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1. 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。

2. 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。

3. 发明授权

US08983686B2 System aboard an aircraft 有权
标题翻译：系统在一架飞机上
公开(公告)号：US08983686B2
公开(公告)日：2015-03-17
申请号：US13109406
申请日：2011-05-17
申请人： Alexandre Broquet , Yannick Deleris , Raphael Andre , Fabien Pascal
发明人： Alexandre Broquet , Yannick Deleris , Raphael Andre , Fabien Pascal
IPC分类号： G05B9/03 , G05B23/02 , G01C23/00 , G08G5/00
CPC分类号： G05B9/03 , G01C23/00 , G01C23/005 , G05B23/0272 , G08G5/0021
摘要： The invention relates to a device aboard an aircraft comprising output means configured to restore information relating to the aircraft status from aircraft systems, the device including a module providing interface between said output means and said aircraft systems, said module being configured to synthesize information from aircraft systems depending on predetermined behavior rules and to transmit said information thus synthesized to said output means.
摘要翻译：本发明涉及一种飞机上的装置，包括输出装置，其配置成从飞行器系统恢复与飞行器状态相关的信息，该装置包括提供所述输出装置和所述飞行器系统之间的接口的模块，所述模块被配置为从飞机系统取决于预定行为规则，并将所合成的所述信息传送到所述输出装置。

4. 发明授权

US08374734B2 Method of controlling an aircraft, the method implementing a vote system 有权
标题翻译：控制飞机的方法，执行投票制的方法
公开(公告)号：US08374734B2
公开(公告)日：2013-02-12
申请号：US12686780
申请日：2010-01-13
申请人： Alexandre Broquet , Fabien Cases , Fabien Pascal
发明人： Alexandre Broquet , Fabien Cases , Fabien Pascal
IPC分类号： G01C23/00 , G05D1/00
CPC分类号： G01P13/025
摘要： In the method of controlling an aircraft, a device implements the steps consisting in determining a first global value on the basis of only some amongst first individual values calculated by respective applications, modifying at least one parameter to take account of how the determination step took place and determining a second global value on the basis of second individual values calculated by the respective applications and on the basis of the parameter(s).
摘要翻译：在控制飞行器的方法中，设备实施步骤包括仅基于由各个应用计算出的第一个别值中的一些来确定第一全局值，修改至少一个参数以考虑确定步骤如何发生以及基于由各个应用程序计算的第二个体值，并且基于参数来确定第二全局值。

5. 发明授权

US08751512B2 Method and device for managing information in an aircraft 有权
标题翻译：用于管理飞机信息的方法和装置
公开(公告)号：US08751512B2
公开(公告)日：2014-06-10
申请号：US12879775
申请日：2010-09-10
申请人： Yannick Deleris , Alexandre Broquet , Fabien Pascal
发明人： Yannick Deleris , Alexandre Broquet , Fabien Pascal
IPC分类号： G06F17/30
CPC分类号： G01C23/00 , G08G5/0021
摘要： A method and a device for managing information in an aircraft, including at least one device for outputting information for the crew and a plurality of equipment items adapted to transmit information items capable of being outputted on the output device. After a plurality of information items from the plurality of equipment items has been acquired and a context has been determined according to a predetermined model, the plurality of information items is filtered according to at least one rule, the at least one rule being associated with the context for selection of at least one information item. At least one selected information item is then outputted on the output device.
摘要翻译：一种用于管理飞行器中的信息的方法和装置，包括至少一个用于输出船员信息的设备和适于发送能够在输出设备上输出的信息项的多个设备项目。在已经获取了来自多个设备项目的多个信息项目并且已经根据预定模型确定了上下文之后，根据至少一个规则对多个信息项目进行过滤，该至少一个规则与用于选择至少一个信息项的上下文。然后在输出设备上输出至少一个选择的信息项。

6. 发明授权

US08638239B2 System and method for managing audio warning messages in an aircraft 有权
标题翻译：用于管理飞机中的音频警告消息的系统和方法
公开(公告)号：US08638239B2
公开(公告)日：2014-01-28
申请号：US13014297
申请日：2011-01-26
申请人： Fabien Cases , Michel Colin , Nicolas Caule , Alexandre Broquet , Fabien Pascal
发明人： Fabien Cases , Michel Colin , Nicolas Caule , Alexandre Broquet , Fabien Pascal
IPC分类号： G08B21/00 , G08B23/00 , G01C21/00 , G01C5/00 , G05D1/00 , G06F7/70 , G06F19/00
CPC分类号： G08B23/00 , G08G5/0021 , G08G5/0078 , G08G5/0086
摘要： The present invention relates to a system (1) and an associated method for managing audio warning messages in an aircraft.The system (1) comprises a plurality of monitoring systems (10, 20) capable of detecting the establishment of at least one warning condition (CA), and comprises a central broadcasting module (40), to which each of the monitoring systems is connected and which is capable of broadcasting an audio message (SIG) corresponding to a detected warning condition.In particular, in this system (1), the said central broadcasting module (40) comprises means (402, 420) for determining at least one priority warning condition among the warning conditions detected by the monitoring systems, and means (410, 430) for generating at least one audio message (SIG) corresponding to the at least one determined priority warning condition, in order to broadcast it.
摘要翻译：本发明涉及一种用于在飞行器中管理音频警告消息的系统（1）和相关联的方法。系统（1）包括能够检测建立至少一个警告状况（CA）的多个监视系统（10,20），并且包括中央广播模块（40），每个监控系统连接到该中央广播模块并且能够广播与检测到的警告条件相对应的音频消息（SIG）。特别地，在该系统（1）中，所述中央广播模块（40）包括用于确定由所述监视系统检测到的所述警告状况中的至少一个优先警告状况的装置（402,420），以及装置（410,430）用于产生与所述至少一个确定的优先警告条件相对应的至少一个音频消息（SIG），以便将其广播。

7. 发明申请

US20110196881A1 METHOD AND DEVICE FOR MANAGING INFORMATION IN AN AIRCRAFT 有权
标题翻译：用于管理飞机信息的方法和装置
公开(公告)号：US20110196881A1
公开(公告)日：2011-08-11
申请号：US12879775
申请日：2010-09-10
申请人： Yannick Deleris , Alexandre Broquet , Fabien Pascal
发明人： Yannick Deleris , Alexandre Broquet , Fabien Pascal
IPC分类号： G06F17/30
CPC分类号： G01C23/00 , G08G5/0021
摘要： The object of the invention is in particular a method and a device for managing information in an aircraft, comprising at least one device for restituting information for the crew and a plurality of equipment items adapted to transmit information items capable of being restituted on the restitution device. After a plurality of information items from the said plurality of equipment items has been acquired and a context has been determined (300) according to a predetermined model, the said plurality of information items is filtered (320) according to at least one rule, the said at least one rule being associated with the said context for selection of at least one information item. At least one selected information item is then restituted on the restitution device.
摘要翻译：本发明的目的特别是一种用于管理飞行器中的信息的方法和设备，包括至少一个用于重新组装用于船员的信息的设备和适于发送能够恢复在恢复设备上的信息项的多个设备项目。在已经获取了来自所述多个设备项目的多个信息项目并且已经根据预定模型确定了上下文（300）之后，根据至少一个规则对所述多个信息项目进行过滤（320），所述至少一个规则与所述上下文相关联，用于选择至少一个信息项。然后至少一个所选择的信息项在恢复装置上恢复。

8. 发明申请

US20110193724A1 SYSTEM AND METHOD FOR MANAGING AUDIO WARNING MESSAGES IN AN AIRCRAFT 有权
标题翻译：用于管理飞机中的音频警告信息的系统和方法
公开(公告)号：US20110193724A1
公开(公告)日：2011-08-11
申请号：US13014297
申请日：2011-01-26
申请人： Fabien Cases , Michel Colin , Nicolas Caule , Alexandre Broquet , Fabien Pascal
发明人： Fabien Cases , Michel Colin , Nicolas Caule , Alexandre Broquet , Fabien Pascal
IPC分类号： G08B21/00
CPC分类号： G08B23/00 , G08G5/0021 , G08G5/0078 , G08G5/0086
摘要： The present invention relates to a system (1) and an associated method for managing audio warning messages in an aircraft.The system (1) comprises a plurality of monitoring systems (10, 20) capable of detecting the establishment of at least one warning condition (CA), and comprises a central broadcasting module (40), to which each of the monitoring systems is connected and which is capable of broadcasting an audio message (SIG) corresponding to a detected warning condition.In particular, in this system (1), the said central broadcasting module (40) comprises means (402, 420) for determining at least one priority warning condition among the warning conditions detected by the monitoring systems, and means (410, 430) for generating at least one audio message (SIG) corresponding to the at least one determined priority warning condition, in order to broadcast it.
摘要翻译：本发明涉及一种用于在飞行器中管理音频警告消息的系统（1）和相关联的方法。系统（1）包括能够检测建立至少一个警告状况（CA）的多个监视系统（10,20），并且包括中央广播模块（40），每个监控系统连接到该中央广播模块并且能够广播与检测到的警告条件相对应的音频消息（SIG）。特别地，在该系统（1）中，所述中央广播模块（40）包括用于确定由所述监视系统检测到的所述警告状况中的至少一个优先警告状况的装置（402,420），以及装置（410,430）用于产生与所述至少一个确定的优先警告条件相对应的至少一个音频消息（SIG），以便将其广播。

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