公开(公告)号：US08984416B2

公开(公告)日：2015-03-17

申请号：US12674812

申请日：2008-08-29

申请人： Pierre Gamet ,  Jean-Louis Dalby ,  Nicolas Marty

发明人： Pierre Gamet ,  Jean-Louis Dalby ,  Nicolas Marty

IPC分类号： G06F3/03 ,  G01C23/00

CPC分类号： G01C23/00

摘要： The invention is situated in the field of displaying on board an aircraft geostationary elements of the navigation database on a screen having different display resolutions for the purpose of this data display, and its subject is a method for simplifying the display of stationary elements of this onboard database. This method is characterized in that it consists in precalculating a “decluttering” during the process of producing the onboard database by meshing the Earth with a Cartesian grid oriented along the latitudes and longitudes of the Earth, and by allowing only the most pertinent obstacle to appear in each rectangle of this grid.

摘要翻译： 本发明位于在用于该数据显示的目的上在具有不同显示分辨率的屏幕上在导航数据库的飞机对地静止元件上显示的领域，并且其主题是用于简化该船上的固定元件的显示的方法 数据库。 这种方法的特征在于，它通过将地球与沿着地球的纬度和经度定向的笛卡尔网格进行网格划分，并且仅允许出现最相关的障碍物来生成车载数据库的过程中预先计算“声望” 在这个网格的每个矩形。

公开(公告)号：US08897935B2

公开(公告)日：2014-11-25

申请号：US12440513

申请日：2007-08-29

申请人： Hugues Meunier ,  Nicolas Marty ,  Julia Percier

发明人： Hugues Meunier ,  Nicolas Marty ,  Julia Percier

IPC分类号： G06F7/00 ,  G08G5/00 ,  G01C23/00 ,  G05D1/06 ,  G08G5/04

CPC分类号： G01C23/005 ,  G05D1/0607 ,  G05D1/0676 ,  G08G5/0086 ,  G08G5/045

摘要： This disclosure relates to a system for preventing collisions with a terrain. The system includes a detecting means for detecting risks of collision with the terrain after a predetermined forecasting delay. The system further includes a determining means for determining, based on a trajectory followed by the aircraft, a possible limit point for success of the vertical terrain avoidance maneuver. The system further includes indication means for giving indications on azimuth clearance sections, around the direction in which the aircraft is moving, suitable for success of the vertical terrain avoidance maneuver. The system further includes means for estimating a free-travel distance in each azimuth clearance sector on a straight distancing trajectory with constant gradient and over a distance correspond to more than one minute of flight, the free-travel distance being free of potential conflicts with the terrain. The system further includes means for signaling azimuth clearance sections and free-travel distances.

摘要翻译： 本公开涉及一种用于防止与地形碰撞的系统。 该系统包括用于在预定的预测延迟之后检测与地形相撞的风险的检测装置。 该系统还包括确定装置，用于基于飞机跟随的轨迹确定用于垂直地形避免机动的成功的可能的极限点。 系统还包括指示装置，用于在方位角间隙部分周围围绕飞行器移动的方向进行指示，适于垂直地形回避机动的成功。 该系统还包括用于在具有恒定梯度的直线间距轨迹上估计每个方位角间隙扇区中的自由行程距离的装置，并且在距离对应于多于一分钟飞行的距离上，自由行程距离没有与 地形。 该系统还包括用于信号传递方位角间隙部分和自由行进距离的装置。

公开(公告)号：US08400347B2

公开(公告)日：2013-03-19

申请号：US12542535

申请日：2009-08-17

申请人： Bernard Fabre ,  Nicolas Marty ,  Hugues Meunier

发明人： Bernard Fabre ,  Nicolas Marty ,  Hugues Meunier

IPC分类号： G01S13/93 ,  G01S13/91 ,  G01S13/00

CPC分类号： G08G5/06

摘要： The invention relates to a monitoring device and method allowing surveillance of an aircraft in relation to aircraft and/or craft on an airport displacement zone. The invention is a system comprising a dedicated transmitter and receiver to receive the information regarding the location and displacement of the cooperative aircraft and to monitor the location of the said aircraft in relation to the cooperative aircraft. The monitoring application is based on the detection of conflict zones by inter-correlation of constraint surfaces of the airport zone. The invention applies to aircraft carrying communication moans for ADS-B networks for an airport zone monitoring application.

摘要翻译： 本发明涉及一种监视装置和方法，其允许飞机相对于机场位移区上的飞行器和/或飞行器进行监视。 本发明是一种包括专用发射机和接收机的系统，用于接收关于合作飞机的位置和位移的信息，并且监视所述飞机相对于协作飞机的位置。 监测应用是基于通过机场区域的约束表面的相互关系来检测冲突区域。 本发明适用于携带用于机场区域监视应用的用于ADS-B网络的通信呻吟机的飞行器。

公开(公告)号：US08306679B2

公开(公告)日：2012-11-06

申请号：US12270305

申请日：2008-11-13

申请人： Hugues Meunier ,  Nicolas Marty ,  Aurélie Sallier

发明人： Hugues Meunier ,  Nicolas Marty ,  Aurélie Sallier

IPC分类号： G01C21/36

CPC分类号： G08G5/0086 ,  G01C23/00 ,  G05D1/0055 ,  G08G5/025

摘要： The present invention relates to a method of protecting an aircraft in approach by signalling against the risks of collision with the terrain in steep-sided environments, in order to avoid unwanted warnings emanating from the clearance sensors of the onboard TAWS system while protecting the aircraft when it fails to observe the published procedure, and this equally in a landing procedure and in a take-off procedure. The method includes conferring an additional function on the conventional TAWS functions, specific to the detection of the potential risks of collision of the aircraft with the terrain when following procedures of reduced protection corridor type, and this without modifying either the logics or the characteristics of the clearance sensor or sensors as currently defined in the TAWSs of the state of the art.

摘要翻译： 本发明涉及通过在陡峭的侧面环境中发信号通知抵抗与地形碰撞的风险的方法来保护飞行器的方法，以避免在机载TAWS系统的间隙传感器发出的不期望的警告，同时保护飞行器时 它没有遵守已发布的程序，同样在着陆程序和起飞程序中也是如此。 该方法包括赋予传统TAWS功能的附加功能，特别是在跟踪减少保护走廊类型的过程时，检测飞机与地形的潜在风险，并且不修改任何逻辑或特性 当前在现有技术的TAWS中定义的间隙传感器或传感器。

公开(公告)号：US08275499B2

公开(公告)日：2012-09-25

申请号：US12579272

申请日：2009-10-14

申请人： Francois Coulmeau ,  Manuel Gutierrez-Castaneda ,  Nicolas Marty

发明人： Francois Coulmeau ,  Manuel Gutierrez-Castaneda ,  Nicolas Marty

IPC分类号： G01C23/00 ,  G06G7/78

CPC分类号： G08G5/006

摘要： The invention relates to a device for formulating a flight plan ensuring sufficient safety margins for a duration of a few minutes in relation to the set of flight constraints that could arise and comprising means for: detecting the surrounding moving objects (aircraft or meteorological phenomena), evaluating their type and the danger that they represent, formulating a reconfiguration flight plan ensuring a separation with these phenomena and taking best account of the constraints of the initially followed flight plan, avoiding prohibited or regulated airspaces and avoiding the surrounding relief with ad hoc operational margins.

摘要翻译： 本发明涉及一种用于制定飞行计划的装置，其确保相对于可能出现的一组飞行约束，持续几分钟的足够的安全裕度，并且包括用于：检测周围的运动物体（飞机或气象现象）的装置， 评估他们的类型和他们所代表的危险，制定重新配置飞行计划，确保与这些现象分离，并充分考虑到最初跟踪的飞行计划的限制，避免被禁止或受规管的空域，并避免周围的特殊运营利润减轻 。

公开(公告)号：US08271184B2

公开(公告)日：2012-09-18

申请号：US12582616

申请日：2009-10-20

申请人： Pascal Gayraud ,  Nicolas Marty ,  Bernard Dubourg ,  Francois Michel

发明人： Pascal Gayraud ,  Nicolas Marty ,  Bernard Dubourg ,  Francois Michel

IPC分类号： G06F19/00

CPC分类号： G08G5/0021 ,  G08G5/065

摘要： The invention relates to the field of monitoring and aid to taxiing of an aircraft at an airport.The invention is a method of checking and monitoring the taxi plan and relates to a monitoring system comprising means for checking the pathway of the plan and means for signalling on the taxi aid the waiting time for the next clearance ahead of the aircraft along the pathway, the means for checking the pathway comprising a device for checking the pathway constraints and a device for checking the clearances, the device for checking the constraints making it possible to test and to display on the taxi plan the information descriptive of the constraints and the device for checking the clearances making it possible to check the clearances and to add the missing clearances to the taxi plan.

摘要翻译： 本发明涉及在机场对飞机的滑行进行监测和援助的领域。 本发明是一种检查和监测出租车计划的方法，涉及一种监测系统，其包括用于检查该计划的路径的装置和用于向出租车援助者发信号的装置，用于沿着该路径在飞行器之前的下一个间隙的等待时间， 用于检查路径的装置包括用于检查路径约束的装置和用于检查间隙的装置，用于检查约束的装置，使得可以在出租车计划上测试和显示描述约束的信息和用于 检查间隙，使得可以检查间隙，并将缺少的间隙添加到出租车计划中。

公开(公告)号：US08223039B2

公开(公告)日：2012-07-17

申请号：US12786180

申请日：2010-05-24

申请人： Pierre Campagne ,  Alexandre Broquet ,  Nicolas Marty

发明人： Pierre Campagne ,  Alexandre Broquet ,  Nicolas Marty

IPC分类号： G01C21/00 ,  G01C23/00

CPC分类号： B64D45/00 ,  B64D31/04

摘要： A method and a device for detecting a thrust dissymmetry of an aircraft during a landing are disclosed. The detection device (6) comprises means (7) for detecting, upon a landing, that at least one of the engine control levers occupies an intermediary position comprised between a position threshold and a maximum speed position, as well as at least another engine control lever occupies an idling position, and means (9, 13) for triggering a warning when a landing condition is validated and at least one of the control levers occupies said intermediary position, at least another control lever occupying said idling position.

摘要翻译： 公开了一种用于在着陆期间检测飞行器的推力不对称性的方法和装置。 检测装置（6）包括用于在着陆时检测发动机控制杆中的至少一个占据位置阈值和最大速度位置之间的中间位置的装置（7），以及至少另一个发动机控制 杠杆占据怠速位置，以及用于当着陆条件被验证并且至少一个控制杆占据所述中间位置时触发警告的装置（9,13），至少另一控制杆占据所述怠速位置。

公开(公告)号：US20100302074A1

公开(公告)日：2010-12-02

申请号：US12786180

申请日：2010-05-24

申请人： Pierre Campagne ,  Alexandre Broquet ,  Nicolas Marty

发明人： Pierre Campagne ,  Alexandre Broquet ,  Nicolas Marty

IPC分类号： G01C21/00

CPC分类号： B64D45/00 ,  B64D31/04

摘要： A method and a device for detecting a thrust dissymmetry of an aircraft during a landing are disclosed. The detection device (6) comprises means (7) for detecting, upon a landing, that at least one of the engine control levers occupies an intermediary position comprised between a position threshold and a maximum speed position, as well as at least another engine control lever occupies an idling position, and means (9, 13) for triggering a warning when a landing condition is validated and at least one of the control levers occupies said intermediary position, at least another control lever occupying said idling position.

摘要翻译： 公开了一种用于在着陆期间检测飞行器的推力不对称性的方法和装置。 检测装置（6）包括用于在着陆时检测发动机控制杆中的至少一个占据位置阈值和最大速度位置之间的中间位置的装置（7），以及至少另一个发动机控制 杠杆占据怠速位置，以及用于当着陆条件被验证并且至少一个控制杆占据所述中间位置时触发警告的装置（9,13），至少另一控制杆占据所述怠速位置。

公开(公告)号：US07693613B2

公开(公告)日：2010-04-06

申请号：US10591593

申请日：2005-02-09

申请人： Elias Bitar ,  Nicolas Marty

发明人： Elias Bitar ,  Nicolas Marty

IPC分类号： G05D1/00 ,  G06F7/00 ,  G06F17/00

CPC分类号： G01C5/00 ,  G01C21/00

摘要： In distance maps used in order to facilitate the navigation of craft such as an aircraft, the distances estimated take into account obstacles to be circumvented but not the maneuverability of the craft. The adaptation route required by the craft in order to take the right direction is not taken into account so that certain distance estimates for accessible points located in the neighborhood of the craft are unrealistic. In order to make a distance map more realistic, it is proposed that an obstacle of concave shape associated with the craft be added behind the position of the craft, forcing the estimations of distances to be circumvented an area that is inaccessible to the craft for reasons of maneuverability.

摘要翻译： 在为了方便飞机等飞机的导航而使用的距离图中，估计的距离考虑到要避开的障碍，而不考虑飞机的机动性。 没有考虑到工艺要求正确方向所需的适应路线，以至于位于工艺附近的无障碍点的某些距离估计是不切实际的。 为了使距离图更逼真，建议将与工艺相关联的凹形形状的障碍物添加到工艺的位置后面，迫使距离的估计被绕过由于原因无法进入的区域 的机动性。

公开(公告)号：US20100057276A1

公开(公告)日：2010-03-04

申请号：US12544926

申请日：2009-08-20

申请人： Nicolas Marty ,  Hugues Meunier ,  Philippe Salmon

发明人： Nicolas Marty ,  Hugues Meunier ,  Philippe Salmon

IPC分类号： G06F19/00 ,  G08B23/00

CPC分类号： G01C23/00 ,  G01C21/00 ,  G01S13/953 ,  Y02A90/18

摘要： The invention relates to a method and a device for monitoring risky atmospheric areas.The invention relates to an onboard device connected to meteorological measurement systems making it possible to calculate danger detection areas in front of the aircraft in order to detect potential areas of penetration of the aircraft into risky atmospheric areas.The areas of intersection between the detection areas and the risky meteorological areas are calculated according to the trajectory of the aircraft stored in the navigation system.The method makes it possible to generate alerts and force the display of the meteorological situation in front of the aircraft in case of danger.

摘要翻译： 本发明涉及一种用于监测大气区风险的方法和装置。 本发明涉及一种连接到气象测量系统的车载设备，使得可以计算飞机前方的危险检测区域，以便检测飞机在危险的大气区域中的穿透的潜在区域。 根据导航系统中存储的飞机的轨迹，计算出检测区域与危险气象区域的交点。 该方法使得有可能产生警报并强制在有危险的情况下显示飞机前面的气象情况。