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1. 发明授权

US07580132B2 Optical device for measuring a doppler frequency shift 有权
标题翻译：用于测量多普勒频移的光学装置
公开(公告)号：US07580132B2
公开(公告)日：2009-08-25
申请号：US11579504
申请日：2005-03-16
申请人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine , Alain Renard
发明人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine , Alain Renard
IPC分类号： G01B9/02
CPC分类号： G01S17/58 , G01P5/26 , G01S7/481 , G01S17/95 , Y02A90/19
摘要： The invention relates to a device for measuring a Doppler frequency shift, including an optical signal channel delivering a signal light beam illuminating a reference medium; and a reference channel delivering a reference light beam for detecting the Doppler frequency shift. The frequency shift is determined from the difference in frequency between the light signal illuminating the reference medium and the light beam returned by the reference medium. The device includes at least two light radiation sources, preferably lasers, with one light radiating source generating the light beam for the signal channel and the other source generating the light beam for the reference channel.
摘要翻译：本发明涉及一种用于测量多普勒频移的装置，包括传送照射参考介质的信号光束的光信号通道; 以及传送用于检测多普勒频移的参考光束的参考通道。频移由照射参考介质的光信号与由参考介质返回的光束之间的频率差确定。该装置包括至少两个光辐射源，优选地是激光器，其中一个光辐射源产生用于信号通道的光束，而另一个光源产生用于参考通道的光束。

2. 发明申请

US20070229799A1 Low-Cost Doppler Frequency Shift Measuring Device 有权
标题翻译：低成本多普勒频移测量装置
公开(公告)号：US20070229799A1
公开(公告)日：2007-10-04
申请号：US11579503
申请日：2005-03-17
申请人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine
发明人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine
IPC分类号： G01P3/36
CPC分类号： G01S17/88 , G01S3/48 , G01S7/4818 , G01S17/58
摘要： The invention relates to a Doppler frequency shift measuring device of the optical type comprising an optical signal channel delivering, through a polarization-splitting coupler, through a bidirectional signal port of the coupler, a signal light beam illuminating a reference medium, the coupler receiving, through said bidirectional port, a backscattered light beam returned by the reference medium; a reference channel providing a reference light beam for detection of the Doppler frequency shift, the frequency shift being determined by the frequency shift between the light signal illuminating the reference medium and the light beam returned by the reference medium. The reference light beam is applied to a reference port of the polarization-splitting coupler, said coupler delivering, at a port, a beat signal between the frequency of the reference light beam applied to the port and the frequency of the backscattered light beam applied to the port, possibly containing the Doppler shift.
摘要翻译：本发明涉及一种光学类型的多普勒频移测量装置，包括一个光信号通道，通过偏振分束耦合器，通过耦合器的双向信号端口，照射参考介质的信号光束，耦合器接收，通过所述双向端口，由参考介质返回的背散射光束; 提供用于检测多普勒频移的参考光束的参考通道，所述频移由照射参考介质的光信号和由参考介质返回的光束之间的频移确定。参考光束被施加到偏振分离耦合器的参考端口，所述耦合器在端口处提供施加到端口的参考光束的频率与施加到端口的反向散射光束的频率之间的拍频信号该端口可能包含多普勒频移。

3. 发明申请

US20070223004A1 Optical Device for Measuring a Doppler Frequency Shift 有权
标题翻译：用于测量多普勒频移的光学装置
公开(公告)号：US20070223004A1
公开(公告)日：2007-09-27
申请号：US11579504
申请日：2005-03-16
申请人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine , Alain Renard
发明人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine , Alain Renard
IPC分类号： G01B9/02
CPC分类号： G01S17/58 , G01P5/26 , G01S7/481 , G01S17/95 , Y02A90/19
摘要： The invention relates to a device for measuring a Doppler frequency shift, comprising: an optical signal channel (60) delivering a signal light beam illuminating a reference medium; a reference channel (80) delivering a reference light beam for detecting the Doppler frequency shift, the frequency shift being determined from the difference in frequency between the light signal illuminating the reference medium and the light beam returned by the reference medium, characterized in that it includes at least two light radiation sources (SL1, SL2), preferably lasers, one light radiating source generating the light beam for the signal channel and the other source generating the light beam for the reference channel.
摘要翻译：本发明涉及一种用于测量多普勒频移的装置，包括：光信号通道（60），其输送照射参考介质的信号光束; 传送用于检测多普勒频移的参考光束的参考通道（80），所述频移是根据照射参考介质的光信号与由参考介质返回的光束之间的频率差确定的，其特征在于，包括至少两个光辐射源（SL 1，SL 2），优选地，激光器，一个产生用于信号通道的光束的光辐射源，而另一个源产生用于参考通道的光束。

4. 发明申请

US20070040730A1 Active optical measurement device with weak signal amplification 失效
标题翻译：主动光学测量装置具有弱信号放大
公开(公告)号：US20070040730A1
公开(公告)日：2007-02-22
申请号：US11429964
申请日：2006-05-09
申请人： Jean-Pierre Schlotterbeck , Bertrand Baillon , Xavier Lacondemine
发明人： Jean-Pierre Schlotterbeck , Bertrand Baillon , Xavier Lacondemine
IPC分类号： G01S13/08
CPC分类号： G01S17/58 , G01S17/88
摘要： The invention relates to an optical measurement device designed notably to evaluate the velocity of an aircraft by detection of a Doppler shift. The device for measurement by optical probe comprises at least two light beams of different wavelengths λ1, λ2, denoted as first beam and second beam, the device illuminating a reference medium MILREF (60) by the first beam and receiving a light echo Sr reflected back by the reference medium, and the device comprising: an optical coupler COUPL (70) receiving, on the one hand, the light echo Sr reflected back by the reference medium MILREF and, on the other, the second beam, the coupler delivering a resultant wave Or comprising the second beam and the light echo Sr; an optical amplification unit AMPLI (80), of bandwidth Bopt, receiving the resultant wave Or and delivering an amplified resultant wave Ora.
摘要翻译：本发明涉及一种光学测量装置，其特别设计用于通过检测多普勒频移来评估飞行器的速度。用于通过光学探针测量的装置包括至少两个不同波长的光束λ1，λ2，表示为第一光束和第二光束，该装置通过第一光束照射参考介质MILREF（60）并接收反射回的光回波Sr 并且所述装置包括：光耦合器COUPL（70），一方面接收由参考介质MILREF反射的光回波Sr，另一方面接收第二光束，所述耦合器输出结果波或包括第二光束和光回波Sr; 具有带宽B opt opt的光放大单元AMPLI（80），接收所得到的波Or并传送放大的合成波Ora。

5. 发明授权

US07352447B2 Active optical measurement device with weak signal amplification 失效
标题翻译：主动光学测量装置具有弱信号放大
公开(公告)号：US07352447B2
公开(公告)日：2008-04-01
申请号：US11429964
申请日：2006-05-09
申请人： Jean-Pierre Schlotterbeck , Bertrand Baillon , Xavier Lacondemine
发明人： Jean-Pierre Schlotterbeck , Bertrand Baillon , Xavier Lacondemine
IPC分类号： G01P3/36
CPC分类号： G01S17/58 , G01S17/88
摘要： The invention relates to an optical measurement device designed notably to evaluate the velocity of an aircraft by detection of a Doppler shift. The device for measurement by optical probe comprises at least two light beams of different wavelengths λ1 , λ2, denoted as first beam and second beam, the device illuminating a reference medium MILREF (60) by the first beam and receiving a light echo Sr reflected back by the reference medium, and the device comprising: an optical coupler COUPL (70) receiving, on the one hand, the light echo Sr reflected back by the reference medium MILREF and, on the other, the second beam, the coupler delivering a resultant wave Or comprising the second beam and the light echo Sr; an optical amplification unit AMPLI (80), of bandwidth Bopt, receiving the resultant wave Or and delivering an amplified resultant wave Ora.
摘要翻译：本发明涉及一种光学测量装置，其特别设计用于通过检测多普勒频移来评估飞行器的速度。用于通过光学探针测量的装置包括至少两个不同波长λ1，λ2的光束，表示为第一光束和第二光束，该装置用第一光束照射参考介质MILREF（60）并接收反射的光回波Sr 并且该装置包括：光耦合器COUPL（70），一方面接收由参考介质MILREF反射的光回波Sr，另一方面接收第二光束，耦合器输出合成波或包括第二光束和光回波Sr; 具有带宽B opt opt的光放大单元AMPLI（80），接收所得到的波Or并传送放大的合成波Ora。

6. 发明授权

US07423736B2 Low-cost doppler frequency shift measuring device 有权
标题翻译：低成本多普勒频移测量装置
公开(公告)号：US07423736B2
公开(公告)日：2008-09-09
申请号：US11579503
申请日：2005-03-17
申请人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine
发明人： Bertrand Baillon , Jean-Pierre Schlotterbeck , Xavier Lacondemine
IPC分类号： G01P3/36
CPC分类号： G01S17/88 , G01S3/48 , G01S7/4818 , G01S17/58
摘要： The invention relates to a Doppler frequency shift measuring device of the optical type comprising an optical signal channel delivering, through a polarization-splitting coupler, through a bidirectional signal port of the coupler, a signal light beam illuminating a reference medium, the coupler receiving, through said bidirectional port, a backscattered light beam returned by the reference medium; a reference channel providing a reference light beam for detection of the Doppler frequency shift, the frequency shift being determined by the frequency shift between the light signal illuminating the reference medium and the light beam returned by the reference medium. The reference light beam is applied to a reference port of the polarization-splitting coupler, said coupler delivering, at a port, a beat signal between the frequency of the reference light beam applied to the port and the frequency of the backscattered light beam applied to the port, possibly containing the Doppler shift.
摘要翻译：本发明涉及一种光学类型的多普勒频移测量装置，包括一个光信号通道，通过偏振分束耦合器，通过耦合器的双向信号端口，照射参考介质的信号光束，耦合器接收，通过所述双向端口，由参考介质返回的背散射光束; 提供用于检测多普勒频移的参考光束的参考通道，所述频移由照射参考介质的光信号和由参考介质返回的光束之间的频移确定。参考光束被施加到偏振分离耦合器的参考端口，所述耦合器在端口处提供施加到端口的参考光束的频率与施加到端口的反向散射光束的频率之间的拍频信号该端口可能包含多普勒频移。

7. 发明授权

US08422001B2 Method of measuring the velocity of an aircraft by laser doppler anemometry 有权
标题翻译：通过激光多普勒血流计测量飞行器速度的方法
公开(公告)号：US08422001B2
公开(公告)日：2013-04-16
申请号：US12821428
申请日：2010-06-23
申请人： Xavier Lacondemine , Jean-Pierre Schlotterbeck , Alain Renard
发明人： Xavier Lacondemine , Jean-Pierre Schlotterbeck , Alain Renard
IPC分类号： G01P3/36
CPC分类号： G01S17/58 , G01P5/26
摘要： Method of measuring the velocity of an aircraft at a given instant, by laser Doppler anemometry, by performing the steps of acquiring a backscattered signal on at least three oriented line-of-sight axes, and calculating the spectrum of the backscattered signal on each of the line-of-sight axes. Further, acquiring an additional backscattered signal on at least one additional line-of-sight axis (X4) not coincident with one of the three first line-of-sight axes (X1, X2, X3), and calculating the spectrum of the backscattered signal on the additional line-of-sight axis (X4). Several candidate velocity vectors ({right arrow over (V)}c) and of the projections of the candidate vectors on at least one line-of-sight axis (X1, X2, X3, X4) are calculated. The consistency of the candidate vectors ({right arrow over (V)}c) is calculated as a function of their projections and as a function of each spectrum of the corresponding backscattered signal on the respective calculation axis (X1, X2, X3, X4). The measured velocity vector ({right arrow over (V)}c) is chosen from among the candidate velocity vectors ({right arrow over (V)}c).
摘要翻译：通过在至少三个定向视线轴上获取反向散射信号的步骤，通过激光多普勒测风法测量给定时刻的飞行器的速度的方法，以及计算每个方向上的反向散射信号的频谱视线轴。此外，在与三个第一视线轴（X1，X2，X3）中的一个不一致的至少一个附加视线轴（X4）上获取附加的反向散射信号，并且计算背向散射的光谱信号在附加的视线轴（X4）上。计算在至少一个视线轴（X1，X2，X3，X4）上的候选候选矢量（{右箭头（V）} c）和候选矢量的投影的几个候选速度矢量。候选矢量的一致性（{右箭头（V）} c）被计算为它们的投影的函数，并且作为相应计算轴上的相应反向散射信号的每个光谱的函数（X1，X2，X3，X4））。测量的速度矢量（{（V）} c）中的右箭头从候选速度矢量（{右箭头（V）} c）中选择。

8. 发明申请

US20110043786A1 METHOD OF MEASURING THE VELOCITY OF AN AIRCRAFT BY LASER DOPPLER ANEMOMETRY 有权
标题翻译：通过激光多普勒测量法测量飞机速度的方法
公开(公告)号：US20110043786A1
公开(公告)日：2011-02-24
申请号：US12821428
申请日：2010-06-23
申请人： Xavier LACONDEMINE , Jean-Pierre Schlotterbeck , Alain Renard
发明人： Xavier LACONDEMINE , Jean-Pierre Schlotterbeck , Alain Renard
IPC分类号： G01P3/36
CPC分类号： G01S17/58 , G01P5/26
摘要： Method of measuring the velocity of an aircraft at a given instant, by laser Doppler anemometry, by performing the steps of acquiring a backscattered signal on at least three oriented line-of-sight axes, and calculating the spectrum of the backscattered signal on each of the line-of-sight axes. Further, acquiring an additional backscattered signal on at least one additional line-of-sight axis (X4) not coincident with one of the three first line-of-sight axes (X1, X2, X3), and calculating the spectrum of the backscattered signal on the additional line-of-sight axis (X4). Several candidate velocity vectors ({right arrow over (V)}c) and of the projections of the candidate vectors on at least one line-of-sight axis (X1, X2, X3, X4) are calculated. The consistency of the candidate vectors ({right arrow over (V)}c) is calculated as a function of their projections and as a function of each spectrum of the corresponding backscattered signal on the respective calculation axis (X1, X2, X3, X4). The measured velocity vector ({right arrow over (V)}c) is chosen from among the candidate velocity vectors ({right arrow over (V)}c).
摘要翻译：通过在至少三个定向视线轴上获取反向散射信号的步骤，通过激光多普勒测风法测量给定时刻的飞行器的速度的方法，以及计算每个方向上的反向散射信号的频谱视线轴。此外，在与三个第一视线轴（X1，X2，X3）中的一个不一致的至少一个附加视线轴（X4）上获取附加的反向散射信号，并且计算背向散射的光谱信号在附加的视线轴（X4）上。计算在至少一个视线轴（X1，X2，X3，X4）上的候选候选矢量（{右箭头（V）} c）和候选矢量的投影的几个候选速度矢量。候选矢量的一致性（{右箭头（V）} c）被计算为它们的投影的函数，并且作为相应计算轴上的相应反向散射信号的每个光谱的函数（X1，X2，X3，X4））。测量的速度矢量（{（V）} c）中的右箭头从候选速度矢量（{右箭头（V）} c）中选择。

9. 发明申请

US20110181863A1 Single-Particle LIDAR Anemometry Method and System 有权
标题翻译：单粒子LIDAR风速计方法和系统
公开(公告)号：US20110181863A1
公开(公告)日：2011-07-28
申请号：US12842872
申请日：2010-07-23
申请人： Alain Renard , Xavier Lacondemine , Jean-Pierre Schlotterbeck
发明人： Alain Renard , Xavier Lacondemine , Jean-Pierre Schlotterbeck
IPC分类号： G01P3/36
CPC分类号： G01N15/1434 , G01N15/1459 , G01N2015/1075 , G01P5/26 , G01S7/493 , G01S17/58
摘要： The present invention concerns a single-particle LIDAR anemometry method and system comprising the continuous emission of one or more light beams through a gas containing particles, said beam being focused onto a measurement volume, a step of detecting a signal backscattered by particles passing through said volume, the method being characterized in that it comprises at least the following phases: determining in a time period Δt the frequency of each of the pulses included in the backscattered signal; distinguishing pulses based on duration and/or intensity and/or frequency-modulation criteria; and estimating the displacement velocity of said beam relative to the gas from several of the frequencies determined over the time period Δt excluding those corresponding to the pulses distinguished during the preceding step A notable application of the invention is for the measurement of the airspeed of an aircraft
摘要翻译：本发明涉及一种单颗粒LIDAR风速测定方法和系统，其包括通过含有颗粒的气体连续发射一个或多个光束，所述光束被聚焦到测量体积上，检测由穿过所述颗粒的颗粒反向散射的信号的步骤该方法的特征在于至少包括以下阶段：在时间段内确定包括在后向散射信号中的每个脉冲的频率; 基于持续时间和/或强度和/或频率调制标准区分脉冲; 并且估计所述光束相对于气体的位移速度，其中从在与之前步骤A中区分的脉冲相对应的那些时间周期＆Dgr; t中确定的几个频率之间确定的频率不同于本发明的显着应用，用于测量空气速度一架飞机

10. 发明授权

US07616294B2 Laser anemometry with improved eye safety 有权
标题翻译：激光风速计改善眼睛安全
公开(公告)号：US07616294B2
公开(公告)日：2009-11-10
申请号：US12067531
申请日：2006-09-22
申请人： Xavier Lacondemine , Jean-Pierre Schlotterbeck
发明人： Xavier Lacondemine , Jean-Pierre Schlotterbeck
IPC分类号： G01P3/36
CPC分类号： G01P5/26 , G01F1/661 , G01F1/663 , G01S17/58 , G01S17/95 , Y02A90/19
摘要： The invention relates to an optical measurement device intended for determining a relative velocity vector {right arrow over (v)} of a carrier, such as an aircraft, with respect to a reference medium MILREF. The device includes an optical signal system EMIREC, delivering an optical signal Sinc that follows a direction called the line of sight LDV and is concentrated in a focusing zone ZOF, and means for displacing the focusing zone ZOF in the reference medium MILREF. According to the invention, the means for displacing the focusing zone ZOF act on the orientation of the line of sight LDV, subjecting it to a known movement, with a nonzero speed, a processing unit UTR determines the vector {right arrow over (v)} in at least one “search” phase based on an identification with an expected waveform of the variation in frequency of an electrical signal as a function of the orientation of the line of sight LDV in order to determine an approximate value of {right arrow over (v)}, followed by a “tracking” phase based on an iterative validation of values of {right arrow over (v)} close to the approximate value of {right arrow over (v)}.
摘要翻译：本发明涉及一种用于确定相对于参考介质MILREF的载体（例如飞机）的相对速度矢量（（v）}的右箭头}的光学测量装置。该装置包括光信号系统EMIREC，其传送遵循称为视线LDV的方向并且集中在聚焦区ZOF中的光信号Sinc，以及用于移动参考介质MILREF中的聚焦区ZOF的装置。根据本发明，用于移动聚焦区域ZOF的装置作用于视线LDV的取向，以非零速度对其进行已知的移动，处理单元UTR确定向量（v）上的向右箭头， }在基于具有作为视线LDV的取向的函数的电信号的频率变化的期望波形的识别的至少一个“搜索”阶段中，以便确定{右箭头超过（v）}，之后是基于{right arrow over（v）}的值的迭代验证，接近{right arrow over（v）}的近似值的“跟踪”阶段。

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