公开(公告)号：US08392038B2

公开(公告)日：2013-03-05

申请号：US12635421

申请日：2009-12-10

申请人： Christophe Caillaud ,  Jérôme Sacle

发明人： Christophe Caillaud ,  Jérôme Sacle

IPC分类号： B64D11/00 ,  G05D1/04

CPC分类号： G01C23/00 ,  G01C21/00 ,  G05D1/0676 ,  G08G5/0039

摘要： The method of generating a secure flight plan portion in the event of depressurization corresponding to a time-conditioned descent profile that may include a succession of levels, comprises: a step of defining a first point of the flight plan, called non-return point, denoted NRP, and a second point of the flight plan, called EOZ, the two points delimiting a portion of the flight plan plotted above an area identified as “with risks”; a step of defining two radials in the horizontal plane respectively passing through the first and the second points; a step of determining a first flight plan portion comprising the definition of a lateral offset angle from the original flight plan; a step of determining a vertical descent profile; a step of displaying time markers indicating the exhaustion of the oxygen reserve.

摘要翻译： 在对应于可以包括一系列级别的时间下降轮廓的减压的情况下产生安全飞行计划部分的方法包括：定义飞行计划的第一点（称为非返回点）的步骤， 表示为NRP，并且飞行计划的第二个点称为EOZ，将飞行计划的一部分划分的两个点绘制在以风险识别的区域之上; 分别在水平面中限定通过第一和第二点的两个径向的步骤; 确定第一飞行平面图部分的步骤，其包括与原始飞行计划的横向偏移角度的定义; 确定垂直下降轮廓的步骤; 显示表示氧气储备用尽的时间标记的步骤。

公开(公告)号：US20110082605A1

公开(公告)日：2011-04-07

申请号：US12876952

申请日：2010-09-07

申请人： François Coulmeau ,  Jérôme Sacle ,  Lionel Verot

发明人： François Coulmeau ,  Jérôme Sacle ,  Lionel Verot

IPC分类号： G05D1/04 ,  G05D1/00

CPC分类号： G08G5/045 ,  G08G5/0056 ,  G08G5/065

摘要： An aircraft piloting assistance method and system including determining at least one flyable slope with which the aircraft is assumed to be able to fly, based on a value of at least one flight parameter including the weight of the aircraft. The step for determining said slope or slopes with which the aircraft is able to fly, called flyable slopes is performed by a computer, and presenting the flyable slope to a decision-maker.

摘要翻译： 一种飞机驾驶辅助方法和系统，包括基于包括飞行器的重量的至少一个飞行参数的值来确定假定飞行器能够飞行的至少一个飞行坡度。 用于确定飞机能够飞行的所述斜坡或斜坡的步骤称为可飞行斜坡，由计算机执行，并将可飞行坡度呈现给决策者。

公开(公告)号：US08467966B2

公开(公告)日：2013-06-18

申请号：US12900783

申请日：2010-10-08

申请人： Bertrand Barnetche ,  François Coulmeau ,  Julien Klotz ,  Jérôme Sacle

发明人： Bertrand Barnetche ,  François Coulmeau ,  Julien Klotz ,  Jérôme Sacle

IPC分类号： G08G1/123

CPC分类号： G01C21/00 ,  G01C23/00

摘要： A device for aiding the flight management of an aircraft includes a navigation display, a personalized database capable of storing navigation-aid data, each datum comprising a classification type representative of a family or of one or more categories of navigation-aid data, one or more periods of validity of the said datum, information relating to at least one geographic zone of the said datum, one graphic and/or textual representation of the said datum, selection means allowing an operator to choose one (or more) type(s) of classification, called selected type(s), extraction means capable of extracting from the personalized database the navigation-aid datum or data called extracted data of which the type is equal to at least one selected type, of which at least one geographic zone is situated at a distance, from the flight plan or from the aircraft, that is less than a predetermined maximum distance and of which at least one period of validity verifies a predefined display time criterion, the said extraction means transmitting the said extracted datum or data to the said navigation display capable of displaying the representations of the said extracted data.

摘要翻译： 一种用于辅助飞行器的飞行管理的设备包括导航显示器，能够存储导航辅助数据的个性化数据库，每个数据包括代表家庭或一个或多个类别的导航辅助数据的分类类型，一个或 所述数据的更多的有效期，与所述数据的至少一个地理区域相关的信息，所述数据的一个图形和/或文本表示，允许操作者选择一个（或多个） 被称为选择类型的提取装置，能够从个性化数据库提取导航辅助数据或称为提取数据的数据，其类型等于至少一个选择的类型，其中至少一个地理区域是 距离飞行计划或飞机距离小于预定的最大距离，其中至少一个有效期验证预定的显示时间标准 所述提取装置将所述提取的数据或数据发送到能够显示所述提取的数据的表示的所述导航显示器。

公开(公告)号：US08180506B2

公开(公告)日：2012-05-15

申请号：US12041731

申请日：2008-03-04

申请人： Jérôme Sacle ,  François Coulmeau

发明人： Jérôme Sacle ,  François Coulmeau

IPC分类号： G05D1/10

CPC分类号： G01C23/005

摘要： The flight management computer discloses and carried onboard an aircraft can be programmed with a newly apparent speed constraint while it ensures the guidance of the aircraft in the course of a landing runway approach. It then takes account of the speed constraint by using it as target speed, when it is greater than an instruction speed which depends on the number of extended flap settings and which corresponds to the addition of a further flap setting. If appropriate, the speed constraint may be bounded below, thus making it possible to remain within the limits of the flight domain of the aircraft in its configuration at the time.

摘要翻译： 飞行管理计算机公开并携带在飞机上，可以以新的速度约束进行编程，同时确保飞机在着陆跑道过程中的引导。 然后，当它大于取决于延长的挡板设置的数量并且对应于另外的挡板设置的添加的指令速度时，将其用作目标速度来考虑速度约束。 如果适当，速度约束可以在下面被界定，从而使得有可能保持在飞行器在当时配置中的飞行领域的限度内。

公开(公告)号：US20100198433A1

公开(公告)日：2010-08-05

申请号：US12634128

申请日：2009-12-09

申请人： Stéphanie Fortier ,  Jérôme Sacle

发明人： Stéphanie Fortier ,  Jérôme Sacle

IPC分类号： G06F19/00 ,  G06F17/16

CPC分类号： G01C23/00 ,  G05D1/0005 ,  G08G5/0021 ,  G08G5/0039

摘要： Flight management system for aircraft comprising computation means capable of determining a gain or a loss in terms of flight time remaining to a point of arrival, and in terms of fuel consumption, following the input by an operator of a modification of an initial flight plan using the Direct To function. The computation means are capable of suggesting to the operator a modification of the lateral flight plan that procures an optimum gain. The flight management system also comprises a display interface capable of presenting to the operator the information concerning the gain or the loss in time and/or consumption, and of prompting the operator to accept or refuse the modification.

摘要翻译： 用于飞行器的飞行管理系统包括计算装置，该计算装置能够根据运营人输入的初始飞行计划的修改，确定在剩余到达点的飞行时间的增益或损失以及燃料消耗。 直接到功能。 计算装置能够向操作者建议获得最佳增益的侧向飞行计划的修改。 飞行管理系统还包括显示界面，能够向操作者呈现关于增益或时间和/或消耗的损失的信息，并且提示操作者接受或拒绝修改。

公开(公告)号：US20050012642A1

公开(公告)日：2005-01-20

申请号：US10483828

申请日：2003-01-31

申请人： Jérôme Sacle

发明人： Jérôme Sacle

IPC分类号： G01C23/00

CPC分类号： G01C23/005

摘要： This attitude indicator comprises a display device (11) with screen (110), producing on a screen background (4, 5), a three-dimensional aircraft silhouette (3), mobile according to the three axes of rotation and viewed from the rear, according to attitude angles which correspond to the attitude angle measurements received by onboard instruments and which are referenced with respect to an aircraft datum having a roll axis perpendicular to the surface of the screen and pitch and yaw axes in the plane of the screen, one, the pitch axis, being horizontal and the other, the yaw axis, vertical. It has the advantage of affording the crew a concrete view of the attitude of the aircraft enabling piloting to be rendered more natural and more intuitive, and hence safety to be improved.

摘要翻译： 该姿势指示器包括具有屏幕（110）的显示装置（11），其在屏幕背景（4,5）上生成，三维飞行器轮廓（3），根据三个旋转轴线可移动并从后方观察 根据对应于车载仪器接收到的姿态角度测量的姿态角度，并且相对于具有垂直于屏幕表面的滚动轴线和在屏幕平面中的俯仰角和偏航轴线的飞行器基准而参考的姿态角度， 俯仰轴线，水平线，另一侧，偏航轴线，垂直线。 它具有为飞行员提供飞机态度的具体观点，使飞行员能够更加自然，更直观，从而提高安全性。

公开(公告)号：US08498769B2

公开(公告)日：2013-07-30

申请号：US12780684

申请日：2010-05-14

申请人： Jérôme Sacle ,  Stéphanie Fortier ,  François Coulmeau

发明人： Jérôme Sacle ,  Stéphanie Fortier ,  François Coulmeau

IPC分类号： G01C22/00

CPC分类号： G01C23/00 ,  G01C21/00 ,  G05D1/0202

摘要： Method of formulating a lateral flight trajectory for the rejoining by an aircraft (200) of a trajectory of a flight plan (910) comprising a plurality of waypoints (911, 912, 913), the aircraft (200) flying outside of the flight plan (910) and according to a divergent track with respect to the trajectory of the flight plan (210), characterized in that the method: determines a waypoint (913) of the flight plan for the rejoining, defined as the first waypoint (913) of the flight plan included in a capture zone defined by the flight plan trajectory situated downstream of the point of intersection between the straight line defined by an angle (α) with the perpendicular to the track of the aircraft and the trajectory of the flight plan, formulates the optimal lateral flight trajectory for a rejoining by the aircraft (200) at the determined waypoint. Advantageously, the flight trajectory formulation method allows the application of speed and/or altitude constraints to the aircraft (200) taking into account speed and/or altitude constraints imposed along the trajectory of the flight plan (910).

摘要翻译： 制定由飞行计划（910）的轨迹的飞行器（200）重新连接的侧向飞行轨迹的方法，该飞行计划包括多个航路点（911,912,913），飞行器（200）飞行在飞行计划之外 （910）并且根据相对于飞行计划（210）的轨迹的发散轨迹，其特征在于，所述方法：确定被定义为所述第一航点（913）的重新连接的飞行计划的航点（913） 飞行计划中包含的飞行计划包括在由飞行计划轨迹定义的捕获区域中，该飞行计划轨迹位于由角度（α）与垂直于飞行器的轨迹的垂线之间的交点点和飞行计划的轨迹之间的交点处的下游， 制定航空器（200）在确定航路点重新连接的最佳横向飞行轨迹。 有利地，飞行轨迹拟合方法允许考虑到沿着飞行计划的轨迹施加的速度和/或高度约束，对飞行器（200）应用速度和/或高度限制（910）。

公开(公告)号：US08447442B2

公开(公告)日：2013-05-21

申请号：US12958820

申请日：2010-12-02

申请人： Jérôme Sacle ,  Christophe Caillaud ,  Lionel Verot

发明人： Jérôme Sacle ,  Christophe Caillaud ,  Lionel Verot

IPC分类号： G05D1/00 ,  G08G5/02 ,  G06F19/00

CPC分类号： G08G5/0039 ,  G05D1/0676 ,  G08G5/025

摘要： A method is provided for assisting in rejoining a vertical descent trajectory that an aircraft is assumed to have to follow, using a flight management system FMS embedded onboard the aircraft, and includes the following steps: calculation of a vertical deviation VDEV, in the vertical plane, between the aircraft and the vertical descent trajectory, and comparison between the vertical deviation VDEV and a predetermined deviation threshold SVDEV; when the vertical deviation VDEV reaches the deviation threshold SVDEV, a step during which the activation of an optimized mode for catching up on the vertical descent trajectory is authorized; if the optimized mode for catching up on the vertical descent trajectory is activated, piloting of the aircraft by the flight management system FMS in optimized catch-up mode, that is to say at minimum thrust with a target rejoining speed in level VCRP and a target rejoining speed in downward trajectory, the target rejoining speed in level VCRP being equal to the maximum L/D ratio speed of the aircraft uprated by a first value V1 of between 5 and 15 knots, and the target rejoining speed in downward trajectory VCRD being equal to the maximum operating speed VMO with which the aircraft is allowed to fly downrated by a second value V2 of between 3 and 10 knots, a knot being equal to 0.514 ms−1.

摘要翻译： 提供了一种使用飞行器上嵌入的飞行管理系统FMS来协助重新连接飞机必须遵循的垂直下降轨迹的方法，并且包括以下步骤：在垂直平面中计算垂直偏差VDEV 在飞行器和垂直下降轨迹之间，垂直偏差VDEV与预定偏差阈值SVDEV之间的比较; 当垂直偏差VDEV达到偏差阈值SVDEV时，授权激活用于追赶垂直下降轨迹的优化模式的步骤; 如果激活用于追赶垂直下降轨迹的优化模式，则飞行管理系统FMS以优化的追赶模式驾驶飞行器，即以VCRP级中的目标重合速度的最小推力和目标 在下降轨迹上重新加速，液位VCRP中的目标重合速度等于升高了5和15节之间的第一值V1的飞机的最大L / D比速度，并且向下轨迹VCRD中的目标重合速度相等 飞行器允许飞行的最大操作速度VMO降低3节和10节之间的第二值V2，结点等于0.514 ms-1。

公开(公告)号：US08046165B2

公开(公告)日：2011-10-25

申请号：US11934751

申请日：2007-11-03

申请人： Jérôme Sacle ,  François Coulmeau

发明人： Jérôme Sacle ,  François Coulmeau

IPC分类号： G01C21/30

CPC分类号： G08G5/065 ,  G08G5/0013

摘要： The invention relates to a device for assisting in the navigation of an aircraft in an airport zone comprising a surface navigation system and means of acquiring in real time, while navigating on the ground or in flight, new information or temporary information relating to the navigation in the airport zone. The surface navigation system uses information relating to the navigation in the airport zone. The information is previously stored in a database on board the aircraft. The device includes means for decoding and analysing the new or temporary information relating to the navigation in the airport zone, means of filtering the information according to the airport concerned and the validity date of the information, means of correlating the information with the information previously stored, and means of displaying the information.

摘要翻译： 本发明涉及一种用于协助航空器在机场区域导航的装置，其包括地面导航系统和在地面上或飞行中实时获取的新信息或与导航相关的临时信息的装置 机场区。 地面导航系统使用与机场区域相关的导航信息。 信息先前存储在飞机上的数据库中。 该装置包括用于解码和分析与机场区域中的导航相关的新的或临时信息的装置，根据有关机场对信息进行过滤的装置和信息的有效日期;将信息与先前存储的信息相关联的装置 ，以及显示信息的方法。

公开(公告)号：US20110137495A1

公开(公告)日：2011-06-09

申请号：US12958820

申请日：2010-12-02

申请人： Jérôme SACLE ,  Christophe CAILLAUD ,  Lionel VEROT

发明人： Jérôme SACLE ,  Christophe CAILLAUD ,  Lionel VEROT

IPC分类号： G05D1/00

CPC分类号： G08G5/0039 ,  G05D1/0676 ,  G08G5/025

摘要： A method is provided for assisting in rejoining a vertical descent trajectory that an aircraft is assumed to have to follow, using a flight management system FMS embedded onboard the aircraft, and includes the following steps: calculation of a vertical deviation VDEV, in the vertical plane, between the aircraft and the vertical descent trajectory, and comparison between the vertical deviation VDEV and a predetermined deviation threshold SVDEV; when the vertical deviation VDEV reaches the deviation threshold SVDEV, a step during which the activation of an optimized mode for catching up on the vertical descent trajectory is authorized; if the optimized mode for catching up on the vertical descent trajectory is activated, piloting of the aircraft by the flight management system FMS in optimized catch-up mode, that is to say at minimum thrust with a target rejoining speed in level VCRP and a target rejoining speed in downward trajectory, the target rejoining speed in level VCRP being equal to the maximum L/D ratio speed of the aircraft uprated by a first value V1 of between 5 and 15 knots, and the target rejoining speed in downward trajectory VCRD being equal to the maximum operating speed VMO with which the aircraft is allowed to fly downrated by a second value V2 of between 3 and 10 knots, a knot being equal to 0.514 ms−1.

摘要翻译： 提供了一种使用飞行器上嵌入的飞行管理系统FMS来协助重新连接飞机必须遵循的垂直下降轨迹的方法，并且包括以下步骤：在垂直平面中计算垂直偏差VDEV 在飞行器和垂直下降轨迹之间，垂直偏差VDEV与预定偏差阈值SVDEV之间的比较; 当垂直偏差VDEV达到偏差阈值SVDEV时，授权激活用于追赶垂直下降轨迹的优化模式的步骤; 如果激活用于追赶垂直下降轨迹的优化模式，则飞行管理系统FMS以优化的追赶模式驾驶飞行器，即以VCRP级中的目标重合速度的最小推力和目标 在下降轨迹中重新加速，液位VCRP中的目标重合速度等于升高了5和15节之间的第一值V1的飞机的最大L / D比速度，并且向下轨迹VCRD中的目标重合速度相等 飞行器允许飞行的最大操作速度VMO降低3节和10节之间的第二值V2，结点等于0.514 ms-1。