机场跑道自动化清理系统方案 Xsight - National agents - CIECC
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• SDU Components SDU组件:
– CCD/NIR
– MMWR – Processor Module 处理模块 – Servo Module 伺服模块 – Communications Module 通信模块 – Switch & Control Module 交换&控制
模块
– Standard Frangible Coupler 标准易碎
• Provide the visual/operational information for correct decision.提供图像/操作信 息,以便作出正确决策
• Capacity 容量
– Maximize capacity and avoid unnecessary halts. 最大化机场容量,避免不必要的 中断
- FOR AIRPORT SAFETY AND CAPACITY
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FOD – Worldwide Aviation Challenge FOD – 世界航空面临的挑战
• FOD Physical Characteristics FOD 的物理特征:
– Any size, material or shape.任意大小、材质、形状 – Parts as small as a rivet. 小至螺丝的零件
• FOD events occur FOD事件发生时间 :
– Day/Night and all weather (To the extent of an operational airport) 白天/夜间,所有气候条件(机场管理所达到的范围)
• Safety Timing安全定时:
– Detection Time检测时间
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– Management 管理
TM
Alon Nitzan, Co-Founder, CEO
创始人之一,CEO
• Served as the CEO of Integritech Systems “Integritech Systems” 的CEO
• Worked on aviation programs with Boeing, Raytheon, Honeywell and USAF.
与Boeing, Raytheon, Honeywell and USAF.共同进行航空项目。
• BSc and MSc in Electrical Engineering from TAU.
“造成的损失约给航空业造成每年40亿美元的损失”
Note: Based on Research done by U.S. Air Hale Waihona Puke Baiduorce Research Lab at Wright Patterson AFB (Squadron Leader Richard Friend)
注释:根据美国空军研究实验室在 Wright Patterson AFB的研究(队长Richard Friend )
• Served 15 years in IAF (Major) 在IAF服役15年(陆军少校) – Head of F-15 avionics engineering division. F-15航空电子工 程师师长
• Served as avionics engineer at the Boeing Company in St. Louis, MO.在圣路易斯波音公司担任航空电子学工程师
TM
FODetect™ System Introduction FODetect™ 系统介绍
National Agents Project – CIECC Dr. Mu Shiqiang April, 2007
This document includes data that shall not be disclosed outside the recipient organizations and shall not be duplicated, used or disclosed, in whole or in part, for any purpose other than to evaluate this technical / concept proposal. The data subject to this restriction are contained on all sheets.
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Current Practice 目前行动 TM
“The resulting damage is estimated to cost the aerospace industry $4 billion a year.”
TM
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Authentic FOD detection at Sdhe-DOV Sdhe-DOV的真实FOD检测
TM
FOD location in sensor’s sensing area.感应器区域内的 FOD定位 FOD location in current image. 目前的FOD定位图像 (in addition to GPS location (除GPS定位和感应器数量 之外)
– Minimize access to runway due to current FOD practice.进行 FOD清扫时,尽量限制 进入跑道
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Xsight Solution Xsight 解决方案
(US PTaMtent granted获得美国专利保护)
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• December 19, 2005 – B747-400, four tires blew during takeoff from LAX. FODs were scattered across airport runways and taxiways. 2005年12月9日,在从LAX起飞之后,波音747-400的四个轮胎 爆炸,FOD散落在机场跑道和滑行道上。
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MeetiTMng Agenda 会议日程
• Company Introduction 公司介绍 • FOD - The Challenge FOD-面临挑战 • System Introduction 系统介绍 • Xsight Current Activities Xsight目前活动 • Discussion. 交流讨论
Destruction Notice: Destroy by any method that will prevent disclosure of contents or reconstruction of the document.
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EXEMPT FROM PUBLIC DISCLOSURE: Information contained herein is privileged or confidential information of XSight Systems and is exempt from public disclosure. Do not disclose outside the recipient organizations.
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TM
– Mission 使命
To provide the most advanced solutions to detect, monitor and avoid FODs.
提供最先进的检测、监控、避免 FOD的解决方案
and sensor number) 。
Real time video, aims to实时图像,目的在于:
•RT direction of the operation team 为行动小组实时指明方向. •Rapid removal of the FOD 快速清除FOD . •Increase Airport capacity 增加机场容量.
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Xsight Solution Xsight 解决方案
TM
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Xsight Sensor Xsight传感器
Surface DTMetection Unit 地表检测元件
AC150-5345-46 易碎型接头- 使用符合AC150-5345-46的标准接头. – Quick-Release Connector – use a quick-release connector according to AC150-5345-26. 快速释放连接器-使用符合AC150-5345-26标准的接口 – Wind - designed and tested to meet AC150-5345-46b. 风速- 设计并经过测试,达到AC150-5345-46b标准
TAU电子工程学士和硕士
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FOTDM Incidents FOD事件
• July 25, 2000 – Concorde crashed minutes after taking off from Charles de Gaulle. 2000年7月25日 – 协和飞机从戴高乐机场起飞后不久坠毁
• July 24, 2003 – B747 returned to Tel Aviv’s Ben-Gurion A/P shortly after take off. 2003年7月24日-在起飞后不久, B747就从特拉维夫Ben-Gurion 机场返回地面
• August 11, 2005 – B747 tire punctured on landing at Tokyo’s Narita A/P. R/W closed for 24 minutes. 2005年8月11日- 在抵达冬季机场之后,波音747轮胎爆炸,机 场跑道关闭24分钟
• FOD must be detected and pinpointed within seconds of aircraft movements.必须 在飞机运行的几秒钟之内检测、定位出FOD
– Decision Time 决策时间
• Decision to divert traffic must be taken before the next movement.在下一项行动 开始之前,必须作出改变交通的决定
• The SDU designed to meet FAA edge light safety requirement SDU设计达到FAA端面照光标准要求:
– 14” Height limitation限高14”. – Frangible Coupler – Use a standard coupler according to
接头
– Line series Power Supply 串联电源
Dep
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System block diagram 系统结构图
TM
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User Interface – Main Screen 用户界面-主屏幕
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User Interface – FOD Alert
用户界面 - FOD 警报
Sensor controls
High Resolution Image
Provided upon FOD detection 根据FOD检测提供的高分辨率图像
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Safety RTM equirements 安全要求