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1.发明申请METHODS AND SYSTEMS FOR PRIORITIZING REPLACEMENT OF AT LEAST ONE PART FOR VEHICLE FAULT ANALYSIS 有权用于车辆故障分析的最小一次替换的方法和系统公开(公告)号：US20160364285A1
公开(公告)日：2016-12-15
申请号：US14737604
申请日：2015-06-12
Applicant: THE BOEING COMPANY
Inventor： Michael T. Swayne , Samantha Schwartz , Matthew B. Hendrian , Lukasz Domaradzki , Nima Barraci
IPC: G06F11/07
CPC classification number: G06F11/0793 , G06F11/0739 , G06Q10/063
Abstract: Methods and systems are provided for prioritizing a plurality of maintenance corrective actions in a troubleshooting chart for a device are provided. The method includes receiving, by a processor, an input from a user indicative of a successful corrective action from the plurality of corrective actions on the troubleshooting chart and incrementing a value of a counter associated with the successful corrective action. The processor then compares values for counters associated with each of the plurality of corrective actions and displays the plurality of corrective actions in hierarchal order based on the values of the counters.
Abstract translation: 提供了方法和系统，用于在提供用于设备的故障排除图表中对多个维护校正动作进行优先级排序。 所述方法包括由处理器从所述用户指示来自所述故障排除图表上的所述多个校正动作的成功校正动作的输入，并且增加与所述成功校正动作相关联的计数器的值。 然后处理器比较与多个校正动作中的每一个相关联的计数器的值，并且基于计数器的值以分级顺序显示多个校正动作。
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2.发明申请公开(公告)号：US20250067224A1
公开(公告)日：2025-02-27
申请号：US18454839
申请日：2023-08-24
Applicant: THE BOEING COMPANY
Inventor： Forest Sutton , Stephen Solomon Altus , Samantha Schwartz , Hendrik Schoeniger , Michael Christian Büddefeld , Maximilian Peter Juengst , Salin Maharjan , Andrea Sanzone
Abstract: A system includes one or more control units configured to determine one or more fuel consumption models for an aircraft. A method includes determining, by one or more control units, one or more fuel consumption models for an aircraft. A non-transitory computer-readable storage medium comprising executable instructions that, in response to execution, cause one or more control units comprising a processor, to perform operations including determining one or more fuel consumption models for an aircraft.
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3.发明授权公开(公告)号：US12276231B2
公开(公告)日：2025-04-15
申请号：US18454839
申请日：2023-08-24
Applicant: THE BOEING COMPANY
Inventor： Forest Sutton , Stephen Solomon Altus , Samantha Schwartz , Hendrik Schoeniger , Michael Christian Büddefeld , Maximilian Peter Juengst , Salin Maharjan , Andrea Sanzone
Abstract: A system includes one or more control units configured to determine one or more fuel consumption models for an aircraft. A method includes determining, by one or more control units, one or more fuel consumption models for an aircraft. A non-transitory computer-readable storage medium comprising executable instructions that, in response to execution, cause one or more control units comprising a processor, to perform operations including determining one or more fuel consumption models for an aircraft.
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公开(公告)号：US10399696B2
公开(公告)日：2019-09-03
申请号：US15252994
申请日：2016-08-31
Applicant: THE BOEING COMPANY
Inventor： Samantha Schwartz , Katie M. Reid
Abstract: A yaw feedback system for use by an aircraft is provided. The yaw feedback system includes a processor, a runway centerline indicator, and a yaw feedback indicator. The processor is configured to determine a yaw difference between a current track of the aircraft and a runway centerline. The runway centerline indicator is configured to virtually extend a runway visual range (RVR) for a pilot of the aircraft. The yaw feedback indicator is coupled to the processor and configured to prompt the pilot for a yaw input to compensate for the yaw difference.
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Patent Agency Ranking
公开(公告)号：US20180057187A1
公开(公告)日：2018-03-01
申请号：US15252994
申请日：2016-08-31
Applicant: THE BOEING COMPANY
Inventor： Samantha Schwartz , Katie M. Reid
CPC classification number: B64D43/00 , B64C13/04 , B64C13/042 , B64D45/0005 , G01C23/00 , G08G5/0021 , G08G5/0065
Abstract: A yaw feedback system for use by an aircraft is provided. The yaw feedback system includes a processor, a runway centerline indicator, and a yaw feedback indicator. The processor is configured to determine a yaw difference between a current track of the aircraft and a runway centerline. The runway centerline indicator is configured to virtually extend a runway visual range (RVR) for a pilot of the aircraft. The yaw feedback indicator is coupled to the processor and configured to prompt the pilot for a yaw input to compensate for the yaw difference.
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公开(公告)号：US20250019091A1
公开(公告)日：2025-01-16
申请号：US18350791
申请日：2023-07-12
Applicant: THE BOEING COMPANY
Inventor： Michael-Christian Büddefeld , Hendrik Schöniger , Samantha Schwartz , Forest Sutton
Abstract: A system and a method include a control unit configured to determine one or more fuel levels for an aircraft at one or more arrival airports for one or more alternate flight plans that divert from an original flight plan. The control unit is configured to determine the one or more fuel levels based on traffic at the one or more arrival airports, and performance data for the aircraft.
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公开(公告)号：US20230386346A1
公开(公告)日：2023-11-30
申请号：US17825195
申请日：2022-05-26
Applicant: THE BOEING COMPANY
Inventor： Samantha Schwartz , Millie Irene Sterling , Theresa Emsbach , Brian Azcuenaga , Jeffrey Lee Williams , Aaron Pilcher
CPC classification number: G08G5/0039 , G08G5/0021 , G01C21/20 , G06F3/0482
Abstract: A system and a method include a rerouting control unit configured to generate one or more reroute options for an aircraft based on an analysis of a current position of the aircraft, a predicted future position of the aircraft, a current position of an in-flight hazard, a predicted future position of the in-flight hazard, and one or both of: (i) a flight path of one or more other aircraft within an airspace, or (ii) one or both of a minimum amount of fuel of the aircraft or a minimum weight of the aircraft at a destination location.
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公开(公告)号：US10909858B2
公开(公告)日：2021-02-02
申请号：US16145705
申请日：2018-09-28
Applicant: THE BOEING COMPANY
Inventor： Samantha Schwartz , Melissa Irene Blackstun , Theresa Ernsbach , Brian Azcuenaga , Stephen Solomon Altus , Aaron Pilcher , Jeffrey Lee Williams
Abstract: An aircraft management system and method includes a flight plan diversion prediction system including a rerouting control unit that is configured to generate one or more reroute options for an aircraft based on an analysis of a current position of the aircraft, a predicted future position of the aircraft, a current position of an in-flight hazard, and a predicted future position of the in-flight hazard.
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9.发明授权公开(公告)号：US09740554B2
公开(公告)日：2017-08-22
申请号：US14737604
申请日：2015-06-12
Applicant: THE BOEING COMPANY
Inventor： Michael T. Swayne , Samantha Schwartz , Matthew B. Hendrian , Lukasz Domaradzki , Nima Barraci
CPC classification number: G06F11/0793 , G06F11/0739 , G06Q10/063
Abstract: Methods and systems are provided for prioritizing a plurality of maintenance corrective actions in a troubleshooting chart for a device are provided. The method includes receiving, by a processor, an input from a user indicative of a successful corrective action from the plurality of corrective actions on the troubleshooting chart and incrementing a value of a counter associated with the successful corrective action. The processor then compares values for counters associated with each of the plurality of corrective actions and displays the plurality of corrective actions in hierarchal order based on the values of the counters.
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