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1. 发明授权

US08255174B2 Method and device for determining critical buffeting loads on a structure of an aircraft 有权
标题翻译：用于确定飞机结构上的关键缓冲载荷的方法和装置
公开(公告)号：US08255174B2
公开(公告)日：2012-08-28
申请号：US12789309
申请日：2010-05-27
申请人： Guillermo Jenaro Rabadan , Juliane Havas , Stéphane Soumillon , Carole Despre-Flachard
发明人： Guillermo Jenaro Rabadan , Juliane Havas , Stéphane Soumillon , Carole Despre-Flachard
IPC分类号： G01L1/00
CPC分类号： G01M9/06 , G01M9/04 , G01M9/08
摘要： A method and device for determining critical buffeting loads on a structure of an aircraft is disclosed. The device (1) comprises means (2, UC) implementing a semi-empirical method for determining the critical loads generated by some buffeting on the structure of the airplane.
摘要翻译：公开了一种用于确定飞机结构上的临界缓冲载荷的方法和装置。装置（1）包括实现半经验方法的装置（2，UC），用于确定由飞机结构上的一些缓冲产生的临界负载。

2. 发明申请

US20100312497A1 METHOD AND DEVICE FOR DETERMINING CRITICAL BUFFETING LOADS ON A STRUCTURE OF AN AIRCRAFT 有权
标题翻译：用于确定飞机结构关键保压载荷的方法和装置
公开(公告)号：US20100312497A1
公开(公告)日：2010-12-09
申请号：US12789309
申请日：2010-05-27
申请人： Guillermo Jenaro Rabadan , Juliane Havas , Stephane Soumillon , Carole Despre-Flachard
发明人： Guillermo Jenaro Rabadan , Juliane Havas , Stephane Soumillon , Carole Despre-Flachard
IPC分类号： G01L1/00 , G06F19/00
CPC分类号： G01M9/06 , G01M9/04 , G01M9/08
摘要： A method and device for determining critical buffeting loads on a structure of an aircraft is disclosed. The device (1) comprises means (2, UC) implementing a semi-empirical method for determining the critical loads generated by some buffeting on the structure of the airplane.
摘要翻译：公开了一种用于确定飞机结构上的临界缓冲载荷的方法和装置。装置（1）包括实现半经验方法的装置（2，UC），用于确定由飞机结构上的一些缓冲产生的临界负载。

3. 发明申请

US20110299062A1 DEVICE AND METHOD FOR DETECTING AND MEASURING WIND FOR AN AIRCRAFT 审中-公开
标题翻译：用于检测和测量飞机的风力的装置和方法
公开(公告)号：US20110299062A1
公开(公告)日：2011-12-08
申请号：US13129054
申请日：2009-11-02
申请人： Guillermo Jenaro Rabadan , Stephane Puig
发明人： Guillermo Jenaro Rabadan , Stephane Puig
IPC分类号： G01P3/36
CPC分类号： G01S17/95 , G01S17/58 , Y02A90/19
摘要： The invention relates to a device for detecting and measuring wind at the front of an aircraft, said device comprising a lidar for the cyclic measurement of wind speeds at least a couple of measuring points located at the same distance, so-called measuring distance, from the nose of the aircraft. The invention is characterised in that it is suitable for measuring wind speeds, at each cycle, by means of the lidar, at a plurality of couples of measuring points (1-12) located at different measuring distances (xp-2, xp-1, xp), the difference between the largest measuring distance and the smallest measuring distance being more than 100 metres. The invention also relates to a method for detecting and measuring wind, which can be implemented by the device according to the invention.
摘要翻译：本发明涉及一种用于检测和测量飞行器前方的风的装置，所述装置包括用于循环测量风速的激光雷达，所述激光雷达至少有一对相同距离的测量点，即所谓的测量距离飞机的鼻子。本发明的特征在于，它适用于通过位于不同测量距离（xp-2，xp-1）处的多个测量点（1-12），通过激光雷达在每个周期测量风速，xp），最大测量距离和最小测量距离之间的差距大于100米。本发明还涉及一种用于检测和测量风的方法，其可以由根据本发明的装置实现。

4. 发明申请

US20110172853A1 METHOD AND DEVICE FOR ATTENUATING THE EFFECTS OF TURBULENCE ON AN AIRCRAFT 有权
标题翻译：用于减轻飞机对涡轮机的影响的方法和装置
公开(公告)号：US20110172853A1
公开(公告)日：2011-07-14
申请号：US13119019
申请日：2009-10-30
申请人： Guillermo Jenaro Rabadan , Stephane Puig
发明人： Guillermo Jenaro Rabadan , Stephane Puig
IPC分类号： G05D1/00
CPC分类号： G05D1/0615
摘要： A method for attenuating effects of turbulence on an aircraft, and a device to implement the method, the method including: using at least one signal on a wind profile signal, along an excitation direction, representing, at a given moment in an aircraft referential, a component along the excitation direction of the wind speed at a front of the aircraft according to a distance along a longitudinal direction of the aircraft; carrying out a frequency determination, in which the wind profile signal is processed to determine a frequential content; and selecting a control strategy to be adopted according to the previously determined frequential content, the strategy enabling at least one applicable control law to be identified.
摘要翻译：一种用于衰减湍流对飞行器的影响的方法以及实现该方法的装置，所述方法包括：在沿着激励方向的风廓线信号上使用至少一个信号，在飞行器参考的给定时刻，根据沿着飞行器的纵向方向的距离沿飞行器前方的风速的激励方向的分量; 执行频率确定，其中处理风廓线信号以确定频率内容; 以及根据先前确定的频率内容选择要采用的控制策略，所述策略使得能够识别至少一个适用的控制规则。

5. 发明授权

US08649919B2 Method and device for attenuating the effects of turbulence on an aircraft 有权
标题翻译：减轻飞机上湍流影响的方法和装置
公开(公告)号：US08649919B2
公开(公告)日：2014-02-11
申请号：US13119019
申请日：2009-10-30
申请人： Guillermo Jenaro Rabadan , Stephane Puig
发明人： Guillermo Jenaro Rabadan , Stephane Puig
IPC分类号： G01C23/00 , G05D1/00 , G05D1/10 , B64C19/00
CPC分类号： G05D1/0615
摘要： A method for attenuating effects of turbulence on an aircraft, and a device to implement the method, the method including: using at least one signal on a wind profile signal, along an excitation direction, representing, at a given moment in an aircraft referential, a component along the excitation direction of the wind speed at a front of the aircraft according to a distance along a longitudinal direction of the aircraft; carrying out a frequency determination, in which the wind profile signal is processed to determine a frequential content; and selecting a control strategy to be adopted according to the previously determined frequential content, the strategy enabling at least one applicable control law to be identified.
摘要翻译：一种用于衰减湍流对飞行器的影响的方法以及实现该方法的装置，所述方法包括：在沿着激励方向的风廓线信号上使用至少一个信号，在飞行器参考的给定时刻，根据沿着飞行器的纵向方向的距离沿飞行器前方的风速的激励方向的分量; 执行频率确定，其中处理风廓线信号以确定频率内容; 以及根据先前确定的频率内容选择要采用的控制策略，所述策略使得能够识别至少一个适用的控制规则。

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