An Optical Fiber Measurement System for Blade Tip Clearance of Engine

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2017/4168150/figures/4168150.fig.004a.svgz" name="4168150.fig.004a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Arrangement of the fiber bundle</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2017/4168150/figures/4168150.fig.004b.svgz" name="4168150.fig.004b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Principle of reflective light intensity-modulated</td></tr></table>

<div>Structure of the reflective intensity-modulated optical fiber bundle.</div>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: An Optical Fiber Measurement System for Blade Tip Clearance of Engine 