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    Cabin altitude alerting systems and methods
    71.
    发明授权
    Cabin altitude alerting systems and methods 有权

    公开(公告)号：US09809313B2

    公开(公告)日：2017-11-07

    申请号：US11625764

    申请日：2007-01-22

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

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

    IPC分类号： B64D13/02

    CPC分类号： B64D13/02

    摘要： Systems and methods for intelligently alerting the flight crew of a cabin depressurization. An example system includes a cabin altimeter that generates a cabin pressure value, an alerting device, such as a speaker system and a processing device in data communication with the cabin altimeter and the alerting device. The processing device determines if there is a problem with the cabin pressure received from the cabin altimeter, determines rate of change of the cabin pressure, and sets at least one of an alert volume or an alert frequency based on the cabin pressure and the rate of change of the cabin pressure if it was determined that a problem exists with the cabin pressure. The processing device also issues a cabin depressurization alert over the alerting device based on at least one of the set alert volume or alert frequency, if there is a problem with the cabin pressure value.

    SYSTEMS AND METHODS FOR ALERTING POTENTIAL TAILSTRIKE DURING LANDING
    74.
    发明申请
    SYSTEMS AND METHODS FOR ALERTING POTENTIAL TAILSTRIKE DURING LANDING 有权
    用于在着陆期间预警潜在的潜艇的系统和方法

    公开(公告)号：US20120095625A1

    公开(公告)日：2012-04-19

    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： G08B23/00

    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。

    SYSTEMS AND METHODS FOR ADJUSTING LANDING GEAR ALERT ENVELOPE FOR OFFSHORE PLATFORMS AND BUILDING-TOP LANDINGS
    75.
    发明申请
    SYSTEMS AND METHODS FOR ADJUSTING LANDING GEAR ALERT ENVELOPE FOR OFFSHORE PLATFORMS AND BUILDING-TOP LANDINGS 有权
    用于海上平台和建筑物起落架的调速齿轮报警装置的系统和方法

    公开(公告)号：US20110273315A1

    公开(公告)日：2011-11-10

    申请号：US12821536

    申请日：2010-06-23

    申请人： Yasuo Ishihara ,  Steve Johnson ,  Gary Ostrom

    发明人： Yasuo Ishihara ,  Steve Johnson ,  Gary Ostrom

    IPC分类号： G08B23/00

    CPC分类号： B64D45/0005

    摘要： Systems and methods for improving landing gear alerting on a rotary wing aircraft. An example system includes a user interface device that allows a user to set a bug altitude value and a radio altimeter that produces an altitude value, both of which are in communication with a processor. The processor receives a bug altitude setting, generates a landing gear alert altitude value based on the received bug altitude setting and a predefined additive, receives a radio altitude value for the rotary-wing aircraft, and generates a landing gear alert if the radio altitude value is less than the landing gear alert altitude value and the landing gear is not in a landing position. An output device in signal communication with the processor, outputs the generated landing gear alert.

    摘要翻译： 用于改进旋翼机上起落架警报的系统和方法。 示例性系统包括允许用户设置错误高度值的用户界面设备和产生高度值的无线电高度计，两者都与处理器通信。 处理器接收到错误高度设置，根据接收到的臭虫高度设置和预定义的添加量生成起落架警报高度值，接收旋翼飞机的无线电高度值，并产生起落架警报，如果无线电高度值 小于起落架报警高度值，起落架不在着陆位置。 与处理器进行信号通信的输出设备输出生成的起落架警报。

    STABILIZED APPROACH MONITOR
    76.
    发明申请
    STABILIZED APPROACH MONITOR 有权
    稳定的方法监视器

    公开(公告)号：US20110118911A1

    公开(公告)日：2011-05-19

    申请号：US12621794

    申请日：2009-11-19

    申请人： Yasuo Ishihara ,  Steve Johnson

    发明人： Yasuo Ishihara ,  Steve Johnson

    IPC分类号： G06F7/00

    CPC分类号： G05D1/0676 ,  G08G5/0021 ,  G08G5/02 ,  G08G5/025

    摘要： Systems and methods for suppressing an unstable alert when the aircraft is in the process of landing on a temporarily displaced threshold. In an example process, a processor on the aircraft determines the aircraft is on an approach to landing on a runway based on information received from one or more data sources on the aircraft, then retrieves predefined glideslope information for the runway from a memory device that is in signal communication with the processor. Next, the processor determines whether position of the aircraft is above the predefined glideslope by a first threshold amount. If the aircraft is determined to be above the predefined glideslope by the first threshold amount, the processor issues an unstable alert only if a flight path angle of the aircraft is greater than an angle of the predefined glideslope by a second threshold amount.

    摘要翻译： 当飞机正在临时移动的阈值上着陆的过程中用于抑制不稳定警报的系统和方法。 在示例过程中，飞行器上的处理器基于从飞机上的一个或多个数据源接收到的信息来确定飞行器正在着陆在跑道上，然后从存储器设备中检索用于跑道的预定滑翔信息， 与处理器进行信号通信。 接下来，处理器确定飞行器的位置是否高于预定滑行边界第一阈值量。 如果飞行器被确定为高于预定滑翔道第一阈值量，则只有当飞行器的飞行路径角度大于预定滑翔坡的角度达到第二阈值量时，处理器才发出不稳定的警报。

    Systems and methods for selectively altering a ground proximity message
    77.
    发明申请
    Systems and methods for selectively altering a ground proximity message 审中-公开
    选择性地改变地面邻近信息的系统和方法

    公开(公告)号：US20110029162A1

    公开(公告)日：2011-02-03

    申请号：US11368973

    申请日：2006-03-06

    申请人： Yasuo Ishihara ,  Steve C. Johnson

    发明人： Yasuo Ishihara ,  Steve C. Johnson

    IPC分类号： G01C5/00

    CPC分类号： G01C23/005 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/045

    摘要： Systems and methods for selectively altering a ground proximity warning message. In an embodiment, a ground proximity warning system for a flight vehicle includes a processor that is configured to generate a look-ahead envelope that defines a region extending outwardly from the flight vehicle and to generate a terrain proximity message when the defined region intersects a terrain feature. An interface device is coupled to the processor that is operable to configure the system in a first operating mode wherein the generated terrain proximity message is selectively suppressed, and a second operating mode wherein the terrain proximity message is not suppressed.

    摘要翻译： 选择性地改变地面接近警告信息的系统和方法。 在一个实施例中，用于飞行器车辆的地面接近警告系统包括处理器，该处理器被配置为产生一个前视信封，该信号限定从飞行车辆向外延伸的区域，并且当定义的区域与地形相交时产生地形接近消息 特征。 接口设备耦合到处理器，其可操作以在第一操作模式中配置系统，其中选择性地抑制所生成的地形接近消息，以及其中不抑制地形接近消息的第二操作模式。

    METHOD AND APPARATUS FOR IMPROVING PILOT SITUATIONAL AWARENESS DURING FLARE TO TOUCHDOWN
    78.
    发明申请
    METHOD AND APPARATUS FOR IMPROVING PILOT SITUATIONAL AWARENESS DURING FLARE TO TOUCHDOWN 有权
    用于改善飞行期间飞行员情绪意识的方法和装置

    公开(公告)号：US20090319105A1

    公开(公告)日：2009-12-24

    申请号：US12141816

    申请日：2008-06-18

    申请人： Kevin J. Conner ,  Yasuo Ishihara

    发明人： Kevin J. Conner ,  Yasuo Ishihara

    IPC分类号： G06F19/00

    CPC分类号： G08G5/02

    摘要： A system and method for selectively alerting a pilot of an aircraft about distance remaining to the end of a runway. A position of the aircraft is received. A position of a runway is retrieved from a runway database. The retrieved position of the runway is compared to the received position of the aircraft to determine if the aircraft is within an alert envelope relative to the retrieved position of the runway. The position of the runway is subtracted from the position of the aircraft to determine a distance to the distal end of the runway. An alert to the pilot is generated based upon the distance to the distal end of the runway.

    摘要翻译： 一种系统和方法，用于选择性地提醒飞机的飞行员关于剩余到跑道末端的距离。 接收到飞机的位置。 从跑道数据库中检索跑道的位置。 将跑道的检索位置与飞机的接收位置进行比较，以确定飞机是否在相对于跑道的检索位置的警报信封内。 从飞机的位置减去跑道的位置，以确定到跑道远端的距离。 基于到跑道远端的距离产生对飞行员的警报。

    METHODS AND SYSTEMS FOR MONITORING APPROACH OF ROTARY WING AIRCRAFT
    80.
    发明申请
    METHODS AND SYSTEMS FOR MONITORING APPROACH OF ROTARY WING AIRCRAFT 审中-公开
    用于监控旋转飞机的方法和系统

    公开(公告)号：US20080173753A1

    公开(公告)日：2008-07-24

    申请号：US11625673

    申请日：2007-01-22

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

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

    IPC分类号： B64D45/04

    CPC分类号： G05B23/0235

    摘要： Systems and methods for generating an alert if a rotary wing aircraft is approaching a hazardous situation. In an example method a processor receives a wind value and a rate of descent value. An alert signal is generated if the received wind value is greater than a tailwind threshold value and the rate of descent value is greater than a rate of descent threshold value. The generated alert is outputted to an output device, such as a display device or speakers. The alert signal is further generated if the rotary wing aircraft is on approach to landing, a rate of change of heading is less than a predefined value, or a rate of change in speed is less than a predefined value.

    摘要翻译： 如果旋翼飞机正在接近危险情况，产生警报的系统和方法。 在示例性方法中，处理器接收风值和下降速率值。 如果接收到的风值大于顺风阈值并且下降速率值大于下降阈值的速率，则产生报警信号。 生成的警报被输出到诸如显示装置或扬声器的输出装置。 如果旋转翼飞机正在着陆，则航向变化率小于预定值，或速度变化率小于预定值，进一步产生报警信号。