electrical connector and to second data communication network and is configured to transmit data received at second electrical connector through second power cable to second data communication network and to transmit data from second data communication network to second power cable through second electrical connector.
Abstract translation: 飞机包括第一电连接器，其被配置为与第一电力电缆，第一数据通信网络和耦合到第一电连接器和第一数据通信网络的第一调制解调器耦合，并且被配置为通过第一电力电缆 到第一数据通信网络并且通过第一电连接器将数据从第一数据通信网络传输到第一电力电缆。 飞机还包括第二电连接器，其被配置为与第二电力电缆，第二数据通信网络和耦合到第二电连接器的第二调制解调器和第二数据通信网络耦合，并且被配置为通过第二电缆将第二电连接器上接收的数据 电力电缆连接到第二数据通信网络，并通过第二电连接器将数据从第二数据通信网络传输到第二电力电缆。
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10.发明申请METHODS AND SYSTEMS FOR USE IN ANALYZING CYBER-SECURITY THREATS IN AN AVIATION PLATFORM 有权用于分析航空平台中的安全威胁的方法和系统公开(公告)号：US20140380485A1
公开(公告)日：2014-12-25
申请号：US13922825
申请日：2013-06-20
Applicant: The Boeing Company
Inventor： Arun Ayyagari , Winfeng Li , John Eric Bush , Sudhakar S. Shetty , Brian C. Grubel , Dion S. Reid
IPC: G06F21/57
CPC classification number: G06F21/577 , H04B7/18506 , H04L63/1433
Abstract: Methods and systems for use in in analyzing cyber-security threats for an aircraft are described herein. One example method includes generating an interconnection graph for a plurality of interconnected aircraft systems. The interconnection graph includes a plurality of nodes and a plurality of links. The method also includes defining a cost function for a cyber-security threat to traverse each link and defining a requirements function for a cyber-security threat to exploit each node. The method further includes generating a set of threat traversal graphs for each cyber-security threat of a plurality of cyber-security threats.
Abstract translation: 本文描述了用于分析飞机的网络安全威胁的方法和系统。 一个示例性方法包括生成多个互连飞行器系统的互连图。 互连图包括多个节点和多个链路。 该方法还包括定义用于网络安全威胁的成本函数，以遍历每个链接，并为网络安全威胁定义需求函数以利用每个节点。 该方法还包括为多个网络安全威胁的每个网络安全威胁生成一组威胁遍历图。
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