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公开(公告)号：US08200421B2
公开(公告)日：2012-06-12
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: An altitude profile representative of the terrain overflown by an aircraft is established. Thereafter, an altitude limit curve which comprises an intersection with the altitude profile upon the engagement of a terrain avoidance maneuver is determined. As soon as there is no longer any intersection of the limit curve with the altitude profile, the terrain avoidance maneuver is interrupted.
Abstract translation: 建立代表航空器溢出的地形的高度剖面。 此后，确定在地形回避机动的接合时包括与高度分布的交点的高度极限曲线。 一旦极限曲线与高度剖面不再有任何交点，地形回避机动就会中断。
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2.发明授权Method and device for aiding the piloting of an airplane during an approach phase 有权在接近阶段帮助驾驶飞机的方法和装置公开(公告)号：US08014912B2
公开(公告)日：2011-09-06
申请号：US11934608
申请日：2007-11-02
Applicant: Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Bénédicte Michal , Adrien Ott , Frédéric Lemoult
Inventor： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Bénédicte Michal , Adrien Ott , Frédéric Lemoult
CPC classification number: G08G5/025 , G08G5/0021
Abstract: A method and device for aiding the piloting of an airplane includes: (1) determining current values of flight parameters of the airplane, (2) determining, with the aid of the current values, an approach distance that corresponds to a distance in a horizontal plane between the current position of the airplane and a position of contact with the ground, and (3) presenting the approach distance on a screen.
Abstract translation: 一种用于辅助飞机驾驶的方法和装置包括：（1）确定飞机的飞行参数的当前值，（2）借助于当前值确定对应于水平距离的接近距离 在飞机的当前位置和与地面接触的位置之间的平面，以及（3）在屏幕上呈现接近距离。
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3.发明授权Method and device for determining the air turbulence likely to be encountered by an aircraft 有权用于确定飞机可能遇到的空气湍流的方法和装置公开(公告)号：US08005583B2
公开(公告)日：2011-08-23
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: A method and device for determining the air turbulence likely to be encountered by a first aircraft may use a turbulence indication from a second aircraft so as to make and use a prediction of the impact of the turbulence on the first aircraft if it is located in a particular position.
Abstract translation: 用于确定可能由第一飞行器遇到的空气湍流的方法和装置可以使用来自第二飞行器的湍流指示，以便如果湍流位于 特殊的位置。
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4.发明申请SYSTEM FOR GUIDING AND PILOTING AN AIRCRAFT IN CASE OF INABILITY OF THE PILOTS 有权用于在飞机失能的情况下引导和驾驶飞机的系统公开(公告)号：US20090319104A1
公开(公告)日：2009-12-24
申请号：US12136599
申请日：2008-06-10
Applicant: Jerome Bailly , Isabelle Lacaze
Inventor： Jerome Bailly , Isabelle Lacaze
CPC classification number: G08G5/025 , B64D45/0015 , B64D2045/0055 , G08G5/0056
Abstract: The system (1) comprises means (3A to 3D) for detecting incapacity of the pilots to control the aircraft, and means (5) for automatically guiding and piloting the aircraft until it lands at an airport, on detection of such an incapacity.
Abstract translation: 系统（1）包括用于检测飞行员无法控制飞行器的能力的装置（3A至3D），以及用于在检测到这种丧失工作能力时自动引导和驾驶飞行器直到飞机降落到机场的装置（5）。
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5.发明申请PROCESS FOR VERIFYING THE COHERENCE BETWEEN AIRCRAFT TAKE-OFF PARAMETERS AND AN AVAILABLE RUNWAY LENGTH 有权验证飞机起飞参数与可行驶长度之间的一致性的过程公开(公告)号：US20100094488A1
公开(公告)日：2010-04-15
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
CPC classification number: G08G5/065 , G08G5/0021 , G08G5/0065
Abstract: A method for verifying the coherence of the takeoff parameters of an aircraft from an airport with an available runway length at the moment of takeoff comprises a step (E20) of identifying a takeoff runway and a step (E30) of validating the 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.Use to make takeoff of an aircraft from an airport safe.
Abstract translation: 一种用于验证来自机场的飞机起飞参数在起飞时具有可用跑道长度的相干性的方法包括识别起飞跑道的步骤（E20）和用起飞参数验证起飞参数的步骤（E30） 如果起飞距离短于与识别的起飞跑道相关的剩余跑道长度，则授权飞机起飞。 用于从机场起飞飞机的安全。
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Patent Agency Ranking
6.发明申请METHOD AND DEVICE FOR ASSISTING AN AIRCRAFT FLIGHT CONTROL DURING LANDING APPROACH 有权用于在着陆方法中辅助飞机飞行控制的方法和装置公开(公告)号：US20100036551A1
公开(公告)日：2010-02-11
申请号：US11911611
申请日：2006-05-03
Applicant: Isabelle Lacaze , Vincent Foucart , Jean-Louis De Menorval , Didier Zadrozynski , Frederic Lemoult , Joelle Barthe , Sebastien Lhote , Irene Hoste Ventos
Inventor： Isabelle Lacaze , Vincent Foucart , Jean-Louis De Menorval , Didier Zadrozynski , Frederic Lemoult , Joelle Barthe , Sebastien Lhote , Irene 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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公开(公告)号：US20080215195A1
公开(公告)日：2008-09-04
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
CPC classification number: G05D1/0646 , G01C5/005 , G08G5/045
Abstract: The invention concerns a terrain avoidance method and system for an aircraft. The system comprises a collision alarm device (3) and an auto-pilot device (5) including means (7) for determining a climbing order with optimal slope for the aircraft, means (12) for checking whether a first altitude gain at the relief, by applying the optimal slope climbing order, is sufficient for clearing said relief, means (11) for finding if there exists at least one heading variation value, for which the corresponding altitude gain is sufficient to clear the relief, and means (17, 22) 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: 本发明涉及一种用于飞机的地形避免方法和系统。 该系统包括碰撞报警装置（3）和自动导向装置（5），包括用于确定飞行器具有最佳斜率的爬坡顺序的装置（7），用于检查救护装置上的第一高度增益的装置（12） 通过应用最佳坡度攀爬顺序，足以清除所述浮雕，用于查找是否存在至少一个航向变化值的装置（11），对于该航向变化值，相应的高度增益足以清除浮雕，以及装置（17） 22）如果第一高度增益是足够的，则适用于第一高度增益的最佳斜坡爬坡顺序，以保持当前航向，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， 对应于所选择的航向变化值的航向顺序。
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8.发明申请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：US20060025901A1
公开(公告)日：2006-02-02
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: G01C23/00
CPC classification number: G05D1/0676
Abstract: System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing. The system (1) comprises information sources (3) able to provide information relating to the aircraft and to its environment, a computation unit (4) which determines, with the aid of information provided by the information sources (3), an energy reference profile which preferably comprises a trajectory reference profile and a speed reference profile and which is intended to allow the aircraft to regain a stabilized approach trajectory, if it follows this reference profile, means of monitoring (7) for verifying that the aircraft is indeed following said reference profile, and means of indication (6) which supply the pilot with piloting indications at least to make it possible to pilot the aircraft in such a way that it always follows said reference profile.
Abstract translation: 在进入跑道的过程中协助驾驶飞机的系统，以便着陆。 系统（1）包括能够提供与飞机及其环境相关的信息的信息源（3），计算单元（4），其借助于由信息源（3）提供的信息确定能量参考 其优选地包括轨迹参考轮廓和速度参考轮廓，并且其旨在允许飞机重新获得稳定的进场轨迹（如果遵循该参考轮廓），则监视装置（7）用于验证飞机是否确实遵循所述 参考简档和指示装置（6），其向飞行员提供驾驶指示，至少使得可以以使其始终遵循所述参考轮廓的方式驾驶飞行器。
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公开(公告)号：US09092980B2
公开(公告)日：2015-07-28
申请号：US12617244
申请日：2009-11-12
Applicant: Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jérôme Bailly , Isabelle Lacaze , Sylvain Thezelais , Jérôme Goyet
Inventor： Paule Botargues , Nicolas Caule , Christelle Ledauphin , Jérôme Bailly , Isabelle Lacaze , Sylvain Thezelais , Jérôme 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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10.发明授权System for guiding and piloting an aircraft in case of inability of the pilots 有权在飞行员无力的情况下指导和驾驶飞机的系统公开(公告)号：US08108086B2
公开(公告)日：2012-01-31
申请号：US12136599
申请日：2008-06-10
Applicant: Jerome Bailly , Isabelle Lacaze
Inventor： Jerome Bailly , Isabelle Lacaze
CPC classification number: G08G5/025 , B64D45/0015 , B64D2045/0055 , G08G5/0056
Abstract: An aircraft guidance and piloting system automatically guides and pilots an aircraft in the event a pilot is unable to guide or pilot the aircraft. Upon determining the pilot's inability to control the aircraft, a processor transmits an automatic engagement command to a control unit. The control unit guides and pilots the aircraft to an alternative airport for landing.
Abstract translation: 如果飞行员无法指导或驾驶飞机，飞机指导和驾驶系统将自动指导和飞行飞机。 在确定飞行员无法控制飞机时，处理器将自动接合命令发送到控制单元。 控制单元引导飞行员到另一个机场着陆。
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