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handbook of modern sensors

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3.11 Temperature and Thermal Properties <strong>of</strong> Materials 97<br />

(A)<br />

(B)<br />

Fig. 3.38. (A) Warping <strong>of</strong> a laminated plate where two materials have different coefficients <strong>of</strong><br />

thermal expansion; (B) a bimetal coil used as a temperature transducer.<br />

where T = T 2 − T 1 . Table A.16 gives values <strong>of</strong> α for different materials 16 . Strictly<br />

speaking, α depends on the actual temperature. However, for most engineering purposes,<br />

small variations in α may be neglected. For the so-called isotropic materials,<br />

α is the same for any direction. The fractional change in area <strong>of</strong> an object and its<br />

volume with a high degree <strong>of</strong> accuracy can be represented, respectively, by<br />

A = 2αAT , (3.111)<br />

V = 3αV T . (3.112)<br />

Thermal expansion is a useful phenomenon that can be employed in many <strong>sensors</strong><br />

where thermal energy is either measured or used as an excitation signal. Consider two<br />

laminated plates, X and Y, that are fused together (Fig. 3.38A). The plates have the<br />

same thickness and surface area and identical moduli <strong>of</strong> elasticity. Their coefficients<br />

<strong>of</strong> thermal expansion, α 1 and α 2 , however, are different. The fused plates are anchored<br />

at the left-hand side to the reference wall. Now, if we apply heat to the structure, (i.e.,<br />

if we increase its temperature from T 1 to T 2 ), plate X will expand more than plate<br />

Y (for α 1 >α 2 ). The lamination area will restrain plate X from a uniform expansion<br />

while forcing plate Y to expand more than its coefficient <strong>of</strong> expansion would require.<br />

This results in the formation <strong>of</strong> the internal stress and the structure will warp downward.<br />

Contrary, if we cool the structure, it will warp upward. The radius <strong>of</strong> warping<br />

can be estimated from [36]<br />

2j<br />

r ≈<br />

3(α X − α Y )(T 2 − T 1 ) . (3.113)<br />

The warping results in deflection <strong>of</strong> the tip that is strongest at the end <strong>of</strong> the structure<br />

anchored at the other end. This deflection can be measured as a representative <strong>of</strong> the<br />

16 More precisely, thermal expansion can be modeled by higher-order polynomials: l 2 = l 1 [1 +<br />

α 1 (T 2 − T 1 ) + α 2 (T 2 − T 1 ) 2 + α 3 (T 2 − T 1 ) 3 +···]; however, for the majority <strong>of</strong> practical<br />

purposes, a linear approximation is usually sufficient.

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