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1. 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。

2. 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。

3. 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。

4. 发明授权

US08190306B2 Method and device for reducing on an aircraft the effects of a vertical turbulence 有权
标题翻译：降低飞机垂直湍流影响的方法和装置
公开(公告)号：US08190306B2
公开(公告)日：2012-05-29
申请号：US12368177
申请日：2009-02-09
申请人： Stephane Puig , Romeo Byzery
发明人： Stephane Puig , Romeo Byzery
IPC分类号： G05D1/00
CPC分类号： G05D1/0623
摘要： Disclosed is a method and device for attenuating vertical turbulence on an aircraft. The method and device involve calculating, by a calculating unit, based on a determined vertical wind component a first control order to control movement of at least one first controllable movable member that acts on aircraft lift, and a second control order that controls movement of at least one second controllable movable member to act on aircraft pitch. A verification unit verifies that activation conditions evidencing severe turbulence are in effect, the vertical turbulence being attenuated.
摘要翻译：公开了一种用于衰减飞机上的垂直湍流的方法和装置。所述方法和装置包括通过计算单元基于所确定的垂直风力分量来计算第一控制顺序，以控制作用在飞机升降台上的至少一个第一可控制的可移动构件的运动，以及控制运动的第二控制顺序至少一秒钟的可控制可动构件作用于飞机俯仰。验证单元验证证明严重湍流的激活条件是有效的，垂直湍流被衰减。

5. 发明申请

US20110071710A1 METHOD AND DEVICE FOR DETECTING AN ERRONEOUS SPEED GENERATED BY AN AIR DATA INERTIAL REFERENCE SYSTEM 有权
标题翻译：用于检测空气数据惯性参考系统产生的错误速度的方法和装置
公开(公告)号：US20110071710A1
公开(公告)日：2011-03-24
申请号：US12887783
申请日：2010-09-22
申请人： Stephane Puig , Pierre Ezerzere
发明人： Stephane Puig , Pierre Ezerzere
IPC分类号： G06F19/00
CPC分类号： G01P21/025 , G01C21/16 , G01P5/16
摘要： Method and device for detecting an erroneous speed generated by an air data inertial reference system. The device (1) comprises means (2) for detecting an erroneous speed provided by an air data and inertial data system (3) and means for generating a substitution speed.
摘要翻译：用于检测由空气数据惯性参考系统产生的错误速度的方法和装置。装置（1）包括用于检测由空气数据和惯性数据系统（3）提供的错误速度的装置（2）和用于产生替代速度的装置。

6. 发明申请

US20110022251A1 METHOD AND DEVICE FOR AIDING THE LATERAL CONTROL OF AN AIRCRAFT DURING AN APPROACH PHASE 有权
标题翻译：用于在方法阶段中对飞机进行侧向控制的方法和装置
公开(公告)号：US20110022251A1
公开(公告)日：2011-01-27
申请号：US12842563
申请日：2010-07-23
申请人： Stephane Puig , Jerome Gauvain
发明人： Stephane Puig , Jerome Gauvain
IPC分类号： G05D1/00
CPC分类号： G05D1/0083 , G05D1/0676
摘要： An assistance method and device for lateral control of an aircraft upon an approach phase is disclosed. The device (1) comprises means (25) to predict in flight a risk of runway lateral excursion and means (20) to advise the pilot of the aircraft about the existence of such a risk.
摘要翻译：公开了一种在接近阶段横向控制飞行器的辅助方法和装置。装置（1）包括用于在飞行中预测跑道横向偏移的风险的装置（25）和用于向飞机的飞行员通知有关这种风险的存在的装置（20）。

7. 发明授权

US08219266B2 Method and device for reducing on an aircraft lateral effects of a turbulence 有权
标题翻译：减少飞机横向湍流影响的方法和装置
公开(公告)号：US08219266B2
公开(公告)日：2012-07-10
申请号：US12368139
申请日：2009-02-09
申请人： Stephane Puig , Romeo Byzery
发明人： Stephane Puig , Romeo Byzery
IPC分类号： B64C13/16 , G05D1/08
CPC分类号： B64C13/18 , G05D1/0623 , G05D1/0816
摘要： Disclosed is a method and device for attenuating lateral effects on an aircraft due to turbulence encountered by the aircraft during flight. The lateral effects are attenuated by applying a roll control order to control a first controllable movable member that acts on aircraft roll and minimizes aircraft roll-wise disturbances due to wind, and a yaw control order that controls a second controllable movable member to act on aircraft yaw. The roll and yaw control orders are calculated based on a sideslip value of the aircraft, while the yaw control order is calculated as a function of the roll control order to compensate for aircraft lateral effects due to turbulence, as well as lateral effects due to application of the roll control order to the first movable member.
摘要翻译：公开了一种用于减少由于飞机在飞行中遇到的湍流而对飞行器的横向影响的方法和装置。通过施加滚动控制命令来控制作用在飞行器辊上的第一可控制的可移动构件并使由于风引起的飞机滚动扰动最小化以及控制第二可控制的可移动构件作用于飞行器的偏航控制命令来减弱侧向效应偏航。基于飞行器的侧滑值来计算滚转和偏航控制次序，而根据滚动控制顺序计算偏航控制顺序以补偿由于湍流引起的飞机横向影响，以及由于应用引起的横向影响的滚动控制顺序发送到第一可移动部件。

8. 发明申请

US20110046823A1 PROCESS AND DEVICE FOR OPTIMISING THE PERFORMANCE OF AN AIRCRAFT IN THE PRESENCE OF A LATERAL DISSYMETRY 有权
标题翻译：用于优化航空器在横向差速器存在下的性能的方法和装置
公开(公告)号：US20110046823A1
公开(公告)日：2011-02-24
申请号：US12780669
申请日：2010-05-14
申请人： Pierre Ezerzere , Stephane Puig , Fabien Calderara
发明人： Pierre Ezerzere , Stephane Puig , Fabien Calderara
IPC分类号： G05D1/00 , G06G7/72
CPC分类号： G05D1/0816
摘要： A process and device for optimising the performance of an aircraft in the presence of a lateral dissymmetry is disclosed. The device (1) includes means (2, 3, 4, 5, 7, 9) for controlling, during a lateral dissymmetry, at least one rudder such as to generate an optimum sideslip for reducing the drag of the aircraft.
摘要翻译：公开了一种用于在存在横向不对称性的情况下优化飞行器的性能的过程和装置。装置（1）包括用于在横向不对称期间控制至少一个方向舵的装置（2,3,4,5,7,9），以产生用于减小飞行器的阻力的最佳侧滑。

9. 发明申请

US20100292872A1 METHOD AND DEVICE FOR AUTOMATICALLY DETECTING A LATERAL DISSYMETRY OF AN AIRCRAFT 有权
标题翻译：用于自动检测飞机横向离差的方法和装置
公开(公告)号：US20100292872A1
公开(公告)日：2010-11-18
申请号：US12780577
申请日：2010-05-14
申请人： Pierre Ezerzere , Stephane Puig
发明人： Pierre Ezerzere , Stephane Puig
IPC分类号： G06F7/00 , G08B23/00
CPC分类号： G01C5/005 , G05D1/0066 , G05D1/0816
摘要： The device (1) includes means (2, 3, 4) for observing the overall conditions of the aircraft and for determining whether the lateral behaviour thereof is normal.
摘要翻译：装置（1）包括用于观察飞行器的整体状况并确定其横向行为是否正常的装置（2,3,4）。

10. 发明授权

US07761197B2 Method and device for detecting air turbulence in the environment of an aircraft 有权
标题翻译：用于检测飞机环境中空气湍流的方法和装置
公开(公告)号：US07761197B2
公开(公告)日：2010-07-20
申请号：US11773309
申请日：2007-07-03
申请人： Stephane Puig
发明人： Stephane Puig
IPC分类号： G06F7/70 , G06F19/00 , G06G7/00 , G06G7/76
CPC分类号： G01W1/10 , G01K2203/00 , G01W1/00 , G01W1/08 , G01W2001/003
摘要： A device and method for detecting air turbulence determine a theoretical height corresponding to the difference between an extrapolated height of an isentropic trajectory and the current height of an aircraft. This theoretical height is compared with a height threshold indicating a risk of turbulence.
摘要翻译：用于检测空气湍流的装置和方法确定对应于等熵轨迹的外推高度与飞行器当前高度之间的差的理论高度。将该理论高度与表示湍流风险的高度阈值进行比较。

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