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1. 发明公开

EP3196863A1 SYSTEM AND METHOD FOR AIRCRAFT DOCKING GUIDANCE AND AIRCRAFT TYPE IDENTIFICATION 有权转让
标题翻译：用于飞机对接引导和飞机类型标识的系统和方法
公开(公告)号：EP3196863A1
公开(公告)日：2017-07-26
申请号：EP15827975.2
申请日：2015-07-02
申请人： Shenzhen Cimc-tianda Airport Support Ltd. , China International Marine Containers (Group) Ltd.
发明人： DENG, Lan , CHANG, Shaomin , XIANG, Wei , YANG, Yuefeng , WANG, Haibin , LIU, Haiqiu
IPC分类号： G08G5/06 , G01S17/06 , G01S17/88 , B64F1/00 , H04N7/00 , G06K9/20 , G06K9/36 , G06K9/60
CPC分类号： G06K9/6202 , B64F1/00 , B64F1/002 , G01S17/06 , G01S17/88 , G06K9/00791 , G06K9/20 , G06K9/36 , G06K9/60 , G08G5/06 , G08G5/065 , H04N7/00
摘要： A system and method for aircraft docking guidance and aircraft type identification. The method is executed in the system for aircraft docking guidance and aircraft type identification comprising a machine vision sub-system, a laser scanning sub-system and a merging module. The method comprises: step 1000, the machine vision sub-system obtains an image via image capturing means, and calculates a first aircraft front wheel position therefrom; step 2000, the laser scanning sub-system obtains the position of the nose of an aircraft via laser scanning means, and extrapolates a second aircraft front wheel position; step 3000, the first aircraft front wheel position and the second aircraft front wheel position are merged according to a merging rule, and an aircraft front wheel deviation is obtained.
摘要翻译：一种用于飞机对接引导和飞机类型识别的系统和方法。该方法在用于飞机对接引导和飞机类型识别的系统中执行，该系统包括机器视觉子系统，激光扫描子系统和合并模块。该方法包括：步骤1000，机器视觉子系统通过图像采集装置获取图像，并由此计算出第一飞机前轮位置; 步骤2000，激光扫描子系统通过激光扫描装置获取飞机机头位置，并推算出第二飞机前轮位置; 步骤3000，根据合并规则合并第一飞机前轮位置和第二飞机前轮位置，得到飞机前轮偏差。

2. 发明授权

EP3196128B1 SYSTEM AND METHOD FOR AIRCRAFT DOCKING GUIDANCE AND AIRCRAFT TYPE IDENTIFICATION 有权转让
公开(公告)号：EP3196128B1
公开(公告)日：2019-04-10
申请号：EP15827108.0
申请日：2015-07-02
申请人： Shenzhen CIMC-TIANDA Airport Support Ltd. , China International Marine Containers (Group) Ltd.
发明人： DENG, Lan , ZHANG, Zhaohong , CHANG, Shaomin , XIANG, Wei , WANG, Haibin , LIU, Haiqiu
IPC分类号： B64F1/00 , G01S17/06 , G01S17/93 , G08G5/06 , B64D45/08

3. 发明公开

EP3511250A1 MOVABLE WALKWAY BRAKING SYSTEM AND PASSENGER BOARDING BRIDGE 有权转让
公开(公告)号：EP3511250A1
公开(公告)日：2019-07-17
申请号：EP17847931.7
申请日：2017-04-20
申请人： China International Marine Containers (Group) Ltd. , Shenzhen CIMC-Tianda Airport Support Ltd.
发明人： LIANG, Lexian , CHANG, Shaomin , SHI, Lei , YAO, Yunjian
IPC分类号： B64F1/305
摘要： A movable walkway braking system, comprising a braking plate (223), a braking pin (67) and a triggering mechanism. A passenger boarding bridge comprising said movable walkway braking system, having three or more walkways, and an extending steel cable (52) and a retracting steel cable (51) connecting multiple walkways. The braking plate (223) is fixedly disposed on a first walkway (22), braking clamping grooves (224) are disposed on the braking plate, and the braking pin (67) is movably disposed on a second walkway (23) that sleeves over the first walkway (22), and is used to engage with a braking clamping groove (224). The triggering mechanism comprises mechanical stopper parts (231, 233), a pull rod mechanism and a tension spring (72), the mechanical stopper parts being fixedly disposed on the second walkway (23), the pull rod mechanism being movably disposed on the second walkway and connected to one end of an extending steel cable (52) or a retracting steel cable (51), and the pull rod mechanism abutting a mechanical stopper part when the extending steel cable (52) or the retracting steel cable (51) is under tension. Two ends of the tension spring (72) are connected to the pull rod mechanism and the second walkway, respectively, the spring being used to drive movement of the pull rod mechanism and make the pull rod mechanism move the braking pin (67) to engage with a braking clamping groove (224) when the extending steel cable (52) or the retracting steel cable (51) breaks, so as to stop the first walkway (22) and the second walkway (23). The structure of the present system is simple and compact, and convenient to install; in addition, the present system can effectively completely stop a movable walkway by means of a mechanical structure if an extending steel cable (52) or a retracting steel cable (51) breaks, thereby protecting the life safety of passengers, and the operation thereof is highly reliable.

4. 发明公开

EP3196128A1 SYSTEM AND METHOD FOR AIRCRAFT DOCKING GUIDANCE AND AIRCRAFT TYPE IDENTIFICATION 有权转让
标题翻译：用于飞机对接引导和飞机类型标识的系统和方法
公开(公告)号：EP3196128A1
公开(公告)日：2017-07-26
申请号：EP15827108.0
申请日：2015-07-02
申请人： Shenzhen Cimc-tianda Airport Support Ltd. , China International Marine Containers (Group) Co., Ltd.
发明人： DENG, Lan , ZHANG, Zhaohong , CHANG, Shaomin , XIANG, Wei , WANG, Haibin , LIU, Haiqiu
IPC分类号： B64D45/08
CPC分类号： B64F1/002 , G01S7/497 , G01S17/06 , G01S17/42 , G01S17/66 , G01S17/936 , G08G5/0026 , G08G5/065
摘要： A laser scanning-based aircraft docking guidance system and method, the method comprising: a capturing step: laser scanning in the horizontal direction is performed on a position where the front of an aircraft is expected to appear, echo data of the laser scanning is obtained, and the echo data is judged according to a judging condition, so as to determine whether the aircraft has appeared; a guiding step: after the aircraft has appeared, laser scanning in the horizontal direction is performed on the front of the aircraft, echo data of the laser scanning is obtained, and the position of the nose of the aircraft is determined; a tracking step: as the aircraft moves forward, the position of the nose is tracked via adjusting the vertical scanning angle of the laser scanning, and the position of the nose is displayed in real time. The system and method implement capturing, guiding and tracking of the aircraft, obtain the real-time position of the aircraft via accurate laser scanning, and perform displaying, so as to provide a pilot with a prompt for berthing. In addition, the system and method automatically identify and verify the aircraft type, improving aircraft docking security.
摘要翻译：一种基于激光扫描的飞机对接引导系统和方法，所述方法包括：捕获步骤：在预期飞机的前部出现的位置上执行水平方向的激光扫描，获得激光扫描的回波数据并根据判断条件判断回波数据，以确定飞机是否出现; 引导步骤：飞机出现后，在飞机前方进行水平方向的激光扫描，得到激光扫描的回波数据，确定飞机机头的位置; 追踪步骤：当飞机向前移动时，通过调整激光扫描的垂直扫描角度来追踪鼻子的位置，并实时显示鼻子的位置。该系统和方法实现对飞机的捕获，引导和跟踪，通过精确的激光扫描获取飞机的实时位置，并进行显示，为飞行员提供靠泊提示。此外，该系统和方法自动识别和验证飞机类型，提高飞机对接安全性。

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