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1.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
申请人： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Benedicte Michal , Adrien Ott , Frederic Lemoult
发明人： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Benedicte Michal , Adrien Ott , Frederic Lemoult
CPC分类号： G08G5/025 , G08G5/0021
摘要： 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).
摘要翻译： 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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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
申请人： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Bénédicte Michal , Adrien Ott , Frédéric Lemoult
发明人： Didier Zadrozynski , Isabelle Lacaze , Jean-Pierre Demortier , Bénédicte Michal , Adrien Ott , Frédéric Lemoult
CPC分类号： G08G5/025 , G08G5/0021
摘要： 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.
摘要翻译： 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
申请人： Benedicte MICHAL , Fabien Pitard , Jean-Pierre Demortier , Christine Charbonnier , Isabelle Lacaze , Gael Marchand , Christine Le Duigou , Jerome Cayrou , Vincent Blondin , Frederic Lemoult
发明人： Benedicte MICHAL , Fabien Pitard , Jean-Pierre Demortier , Christine Charbonnier , Isabelle Lacaze , Gael Marchand , Christine Le Duigou , Jerome Cayrou , Vincent Blondin , Frederic Lemoult
CPC分类号： G08G5/065 , G08G5/0021 , G08G5/0065
摘要： 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.
摘要翻译： 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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4.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
申请人： Benedicte Michal , Fabien Pitard , Jean-Pierre Demortier , Christine Charbonnier , Isabelle Lacaze , Gael Marchand , Christine Le Duigou , Jerome Cayrou , Vincent Blondin , Frederic Lemoult
发明人： Benedicte Michal , Fabien Pitard , Jean-Pierre Demortier , Christine Charbonnier , Isabelle Lacaze , Gael Marchand , Christine Le Duigou , Jerome Cayrou , Vincent Blondin , Frederic Lemoult
IPC分类号： G06F19/00
CPC分类号： G08G5/065 , G08G5/0021 , G08G5/0065
摘要： 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.
摘要翻译： 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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5.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
申请人： Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
发明人： Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
CPC分类号： G05B23/0235 , G05D1/0083
摘要： 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.
摘要翻译： 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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6.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
申请人： Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
发明人： Frederic Lemoult , Jean-Pierre Demortier , Fabien Pitard , Damien Betouret , Frederic Marani , Isabelle Lacaze , Jean-Louis De Menorval , Gael Marchand , Adrien Ott , Maxime Wachenheim
IPC分类号： G06F19/00
CPC分类号： G05B23/0235 , G05D1/0083
摘要： 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.
摘要翻译： 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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7.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
IPC分类号： G01C23/00
CPC分类号： G05D1/0676
摘要： 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.
摘要翻译： 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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8.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
IPC分类号： G06F19/00
CPC分类号： G05D1/0676
摘要： 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.
摘要翻译： 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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9.发明授权公开(公告)号：US07761193B2
公开(公告)日：2010-07-20
申请号：US11128299
申请日：2005-05-13
申请人： Franck Artini , Jean-Pierre Demortier , Christophe Bouchet , Jacques Espinasse , Edward Strongman
发明人： Franck Artini , Jean-Pierre Demortier , Christophe Bouchet , Jacques Espinasse , Edward Strongman
IPC分类号： G01C23/00 , G05D1/00 , G05D3/00 , G06F7/00 , G06F17/00 , G05D1/08 , G05D1/06 , G01C5/00 , G01C21/00 , G06F19/00 , G06G7/70 , G08B21/00 , G08B23/00
CPC分类号： G05D1/0646 , G01C5/005
摘要： Method and device for ensuring the safety of a low-altitude flight of an aircraft.A device (1) for ensuring the safety of a low-altitude flight comprises information sources (5) able to determine current flight conditions, a monitoring unit (6) for realizing, with the aid of said current flight conditions, a function for global and autonomous monitoring of said low-altitude flight of the aircraft, making it possible to preserve the integrity of said aircraft during said flight, and means (13) for presenting the results of the monitoring function realized by said monitoring unit (6) to an operator.
摘要翻译： 确保飞机低空飞行安全的方法和装置。 一种用于确保低空飞行的安全性的装置（1）包括能够确定当前飞行情况的信息源（5），用于在所述当前飞行条件的帮助下实现全局的功能的监视单元（6） 以及对所述飞机的所述低空飞行进行自主监视，使得能够在所述飞行期间保持所述飞行器的完整性;以及用于将由所述监视单元（6）实现的监视功能的结果呈现给 操作员。
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10.发明申请公开(公告)号：US20070124034A1
公开(公告)日：2007-05-31
申请号：US11563743
申请日：2006-11-28
申请人： Fabien Pitard , Jean-Pierre Demortier , Serge Laporte , Serge Boyer , Bernard Deret , Laurent Fonteneau
发明人： Fabien Pitard , Jean-Pierre Demortier , Serge Laporte , Serge Boyer , Bernard Deret , Laurent Fonteneau
IPC分类号： G06F19/00
CPC分类号： G05D1/0083
摘要： A method for checking takeoff or landing parameters of an aircraft comprises a step (E101) of determining takeoff or landing parameters on the basis of a series of input conditions. It additionally comprises the following steps: calculation (E103) of regulatory data on the basis of determined takeoff or landing parameters; and comparison (E104) of the calculated regulatory data with predefined threshold values, with a view to establishing whether the determined takeoff or landing parameters are valid or invalid. Use to ensure reliability of the determination of optimized takeoff or landing parameters.
摘要翻译： 用于检查飞行器起飞或着陆参数的方法包括基于一系列输入条件来确定起飞或着陆参数的步骤（E 101）。 它还包括以下步骤：根据确定的起飞或着陆参数来计算（E 103）监管数据; 以及计算的调节数据与预定阈值的比较（E 104），以便确定所确定的起飞或着陆参数是有效还是无效。 用于确定优化起飞或着陆参数的可靠性。
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