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1. 发明申请

US20150325131A1 PASSIVE AIRCRAFT WINGTIP STRIKE DETECTION SYSTEM AND METHOD 有权
标题翻译：被动飞机WINGTIP STRIKE检测系统及方法
公开(公告)号：US20150325131A1
公开(公告)日：2015-11-12
申请号：US14561920
申请日：2014-12-05
申请人： Kevin J. Conner , Yasuo Ishihara
发明人： Kevin J. Conner , Yasuo Ishihara
IPC分类号： G08G5/04 , G08G5/00
CPC分类号： G08G5/04 , G08G5/0021 , G08G5/065
摘要： A system and method for passively detecting aircraft wingtip strikes includes generating a digital base map represented by a plurality of aerodrome cells. A numeric value representative of the specific wingtip is assigned to each of the aerodrome cells. An index count array is generated that has a separate entry for each numeric value. A digital aircraft structure representative of an aircraft is generated, and is represented by a plurality of aircraft cells. A determination is made as to whether a portion of the aerodrome cells are or would be replaced with the plurality of aircraft cells. Each numeric value of the aerodrome cells that are or would be replaced is counted to determine a replacement count associated therewith and that is entered into the separate entry in the index count array for that numeric value. One or more potential aircraft wingtip strikes are detected based on the replacement counts.
摘要翻译：用于被动地检测飞行器翼尖撞击的系统和方法包括生成由多个机场小区表示的数字基地图。代表特定翼尖的数值被分配给每个机场细胞。生成索引计数数组，每个数值都有一个单独的条目。产生代表飞行器的数字飞机结构，并由多个飞机单元表示。确定一部分机场细胞是否将被多个飞行器细胞代替。计算将要或将被替换的机场单元的每个数值，以确定与之相关联的替换计数，并输入到该数值的索引计数数组中的单独条目中。基于替换计数检测到一个或多个潜在的飞机翼尖撞击。

2. 发明授权

US08483889B2 Systems and methods for selectively altering a ground proximity message 有权
标题翻译：选择性地改变地面邻近信息的系统和方法
公开(公告)号：US08483889B2
公开(公告)日：2013-07-09
申请号：US12696555
申请日：2010-01-29
申请人： Yasuo Ishihara , Steve C Johnson
发明人： Yasuo Ishihara , Steve C Johnson
IPC分类号： G08G5/04
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。

3. 发明授权

US08098176B2 Systems and methods for adjusting landing gear alert envelope for offshore platforms and building-top landings 有权
标题翻译：调整离岸平台和建筑物顶部着陆装置报警信号的系统和方法
公开(公告)号：US08098176B2
公开(公告)日：2012-01-17
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。

4. 发明申请

US20110320070A1 SYSTEMS AND METHODS FOR ADJUSTING TARGET APPROACH SPEED 有权
标题翻译：用于调整目标方法速度的系统和方法
公开(公告)号：US20110320070A1
公开(公告)日：2011-12-29
申请号：US12821445
申请日：2010-06-23
申请人： Yasuo Ishihara , Steve Johnson
发明人： Yasuo Ishihara , Steve Johnson
IPC分类号： G06F19/00 , G05D1/06
CPC分类号： G05D1/0676 , B64D43/02 , G08G5/0091 , G08G5/025
摘要： Systems and methods for adjusting target approach speed for use in a “Too Fast” approach to landing condition. An exemplary system stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point.
摘要翻译：调整目标进近速度的系统和方法用于“太快”的着陆条件。示例性系统存储预定义的最大风力设定和预定的参考速度和飞行员设置的错误速度值。如果错误速度小于参考速度加上与预定义的最大风力设定相关联的值，则处理设备将目标速度设置为等于故障速度，并将目标速度设置为等于参考速度加上最大风力附加值，如果手动的错误速度不低于参考速度加上最大风量附加值。如果所接收的飞行器位置在接地点的阈值内，则所接收到的飞行器速度大于设定的目标速度加上预定义的误差值，则输出设备输出报警。

5. 发明申请

US20110118909A1 SYSTEMS AND METHODS OF DETECTING LOW TAKEOFF PERFORMANCE DUE TO INCORRECT WEIGHT INFORMATION 审中-公开
标题翻译：检测不正确重量信息的低劣性能的系统和方法
公开(公告)号：US20110118909A1
公开(公告)日：2011-05-19
申请号：US12621842
申请日：2009-11-19
申请人： Yasuo Ishihara , Steve Johnson
发明人： Yasuo Ishihara , Steve Johnson
IPC分类号： G06G7/70 , G06F19/00
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., V1) and engine takeoff setting, the predicted point (based on the actual aircraft acceleration) to reach V1 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：用于执行V速度验证的系统和方法。一个示例系统确定在起飞卷期间是否有足够的跑道以使飞机以预定的制动力停止。如果使用不正确的“太小”重量来预先计算Vspeeds（例如V1）和发动机起飞设置，则达到V1的预测点（基于实际飞机加速度）不足以停止剩余的跑道长度。如果确定这样的情况，则向机组人员输出警报。

6. 发明申请

US20100286851A1 SYSTEMS AND METHODS FOR SELECTIVELY ALTERING A GROUND PROXIMITY MESSAGE 有权
标题翻译：用于选择地面邻近信息的系统和方法
公开(公告)号：US20100286851A1
公开(公告)日：2010-11-11
申请号：US12696555
申请日：2010-01-29
申请人： Yasuo Ishihara , Steve C. Johnson
发明人： Yasuo Ishihara , Steve C. Johnson
IPC分类号： G08G5/04
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。

7. 发明申请

US20100198432A1 STABLE APPROACH MONITOR (SAM) SYSTEM 有权
标题翻译：稳定的方法监视器（SAM）系统
公开(公告)号：US20100198432A1
公开(公告)日：2010-08-05
申请号：US12365751
申请日：2009-02-04
申请人： Yasuo Ishihara , Kevin J. Conner , Steve Johnson
发明人： Yasuo Ishihara , Kevin J. Conner , Steve Johnson
IPC分类号： G05D1/00
CPC分类号： G08G5/025 , G01C23/005 , G05D1/0676
摘要： An improved stable approach monitor (SAM) system provides an audible advisory to a pilot when an aircraft is on a final landing approach. More specifically, the SAM system 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：改进的稳定进场监视（SAM）系统为飞行员在最终着陆方法时提供可听见的咨询。更具体地，SAM系统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来部署襟翼，从而将飞行员的注意力集中在手头的问题上，这将是减少飞机的空速。一旦空速等于或低于预定的翼片标示速度，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。

8. 发明申请

US20100030408A1 INTEGRATED INCORRECT TAKE-OFF-SETTING ALERTING SYSTEM 审中-公开
标题翻译：集成不正确的设置报警系统
公开(公告)号：US20100030408A1
公开(公告)日：2010-02-04
申请号：US12184092
申请日：2008-07-31
申请人： Ratan Khatwa , Kevin J. Conner , Yasuo Ishihara
发明人： Ratan Khatwa , Kevin J. Conner , Yasuo Ishihara
IPC分类号： G08G5/06 , G06G7/70 , G06F19/00
CPC分类号： B64D45/0005 , G08G5/0065
摘要： A system implementable in an aircraft for generating a warning includes a processor, a first component configured to receive from a user a desired aircraft control-surface takeoff configuration, a second component configured to provide to the processor a first signal indicative of a current control-surface configuration of the aircraft, and a third component configured to provide to the processor a second signal indicative of the position of the aircraft. The processor may be configured to compare the aircraft position to the contents of a database, determine, based on the comparison, whether the aircraft is on a departure runway from which the aircraft is to depart, and generate an alarm if the aircraft is on the departure runway and the current control-surface configuration is different from the desired control-surface takeoff configuration.
摘要翻译：在飞机中可实现的用于产生警告的系统包括处理器，被配置为从用户接收期望的飞行器控制表面起飞配置的第一部件，配置成向处理器提供指示当前控制 - 飞行器的表面配置，以及被配置为向处理器提供指示飞行器的位置的第二信号的第三组件。处理器可以被配置为将飞机位置与数据库的内容进行比较，基于比较来确定飞机是否在飞机将要离开的起飞跑道上，并且如果飞机在起飞跑道和当前的控制面配置不同于所需的控制面起飞配置。

9. 发明授权

US07626514B2 Systems and methods for reducing nuisance alerts for helicopter enhanced ground proximity warning systems 有权
标题翻译：减少直升机强化地面邻近警报系统的滋扰警报的系统和方法
公开(公告)号：US07626514B2
公开(公告)日：2009-12-01
申请号：US11538593
申请日：2006-10-04
申请人： Yasuo Ishihara , Charles D. Bateman
发明人： Yasuo Ishihara , Charles D. Bateman
IPC分类号： G08G5/00
CPC分类号： G01C5/005
摘要： Systems and methods for controlling activation of a look-ahead function of a terrain alert and warning system. The system receives rate of climb and aircraft speed information, compares the rate of climb and aircraft speed information to a predefined threshold, and deactivates a look-ahead function based on the comparison.
摘要翻译：用于控制地形警报和警告系统的前瞻功能的激活的系统和方法。系统接收爬升速度和飞行速度信息，将爬升速度和飞行速度信息与预定义的阈值进行比较，并根据比较关闭前视功能。

10. 发明授权

US07571031B2 Systems and methods for broadcasting an unknown airport advisory 有权
标题翻译：用于广播未知机场咨询的系统和方法
公开(公告)号：US07571031B2
公开(公告)日：2009-08-04
申请号：US11469802
申请日：2006-09-01
申请人： Kevin J Conner , Yasuo Ishihara
发明人： Kevin J Conner , Yasuo Ishihara
IPC分类号： G06G7/70
CPC分类号： G01C23/005 , G08G5/0021 , G08G5/025
摘要： Systems and methods for advising a flight crew member that an enhanced ground proximity warning system (EGPWS), for example, may continue to provide terrain alerts, cautions, warnings, or the like because an intended landing site for the aircraft is not recognized within a database of airports. An unknown airport advisory is generated and broadcast after the aircraft is in a landing configuration, when the aircraft is greater than a threshold distance from the nearest landing site in the database, but before the terrain alerts are broadcast. The pilot may actuate a “terrain inhibit” selection device after receiving the advisory. The inhibit device may deactivate or mute subsequent alerts generated by the EGPWS during that particular landing sequence.
摘要翻译：为飞行机组成员提供建议的系统和方法，例如，增强的地面接近警告系统（EGPWS）可能会继续提供地形警报，警告，警告等，因为飞机的预定着陆点在机场数据库在飞机处于着陆配置之后，当飞行器大于距离数据库中最近的着陆点的阈值距离之前，但在广播地形警报之前，将产生一个未知的机场咨询。飞行员可以在收到建议书后启动“地形禁止”选择装置。禁止装置可以在该特定着陆序列期间停用或静音由EGPWS产生的后续警报。

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