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公开(公告)号：US20100100261A1
公开(公告)日：2010-04-22
申请号：US12582240
申请日：2009-10-20
Applicant: Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jerome Bailly , Isabelle Lacaze , Sylvain Thezelais , Jerome Goyet
Inventor： Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jerome Bailly , Isabelle Lacaze , Sylvain Thezelais , Jerome Goyet
CPC classification number: G08G5/04 , G01C5/005 , G05D1/0646
Abstract: According to the invention, an altitude profile (PA) representative of the terrain overflown by the aircraft (AC) is established, and then an altitude limit curve (C) which comprises an intersection with said profile (PA) upon the engagement of a terrain avoidance maneuver is determined. As soon as there is no longer any intersection of the limit curve (C) with the altitude profile (PA), said terrain avoidance maneuver is interrupted.
Abstract translation: 根据本发明，建立了代表由飞行器（AC）溢出的地形的高度分布（PA），然后在地形接合时包括与所述轮廓（PA）的交点的高度极限曲线（C） 确定回避机动。 一旦极限曲线（C）与高度剖面（PA）不再有任何交点，则所述的地形回避机动被中断。
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12.发明授权System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing 有权在进入跑道的过程中协助驾驶飞机的系统，以便着陆公开(公告)号：US07647140B2
公开(公告)日：2010-01-12
申请号：US11145951
申请日：2005-06-07
Applicant: Jean-Pierre Demortier , Isabelle Lacaze , Jean-Louis De Menorval
Inventor： Jean-Pierre Demortier , Isabelle Lacaze , Jean-Louis De Menorval
IPC: G06F19/00
CPC classification number: G05D1/0676
Abstract: A system for aiding the piloting of an aircraft during a runway approach includes an information source that provides information relating to the aircraft and its environment. A computation unit determines, with the aid of information provided by the information source, an energy reference profile having a trajectory reference profile and a speed reference profile that allows the aircraft to regain a stabilized approach trajectory, if it follows the reference profile. A monitor verifies that the aircraft is following the reference profile. An indicator supplies the pilot with piloting indications for piloting the aircraft so as to follow the reference profile.
Abstract translation: 在跑道方法中辅助飞机驾驶的系统包括提供与飞行器及其环境有关的信息的信息源。 计算单元借助于由信息源提供的信息确定具有轨迹参考轮廓和速度参考轮廓的能量参考轮廓，其允许飞机重新获得稳定的进场轨迹，如果它遵循参考轮廓。 监视器验证飞机是否遵循参考资料。 一个指示器为飞行员提供驾驶飞行员的驾驶指示，以便遵循参考资料。
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13.发明申请METHOD AND DEVICE FOR AIDING THE PILOTING OF AN AIRPLANE DURING AN APPROACH PHASE 有权方法和装置，用于在方法阶段中用于驾驶飞机的飞行公开(公告)号：US20080140272A1
公开(公告)日：2008-06-12
申请号：US11934608
申请日：2007-11-02
Applicant: Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Benedicte Michal , Adrien Ott , Frederic Lemoult
Inventor： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Benedicte Michal , Adrien Ott , Frederic Lemoult
CPC classification number: G08G5/025 , G08G5/0021
Abstract: The device (1) comprises means (3) for determining the current values of flight parameters of the airplane, means (4) for determining, at least with the aid of said current values, an approach distance which corresponds to a distance in a horizontal plane between the current position of the airplane and a position of contact with the ground, and display means (6) for presenting this approach distance on a screen (8).
Abstract translation: 装置（1）包括用于确定飞机的飞行参数的当前值的装置（3），用于至少借助所述当前值确定对应于水平距离的接近距离的装置（4） 在飞机的当前位置和与地面接触的位置之间的平面以及用于在屏幕（8）上呈现该接近距离的显示装置（6）。
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公开(公告)号：US07899620B2
公开(公告)日：2011-03-01
申请号：US11908786
申请日：2006-03-01
Applicant: Christophe Jourdan , Pierre Fabre , Stephane Walter , Isabelle Lacaze
Inventor： Christophe Jourdan , Pierre Fabre , Stephane Walter , Isabelle Lacaze
IPC: G08G1/16
CPC classification number: G05D1/0646 , G01C5/005 , G08G5/045
Abstract: A terrain avoidance method and system for an aircraft includes a collision alarm device and an auto-pilot device including a first determination unit for determining a climbing order with optimal slope for the aircraft, a checking unit for checking whether a first altitude gain at the relief, by applying the optimal slope climbing order, is sufficient for clearing said relief, a finding unit for finding if at least one heading variation value exists, for which the corresponding altitude gain is sufficient to clear the relief, and a switching and calculating unit for applying to the aircraft, if the first altitude gain is sufficient, an optimal slope climbing order with an order to maintain the current heading and, if the first altitude gain is insufficient, a particular climbing order sufficient to clear the relief, with a heading order which corresponds to the selected heading variation value.
Abstract translation: 一种用于飞行器的地形回避方法和系统包括一个碰撞报警装置和一个自动导航装置，包括用于确定飞机具有最佳坡度的爬坡顺序的第一确定单元，用于检查浮雕处的第一高度增益的检查单元 通过应用最佳坡度爬坡顺序，足以清除所述浮雕，找出单元，用于确定是否存在至少一个航向变化值，相应的高度增益足以使其消除浮力;以及切换和计算单元，用于 如果第一高度增益足够，则适用于飞机，具有维持当前航向的最佳斜坡爬升顺序，如果第一高度增益不足，则具有足以清除浮雕的特定爬坡顺序 其对应于所选择的航向变化值。
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15.发明授权Process for verifying the coherence between aircraft take-off parameters and an available runway length 有权用于验证飞机起飞参数和可用跑道长度之间的一致性的过程公开(公告)号：US08380372B2
公开(公告)日：2013-02-19
申请号：US12537478
申请日：2009-08-07
Applicant: Benedicte Michal , Fabien Pitard , Jean-Pierre Demortier , Christine Charbonnier , Isabelle Lacaze , Gael Marchand , Christine Le Duigou , Jerome Cayrou , Vincent Blondin , Frederic Lemoult
Inventor： Benedicte Michal , Fabien Pitard , Jean-Pierre Demortier , Christine Charbonnier , Isabelle Lacaze , Gael Marchand , Christine Le Duigou , Jerome Cayrou , Vincent Blondin , Frederic Lemoult
IPC: G06F19/00
CPC classification number: G08G5/065 , G08G5/0021 , G08G5/0065
Abstract: A method for verifying coherence of takeoff parameters of an aircraft from an airport with an available runway length at a moment of takeoff comprises a step of identifying a takeoff runway and a step of validating takeoff parameters with a view to authorizing takeoff of the aircraft if the takeoff distance is shorter than the remaining runway length associated with the identified takeoff runway.
Abstract translation: 一种用于在起飞时刻检验具有可用跑道长度的来自机场的飞行器的起飞参数的一致性的方法包括识别起飞跑道的步骤和验证起飞参数的步骤，以便授权起飞飞机，如果 起飞距离比与识别的起飞跑道相关的跑道长度短。
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Patent Agency Ranking
16.发明授权Method and device for assisting an aircraft flight control during landing approach 有权在着陆过程中协助飞机飞行控制的方法和装置公开(公告)号：US08346412B2
公开(公告)日：2013-01-01
申请号：US11911611
申请日：2006-05-03
Applicant: Isabelle Lacaze , Vincent Foucart , Jean-Louis De Menorval , Didier Zadrozynski , Frédéric Lemoult , Joëlle Barthe , Sébastien Lhote , Irène Hoste Ventos
Inventor： Isabelle Lacaze , Vincent Foucart , Jean-Louis De Menorval , Didier Zadrozynski , Frédéric Lemoult , Joëlle Barthe , Sébastien Lhote , Irène Hoste Ventos
CPC classification number: G05D1/0676 , G01C23/00 , G08G5/025
Abstract: The inventive flight control assisting device comprises first means (4) for determining the actual aircraft flight conditions, second means (5) for determining, with the aid of said actual flight conditions and a predetermined pattern, a minimum approaching distance corresponding to a minimum distance between projections on the horizontal plane of the aircraft actual position and a touch-down point when said aircraft moves downwards and decelerates according to an optimised approach in such a way that stabilised approaching conditions are attained, and display means (7) for displaying at least said minimum approaching distance on a navigation screen (9) in the form of a first circular arc focused on a position relative to the aircraft which displays the touch-down position.
Abstract translation: 本发明的飞行控制辅助装置包括用于确定实际飞行器飞行情况的第一装置（4），用于借助于所述实际飞行状况和预定模式来确定对应于最小距离的最小接近距离的第二装置（5） 在飞行器实际位置的水平面上的突起之间和当所述飞行器向下移动并且以达到稳定的接近状态的方式的优化方式减速时的接触点;以及至少显示至少 所述最小逼近距离在导航屏幕（9）上以第一圆弧的形式聚焦在相对于飞行器的位置上，该第一圆弧显示了下降位置。
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17.发明授权Method for detecting an error in input of one of the takeoff parameters into a flight management system 有权用于检测飞行管理系统中的一个起飞参数的输入中的错误的方法公开(公告)号：US07885734B2
公开(公告)日：2011-02-08
申请号：US11559917
申请日：2006-11-15
Applicant: Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
Inventor： Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
CPC classification number: G05B23/0235 , G05D1/0083
Abstract: A method for detecting an error in input of one of the takeoff parameters into a flight management system includes a step of calculating a limit value based on one or more takeoff parameters input into the flight management system. The method further includes a step of comparing the calculated limit value with characteristic takeoff values.
Abstract translation: 一种用于检测飞行管理系统中的一个起飞参数的输入中的错误的方法包括基于输入到飞行管理系统中的一个或多个起飞参数来计算极限值的步骤。 该方法还包括将所计算的极限值与特征起飞值进行比较的步骤。
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公开(公告)号：US20100125381A1
公开(公告)日：2010-05-20
申请号：US12617244
申请日：2009-11-12
Applicant: Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jerome Bailly , Isabelle Lacaze , Sylvain Thezelais , Jerome Goyet
Inventor： Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jerome Bailly , Isabelle Lacaze , Sylvain Thezelais , Jerome Goyet
CPC classification number: G08G5/04 , G01C5/005 , G05D1/0646 , G08G5/0008 , G08G5/045
Abstract: According to the invention, a terrain avoidance maneuver is engaged when the alerts of a given pair of alerts are emitted simultaneously, the triggering of one of the alerts depending on the information provided by a first measurement chain and the triggering of the other alert of the pair relying on information provided by a second measurement chain, distinct from and independent of the first chain.
Abstract translation: 根据本发明，当给定的一对警报的警报同时发射时，进行地形回避机动，根据由第一测量链提供的信息触发其中一个警报，并触发另一警报的警报 依赖于第二测量链提供的信息，与第一链不同且独立于第一链。
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19.发明申请METHOD FOR DETECTING AN ERROR IN INPUT OF ONE OF THE TAKEOFF PARAMETERS INTO A FLIGHT MANAGEMENT SYSTEM 有权检测飞行管理系统中的一个参数的输入错误的方法公开(公告)号：US20070288130A1
公开(公告)日：2007-12-13
申请号：US11559917
申请日：2006-11-15
Applicant: Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
Inventor： Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
IPC: G06F19/00
CPC classification number: G05B23/0235 , G05D1/0083
Abstract: A method for detecting an error in input of one of the takeoff parameters into a flight management system includes a step of calculating a limit value based on one or more takeoff parameters input into the flight management system. The method further includes a step of comparing the calculated limit value with characteristic takeoff values.
Abstract translation: 一种用于检测飞行管理系统中的一个起飞参数的输入中的错误的方法包括基于输入到飞行管理系统中的一个或多个起飞参数来计算极限值的步骤。 该方法还包括将所计算的极限值与特征起飞值进行比较的步骤。
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20.发明申请METHOD AND DEVICE FOR DETERMINING THE AIR TURBULENCE LIKELY TO BE ENCOUNTERED BY AN AIRCRAFT 有权用于确定航空器所确定的空气湍流的方法和装置公开(公告)号：US20070260366A1
公开(公告)日：2007-11-08
申请号：US11693191
申请日：2007-03-29
Applicant: Isabelle Lacaze , Jacques Rosay , Jean-Pierre Daniel
Inventor： Isabelle Lacaze , Jacques Rosay , Jean-Pierre Daniel
CPC classification number: G01C23/00 , G01W1/00 , G01W2001/003
Abstract: Method and device for determining the air turbulence likely to be encountered by an aircraft. The device (1) which is provided on a second aircraft comprises a means (12) for using a turbulence indication from a first aircraft to make a prediction of the impact of the turbulence on this second aircraft if it is located in a particular position, and a means (13, 14) for using this prediction.
Abstract translation: 用于确定飞机可能遇到的空气湍流的方法和装置。 设置在第二飞行器上的装置（1）包括用于使用来自第一飞行器的湍流指示的装置（12），以便如果湍流位于特定位置时预测湍流对该第二飞行器的影响， 以及用于使用该预测的装置（13,14）。
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