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Detection System for Coherent Light Beams

机译:相干光束检测系统

摘要

1,163,313. Photo-electric detection apparatus. NORTH AMERICAN AVIATION Inc. Sept. 1, 1966 [Oct. 1, 1965], No.39146/66. Heading G1A. [Also in Division H1| The information signal modulating a coherent carrier light beam is extracted by mixing with the carrier beam a reference light beam so as to produce an interference pattern of fringes the variations in intensity and/or movement of which are detected photo-electrically as representative of the modulations on the carrier beam. The light used is that from laser sources. The modulations impressed on the carrier may be of the amplitude of the light beam, in which case the fringes of the interference pattern vary in intensity, or of the frequency, phase or polarization, when they appear to move across the pattern. In detecting frequency modulations on a carrier beam 13 of varying frequency f 1 , Fig. 2, a reference beam 14 of a fixed frequency f 2 is mixed with the carrier beam and an optical system used to focus and locate the interference pattern formed on the surface of a detector means 7. This comprises two photo-diodes 11, 12 with interlocking fingers each of one (dark or light) fringe width. The outputs of detectors 11, 12 are two signals representing the movement of the fringes across detector, the speed of which movement is proportional to the frequencies f 1 and f 2 i.e. proportional to the information signal. The components of this signal in the output on lines 17 and 18 are 180 degrees out-of-phase, while noise signals generated by the incidence of stray light on the detector are in phase in the two outputs. Thus subtraction of the outputs by transformer 20 produces a signal 19 representing the information required, while noise signals cancel out. The sign of the frequency difference of f 1 and f 2 is given by the direction of fringe movement. In a modification of the detector construction, Fig. 4a (not shown), a block of rectangular photodiodes, each of width equal to half a fringe, is connected to a two-transformer circuit, to enable the sign of the frequency difference to be readily detected using an oscilloscope display. In another arrangement (not shown), a mirror provided with an array of slits passes alternate fringes to a detector behind it, and reflects the rest of the fringes towards a further detector. These detectors are connected to subtraction means as before. Alternatively, a double photo-multiplier is used, having a transparent photo-cathode coated on one side with a photo-sensitive layer of the configuration of diode 11, Fig. 2, and on the other, a layer of the configuration of diode 12, Fig. 2, activated by light transmitted through the electrode. These layers each have their own associated accelerating electrodes and anode, feeding a common subtraction circuit. Instead of a rectangular fringe pattern, a circular one may be used with appropriately designed detectors.
机译:1,163,313。光电检测装置。北美航空有限公司1966年9月1日[Oct. [1965年1月],编号39146/66。标题G1A。 [也在H1分区|通过将参考光束与载波相混合来提取调制相干载波光束的信息信号,以产生条纹的干涉图样,以光电方式检测其强度和/或运动的变化,以代表调制在载架上。所使用的光是来自激光源的光。施加在载体上的调制可以是光束的幅度,在这种情况下,当干涉图样的条纹似乎在整个图样上移动时,它们的强度或频率,相位或极化都会发生变化。在检测图2所示频率变化为f 1的载波光束13上的调频时,将固定频率为f 2的参考光束14与该载波光束混合,并使用光学系统聚焦和定位形成在其上的干涉图样。探测器装置7的表面。这包括两个具有互锁指状件的光电二极管11、12,每个互锁指状件具有一个(暗或亮)条纹宽度。检测器11、12的输出是两个信号,它们表示条纹在检测器上的运动,其运动速度与频率f 1和f 2成正比,即与信息信号成正比。线路17和18上的输出中此信号的分量异相180度,而杂散光在检测器上入射产生的噪声信号在两个输出中同相。因此,变压器20对输出的减法产生代表所需信息的信号19,而噪声信号被抵消。 f 1和f 2的频率差的符号由边缘移动的方向给出。在图4a的检测器结构的修改中(未示出),将矩形光电二极管块(每个宽度等于半个条纹)连接到两个变压器电路,以使频率差的符号为使用示波器显示屏可以轻松检测到。在另一种布置(未示出)中,设置有狭缝阵列的反射镜将交替的条纹传递到其后面的检测器,并将其余的条纹反射向另一个检测器。这些检测器如前所述连接到减法装置。替代地,使用双光电倍增器,其具有在一侧上涂覆有二极管11的构造的光敏层(图2)的透明光电阴极,并且在另一侧上具有二极管12的构造的层的透明光电阴极。如图2所示,被穿过电极的光激活。这些层各自具有各自关联的加速电极和阳极,为共同的减法电路供电。代替矩形条纹图案,可以将圆形的条纹与适当设计的检测器一起使用。

著录项

  • 公开/公告号GB1163313A

    专利类型

  • 公开/公告日1969-09-04

    原文格式PDF

  • 申请/专利权人 NORTH AMERICAN AVIATION INC.;

    申请/专利号GB19660039146

  • 发明设计人

    申请日1966-09-01

  • 分类号G02F2/00;H04B10/06;

  • 国家 GB

  • 入库时间 2022-08-23 11:49:48

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