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1. 发明授权

US09196167B2 Process and device for managing the activating of a warning message in an aircraft 有权
标题翻译：用于管理在飞行器中激活警告消息的过程和设备
公开(公告)号：US09196167B2
公开(公告)日：2015-11-24
申请号：US12145793
申请日：2008-06-25
申请人： Pierre Campagne , Boris Sorbier , Baptiste Maylin
发明人： Pierre Campagne , Boris Sorbier , Baptiste Maylin
IPC分类号： G08B21/00 , G08C23/00 , G08G5/00
CPC分类号： G08G5/0091 , G08G5/0021 , G08G5/0078 , G08G5/0086
摘要： A process for managing the activating of emission of a given warning message in an aircraft comprises transmission, from a monitoring system to an authorization-issuing system, of an emission authorization request. The request has a priority attribute known as request priority attribute. The process also includes transmission, from the authorization-issuing system to the monitoring system, of an emission authorization. The transmission of the emission authorization is effected if the request priority attribute is higher than a current priority threshold. In addition, the process includes activation of emission of the given warning message. The activation may be effected if an alert condition associated with the given warning message is detected and if a priority attribute associated with the alert condition is higher than or equal to the request priority attribute.
摘要翻译：用于管理飞行器中的给定警告消息的发射的激活的过程包括从监视系统向授权发布系统发送排放授权请求。请求具有被称为请求优先级属性的优先级属性。该过程还包括从授权发布系统向监控系统传输排放授权。如果请求优先级属性高于当前优先权阈值，则发送排放授权是有效的。此外，该过程包括激活给定警告消息的发射。如果检测到与给定警告消息相关联的警报条件以及与警报状况相关联的优先级属性是否高于或等于请求优先级属性，则可以实现激活。

2. 发明申请

US20090015437A1 PROCESS AND DEVICE FOR MANAGING THE ACTIVATING OF A WARNING MESSAGE IN AN AIRCRAFT 有权
标题翻译：用于管理飞机中警告信息的活动的过程和设备
公开(公告)号：US20090015437A1
公开(公告)日：2009-01-15
申请号：US12145793
申请日：2008-06-25
申请人： Pierre Campagne , Boris Sorbier , Baptiste Maylin
发明人： Pierre Campagne , Boris Sorbier , Baptiste Maylin
IPC分类号： G08B21/00
CPC分类号： G08G5/0091 , G08G5/0021 , G08G5/0078 , G08G5/0086
摘要： The invention relates to a process for managing the activating of emission of a given warning message in an aircraft, characterized in that it comprises the following successive steps: transmission (E2), from an alert system (10) to an authorization-issuing system (20), of an emission authorization request, the said request having a priority attribute known as request priority, transmission (E3), from the said authorization-issuing system (20) to the said alert system (10), of an emission authorization, the transmission of the said emission authorization being effected if the said request priority attribute is higher than a current priority threshold, activation of emission of the given warning message, the said activation being effected if an alert condition associated with the given warning message is detected and if a priority attribute associated with the said alert condition is higher than or equal to the said request priority attribute.
摘要翻译：本发明涉及一种用于管理飞行器中给定警告消息的发射的激活的过程，其特征在于，其包括以下连续步骤：从警报系统（10）传输（E2）到授权发布系统（ 20）发射授权请求，所述请求具有被称为请求优先级的优先级属性，从所述授权发行系统（20）向所述警报系统（10）发送排放授权的传输（E3）如果所述请求优先级属性高于当前优先级阈值，激活所述给定警告消息的发射，则如果检测到与给定警告消息相关联的警报条件，则所述激活被实现; 如果与所述警报条件相关联的优先级属性高于或等于所述请求优先级属性。

3. 发明授权

US08223039B2 Method and a device for detecting a thrust dissymmetry of an aircraft during landing 有权
标题翻译：方法和用于在着陆期间检测飞行器的推力不对称性的装置
公开(公告)号：US08223039B2
公开(公告)日：2012-07-17
申请号：US12786180
申请日：2010-05-24
申请人： Pierre Campagne , Alexandre Broquet , Nicolas Marty
发明人： Pierre Campagne , Alexandre Broquet , Nicolas Marty
IPC分类号： G01C21/00 , G01C23/00
CPC分类号： B64D45/00 , B64D31/04
摘要： A method and a device for detecting a thrust dissymmetry of an aircraft during a landing are disclosed. The detection device (6) comprises means (7) for detecting, upon a landing, that at least one of the engine control levers occupies an intermediary position comprised between a position threshold and a maximum speed position, as well as at least another engine control lever occupies an idling position, and means (9, 13) for triggering a warning when a landing condition is validated and at least one of the control levers occupies said intermediary position, at least another control lever occupying said idling position.
摘要翻译：公开了一种用于在着陆期间检测飞行器的推力不对称性的方法和装置。检测装置（6）包括用于在着陆时检测发动机控制杆中的至少一个占据位置阈值和最大速度位置之间的中间位置的装置（7），以及至少另一个发动机控制杠杆占据怠速位置，以及用于当着陆条件被验证并且至少一个控制杆占据所述中间位置时触发警告的装置（9,13），至少另一控制杆占据所述怠速位置。

4. 发明申请

US20100302074A1 METHOD AND A DEVICE FOR DETECTING A THRUST DISSYMMETRY OF AN AIRCRAFT DURING LANDING 有权
标题翻译：方法和装置，用于检测在陆地期间飞机的扭转对称性
公开(公告)号：US20100302074A1
公开(公告)日：2010-12-02
申请号：US12786180
申请日：2010-05-24
申请人： Pierre Campagne , Alexandre Broquet , Nicolas Marty
发明人： Pierre Campagne , Alexandre Broquet , Nicolas Marty
IPC分类号： G01C21/00
CPC分类号： B64D45/00 , B64D31/04
摘要： A method and a device for detecting a thrust dissymmetry of an aircraft during a landing are disclosed. The detection device (6) comprises means (7) for detecting, upon a landing, that at least one of the engine control levers occupies an intermediary position comprised between a position threshold and a maximum speed position, as well as at least another engine control lever occupies an idling position, and means (9, 13) for triggering a warning when a landing condition is validated and at least one of the control levers occupies said intermediary position, at least another control lever occupying said idling position.
摘要翻译：公开了一种用于在着陆期间检测飞行器的推力不对称性的方法和装置。检测装置（6）包括用于在着陆时检测发动机控制杆中的至少一个占据位置阈值和最大速度位置之间的中间位置的装置（7），以及至少另一个发动机控制杠杆占据怠速位置，以及用于当着陆条件被验证并且至少一个控制杆占据所述中间位置时触发警告的装置（9,13），至少另一控制杆占据所述怠速位置。

5. 发明申请

US20100045486A1 METHOD AND DEVICE FOR AUDIBLE WARNING WHEN AN AIRCRAFT AUTOPILOT IS DEACTIVATED 有权
标题翻译：当飞机自动驾驶仪被停用时，可以进行可信警报的方法和装置
公开(公告)号：US20100045486A1
公开(公告)日：2010-02-25
申请号：US11722433
申请日：2005-12-19
申请人： Fabien Daveze , Christel Ravier , Pierre Campagne
发明人： Fabien Daveze , Christel Ravier , Pierre Campagne
IPC分类号： G08B23/00
CPC分类号： G05D1/0061
摘要： The invention relates to a method for producing an audible warning when an aircraft autopilot (2) is deactivated consisting: a) in transmitting a first sound in the aircraft cockpit during a time ranging from a first predetermined value (d1) and a second predetermined value (d2) and b) in transmitting a second sound in the aircraft cockpit. Said invention also relates to an audible warning device (1) comprising first means (10) for monitoring the deactivation of the aircraft autopilot (2) and means (12) for emitting an audible warning in the cockpit, wherein said second means is constructed in such a way that it activates the first sound emission whose length ranges from the first predetermined value (d1) and a second predetermined value (d2) and a second sound when the first means detects the deactivation of the autopilot.
摘要翻译：本发明涉及一种当航空器自动驾驶仪（2）停用时产生听觉警告的方法，该方法包括：a）在从第一预定值（d1）和第二预定值（d2）和b）在飞行器驾驶舱中发送第二声音。所述发明还涉及一种可听警报装置（1），包括用于监视飞行器自动驾驶仪（2）的停用的第一装置（10）和用于在驾驶舱内发出可听见警告的装置（12），其中所述第二装置这样一种方式，当第一装置检测到自动驾驶仪的停用时，它激活其长度范围从第一预定值（d1）和第二预定值（d2）起的第一声发射和第二声音。

6. 发明申请

US20090015438A1 PROCESS AND SYSTEM FOR MANAGING AN INTERRUPTION OF A BROADCAST OF A SONOROUS MESSAGE IN AN AIRCRAFT 有权
标题翻译：用于管理航空器中声音消息的广播的中断的过程和系统
公开(公告)号：US20090015438A1
公开(公告)日：2009-01-15
申请号：US12145849
申请日：2008-06-25
申请人： Boris SORBIER , Pierre CAMPAGNE , Baptiste MAYLIN
发明人： Boris SORBIER , Pierre CAMPAGNE , Baptiste MAYLIN
IPC分类号： G08B23/00
CPC分类号： G08G5/0078 , G08G5/0021 , G08G5/0086
摘要： The invention relates to a method for managing an interruption of emission, in an aircraft, of an acoustic message comprising an information item about a state of part of the said aircraft and/or about its environment, characterized in that, the acoustic message being structured into one or more successive acoustic fragments each representative of the said information item, the said method comprises the steps: of delaying (E3), starting from a given moment, the execution of a decision to interrupt the emission of the acoustic message until the end of emission of an acoustic fragment that is in the course of emission at the said given moment, and of executing (E4) the said interruption decision.
摘要翻译：本发明涉及一种用于管理飞机中的发射中断的方法，该声音消息包括关于所述飞行器的一部分的状态和/或其环境的信息项，其特征在于，声音消息被构造分成代表所述信息项的一个或多个连续的声音片段，所述方法包括以下步骤：从给定时刻开始延迟（E3）执行决定以中断声音消息的发射直到结束在所述给定时刻处于发射过程中的声音片段的发射，以及执行（E4）所述中断判定。

7. 发明授权

US07990285B2 Method and device for audible warning when an aircraft autopilot is deactivated 有权
标题翻译：航空器自动驾驶仪停用时的声音报警方法和设备
公开(公告)号：US07990285B2
公开(公告)日：2011-08-02
申请号：US11722433
申请日：2005-12-19
申请人： Fabien Daveze , Christel Ravier , Pierre Campagne
发明人： Fabien Daveze , Christel Ravier , Pierre Campagne
IPC分类号： G08B23/00
CPC分类号： G05D1/0061
摘要： The invention relates to a method for producing an audible warning when an aircraft autopilot is deactivated. The method includes a) transmitting a first sound in the aircraft cockpit during a time ranging from a first predetermined value and a second predetermined value and b) transmitting a second sound in the aircraft cockpit. The invention also relates to an audible warning device having a monitoring unit for monitoring the deactivation of the aircraft autopilot and an activation unit for emitting an audible warning in the cockpit, where the activation unit is constructed such that it activates the first sound emission whose length ranges from the first predetermined value and a second predetermined value and a second sound when the monitoring unit detects the deactivation of the autopilot.
摘要翻译：本发明涉及当航空器自动驾驶仪停用时产生可听警告的方法。该方法包括：a）在从第一预定值和第二预定值开始的时间内，在飞行器驾驶舱中发送第一声音，以及b）在飞机驾驶舱中传送第二声音。本发明还涉及一种具有用于监视飞行器自动驾驶仪的停用的监视单元和用于在驾驶舱中发出可听见警告的激活单元的声音报警装置，其中启动单元被构造成使得其激活第一声发射，其长度范围从第一预定值和第二预定值和第二声音，当监视单元检测到自动驾驶仪的停用时。

8. 发明授权

US08712604B2 Method and device for accessing the documentation of an aircraft according to alarms generated therein 有权
标题翻译：根据其中生成的报警来访问飞机文件的方法和装置
公开(公告)号：US08712604B2
公开(公告)日：2014-04-29
申请号：US12879639
申请日：2010-09-10
申请人： Pierre Campagne , Jerome Treanton , Xavier Geay , Laval Louis Chan Kam Fai , Christophe Jotz , Thierry Paya-Arnaud , Jerome Pouyfaucon
发明人： Pierre Campagne , Jerome Treanton , Xavier Geay , Laval Louis Chan Kam Fai , Christophe Jotz , Thierry Paya-Arnaud , Jerome Pouyfaucon
IPC分类号： G06F17/30 , G06F11/32 , G05B23/02
CPC分类号： G06F11/321 , G05B23/027
摘要： A method and a device for accessing the documentation of an aircraft according to alarms generated therein, where the documentation includes at least one document that is modifiable independently of the manufacturer of the aircraft. After having received at least one indication relating to at least one alarm generated by the avionics of the aircraft, at least one datum relating to the at least one alarm, including a link to at least one element of the documentation, is extracted and displayed.
摘要翻译：根据其中生成的报警来访问飞机文件的方法和装置，其中文件包括至少一个独立于飞机制造商可修改的文件。在已经收到至少一个关于由飞行器的航空电子设备产生的至少一个警报的指示之后，提取并显示与至少一个警报有关的至少一个数据，包括到文档的至少一个元件的链接。

9. 发明授权

US07994941B2 Process and system for managing an interruption of a broadcast of a sonorous message in an aircraft 有权
标题翻译：用于管理航空器中嘈杂消息的广播的中断的过程和系统
公开(公告)号：US07994941B2
公开(公告)日：2011-08-09
申请号：US12145849
申请日：2008-06-25
申请人： Boris Sorbier , Pierre Campagne , Baptiste Maylin
发明人： Boris Sorbier , Pierre Campagne , Baptiste Maylin
IPC分类号： G08B23/00
CPC分类号： G08G5/0078 , G08G5/0021 , G08G5/0086
摘要： A method for managing an interruption of emission, in an aircraft, of an acoustic message including an information item about a state of part of the said aircraft and/or about its environment, wherein the acoustic message is structured into one or more successive acoustic fragments each representative of the information item, the method includes the steps of: delaying, starting from a given moment, the execution of a decision to interrupt the emission of the acoustic message until the end of emission of an acoustic fragment that is in the course of emission at the given moment; and executing the interruption decision.
摘要翻译：一种用于管理航空器中的发射中断的方法，所述声音消息包括关于所述飞行器的一部分的状态和/或其环境的信息项，其中所述声学消息被构造成一个或多个连续的声音片段信息项的每个代表，该方法包括以下步骤：从给定时刻起，延迟执行决定以中断声音消息的发射，直到声音片段的发射结束在给定时刻的排放; 并执行中断决定。

10. 发明申请

US20110160936A1 METHOD AND DEVICE FOR ACCESSING THE DOCUMENTATION OF AN AIRCRAFT ACCORDING TO ALARMS GENERATED THEREIN 有权
标题翻译：用于访问根据其生成的报警的飞机的文档的方法和装置
公开(公告)号：US20110160936A1
公开(公告)日：2011-06-30
申请号：US12879639
申请日：2010-09-10
申请人： Pierre CAMPAGNE , Jerome Treanton , Xavier Geay , Laval Louis Chan Kam Fai , Christophe Jotz , Thierry Paya-Arnaud , Jerome Pouyfaucon
发明人： Pierre CAMPAGNE , Jerome Treanton , Xavier Geay , Laval Louis Chan Kam Fai , Christophe Jotz , Thierry Paya-Arnaud , Jerome Pouyfaucon
IPC分类号： G08B23/00 , G06F17/30
CPC分类号： G06F11/321 , G05B23/027
摘要： The invention in particular has as an object a method and a device for accessing the documentation of an aircraft according to alarms generated therein, the documentation comprising at least one document modifiable independently of the manufacturer of the aircraft. After having received (305) at least one indication relating to at least one alarm generated by the avionics of the said aircraft, at least one datum relating to the said at least one alarm, comprising a link to at least one element of the said documentation, is extracted (315) and displayed (325).
摘要翻译：本发明特别地具有用于根据其中产生的报警来访问飞行器的文件的方法和装置，所述文件包括可独立于飞行器的制造商修改的至少一个文件。在接收到（305）至少一个与所述飞行器的航空电子设备产生的警报有关的指示之后，至少一个与所述至少一个警报器有关的数据，包括到所述文件的至少一个元件的链接（315）并显示（325）。

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