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公开(公告)号：US11011836B2
公开(公告)日：2021-05-18
申请号：US15384954
申请日：2016-12-20
Applicant: The Boeing Company
Inventor： Jeffrey D. Postetter , William Preston Geren , Hwai-Kee Tsiang , Timothy Allen Murphy
Abstract: A system for mitigating radio frequency interference includes a multiple patch antenna array including a multiplicity of patch antenna elements. The multiple patch antenna array is positioned relative to an interfering antenna such that signals from the interfering antenna cause interference with the multiple patch antenna array. The system also includes an auxiliary antenna positioned relative to the multiple patch antenna array. The system additionally includes a device to generate a spatial null in a direction to the interfering antenna from the multiple patch antenna array in response to a first signal from the auxiliary antenna and a second signal from the multiple patch antenna array. The first signal and the second signal are generated in response to a transmitted signal being received by the auxiliary antenna and the multiple patch antenna array. The spatial null permits simultaneous operation of the multiple patch antenna array and the interfering antenna.
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公开(公告)号：US20170082455A1
公开(公告)日：2017-03-23
申请号：US14858235
申请日：2015-09-18
Applicant: The Boeing Company
Inventor： Charles Otis Adler , Ted Eigle , William Raymond Richards , Timothy Allen Murphy , John Harvey Roberson , Thomas Jose Thalakottur , Ricardo Messias Fricks , Fadl Ibrahim Khalil , Steven Mark Walstrom , Daniel Bruce Holton , Jessie Turner , Timothy Edward Jackson
CPC classification number: G01C23/00 , B64D45/00 , B64D2045/0045 , B64D2045/0065 , G01S13/91 , G01S19/17 , G01S2205/002 , G07C5/008 , G07C5/085 , G08G5/0013 , G08G5/0021 , G08G5/0056
Abstract: A method, apparatus, and aircraft tracker system for reporting state information for an aircraft. A state of the aircraft is identified using sensor data received from an aircraft sensor system in the aircraft. The state information is transmitted at a reporting rate set using the state of the aircraft identified from the sensor data, at least one of a crew command or a ground command when at least one of the crew command is received from a crew interface or the ground command is received from a ground source, and a policy defining priorities for reporting that are based on at least one of the crew command, the ground command, or the state of the aircraft identified from the sensor data.
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3.发明申请公开(公告)号：US20130282209A1
公开(公告)日：2013-10-24
申请号：US13920355
申请日：2013-06-18
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy
CPC classification number: G01C23/00 , B64D45/04 , G01S7/003 , G01S13/882 , G01S19/32 , G05D1/0676 , G08G5/0021 , G08G5/025
Abstract: A monitor on-board an aircraft which uses radio altitude measurements as the basic observable altitude during runway approach. The basic concept utilizes the aircraft's navigation system, which includes means to store and retrieve radio altitude thresholds as a function of the distance along the desired path from the runway thresholds. These threshold functions are determined in advance based on a radio altitude reference which is defined as the expected radio altimeter measurement that would be made if the airplane were exactly on the desired reference path. Vertical containment monitoring is achieved by comparing the radio altitude measurement to computed thresholds for both too high and too low. During the approach, an annunciation message can be generated if the radio altitude measurement is above or below the threshold limits.
Abstract translation: 飞机上的监视器，其使用无线电高度测量作为跑道进近期间的基本可观测高度。 基本概念利用飞机的导航系统，其中包括存储和检索无线电高度阈值的方式，作为沿着跑道阈值所需路径的距离的函数。 这些阈值函数是基于无线电高度参考预先确定的，该无线电高度参考被定义为如果飞机正好位于期望的参考路径上将要进行的预期无线电高度计测量。 通过将无线电高度测量值与计算的阈值进行比较来实现垂直安全监控，这两者都是太高和过低的。 在接近期间，如果无线电高度测量值高于或低于阈值限度，则可以生成通知消息。
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公开(公告)号：US20190025436A1
公开(公告)日：2019-01-24
申请号：US16142555
申请日：2018-09-26
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy
Abstract: An apparatus and method of delivering an alert from an aircraft to a search and rescue system. An alert from an aircraft is received via a communications satellite. The alert comprises identification information identifying the aircraft and position information identifying the position of the aircraft. In response to receiving the alert, an emulated distress radio beacon signal is generated. The emulated distress radio beacon signal comprises the identification information and the position information in a standard format of a signal generated by a distress radio beacon. The emulated distress radio beacon signal is broadcast from a location other than the aircraft as an emulated distress radio beacon transmission that is configured to be received and processed by the search and rescue system.
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公开(公告)号：US20180175496A1
公开(公告)日：2018-06-21
申请号：US15384954
申请日：2016-12-20
Applicant: The Boeing Company
Inventor： Jeffrey D. Postetter , William Preston Geren , Hwai-Kee Tsiang , Timothy Allen Murphy
CPC classification number: H01Q1/523 , H01Q1/521 , H01Q3/2629 , H01Q21/065 , H04B1/126
Abstract: A system for mitigating radio frequency interference includes a multiple patch antenna array including a multiplicity of patch antenna elements. The multiple patch antenna array is positioned relative to an interfering antenna such that signals from the interfering antenna cause interference with the multiple patch antenna array. The system also includes an auxiliary antenna positioned relative to the multiple patch antenna array. The system additionally includes a device to generate a spatial null in a direction to the interfering antenna from the multiple patch antenna array in response to a first signal from the auxiliary antenna and a second signal from the multiple patch antenna array. The first signal and the second signal are generated in response to a transmitted signal being received by the auxiliary antenna and the multiple patch antenna array. The spatial null permits simultaneous operation of the multiple patch antenna array and the interfering antenna.
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Patent Agency Ranking
公开(公告)号：US20170052258A1
公开(公告)日：2017-02-23
申请号：US14832879
申请日：2015-08-21
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy
CPC classification number: G01S19/14 , G01S5/0027 , G01S19/17 , G01S19/24 , G01S19/34 , G01S19/35 , G01S19/42 , G08G5/0013 , G08G5/0021 , G08G5/0056 , G08G5/0082
Abstract: A method and apparatus for tracking the position of an aircraft. A tracking device comprises a satellite navigation system receiver, a satellite communications transceiver, and a processor hermetically sealed within a housing attached on an outside of the aircraft. The satellite navigation system receiver is used to identify the position of the aircraft using navigation signals received from a satellite navigation system. The processor generates position information identifying the position of the aircraft as identified using the navigation system receiver. The processor sends the position information to a receiving station via a communications satellite in a low Earth orbit using the satellite communications transceiver. The position information is automatically generated by the processor and sent to the receiving station at a desired rate.
Abstract translation: 一种追踪飞机位置的方法和装置。 跟踪装置包括卫星导航系统接收器，卫星通信收发器和密封在附接在飞机外部的壳体内的处理器。 卫星导航系统接收机用于使用从卫星导航系统接收的导航信号来识别飞机的位置。 处理器产生识别使用导航系统接收器识别的飞机的位置的位置信息。 处理器通过使用卫星通信收发器的低地球轨道中的通信卫星将位置信息发送到接收站。 位置信息由处理器自动生成并以期望的速率发送到接收站。
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公开(公告)号：US10030995B2
公开(公告)日：2018-07-24
申请号：US14858235
申请日：2015-09-18
Applicant: The Boeing Company
Inventor： Charles Otis Adler , Ted Eigle , William Raymond Richards , Timothy Allen Murphy , John Harvey Roberson , Thomas Jose Thalakottur , Ricardo Messias Fricks , Fadl Ibrahim Khalil , Steven Mark Walstrom , Daniel Bruce Holton , Jessie Turner , Timothy Edward Jackson
CPC classification number: G01C23/00 , B64D45/00 , B64D45/0059 , B64D2045/0065 , G01S13/91 , G01S19/17 , G01S2205/002 , G07C5/008 , G07C5/085 , G08G5/0013 , G08G5/0021 , G08G5/0056
Abstract: A method, apparatus, and aircraft tracker system for reporting state information for an aircraft. A state of the aircraft is identified using sensor data received from an aircraft sensor system in the aircraft. The state information is transmitted at a reporting rate set using the state of the aircraft identified from the sensor data, at least one of a crew command or a ground command when at least one of the crew command is received from a crew interface or the ground command is received from a ground source, and a policy defining priorities for reporting that are based on at least one of the crew command, the ground command, or the state of the aircraft identified from the sensor data.
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公开(公告)号：US09964646B2
公开(公告)日：2018-05-08
申请号：US14832879
申请日：2015-08-21
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy
CPC classification number: G01S19/14 , G01S5/0027 , G01S19/17 , G01S19/24 , G01S19/34 , G01S19/35 , G01S19/42 , G08G5/0013 , G08G5/0021 , G08G5/0056 , G08G5/0082
Abstract: A method and apparatus for tracking the position of an aircraft. A tracking device comprises a satellite navigation system receiver, a satellite communications transceiver, and a processor hermetically sealed within a housing attached on an outside of the aircraft. The satellite navigation system receiver is used to identify the position of the aircraft using navigation signals received from a satellite navigation system. The processor generates position information identifying the position of the aircraft as identified using the navigation system receiver. The processor sends the position information to a receiving station via a communications satellite in a low Earth orbit using the satellite communications transceiver. The position information is automatically generated by the processor and sent to the receiving station at a desired rate.
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9.发明授权Device, system and methods using angle of arrival measurements for ADS-B authentication and navigation 有权使用ADS-B认证和导航的到达角测量装置，系统和方法公开(公告)号：US09476962B2
公开(公告)日：2016-10-25
申请号：US13875749
申请日：2013-05-02
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy , William Matthew Harris
CPC classification number: G01S19/04 , G01S3/043 , G01S3/46 , G01S5/0072 , G01S5/021 , G01S5/08 , G01S19/215
Abstract: The present disclosure is directed to a receiver for Automatic Dependent Surveillance Broadcast (ADS-B) verification of a target aircraft including a first input for receiving flight tracking information from a target aircraft that indicates positional information of the target aircraft. The receiver further includes a second input for receiving positional and heading information indicating the location and orientation of a multi-element array antenna configured to be attached to the receiver, and a processing module that generates a measured bearing derived from angle of arrival data, and an expected bearing of the target aircraft derived from the indicated positional information of the target aircraft and the positional and heading information defining the receiver location and orientation. A comparator compares the expected bearing to the measured bearing and verifies the ADS-B flight tracking information of the target aircraft and outputs an indication of authenticity based on the verification.
Abstract translation: 本公开涉及用于目标飞行器的自动相关监视广播（ADS-B）验证的接收机，其包括用于从目标飞行器接收指示目标飞行器的位置信息的飞行跟踪信息的第一输入。 接收机还包括第二输入端，用于接收指示被配置为附接到接收机的多元件阵列天线的位置和方向的位置和方位信息;以及处理模块，其生成从到达数据数据得到的测量轴承，以及 从目标飞行器的指示的位置信息得到的目标飞行器的预期方位和定义接收机位置和方向的位置和航向信息。 比较器将预期方向与测量方位进行比较，并验证目标飞机的ADS-B航班跟踪信息，并根据验证输出真实性指示。
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公开(公告)号：US11163067B2
公开(公告)日：2021-11-02
申请号：US16838990
申请日：2020-04-02
Applicant: The Boeing Company
Inventor： Timothy Allen Murphy , William Matthew Harris , Janet Suzanne Booth
Abstract: An interface device that enables a GNSS-based precision approach through the Ground Base Augmentation System (GBAS) function known as the GNSS Landing System (GLS) and/or through Satellite Based Augmentation Systems (SBAS) based Localizer Performance with Vertical Guidance (LPV). The GLS interface device allows a GLS-capable multi-mode receiver to be used on a non-GLS-capable airplane without extensive changes to other airplane systems. The GLS interface device works by intercepting information to and from the multi-mode receiver and modifying the information to make the interface compatible with an airplane that uses ILS guidance. Similarly, the information modifications will make the airplane appear to the multi-mode receiver as if it were a GLS-capable airplane.
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