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1. 发明申请

US20100036550A1 SYSTEMS AND METHODS FOR IMPROVING PILOT SITUATIONAL AWARENESS DURING LANDING 审中-公开
标题翻译：用于改善陆地期间导弹状态意识的系统和方法
公开(公告)号：US20100036550A1
公开(公告)日：2010-02-11
申请号：US12186386
申请日：2008-08-05
申请人： Kevin J Conner , Yasuo Ishihara , C. Don Bateman
发明人： Kevin J Conner , Yasuo Ishihara , C. Don Bateman
IPC分类号： G05D1/00
CPC分类号： B64D45/04
摘要： Systems and methods for generating an alert to the pilot of an aircraft during a deep/long landing situation. An example system includes a database that stores runway information, a position sensor that produces aircraft position information and a processor that is in data communication with the database and the position sensor. The processor includes an advisory condition detection component that compares altitude of the aircraft to a predefined altitude limit, determines if the aircraft is beyond an airline defined landing zone limit and not on the ground, and generates an alert to the pilot based upon the comparison and the determination. An output device outputs the generated alert. The airline defined landing zone limit is a fixed distance value from the approach end of a runway or a percentage of the total length of a runway, whichever allows for greatest amount of runway remaining.
摘要翻译：在深/长着陆情况下，向飞机飞行员生成警报的系统和方法。示例性系统包括存储跑道信息的数据库，产生飞行员位置信息的位置传感器和与数据库和位置传感器进行数据通信的处理器。所述处理器包括将所述飞行器的高度与预定义的高度极限进行比较的建议条件检测部件，确定所述飞行器是否超出航空公司限定的着陆区域限制而不是在地面上，并且基于所述比较并且向所述飞行员生成警报，决心。输出设备输出生成的警报。航空公司定义的着陆区域限制是距跑道接近端的固定距离值或跑道总长度的百分比，以允许最大跑道数量为准。

2. 发明申请

US20120038493A1 SYSTEMS AND METHODS FOR REAL-TIME DATA LOGGING OF AN ENHANCED GROUND PROXIMITY SYSTEM 有权
标题翻译：用于增强地面接近系统实时数据记录的系统和方法
公开(公告)号：US20120038493A1
公开(公告)日：2012-02-16
申请号：US12854494
申请日：2010-08-11
申请人： Kevin J Conner , Gary A. Ostrom , C. Don Bateman
发明人： Kevin J Conner , Gary A. Ostrom , C. Don Bateman
IPC分类号： G01C21/00 , H04W40/00
CPC分类号： G07C5/085
摘要： Systems and methods for performing efficient, inexpensive data logging of aircraft sensor data. An example system on board an aircraft includes a plurality of data sources that provide sensor data associated with a plurality of avionic components, a line replaceable processing unit that is in signal communication with the plurality of data sources via one or more databuses, a wireless router connected to the line replaceable processing unit via a data cable and a portable data unit in wireless data communication with the wireless router. The wireless router receives at least a portion of the sensor data from the line replaceable processing unit and sends the received sensor data to the portable data unit.
摘要翻译：用于执行飞行器传感器数据的有效，便宜的数据记录的系统和方法。飞机上的示例系统包括提供与多个航空电子部件相关联的传感器数据的多个数据源，经由一个或多个数据总线与多个数据源进行信号通信的线路可替换处理单元，无线路由器通过与无线路由器的无线数据通信中的数据电缆和便携式数据单元连接到线路可更换处理单元。无线路由器从线路可替换处理单元接收传感器数据的至少一部分，并将接收到的传感器数据发送到便携式数据单元。

3. 发明授权

US06501392B2 Aircraft weather information system 有权
标题翻译：飞机天气信息系统
公开(公告)号：US06501392B2
公开(公告)日：2002-12-31
申请号：US09907730
申请日：2001-07-17
申请人： Scott Gremmert , Kevin J Conner , C. Don Bateman , John Hruby
发明人： Scott Gremmert , Kevin J Conner , C. Don Bateman , John Hruby
IPC分类号： G01C2100
CPC分类号： G01S13/95 , G01S7/003 , G01W1/10 , G08G5/0013 , G08G5/0021 , G08G5/0039 , G08G5/0052 , G08G5/0091 , Y02A90/18
摘要： A system and method that downlinks weather data, generated by existing weather and data sensors, to a groundstation. The groundstation utilizes data from multiple aircraft to form refined weather information, and uplinks the refined weather information to the aircraft. The refined weather information is stored at the aircraft and picture generating equipment, such as an existing on-board ground proximity terrain picture and symbol generator, generates pictorial information depicting the weather information. The pictorial information is displayed, for example by an existing EFIS or weather radar display, in the form of polygons.
摘要翻译：将现有天气和数据传感器产生的天气数据下载到地面站的系统和方法。地面站利用来自多架飞机的数据形成精细的天气信息，并将精致的天气信息上传到飞机。精细天气信息存储在飞机和图像生成设备（例如现有的车载地面接近地形图像和符号发生器）中，产生描绘天气信息的图形信息。图形信息例如通过现有的EFIS或天气雷达显示器以多边形的形式显示。

4. 发明授权

US08258983B2 Systems and methods for real-time data logging of an enhanced ground proximity system 有权
标题翻译：增强型地面接近系统的实时数据记录系统和方法
公开(公告)号：US08258983B2
公开(公告)日：2012-09-04
申请号：US12854494
申请日：2010-08-11
申请人： Kevin J Conner , Gary A. Ostrom , C. Don Bateman
发明人： Kevin J Conner , Gary A. Ostrom , C. Don Bateman
IPC分类号： G01C21/00
CPC分类号： G07C5/085
摘要： Systems and methods for performing efficient, inexpensive data logging of aircraft sensor data. An example system on board an aircraft includes a plurality of data sources that provide sensor data associated with a plurality of avionic components, a line replaceable processing unit that is in signal communication with the plurality of data sources via one or more databuses, a wireless router connected to the line replaceable processing unit via a data cable and a portable data unit in wireless data communication with the wireless router. The wireless router receives at least a portion of the sensor data from the line replaceable processing unit and sends the received sensor data to the portable data unit.
摘要翻译：用于执行飞行器传感器数据的有效，便宜的数据记录的系统和方法。飞机上的示例系统包括提供与多个航空电子部件相关联的传感器数据的多个数据源，经由一个或多个数据总线与多个数据源进行信号通信的线路可替换处理单元，无线路由器通过与无线路由器的无线数据通信中的数据电缆和便携式数据单元连接到线路可更换处理单元。无线路由器从线路可替换处理单元接收传感器数据的至少一部分，并将接收到的传感器数据发送到便携式数据单元。

5. 发明授权

US06828922B1 Synthetic airborne hazard display 有权
标题翻译：合成机载危害显示
公开(公告)号：US06828922B1
公开(公告)日：2004-12-07
申请号：US09721294
申请日：2000-11-22
申请人： Scott Gremmert , Kevin J Conner , C. Don Bateman , John Hruby
发明人： Scott Gremmert , Kevin J Conner , C. Don Bateman , John Hruby
IPC分类号： G08G500
CPC分类号： G01S7/003 , G01C23/00 , G01S13/95 , G01W1/10 , G08G5/0013 , G08G5/0021 , G08G5/0091 , Y02A90/18
摘要： A system and method for downlinking weather data, generated by existing weather and data sensors, to a ground station. The ground station utilizes data from multiple aircraft to form refined weather information, and uplinks the refined weather information to the aircraft. The refined weather information is stored at the aircraft and picture generating equipment, such as an existing onboard ground proximity terrain or weather radar picture and symbol generator, generates pictorial information depicting weather. The pictorial information is displayed, for example by an existing EFIS or weather radar display, in the form of polygons.
摘要翻译：用于将由现有天气和数据传感器产生的天气数据下行到地面站的系统和方法。地面站利用来自多架飞机的数据形成精细的天气信息，并将精致天气信息上传到飞机。精致的天气信息存储在飞机上，诸如现有的陆上接近地形或气象雷达图像和符号发生器的图像生成设备产生描绘天气的图形信息。图形信息例如通过现有的EFIS或天气雷达显示器以多边形的形式显示。

6. 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。

7. 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。

8. 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。

9. 发明授权

US09809313B2 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.

10. 发明授权

US07670214B2 Systems and methods for intelligent alerting for cabin altitude depressurization 有权
标题翻译：用于机舱高度减压的智能报警系统和方法
公开(公告)号：US07670214B2
公开(公告)日：2010-03-02
申请号：US11469376
申请日：2006-08-31
申请人： Kevin J Conner , Yasuo Ishihara , Charles D. Bateman
发明人： Kevin J Conner , Yasuo Ishihara , Charles D. Bateman
IPC分类号： B64D13/02 , B64D13/00 , B60H1/00
CPC分类号： B64D13/02
摘要： Methods and systems for providing a depressurization alert. An example method includes receiving a cabin depressurization discrete signal, determining if the cabin depressurization discrete signal is valid, and issuing a cabin depressurization alert, if the cabin depressurization discrete signal was determined to be valid. In accordance with further aspects of the invention, a time delay is executed before the receiving, determining, and issuing steps are repeated. The cabin depressurization discrete signal is determined not valid if uncorrected pressure is not greater than a predefined altitude. The uncorrected pressure is a raw pressure value produced by a Pitot-Static system. Also, the cabin depressurization discrete signal is determined not valid if the aircraft's altitude above an intended runway is not greater than a first predefined value. Additionally, the cabin depressurization discrete signal is determined not valid if an aircraft's altitude above terrain is not greater than a second predefined value.
摘要翻译：提供减压警报的方法和系统。一种示例性方法包括：如果客舱减压离散信号被确定为有效，则接收客舱减压离散信号，确定客舱减压离散信号是否有效，并发出机舱减压警报。根据本发明的其它方面，在重复接收，确定和发出步骤之前执行时间延迟。如果未校正的压力不大于预定高度，则舱室减压离散信号被确定为无效。未校正的压力是由皮托静力系统产生的原始压力值。此外，如果飞机在预期跑道上方的高度不大于第一预定值，则机舱减压离散信号被确定为无效。此外，如果飞机在地形上方的高度不大于第二预定义值，则机舱减压离散信号被确定为无效。

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