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    • 7. 发明授权
    • Active optical measurement device with weak signal amplification
    • 主动光学测量装置具有弱信号放大
    • US07352447B2
    • 2008-04-01
    • US11429964
    • 2006-05-09
    • Jean-Pierre SchlotterbeckBertrand BaillonXavier Lacondemine
    • Jean-Pierre SchlotterbeckBertrand BaillonXavier Lacondemine
    • G01P3/36
    • G01S17/58G01S17/88
    • 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.
    • 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。
    • 8. 发明授权
    • Device for detecting atmospheric turbulence
    • 用于检测大气湍流的装置
    • US07352476B2
    • 2008-04-01
    • US11313663
    • 2005-12-22
    • Bertrand BaillonLaurence MutuelJean-Pierre Schlotterbeck
    • Bertrand BaillonLaurence MutuelJean-Pierre Schlotterbeck
    • G01B9/02
    • G01S17/95G01S7/4816Y02A90/19
    • The invention relates to a device for remote measurement of the properties of the atmosphere, more particularly a device used to detect atmospheric turbulence. The device operates on the lidar principle, using the backscattering of a laser beam by the air. The device comprises a laser emission source (1), optical means (5) for collecting a backscattered beam (3) that is backscattered by targets illuminated by the emission source (1), the backscattered beam (3) being substantially centerd about the wavelength of the emission source (1), and means (9) for generating interference fringes (24) resulting from the backscattered beam (3). The device also includes a spatial filter (11) allowing only a central spot of the interference fringes to be seen and, at the center of the spatial filter (11), a mask for blocking off the center of the central spot and more particularly the Mie line of the backscattered beam.
    • 本发明涉及用于远程测量大气特性的装置,更具体地说,涉及用于检测大气湍流的装置。 该装置以激光雷达原理工作,使用空气中的激光束的后向散射。 该装置包括激光发射源(1),用于收集由发射源(1)照射的靶反向散射的背散射束(3)的光学装置(5),背散射光束(3)基本上围绕波长 和用于产生由后向散射光束(3)产生的干涉条纹(24)的装置(9)。 该装置还包括仅能够看到干涉条纹的中心点的空间滤波器(11),并且在空间滤波器(11)的中心处具有用于阻挡中心点的中心的掩模,更具体地, 背散射梁的三重线。
    • 9. 发明申请
    • Low-Cost Doppler Frequency Shift Measuring Device
    • 低成本多普勒频移测量装置
    • US20070229799A1
    • 2007-10-04
    • US11579503
    • 2005-03-17
    • Bertrand BaillonJean-Pierre SchlotterbeckXavier Lacondemine
    • Bertrand BaillonJean-Pierre SchlotterbeckXavier Lacondemine
    • G01P3/36
    • G01S17/88G01S3/48G01S7/4818G01S17/58
    • 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.
    • 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。
    • 10. 发明申请
    • Active optical measurement device with weak signal amplification
    • 主动光学测量装置具有弱信号放大
    • US20070040730A1
    • 2007-02-22
    • US11429964
    • 2006-05-09
    • Jean-Pierre SchlotterbeckBertrand BaillonXavier Lacondemine
    • Jean-Pierre SchlotterbeckBertrand BaillonXavier Lacondemine
    • G01S13/08
    • G01S17/58G01S17/88
    • 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.
    • 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。