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    SYSTEM AND METHOD FOR USING AIRPORT INFORMATION BASED ON FLYING ENVIRONMENT
    1.
    发明申请
    SYSTEM AND METHOD FOR USING AIRPORT INFORMATION BASED ON FLYING ENVIRONMENT 审中-公开
    使用基于飞行环境的机场信息的系统和方法

    公开(公告)号：US20060080008A1

    公开(公告)日：2006-04-13

    申请号：US11161346

    申请日：2005-07-29

    申请人： Yasuo Ishihara ,  Steve Johnson ,  Kevin Conner

    发明人： Yasuo Ishihara ,  Steve Johnson ,  Kevin Conner

    IPC分类号： G01C23/00

    CPC分类号： G08G5/025 ,  G08G5/0065 ,  G08G5/0078

    摘要： Methods, systems, and computer program products for using airport information based on the flying environment. In one embodiment, a method of using airport information based on the flying environment includes determining height, ground speed, and if a helicopter is taking off based on determined height, determined ground speed, a takeoff height value and a takeoff speed value. In one embodiment, the helicopter is determined to be taking off when the determined height is less than the takeoff height value and when the determined ground speed is less than the takeoff speed value.

    摘要翻译： 基于飞行环境使用机场信息的方法，系统和计算机程序产品。 在一个实施例中，基于飞行环境使用机场信息的方法包括确定高度，地面速度，以及如果直升机基于确定的高度，确定的地面速度，起飞高度值和起飞速度值起飞。 在一个实施例中，当确定的高度小于起飞高度值时以及当确定的地面速度小于起飞速度值时，确定直升机正在起飞。

    METHODS AND SYSTEMS FOR MONITORING AIRCRAFT APPROACH BETWEEN APPROACH GATES
    2.
    发明申请
    METHODS AND SYSTEMS FOR MONITORING AIRCRAFT APPROACH BETWEEN APPROACH GATES 审中-公开
    用于监控方法门的航空方法的方法和系统

    公开(公告)号：US20070120708A1

    公开(公告)日：2007-05-31

    申请号：US11470188

    申请日：2006-09-05

    申请人： Yasuo Ishihara ,  Steve Johnson ,  Kevin Conner

    发明人： Yasuo Ishihara ,  Steve Johnson ,  Kevin Conner

    IPC分类号： G08B23/00 ,  G08B21/00

    CPC分类号： G08G5/0082 ,  G08G5/025

    摘要： Using signals available into an Enhanced Ground Proximity Warning System (EGPWS), approach monitor systems and methods compare approach speed, approach angle and amount of tailwind/crosswind to the pre-selected envelopes. When the aircraft approach speed, approach angle, or tailwind/crosswind is greater than the pre-defined envelope, the approach monitor system generates an aural/visual advisory indicating the violation. The envelope is set as a function of “height above runway elevation”.

    摘要翻译： 使用可用于增强型地面接近警告系统（EGPWS）中的信号，接近监视系统和方法可将进近速度，接近角度和后风/侧风量与预先选定的信封进行比较。 当飞机接近速度，进近角度或逆风/侧风大于预定义的包络时，进近监视系统产生指示违规的听觉/视觉咨询。 信封被设置为“跑道高度以上的高度”的函数。

    Systems and methods for alerting potential tailstrike during landing
    8.
    发明授权
    Systems and methods for alerting potential tailstrike during landing 有权
    在着陆期间提醒潜在尾迹的系统和方法

    公开(公告)号：US08532848B2

    公开(公告)日：2013-09-10

    申请号：US12907392

    申请日：2010-10-19

    申请人： Yasuo Ishihara ,  Steve Johnson

    发明人： Yasuo Ishihara ,  Steve Johnson

    IPC分类号： G05D1/08

    CPC分类号： B64D45/04 ,  B64C25/00 ,  B64D2045/008

    摘要： Systems and methods for alerting for potential tailstrike during landing. A processing device located onboard an aircraft determines whether the aircraft is in a landing operational mode. If the aircraft is determined within the landing operational mode, the processing device determines whether aircraft speed is less than a previously defined threshold speed and generates an alert signal if it is determined that the aircraft's speed is less than the previously defined threshold speed. An output device located onboard the aircraft, outputs an alert based on the generated alert signal.

    摘要翻译： 用于在着陆期间潜在尾迹的警报的系统和方法。 位于飞行器上的处理装置确定飞行器是否处于着陆操作模式。 如果在着陆操作模式下确定飞行器，则处理装置确定飞行器速度是否小于先前定义的阈值速度，并且如果确定飞行器的速度小于先前定义的阈值速度，则产生报警信号。 位于飞机上的输出设备基于生成的警报信号输出警报。

    Flaps overspeed advisory system
    9.
    发明授权
    Flaps overspeed advisory system 有权
    襟翼超速咨询系统

    公开(公告)号：US08451144B2

    公开(公告)日：2013-05-28

    申请号：US12365778

    申请日：2009-02-04

    申请人： Yasuo Ishihara ,  Steve Johnson ,  Kevin J Conner

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

    IPC分类号： G08B23/00

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

    摘要： A flap advisory system 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： 襟翼咨询系统向飞行员提供通知，指示飞机的速度应由于当前或期望的襟翼设置而受到照顾。 更具体地，襟翼咨询系统将飞行器的测量空速直接与折翼标牌速度相比较，或者对于给定的襟翼设置，将设置在襟翼标牌速度下方的边缘速度范围进行比较。 如果测量的空速被确定为过高，则系统提供一个指示空速太快的建议。 此外，当检测到襟翼手柄的移动时，系统可以提供咨询，使得襟翼手柄的持续移动将襟翼置于不适于测量的空速的设置中。

    SYSTEMS AND METHODS FOR ADJUSTING SINK RATE ALERT ENVELOPE FOR SPECIAL LANDING ZONES
    10.
    发明申请
    SYSTEMS AND METHODS FOR ADJUSTING SINK RATE ALERT ENVELOPE FOR SPECIAL LANDING ZONES 有权
    用于调整特殊土地区的波动警报信号的系统和方法

    公开(公告)号：US20130106623A1

    公开(公告)日：2013-05-02

    申请号：US13286141

    申请日：2011-10-31

    申请人： Yasuo Ishihara ,  Steve Johnson ,  Gary A. Ostrom

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

    IPC分类号： G08B23/00

    CPC分类号： G01C23/00 ,  B64D45/04 ,  G01C21/00 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/025

    摘要： Systems and methods for improving sink rate alerting for rotary wing aircraft. In one example, the system includes a radio altimeter that produces an altitude value, a processor that is in signal communication with the user interface device and the radio altimeter. The processor receives an altitude value, a position value for the aircraft and landing zone (LZ) information. The processor determines if the aircraft is on an approach to land at an LZ that is raised above surrounding terrain based on the received position value and LZ information. The processor receives sink rate information for the aircraft and generates a sink rate alert based on the received sink rate information and the aircraft altitude value if the sink rate information is greater than a sink rate value adjusted according to the LZ information. An output device outputs the generated sink rate alert. The LZ information includes an altitude value.

    摘要翻译： 用于改善旋翼飞机的下沉速率警报的系统和方法。 在一个示例中，系统包括产生高度值的无线电高度计，与用户接口设备和无线电高度计信号通信的处理器。 处理器接收高度值，飞机和着陆区（LZ）信息的位置值。 处理器根据接收到的位置值和LZ信息确定飞机是否处于在周围地形以上升起的LZ的地面上。 处理器接收飞行器的汇率信息，并且如果汇率信息大于根据LZ信息调整的汇率值，则基于接收的汇率信息和飞机高度值，生成汇率报警。 输出设备输出生成的下降速率警报。 LZ信息包括高度值。