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handbook of modern sensors

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372 11 Flow Sensors<br />

Fig. 11.12. Micromachined gas flow sensor.<br />

11.6 Micr<strong>of</strong>low Sensors<br />

In some applications, such as process control in precise semiconductor manufacturing,<br />

chemical and pharmaceutical industries, and biomedical engineering, miniaturized<br />

gas flow <strong>sensors</strong> are encountered with increasing frequency. Most <strong>of</strong> them operate on<br />

the method <strong>of</strong> thermal transport (see Section 11.3) and are fabricated from a silicon<br />

crystal by using micromachining technology. Many <strong>of</strong> the micr<strong>of</strong>low <strong>sensors</strong> use a<br />

thermopile as a temperature sensor [6]; however, the thermoelectric coefficient [Eq.<br />

(3.91) <strong>of</strong> Chapter 3] <strong>of</strong> standard elements used in the integrated circuit (IC) processing<br />

(silicon and aluminum) is smaller than that <strong>of</strong> conventional thermocouples by factors<br />

ranging from 10 to 100. Thus, a resulting output signal may be very small, which<br />

requires amplification by amplifiers integrated directly into the sensor.<br />

A cantilever design <strong>of</strong> a micr<strong>of</strong>low sensor is shown in Fig. 11.12. The thickness<br />

<strong>of</strong> the cantilever may be as low as 2 µm. It is fabricated in the form <strong>of</strong> a sandwich<br />

consisting <strong>of</strong> layers <strong>of</strong> field oxide, chemical vapor deposition (CVD) oxide, and<br />

nitrate [7]. The cantilever sensor is heated by an imbedded resistor with a rate <strong>of</strong> 26<br />

K/mW <strong>of</strong> applied electric power, and a typical transfer function <strong>of</strong> the flow sensor<br />

has a negative slope <strong>of</strong> about 4 mV/m/s.<br />

The heat is removed from the sensor by three means: conductance L b through<br />

the cantilever beam, gas flow h(v), and thermal radiation, which is governed by the<br />

Stefan–Boltzmann law:<br />

P = L b (T s − T b ) + h(v)(T s − T b ) + aσε(Ts 4 − T b 4 ), (11.24)<br />

where σ is the Stefan–Boltzmann constant, a is the area along which the beam-togas<br />

heat transfer occurs, ε is surface emissivity, and v is the gas velocity. From the<br />

principles <strong>of</strong> energy and particle conservation, we deduce a generalized heat-transport<br />

equation governing the temperature distribution T (x,y) in the gas flowing near the

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