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86 条记录 (耗时 0.029 秒)

    System and method for runway selection through scoring
    5.
    发明公开
    System and method for runway selection through scoring 审中-公开
    系统和Verfahren zur Landebahnauswahl mittels Bewertung

    公开(公告)号：EP2913813A1

    公开(公告)日：2015-09-02

    申请号：EP15155249.4

    申请日：2015-02-16

    申请人： Honeywell International Inc.

    发明人： Conner, Kevin J. ,  Ishihara, Yasuo ,  Johnson, Steve

    IPC分类号： G08G5/02 ,  G08G5/00

    CPC分类号： B64D45/00 ,  G08G5/0021 ,  G08G5/025

    摘要： A system and method for selecting a runway, comprises retrieving runway feature data and aircraft data including aircraft heading with respect to the bearing of first and second runways. Runway boundary envelopes are created for each of the first and second runways, each having a predetermined score. A total score for each of the first and second runways is compared to determine which of the runways is selected.

    摘要翻译： 一种用于选择跑道的系统和方法，包括检索跑道特征数据和飞行器数据，其包括相对于第一和第二跑道的轴承航向的航空器数据。 为每个第一和第二跑道创建每个具有预定分数的跑道边界信封。 比较第一和第二跑道中的每一个的总分，以确定选择哪条跑道。

    Aircraft systems and methods for attitude recovery
    8.
    发明公开
    Aircraft systems and methods for attitude recovery 有权
    Flugzeugsysteme und -verfahren zur Wiederherstellung der Fluglage

    公开(公告)号：EP2679961A2

    公开(公告)日：2014-01-01

    申请号：EP13172923.8

    申请日：2013-06-19

    申请人： Honeywell International Inc.

    发明人： Conner, Kevin J ,  Ishihara, Yasuo ,  Feyereisen, Thea L. ,  Morgan, John Allan

    IPC分类号： G01C23/00

    摘要： A vehicle system is provided. The system includes a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude. The system further includes a display device configured to receive the display signals and operable to selectively render an image including roll angle alert symbology. The roll angle alert symbology includes a first curved arrow.

    摘要翻译： 提供车辆系统。 该系统包括处理器，其被配置为接收表示当前姿态和期望姿态的数据，并产生与当前姿态和期望姿态相关联的显示信号。 该系统还包括被配置为接收显示信号并且可操作以选择性地呈现包括侧倾角警报符号系统的图像的显示装置。 滚角警报符号系统包括第一个弯曲箭头。

    Stable approach monitor (SAM) system
    9.
    发明公开
    Stable approach monitor (SAM) system 有权
    系统zurÜberwachungdes stableen Anflugs（SAM系统）

    公开(公告)号：EP2216625A3

    公开(公告)日：2012-06-13

    申请号：EP10151599.7

    申请日：2010-01-25

    申请人： Honeywell International Inc.

    发明人： Ishihara, Yasuo ,  Conner, Kevin J. ,  Johnson, Steve

    IPC分类号： G01C23/00 ,  G05D1/06 ,  G08G5/02

    CPC分类号： G08G5/025 ,  G01C23/005 ,  G05D1/0676

    摘要： An improved stable approach monitor (SAM) system 100 provides an audible advisory to a pilot when an aircraft is on a final landing approach. More specifically, the SAM system 100 compares a measured airspeed of the aircraft to a predetermined flap placard speed. If the measured airspeed exceeds the predetermined flap placard speed then the improved SAM system provides an audible advisory indicating the airspeed of the aircraft is too fast. Advantageously, this audible advisory should prevent the pilot from attempting to deploy the flaps at an excessive airspeed and in turn focuses the pilot's attention on the problem at hand, which would be to reduce the airspeed of the aircraft. Once the airspeed is equal to or below the predetermined flap placard speed, the improved SAM system may provide another audible advisory informing the pilot to commence deployment of the flaps.

    摘要翻译： 改进的稳定进近监视器（SAM）系统100在飞行器处于最终着陆方法时向飞行员提供可听见的咨询。 更具体地，SAM系统100将飞行器的测量空速与预定的挡板标示速度进行比较。 如果测量的空速超过预定的挡板标示速度，则改进的SAM系统提供了一个可听见的建议，指示飞机的空速太快。 有利的是，这种可听见的咨询应该防止飞行员试图以过高的空速部署襟翼，从而将飞行员的注意力集中在手头的问题上，这将是降低飞机的空速。 一旦空速等于或低于预定的挡板标示速度，改进的SAM系统可以提供另一个可听见的建议，通知飞行员开始襟翼的展开。

    System and method for performing an excessive negative pitch alert and for biasing a sink rate alert
    10.
    发明公开
    System and method for performing an excessive negative pitch alert and for biasing a sink rate alert 有权
    系统和方法，用于执行一个报警时过度的负斜率，并用于调节Sinkgeschwindigkeitsalarms

    公开(公告)号：EP2385436A2

    公开(公告)日：2011-11-09

    申请号：EP11164861.4

    申请日：2011-05-04

    申请人： Honeywell International Inc.

    发明人： Ishihara, Yasuo ,  Johnson, Steve ,  Ostrom, Gary

    IPC分类号： G05D1/08

    CPC分类号： G05D1/0858 ,  G01C23/00

    摘要： Systems and methods that alert the pilot of the unusual negative pitch attitude. Additionally, the system can bias a "sink rate" envelope toward a more sensitive direction, such that the pilot can be alerted while (or before) a large sink rate is built up during an unusual negative pitch attitude condition.

    摘要翻译： 系统和方法做了提醒不寻常的负俯仰姿态的试点。 另外，该系统可以偏置“下降率”信封向着更加敏感的方向，检查确实而（或之前）一个大的下降率是在负到异常俯仰姿态条件建立起来的导频可被警告。