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laser system for measuring the anstellwinkels of an aircraft.

机译:激光系统,用于测量飞机的羚羊角。

摘要

The system comprises at least one probe (1) comprising a laser generator (6), transmission optics (7, 8, 9, 10), optics (10, 9, 30) for receiving a radiation back-scattered by aerosols, means (3) of pumping the laser generator, a detection interferometer (4) receiving a portion of the transmitted laser beam and the back-scattered radiation and means (5) for, after beating of the transmitted and back-scattered beams, determining the Doppler shift of the back-scattered beam and from this deriving the air speed along the axis of the transmitted beam. The transmitted beam is focused on a section of air distant from the aircraft, the laser generator (6) is disposed in the vicinity of the skin of the aircraft, the pumping means (3) and the interferometer (4) are remotely installed in the aircraft and the frequency of the laser line is adapted such that the connections between the probe (1), on the one hand, and the pumping means (3) and the interferometer (4), on the other hand, are carried out by monomode optical fibres with maintained polarisation (13, 23; 17, 19, 20, 22). …IMAGE…
机译:该系统包括至少一个探针(1),其包括激光发生器(6),传输光学器件(7、8、9、10),光学器件(10、9、30),用于接收被气溶胶反向散射的辐射,装置( 3)泵浦激光发生器,检测干涉仪(4)接收一部分透射的激光束和后向散射辐射,以及在跳动后向和后向散射束之后确定多普勒频移的装置(5)反向散射光束的角速度,由此得出沿透射光束轴的空气速度。透射光束聚焦在远离飞机的一段空气上,激光发生器(6)放置在飞机皮肤附近,泵浦装置(3)和干涉仪(4)远程安装在飞机上调整飞机的飞行器和激光线的频率,以便一方面通过单模实现探头(1)与泵浦装置(3)和干涉仪(4)之间的连接保持偏振的光纤(13,23; 17,19,20,22)。 …<图像>…

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