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公开(公告)号：US09472110B2
公开(公告)日：2016-10-18
申请号：US14095037
申请日：2013-12-03
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Muthukumar Murthy , Alpana Priyamvada , Rocco DiVito
CPC classification number: G08G5/06 , G08G5/0021 , G08G5/065
Abstract: An aircraft taxi path guidance and display system is provided. The aircraft taxi path guidance and display system includes or cooperates with at least one source of aircraft status data, and a source of airport feature data associated with an airport field. The aircraft taxi path guidance and display system includes a processor operationally coupled to the source of aircraft status data and to the source of airport feature data. In response to aircraft status data and airport feature data, the processor predicts undesired deviations from an active surface area (e.g., an excursion). The processor generates corrective action associated with the excursion, and displays symbology that is graphically representative of the corrective action.
Abstract translation: 提供飞机出租车路径指导和显示系统。 飞机出租车路径指导和显示系统包括或与至少一个飞行器状态数据源配合，以及与机场领域相关联的机场特征数据源。 飞机出租车路径指导和显示系统包括可操作地耦合到飞机状态数据源和机场特征数据源的处理器。 响应于飞机状态数据和机场特征数据，处理器预测与有效表面区域（例如，偏移）的不期望的偏差。 处理器产生与偏移相关联的校正动作，并显示以图形方式代表校正动作的符号系统。
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公开(公告)号：US09787101B2
公开(公告)日：2017-10-10
申请号：US14480820
申请日：2014-09-09
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rocco DiVito , Hassan Ali Kojori , Nicolae Morcov , Wayne Pearson , Cristian Anghel
IPC: H02J4/00 , B60L7/16 , B64C25/40 , B64C25/42 , H02J7/00 , H02P3/14 , H02J1/00 , H02J7/14 , H02J7/34 , B60L7/10
CPC classification number: H02J4/00 , B60L7/10 , B60L7/16 , B60L11/1862 , B60L11/1868 , B60L2200/10 , B60L2210/10 , B60L2220/42 , B60L2240/547 , B64C25/405 , B64C25/42 , B64D2221/00 , H02J1/00 , H02J1/08 , H02J1/12 , H02J7/0055 , H02J7/14 , H02J7/345 , H02J2007/0059 , H02P3/14 , Y02T10/646 , Y02T10/7005 , Y02T10/7044 , Y02T10/7066 , Y02T10/7216 , Y02T50/823
Abstract: An electrical system for an aircraft with an electric taxi system (ETS), the electrical system may include at least one traction motor, a DC link and at least one traction-motor bidirectional DC-AC converter interposed between the at least one traction motor and the DC link. An engine-driven power source may be configured to provide DC power to the DC link or extract DC power from the DC link. A battery unit may be configured to provide DC power to the DC link or extract DC power from the DC link. An adaptive power controller may be interconnected with the power source, the battery unit and the at least one traction-motor bidirectional DC-AC converter and configured to regulate voltage of DC power delivered to the DC link.
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公开(公告)号：US20160070266A1
公开(公告)日：2016-03-10
申请号：US14480820
申请日：2014-09-09
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Rocco DiVito , Hassan Ali Kojori , Nicolae Morcov , Wayne Pearson , Cristian Anghel
CPC classification number: H02J4/00 , B60L7/10 , B60L7/16 , B60L11/1862 , B60L11/1868 , B60L2200/10 , B60L2210/10 , B60L2220/42 , B60L2240/547 , B64C25/405 , B64C25/42 , B64D2221/00 , H02J1/00 , H02J1/08 , H02J1/12 , H02J7/0055 , H02J7/14 , H02J7/345 , H02J2007/0059 , H02P3/14 , Y02T10/646 , Y02T10/7005 , Y02T10/7044 , Y02T10/7066 , Y02T10/7216 , Y02T50/823
Abstract: An electrical system for an aircraft with an electric taxi system (ETS), the electrical system may include at least one traction motor, a DC link and at least one traction-motor bidirectional DC-AC converter interposed between the at least one traction motor and the DC link. An engine-driven power source may be configured to provide DC power to the DC link or extract DC power from the DC link. A battery unit may be configured to provide DC power to the DC link or extract DC power from the DC link. An adaptive power controller may be interconnected with the power source, the battery unit and the at least one traction-motor bidirectional DC-AC converter and configured to regulate voltage of DC power delivered to the DC link.
Abstract translation: 一种用于具有电动出租车系统（ETS）的飞机的电气系统，所述电气系统可以包括至少一个牵引电动机，DC链路和至少一个牵引电动机双向DC-AC转换器，其被插入在所述至少一个牵引电动机和 直流链路。 发动机驱动的电源可以被配置为向DC链路提供DC电力或从DC链路提取DC电力。 电池单元可以被配置为向DC链路提供DC电力或从DC链路提取DC电力。 自适应功率控制器可以与电源，电池单元和至少一个牵引电动机双向DC-AC转换器互连，并且被配置为调节传递到DC链路的DC功率的电压。
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公开(公告)号：US20150154874A1
公开(公告)日：2015-06-04
申请号：US14095037
申请日：2013-12-03
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Muthukumar Murthy , Alpana Priyamvada , Rocco DiVito
IPC: G08G5/06
CPC classification number: G08G5/06 , G08G5/0021 , G08G5/065
Abstract: An aircraft taxi path guidance and display system is provided. The aircraft taxi path guidance and display system includes or cooperates with at least one source of aircraft status data, and a source of airport feature data associated with an airport field. The aircraft taxi path guidance and display system includes a processor operationally coupled to the source of aircraft status data and to the source of airport feature data. In response to aircraft status data and airport feature data, the processor predicts undesired deviations from an active surface area (e.g., an excursion). The processor generates corrective action associated with the excursion, and displays symbology that is graphically representative of the corrective action.
Abstract translation: 提供飞机出租车路径指导和显示系统。 飞机出租车路径指导和显示系统包括或与至少一个飞行器状态数据源配合，以及与机场领域相关联的机场特征数据源。 飞机出租车路径指导和显示系统包括可操作地耦合到飞机状态数据源和机场特征数据源的处理器。 响应于飞机状态数据和机场特征数据，处理器预测与有效表面区域（例如，偏移）的不期望的偏差。 处理器产生与偏移相关联的校正动作，并显示以图形方式代表校正动作的符号系统。
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