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    Systems and methods for sonic boom aware flight planning
    1.
    发明授权
    Systems and methods for sonic boom aware flight planning 有权

    公开(公告)号：US10699584B2

    公开(公告)日：2020-06-30

    申请号：US15910072

    申请日：2018-03-02

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Jerry Ball ,  Troy Nichols ,  Mark A. Giddings

    IPC: G08G5/00 ,  G01C23/00 ,  B64C30/00

    Abstract: Flight planning systems and methods are provided, which augment supersonic flight planning via the integration of sonic boom forecast data. In embodiments, the flight planning system includes a display device, a pilot input interface, and a controller architecture coupled to the display device and to the pilot input interface. During system operation, the controller architecture receives flight plan criteria entered via the pilot input interface. The controller architecture then endeavors to generate or construct a boom-regulated flight plan, which includes at least one supersonic flight plan segment, in accordance with the flight plan criteria. If unable to construct a boom-regulated flight plan, the controller architecture generates a visual notification on the display device. The visual notification can include, for example, a warning that an excessive sonic boom or overpressure event may occur during execution of the flight plan by an aircraft, absent modifications to the flight plan.

    SYSTEM AND METHOD FOR DISPLAYING A RUNWAY POSITION INDICATOR
    3.
    发明申请
    SYSTEM AND METHOD FOR DISPLAYING A RUNWAY POSITION INDICATOR 有权
    用于显示跑道位置指示器的系统和方法

    公开(公告)号：US20140354456A1

    公开(公告)日：2014-12-04

    申请号：US13904241

    申请日：2013-05-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Aaron Gannon ,  Ivan Sandy Wyatt ,  Troy Nichols ,  John G. Suddreth

    IPC: G08G5/00

    CPC classification number: G08G5/025 ,  G08G5/0021 ,  G08G5/0047

    Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.

    Abstract translation: 一个动态跑道指示器显示在一个保形跑道上，以协助飞行员完成在跑道上着陆的方法。 动态跑道指示器包括多边形，其通过相对于保形跑道改变位置，向飞行员提供高级仪表线索，用于调整飞行器飞行路径到达跑道的正常或推荐路径以降落，从而辅助飞行员 提高进场和落地的准确性和安全性。

    System and method for displaying a runway position indicator
    5.
    发明授权
    System and method for displaying a runway position indicator 有权
    用于显示跑道位置指示器的系统和方法

    公开(公告)号：US09129521B2

    公开(公告)日：2015-09-08

    申请号：US13904241

    申请日：2013-05-29

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Aaron Gannon ,  Ivan Sandy Wyatt ,  Troy Nichols ,  John G. Suddreth

    IPC: G01C21/00 ,  G08G5/00 ,  G08G5/02

    CPC classification number: G08G5/025 ,  G08G5/0021 ,  G08G5/0047

    Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.

    Abstract translation: 一个动态跑道指示器显示在一个保形跑道上，以协助飞行员完成在跑道上着陆的方法。 动态跑道指示器包括多边形，其通过相对于保形跑道改变位置，向飞行员提供高级仪表线索，用于调整飞行器飞行路径到达跑道的正常或推荐路径以降落，从而辅助飞行员 提高进场和落地的准确性和安全性。

    SYSTEM AND METHODS FOR RENDERING TAXIWAY AND RUNWAY SIGNAGE IN A SYNTHETIC DISPLAY OF AN AIRPORT FIELD
    6.
    发明申请
    SYSTEM AND METHODS FOR RENDERING TAXIWAY AND RUNWAY SIGNAGE IN A SYNTHETIC DISPLAY OF AN AIRPORT FIELD 审中-公开
    在机场合成显示中提高税费和运行信号的系统和方法

    公开(公告)号：US20130231853A1

    公开(公告)日：2013-09-05

    申请号：US13890568

    申请日：2013-05-09

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Thea L. Feyereisen ,  Troy Nichols ,  John G. Suddreth ,  Ivan Sandy Wyatt ,  Jary Engels ,  Gang He

    IPC: G08G5/00

    CPC classification number: G08G5/0043 ,  G01C21/00 ,  G01C23/00 ,  G08G5/0021 ,  G08G5/065

    Abstract: A system and methods of displaying airport field features on a flight deck display element of an aircraft are provided. The flight deck display system obtains geographic position data and heading data for the aircraft, accesses airport feature data associated with synthetic graphical representations of an airport field, and renders a dynamic synthetic display of the airport field on the flight deck display element. The dynamic synthetic display is rendered in accordance with the geographic position data, the heading data, and the airport feature data. In certain embodiments the synthetic display includes graphical representations of taxiways/runways, along with signage that is conformally rendered on the exposed taxiway surfaces. Display characteristics of the signage may be influenced by the actual physical and/or temporal proximity of the aircraft relative to reference locations on the airport field. In some embodiments, the taxiway/runway signage includes dynamic directional indicators corresponding to the intended directions of travel on the taxiways/runways. Moreover, the taxiway/runway signage can be dynamically rendered in a forward-facing manner at all times on the flight deck display element.

    Abstract translation: 提供了一种在飞机的飞行甲板显示元件上显示机场场特征的系统和方法。 飞行甲板显示系统获取飞机的地理位置数据和航标数据，访问与机场领域的合成图形表示相关联的机场特征数据，并且在飞行甲板显示单元上呈现机场场的动态合成显示。 根据地理位置数据，标题数据和机场特征数据，呈现动态合成显示。 在某些实施例中，合成显示器包括滑行道/跑道的图形表示，以及在暴露的滑行道表面上保形地呈现的标牌。 标牌的显示特征可能受飞机相对于机场领域的参考位置的实际物理和/或时间接近度的影响。 在一些实施例中，滑行道/跑道标牌包括对应于滑行道/跑道上的行驶方向的动态方向指示器。 此外，滑行道/跑道标牌可以在飞行甲板显示元件上始终以向前的方式动态地呈现。

    SYSTEM AND METHOD FOR DISPLAYING A RUNWAY POSITION INDICATOR
    8.
    发明申请
    SYSTEM AND METHOD FOR DISPLAYING A RUNWAY POSITION INDICATOR 审中-公开
    用于显示跑道位置指示器的系统和方法

    公开(公告)号：US20150371545A1

    公开(公告)日：2015-12-24

    申请号：US14840908

    申请日：2015-08-31

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Aaron Gannon ,  Ivan Sandy Wyatt ,  Troy Nichols ,  John G. Suddreth

    IPC: G08G5/02

    CPC classification number: G08G5/025 ,  G08G5/0021 ,  G08G5/0047

    Abstract: A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.

    Abstract translation: 一个动态跑道指示器显示在一个保形跑道上，以协助飞行员完成在跑道上着陆的方法。 动态跑道指示器包括多边形，其通过相对于保形跑道改变位置，向飞行员提供高级仪表线索，用于调整飞行器飞行路径到达跑道的正常或推荐路径以降落，从而辅助飞行员 提高进场和落地的准确性和安全性。

    SYSTEMS AND METHODS FOR SONIC BOOM AWARE FLIGHT PLANNING
    9.
    发明申请
    SYSTEMS AND METHODS FOR SONIC BOOM AWARE FLIGHT PLANNING 审中-公开

    公开(公告)号：US20190272762A1

    公开(公告)日：2019-09-05

    申请号：US15910072

    申请日：2018-03-02

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： John G. Suddreth ,  Jerry Ball ,  Troy Nichols ,  Mark A. Giddings

    IPC: G08G5/00

    Abstract: Flight planning systems and methods are provided, which augment supersonic flight planning via the integration of sonic boom forecast data. In embodiments, the flight planning system includes a display device, a pilot input interface, and a controller architecture coupled to the display device and to the pilot input interface. During system operation, the controller architecture receives flight plan criteria entered via the pilot input interface. The controller architecture then endeavors to generate or construct a boom-regulated flight plan, which includes at least one supersonic flight plan segment, in accordance with the flight plan criteria. If unable to construct a boom-regulated flight plan, the controller architecture generates a visual notification on the display device. The visual notification can include, for example, a warning that an excessive sonic boom or overpressure event may occur during execution of the flight plan by an aircraft, absent modifications to the flight plan.

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