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公开(公告)号：US09037319B2
公开(公告)日：2015-05-19
申请号：US14035114
申请日：2013-09-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Kevin J Conner , Yasuo Ishihara , Ray Berry
IPC: G01W1/08 , G01W1/10 , B64D43/00 , G01S13/95 , B64D45/00 , G08G5/00 , G01C23/00 , G05D1/04 , G01W1/00
CPC classification number: B64D45/00 , B64D43/00 , G01C23/005 , G01S13/953 , G01W1/08 , G01W1/10 , G01W2001/003 , G05D1/046 , G08G5/0008 , G08G5/0021 , G08G5/0078 , G08G5/0091
Abstract: A system and method to display, when within an envelope of an ownship's flight path, a symbol representing wake turbulence from another aircraft based on aircraft type and flight parameters received from the other aircraft, the symbol being formatted to indicate the severity of portions of the wake turbulence. The format is modified periodically in accordance with the aircraft's flight path and a decay rate of the wake turbulence.
Abstract translation: 一种系统和方法，用于根据从另一架飞机接收到的飞机类型和飞行参数，在自己的飞行路线的信封内显示表示来自另一架飞机的尾流湍流的符号，该符号被格式化以指示该部分的严重性 尾流湍流。 该格式根据飞机的飞行路径和尾流湍流的衰减速率周期性地修改。
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公开(公告)号：US20150213721A1
公开(公告)日：2015-07-30
申请号：US14258839
申请日：2014-04-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Kevin J. Conner , Yasuo Ishihara , Steve Johnson , Ray Berry
CPC classification number: G08G5/04 , G05D1/0083 , G08G5/0021 , G08G5/0078 , G08G5/0086 , G08G5/06 , G08G5/065 , G09B9/052 , G09B29/006 , G09B29/007
Abstract: 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 is assigned to each of the aerodrome cells that is representative of the specific wingtip strike threat associated with that aerodrome cell. An index count array is generated that has a separate entry for each numeric value. A digital aircraft structure is generated that is representative of an aircraft, and is represented by a plurality of aircraft cells. A portion of the aerodrome cells are replaced with the plurality of aircraft cells. Each numeric value of the aerodrome cells that are 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.
Abstract translation: 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。 每个机场细胞都分配一个数字值，这些单元格代表与该机场细胞相关的特定的机翼罢工威胁。 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，并且由多个飞机单元表示。 机场细胞的一部分被多个飞行器细胞代替。 对所替换的机场细胞的每个数值进行计数，以确定与之相关联的替换计数，并将其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。
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公开(公告)号：US20150088342A1
公开(公告)日：2015-03-26
申请号：US14035114
申请日：2013-09-24
Applicant: Honeywell International Inc.
Inventor： Kevin J Conner , Yasuo Ishihara , Ray Berry
IPC: B64D45/00
CPC classification number: B64D45/00 , B64D43/00 , G01C23/005 , G01S13/953 , G01W1/08 , G01W1/10 , G01W2001/003 , G05D1/046 , G08G5/0008 , G08G5/0021 , G08G5/0078 , G08G5/0091
Abstract: A system and method to display, when within an envelope of an ownship's flight path, a symbol representing wake turbulence from another aircraft based on aircraft type and flight parameters received from the other aircraft, the symbol being formatted to indicate the severity of portions of the wake turbulence. The format is modified periodically in accordance with the aircraft's flight path and a decay rate of the wake turbulence.
Abstract translation: 一种系统和方法，用于根据从另一架飞机接收到的飞机类型和飞行参数，在自己的飞行路线的信封内显示表示来自另一架飞机的尾流湍流的符号，该符号被格式化以指示该部分的严重性 尾流湍流。 该格式根据飞机的飞行路径和尾流湍流的衰减速率周期性地修改。
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