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1. 发明授权

US08451144B2 Flaps overspeed advisory system 有权
标题翻译：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。

2. 发明授权

US08600586B2 Stable approach monitor (SAM) system 有权
标题翻译：稳定进场监视（SAM）系统
公开(公告)号：US08600586B2
公开(公告)日：2013-12-03
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。

3. 发明申请

US20100194599A1 FLAPS OVERSPEED ADVISORY SYSTEM 有权
标题翻译： FLAPS OVERSPEED咨询系统
公开(公告)号：US20100194599A1
公开(公告)日：2010-08-05
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。

4. 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。

5. 发明授权

US08271191B2 Method of detecting erroneous GPS ground speed on ground 有权
标题翻译：检测地面上错误的GPS地面速度的方法
公开(公告)号：US08271191B2
公开(公告)日：2012-09-18
申请号：US11426547
申请日：2006-06-26
申请人： Yasuo Ishihara , Kevin J Conner , Steve C. Johnson
发明人： Yasuo Ishihara , Kevin J Conner , Steve C. Johnson
IPC分类号： G01C23/00
CPC分类号： G01S19/52 , G01S19/20 , G01S19/48
摘要： Methods and systems for determining reliability of Global Positioning System (GPS) ground speed. An example system receives GPS track information and GPS ground speed, determines a change in GPS track information and determines reliability of the GPS ground speed based on the determined change in GPS track information relative to the GPS ground speed. The system sets a GPS ground speed based on the determined reliability. A GPS ground speed output is set to zero, if the GPS ground speed is determined unreliable and the GPS ground speed output is set to the GPS ground speed, if the GPS ground speed is determined reliable. The system sends the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). Also, the system sets the GPS ground speed output to zero, if a received GPS ground speed validity signal or a received GPS track validity signal indicate invalid.
摘要翻译：确定全球定位系统（GPS）地面速度的可靠性的方法和系统。示例系统接收GPS轨道信息和GPS地面速度，确定GPS轨道信息的变化，并且基于GPS轨迹信息相对于GPS地面速度确定的变化来确定GPS地面速度的可靠性。系统根据确定的可靠性设置GPS地面速度。如果GPS地面速度被确定为可靠，则GPS地面速度输出被设置为零，如果GPS地面速度被确定为不可靠，并且将GPS地面速度输出设置为GPS地面速度。系统将GPS地面速度输出发送到跑道意识和咨询系统（RAAS）。此外，如果接收的GPS地面速度有效信号或接收的GPS轨道有效信号指示无效，则系统将GPS地面速度输出设置为零。

6. 发明申请

US20080176501A1 CABIN ALTITUDE ALERTING STYSEMS AND METHODS 有权
标题翻译：报警系统和方法
公开(公告)号：US20080176501A1
公开(公告)日：2008-07-24
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.
摘要翻译：机舱减压的飞行机组智能报警的系统和方法。示例系统包括产生客舱压力值的舱高度计，诸如扬声器系统的报警设备和与客舱高度计和报警设备进行数据通信的处理设备。处理装置确定从客舱高度计接收到的客舱压力是否存在问题，确定客舱压力的变化率，并且基于客舱压力和车厢压力的速率来设置报警量或报警频率中的至少一个如果确定客舱压力存在问题，则更改客舱压力。如果存在舱室压力值的问题，则处理装置还基于设定的报警量或警报频率中的至少一个，在警报装置上发出舱室减压警报。

7. 发明授权

US07206698B2 Ground operations and imminent landing runway selection 有权
标题翻译：地面作战和迫切的着陆跑道选择
公开(公告)号：US07206698B2
公开(公告)日：2007-04-17
申请号：US11009874
申请日：2004-12-10
申请人： Kevin J Conner , Scott R. Gremmert , Yasuo Ishihara , Ratan Khatwa , John J. Poe , James J. Corcoran, III
发明人： Kevin J Conner , Scott R. Gremmert , Yasuo Ishihara , Ratan Khatwa , John J. Poe , James J. Corcoran, III
IPC分类号： G06F17/00
CPC分类号： G08G5/065 , G01S19/15 , G01S19/51 , G01S2013/916 , G08G5/0013 , G08G5/025
摘要： A method, computer program product and apparatus for locating aircraft with respect to airport runways and environs, generating a graphical display of the aircraft position, heading and ground speed information relative to the aircraft runways and environs, and annunciating situational awareness advisories as a function of aircraft information relative to the airport runways and environs.
摘要翻译：一种用于相对于机场跑道和环境定位飞行器的方法，计算机程序产品和装置，产生相对于飞机跑道和周围环境的飞行器位置，航向和地面速度信息的图形显示，以及指示状态感知咨询作为飞机信息相对于机场跑道和周边环境。

8. 发明授权

US09805610B2 Passive aircraft wingtip strike detection system and method 有权
公开(公告)号：US09805610B2
公开(公告)日：2017-10-31
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 , G08G1/16 , G08G5/00 , G08G5/06
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.

9. 发明申请

US20080059010A1 SYSTEMS AND METHODS FOR BROADCASTING AN UNKNOWN AIRPORT ADVISORY 有权
标题翻译：广播未知机场咨询的系统和方法
公开(公告)号：US20080059010A1
公开(公告)日：2008-03-06
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： G01C23/00 , G06F19/00
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。

10. 发明申请

US20070299608A1 METHOD OF DETECTING ERRONEOUS GPS GROUND SPEED ON GROUND 有权
标题翻译：检测地面上GPS错误地球速度的方法
公开(公告)号：US20070299608A1
公开(公告)日：2007-12-27
申请号：US11426547
申请日：2006-06-26
申请人： Yasuo Ishihara , Kevin J. Conner , Steve C. Johnson
发明人： Yasuo Ishihara , Kevin J. Conner , Steve C. Johnson
IPC分类号： G01C23/00
CPC分类号： G01S19/52 , G01S19/20 , G01S19/48
摘要： Methods and systems for determining reliability of Global Positioning System (GPS) ground speed. An example system receives GPS track information and GPS ground speed, determines a change in GPS track information and determines reliability of the GPS ground speed based on the determined change in GPS track information relative to the GPS ground speed. The system sets a GPS ground speed based on the determined reliability. A GPS ground speed output is set to zero, if the GPS ground speed is determined unreliable and the GPS ground speed output is set to the GPS ground speed, if the GPS ground speed is determined reliable. The system sends the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). Also, the system sets the GPS ground speed output to zero, if a received GPS ground speed validity signal or a received GPS track validity signal indicate invalid.
摘要翻译：确定全球定位系统（GPS）地面速度的可靠性的方法和系统。示例系统接收GPS轨道信息和GPS地面速度，确定GPS轨道信息的变化，并且基于GPS轨迹信息相对于GPS地面速度确定的变化来确定GPS地面速度的可靠性。系统根据确定的可靠性设置GPS地面速度。如果GPS地面速度被确定为可靠，则GPS地面速度输出被设置为零，如果GPS地面速度被确定为不可靠，并且将GPS地面速度输出设置为GPS地面速度。系统将GPS地面速度输出发送到跑道意识和咨询系统（RAAS）。此外，如果接收的GPS地面速度有效信号或接收的GPS轨道有效信号指示无效，则系统将GPS地面速度输出设置为零。

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