An optical displacement transducer for aerospace applications

J. Manwell , G. Bailey, P. Parsons, P. Richards, D. Kreit
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引用次数: 7

Abstract

A passive optical linear displacement transducer for aerospace applications has been developed. The principle of operation is the wavelength encoding of the position of a reflective Gray code. The design allows the sensor to be passively interrogated using only two optical fibres. The example described here has a 38 mm stroke with a 38 μm resolution. The same principle can be applied to longer stroke linear sensors and rotary displacement sensors.

The optical design is based on the wavelength division of a broad-band source into 11 spectral bands, which are directed onto a reflective Gray code. The reflected light is decoded by a second wavelength division multi-plexer in the electronics housing and the position of the Gray code is determined by the respective on/off states of the channels. The transducer has been designed to operate in the harsh aerospace environment. The housing is of rugged construction to withstand the standard range of temperature, vibration, pressure and contamination conditions.

一种用于航空航天应用的光学位移传感器
研制了一种用于航空航天的无源光学线性位移传感器。其工作原理是对波长编码的位置进行反射的格雷码。该设计允许仅使用两根光纤对传感器进行被动询问。这里描述的示例具有38 mm行程和38 μm分辨率。同样的原理可以应用于较长行程的线性传感器和旋转位移传感器。光学设计基于宽带光源的波长划分为11个光谱带,这些光谱带直接指向反射的格雷码。反射光由电子外壳中的第二波分多路复用器解码,并且格雷码的位置由通道的各自开/关状态确定。该换能器设计用于恶劣的航空航天环境。外壳坚固耐用,可承受标准范围的温度、振动、压力和污染条件。
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