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：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：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：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：US08306677B2

公开(公告)日：2012-11-06

申请号：US11942240

申请日：2007-11-19

申请人： Guy Deker ,  Jérôme Sacle ,  François Coulmeau

发明人： Guy Deker ,  Jérôme Sacle ,  François Coulmeau

IPC分类号： G08B21/00 ,  B64D45/00

CPC分类号： G08G5/0091 ,  G01W1/10 ,  G01W2001/003 ,  G08G5/0008

摘要： The invention relates to a method for automatic detection of turbulence by a second aircraft, by information exchange between the second aircraft and at least a first aircraft. The first aircraft has means for transmitting information and the second aircraft has means for receiving the information transmitted by the first aircraft. The method includes the identification of information about turbulence liable to be encountered by the second aircraft, by analyzing the information received from the first aircraft. An alarm is activated on the basis of the turbulence information.

摘要翻译： 本发明涉及一种通过第二飞行器与至少第一飞行器之间的信息交换自动检测第二飞行器的湍流的方法。 第一架飞机具有发送信息的手段，第二架飞机具有接收第一架飞机发送的信息的装置。 该方法包括通过分析从第一架飞机接收到的信息来识别有关第二架飞机可能遇到的湍流的信息。 基于湍流信息激活报警。

公开(公告)号：US20100161156A1

公开(公告)日：2010-06-24

申请号：US12633994

申请日：2009-12-09

申请人： François Coulmeau ,  Christophe Caillaud ,  Jérôme Sacle

发明人： François Coulmeau ,  Christophe Caillaud ,  Jérôme Sacle

IPC分类号： G01C23/00 ,  G06F19/00

CPC分类号： G08G5/0039 ,  G01C23/005 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/0056

摘要： The invention relates to a device for assisting in the choice of a diversion airport for an aircraft piloted by a crew (200), said aircraft comprising a flight management system including location means (207) calculating the position of the aircraft, said device comprising a navigation database (202) and a performance database (203) of the aircraft, said device being characterized in that it comprises: a company database (201) comprising airports and characteristics of said airports, means (205) of calculating a list of airports, called candidate airports, from the airports in the company database, from the navigation database and from the selected characteristics by the crew, means (204) for calculating remaining flight time and fuel consumption predictions for each of the candidate airports from the position of the aircraft, from weather conditions and from the performance database, an interface giving the favoured airports for diversion according to pre-established criteria or determined in real time using the interface.

摘要翻译： 本发明涉及一种用于协助选择由机组（200）驾驶的飞机的转向机场的装置，所述飞机包括一个飞行管理系统，该飞行管理系统包括计算飞机位置的位置装置（207），所述装置包括一个 导航数据库（202）和飞行器的演奏数据库（203），所述装置的特征在于它包括：包括所述机场的机场和特征的公司数据库（201），计算机场列表的装置（205） 所谓的候选机场，从公司数据库中的机场，从导航数据库和船员的选定特征，用于从飞机位置计算每个候选机场的剩余飞行时间和燃料消耗预测的装置（204） ，从天气状况和性能数据库，根据预先确定的标准或阻止，给予偏好机场转移的接口 使用界面实时开采。

公开(公告)号：US08676481B2

公开(公告)日：2014-03-18

申请号：US12633994

申请日：2009-12-09

申请人： François Coulmeau ,  Christophe Caillaud ,  Jérôme Sacle

发明人： François Coulmeau ,  Christophe Caillaud ,  Jérôme Sacle

IPC分类号： G06F17/30 ,  G08G5/00 ,  G05D1/06 ,  G01C23/00

CPC分类号： G08G5/0039 ,  G01C23/005 ,  G05D1/0676 ,  G08G5/0021 ,  G08G5/0056

摘要： The invention relates to a device for assisting in the choice of a diversion airport for an aircraft piloted by a crew (200), said aircraft comprising a flight management system including location means (207) calculating the position of the aircraft, said device comprising a navigation database (202) and a performance database (203) of the aircraft, said device being characterized in that it comprises a company database (201) comprising airports and characteristics of said airports, means (205) of calculating a list of airports, called candidate airports, from the airports in the company database, from the navigation database and from the selected characteristics by the crew, means (204) for calculating remaining flight time and fuel consumption predictions for each of the candidate airports from the position of the aircraft, from weather conditions and from the performance database, and an interface giving the favored airports for diversion according to pre-established criteria or determined in real time using the interface.

摘要翻译： 本发明涉及一种用于协助选择由机组（200）驾驶的飞机的转向机场的装置，所述飞机包括一个飞行管理系统，该飞行管理系统包括计算飞机位置的位置装置（207），所述装置包括一个 导航数据库（202）和飞行器的性能数据库（203），所述设备的特征在于，其包括包括机场和所述机场的特征的公司数据库（201），计算机场列表的方法（205），称为 候选机场，从公司数据库中的机场，从导航数据库和船员的选定特征，用于从飞机位置计算每个候选机场的剩余飞行时间和燃料消耗预测的装置（204） 从天气条件和性能数据库，以及根据预先确定的标准给予优惠机场转移的接口 使用界面实时切断。

公开(公告)号：US20100324812A1

公开(公告)日：2010-12-23

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： G01C21/00

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） 包括在由飞行计划轨迹定义的捕获区域中的飞行计划，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：US07853370B2

公开(公告)日：2010-12-14

申请号：US11856019

申请日：2007-09-15

申请人： François Coulmeau ,  Jérôme Sacle

发明人： François Coulmeau ,  Jérôme Sacle

IPC分类号： G06F19/00 ,  G06F17/11

CPC分类号： G08G5/025 ,  G05D1/0676 ,  G08G5/0021

摘要： The present invention relates to a method for estimating the touchdown point of the wheels of an aircraft on a landing runway and the distance to be traveled by the aircraft on the runway from the touchdown point to reach a controlled speed below which it can perform any maneuver on the ground. The method comprises an in-flight step of estimating a height and a speed of passage above the threshold of the runway. It also comprises an in-flight step of estimating the touchdown point of the wheels of the aircraft on the landing runway and the distance to be traveled to reach the controlled speed, on the basis of the estimation of the height and the speed of passage above the threshold of the runway. It also comprises a step while going on the runway of estimating the distance to be traveled from the real touchdown point to reach the controlled speed, taking account of the braking forces provided by the brakes, the airbrakes and the thrust reversers.

摘要翻译： 本发明涉及一种用于估计飞机在着陆跑道上的落地点的距离以及飞机从着陆点在跑道上行驶的距离以达到可控制速度的方法，在该速度下可以进行任何操纵 在地上。 该方法包括估计在跑道的阈值之上的高度和通过速度的飞行中步骤。 它还包括在飞行中步骤，基于对上述通道的高度和通过速度的估计，估计着陆跑道上飞行器的车轮的着陆点和待行驶的距离以达到受控速度 跑道的门槛。 考虑到制动器，制动器和推力反向器提供的制动力，它还包括在跑道上进行估计从实际着陆点行进的距离以达到受控速度的步骤。