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43 条记录 (耗时 0.031 秒)

    System and method for runway selection through scoring
    4.
    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。

    Stable approach monitor (SAM) system
    5.
    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
    6.
    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。

    Systems and methods of detecting low takeoff performance due to incorrect weight information
    7.
    发明公开
    Systems and methods of detecting low takeoff performance due to incorrect weight information 审中-公开
    用于检测小起飞作为不正确的重量信息的结果的系统和方法

    公开(公告)号：EP2328054A1

    公开(公告)日：2011-06-01

    申请号：EP10186626.7

    申请日：2010-10-05

    申请人： Honeywell International Inc.

    发明人： Ishihara, Yasuo ,  Johnson, Steve

    IPC分类号： G05D1/00

    CPC分类号： G05D1/0083

    摘要： Systems and methods for performing V speeds verification. An example system determines if during a takeoff roll there is enough runway left for the aircraft to stop with a predetermined braking force. If an incorrect "too small" weight had been used to previously compute Vspeeds (e.g., V 1 ) and engine takeoff setting, the predicted point (based on the actual aircraft acceleration) to reach V 1 provides not enough runway length remaining to stop. If such a situation is determined, an alert is outputted to the flight crew.

    摘要翻译： 系统和执行V速度验证方法。 一个例子系统bestimmt如果起飞滑跑过程中有足够的跑道上留下的飞机停止与预定的制动力。 如果不正确“太小”的体重已经被用来此前计算Vspeeds（例如，V 1）和发动机起飞设置，预测点（根据飞机的实际加速度）到达V 1提供剩余停止没有足够的跑道长度。 如果寻求一个情况是确定性的开采对警报输出的机组人员。

    Flaps overspeed advisory system
    8.
    发明公开
    Flaps overspeed advisory system 有权
    Bre en en en en en en en en en en en en en en en en en en en en en

    公开(公告)号：EP2224215A1

    公开(公告)日：2010-09-01

    申请号：EP10151696.1

    申请日：2010-01-26

    申请人： Honeywell International Inc.

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

    IPC分类号： G01C23/00 ,  G05D1/00

    CPC分类号： G01C23/00 ,  B64D43/02 ,  G05D1/0055

    摘要： A flap advisory system 100 provides an advisory to a pilot informing that a speed of the aircraft should be attended to because of a current or desired flap setting. More specifically, the flap advisory system compares a measured airspeed of the aircraft either directly to a flap placard speed or to a marginal speed range set below the flap placard speed for a given flap setting. If the measured airspeed is determined to be excessive then the system provides an advisory indicating the airspeed is too fast. Further, the system may provide an advisory when a movement of a flap handle is detected such that continued movement of the flap handle would place the flaps in a setting that is inappropriate for the measured airspeed.

    摘要翻译： 襟翼咨询系统100向飞行员提供通知，指示由于当前或期望的襟翼设置而应该考虑飞机的速度。 更具体地，襟翼咨询系统将飞行器的测量空速直接与皮瓣标牌速度或设置在翼襟标记速度下方的边缘速度范围进行比较，以获得给定的襟翼设置。 如果测量的空速被确定为过大，则系统提供一个指示空速太快的建议。 此外，当检测到翼片手柄的运动时，该系统可以提供咨询，使得翼片手柄的持续移动将襟翼放置在不适于测量的空速的设置中。