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1. 发明申请

WO2002059547A2 EGPWS CUTOFF ALTITUDE FOR HELICOPTERS 审中-公开
标题翻译： EGPWS CUTOFF直升机的高度
公开(公告)号：WO2002059547A2
公开(公告)日：2002-08-01
申请号：PCT/US2002/002030
申请日：2002-01-23
申请人： HONEYWELL INTERNATIONAL INC.
发明人： CONNER, Kevin , ISHIHARA, Yasuo , JOHNSON, Steven
IPC分类号： G01C5/00
CPC分类号： G01C5/005
摘要： An apparatus, method and computer program product for suppressing an alert generated by a terrain awareness system rotary wing aircraft of potentially hazardous proximity to terrain also reduces nuisance warnings and provides a terrain display consistent with the unique performance capabilities of such aircraft.
摘要翻译：用于抑制由地形识别系统旋转翼飞机产生的潜在危险接近地形的装置，方法和计算机程序产品还减少了妨扰警告并提供与这种飞机的独特性能能力一致的地形显示。

2. 发明申请

WO2002059546A1 GROUND PROXIMITY WARNING SYSTEM 审中-公开
标题翻译：地面临近警告系统
公开(公告)号：WO2002059546A1
公开(公告)日：2002-08-01
申请号：PCT/US2001/023674
申请日：2001-07-27
申请人： HONEYWELL INTERNATIONAL INC.
发明人： CONNER, Kevin , ISHIHARA, Yasuo , JOHNSON, Steven, C.
IPC分类号： G01C5/00
CPC分类号： G01C5/005 , G05D1/0607
摘要： A terrain avoidance system, method and computer program product for reducing nuisance alarms. The system includes a geometric altitude component, first and second vertical safety margin generators, and an alert component.
摘要翻译：减少有害报警的地形回避系统，方法和计算机程序产品。该系统包括几何高度分量，第一和第二垂直安全边界发生器以及警报组件。

3. 发明申请

WO2007005959A1 METHOD, APPARATUS, AND DATABASE PRODUCTS FOR AUTOMATED RUNWAY SELECTION 审中-公开
标题翻译：用于自动选路的方法，装置和数据库产品
公开(公告)号：WO2007005959A1
公开(公告)日：2007-01-11
申请号：PCT/US2006/026181
申请日：2006-07-05
申请人： HONEYWELL INTERNATIONAL INC. , ISHIHARA, Yasuo , GREMMERT, Scott, R.
发明人： ISHIHARA, Yasuo , GREMMERT, Scott, R.
IPC分类号： G08G5/02
CPC分类号： G08G5/0021 , G08G5/025
摘要： An apparatus and method for predicting which one of at least two candidate runways on which an aircraft is most likely to land includes a database. The database (24) is configured to contain at least two runway data. The runway data includes an empirical glide slope angle and a location associated with each candidate runway. A position sensor (16) is configured to determine a position of the aircraft. A processor (12) is configured to retrieve the glide slope angle and location data associated with each of the at least two candidate runways. The processor calculates an aircraft glide slope angle relative to each of the at least two candidate runways based upon the position of the aircraft, and derives a first likelihood of landing value for each of the at least twocandidate runways based upon the empirical glide slope angle and the aircraft glide slope
摘要翻译：一种用于预测飞机最有可能着陆的至少两个候选跑道中的哪一个的装置和方法包括数据库。数据库（24）被配置为包含至少两条跑道数据。跑道数据包括经验滑翔坡角和与每个候选跑道相关联的位置。位置传感器（16）被配置为确定飞机的位置。处理器（12）被配置为检索与所述至少两个候选跑道中的每一个相关联的滑翔坡角和位置数据。基于飞机的位置，处理器计算相对于至少两个候选跑道中的每一个的飞行器滑行倾斜角度，并且基于经验滑翔坡度角度为所述至少两条跑道中的每一个导出第一可能性的着陆值，并且飞机滑翔坡

4. 发明申请

WO2004044667A3 SYSTEM AND METHOD FOR USING AIRPORT INFORMATION 审中-公开
公开(公告)号：WO2004044667A3
公开(公告)日：2004-05-27
申请号：PCT/US2003/035654
申请日：2003-11-10
申请人： HONEYWELL INTERNATIONAL INC.
发明人： CONNER, Kevin, J. , JOHNSON, Steven, C. , ISHIHARA, Yasuo
IPC分类号： G08G5/00
摘要： A method, system, and computer program product for using airport information based on the flying environment are provided. When a helicopter is determined to be approaching a runway, ground proximity warning envelopes are automatically reduced to prevent unwanted, or nuisance, terrain alerts. On the other hand, when a helicopter is flown near a runway without intent to land or when a helicopter is taking off, ground proximity warning envelopes may remain unchanged. As a result, nuisance alerts are reduced when a helicopter is approaching a runway for landing and ground proximity warnings may remain in effect to maximize protection when a helicopter is flying near a runway without an intent to land or is taking off from a runway.

5. 发明申请

WO2006101806A1 TAILWIND ALERTING SYSTEM TO PREVENT RUNWAY OVERRUNS 审中-公开
标题翻译： TAILWIND报警系统，以防止RUNWAY OVERRUNS
公开(公告)号：WO2006101806A1
公开(公告)日：2006-09-28
申请号：PCT/US2006/008931
申请日：2006-03-10
申请人： HONEYWELL INC. , ISHIHARA, Yasuo , JOHNSON, Steve, C.
发明人： ISHIHARA, Yasuo , JOHNSON, Steve, C.
IPC分类号： G05D1/06 , G01C5/00
CPC分类号： G05D1/0676 , G01C5/005
摘要： Systems, methods and computer program products for alerting a flight crew during landing that the tailwind exceeds acceptable limits. The system determines a base tailwind threshold speed for a candidate runway based on a performance constant associated with an aircraft and candidate runway information and determines present tailwind speed. If the tailwind speed is greater than the base tailwind threshold speed, a tailwind alert is generated. Also, the system determines if the aircraft is in a tailwind alerting mode based on configuration of the aircraft and activates tailwind alerting, if it is determined that the aircraft is in the tailwind alerting mode.
摘要翻译：系统，方法和计算机程序产品，用于在着陆期间提醒飞行机组人员，后排超过可接受的限制。系统基于与飞行器和候选跑道信息相关联的性能常数来确定候选跑道的基本倒带阈值速度，并确定当前的顺风速度。如果顺风速度大于基本的倒档阈值速度，则会产生顺风警报。此外，如果确定飞行器处于顺风警报模式，则系统基于飞行器的配置来确定飞行器是否处于顺风警报模式，并且启动顺风警报。

6. 发明申请

WO2003098576A1 SYSTEM FOR LANDING RUNWAY SELECTION 审中-公开
标题翻译：陆路选线系统
公开(公告)号：WO2003098576A1
公开(公告)日：2003-11-27
申请号：PCT/US2003/015668
申请日：2003-05-15
申请人： HONEYWELL INTERNATIONAL INC.
发明人： CONNER, Kevin, J. , POE, John, J. , KHATWA, Ratan , ISHIHARA, Yasuo , GREMMERT, Scott, R.
IPC分类号： G08G5/02
CPC分类号： G08G5/0008 , G08G5/0043 , G08G5/0078 , G08G5/0082 , G08G5/065
摘要： A method for locating aircraft with respect to airport runways and taxiways, generating and annunciating situational awareness advisories as a function of aircraft state parameters relative to the aircraft location determination.
摘要翻译：一种相对于机场跑道和滑行道路定位飞行器的方法，根据飞行器状态参数相对于飞机位置确定生成和通报情境意识咨询。

7. 发明申请

WO2002059705A1 VARIABLE ENHANCED GROUND PROXIMITY WARNING SYSTEM LOOK-AHEAD OFFSET AND SUB-OFFSET 审中-公开
标题翻译：可变增强的地面临近警告系统LOOK-AHEAD OFFSET和SUB-OFFSET
公开(公告)号：WO2002059705A1
公开(公告)日：2002-08-01
申请号：PCT/US2001/023738
申请日：2001-07-27
申请人： HONEYWELL INTERNATIONAL INC.
发明人： JOHNSON, Steve , ISHIHARA, Yasuo , CONNER, Kevin
IPC分类号： G05D1/06
CPC分类号： G05D1/0676 , G01C5/005
摘要： The present invention includes a system, method and computer program product for reducing nuisance warnings during low altitude flight conditions and in the presence of low position uncertainty. The system includes a first component that determines whether the aircraft is in a low altitude flight condition and a second component that determines the position, positional uncertainty, and the heading. The system also includes a third component that attenuates and refines the look-ahead envelope in accord with the determined condition of flight and positional uncertainty.
摘要翻译：本发明包括用于在低空飞行条件下和存在低位置不确定性的情况下减少有害警告的系统，方法和计算机程序产品。该系统包括确定飞机是否处于低空飞行状态的第一部件和确定位置，位置不确定性和航向的第二部件。该系统还包括根据确定的飞行条件和位置不确定性来衰减和提炼先行信封的第三部件。

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