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STANDARD HANDBOOK OF PETROLEUM & NATURAL GAS ...

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868 Drilling and Well Completions<br />

The stall torque Ms (ft-lb) for any turbine motor can be determined from [86]<br />

where q, = hydraulic efficiency<br />

q, = mechanical efficiency<br />

n, = number of stages<br />

7, = specific weight of mud in lb/gal<br />

q = circulation flowrate in gal/min<br />

p = exit blade angle in degrees<br />

h = radial width of the blades in in.<br />

(4-138)<br />

Figure 4-193 is the side view of a single-turbine stage and describes the geometry<br />

of the rotor and stator.<br />

The runaway speed Nr (rpm) for any turbine motor can be determined from<br />

(4-139)<br />

where qv = volumetric efficiency<br />

rm = mean blade radius in in.<br />

The turbine motor instantaneous torque M (ft-lb) for any speed N (rpm) is<br />

M = Ms(l-$)<br />

(4-140)<br />

The turbine motor horsepower HP (hp) for any speed is<br />

2 nM ,N<br />

HP = -<br />

33,000 (’- $)<br />

(4-141)<br />

The maximum turbine motor horsepower is at the optimum speed, No, which<br />

is one-half of the runaway speed. This is<br />

N<br />

No = I (4-142)<br />

2<br />

Thus the maximum horsepower HP,,, is<br />

HP,,<br />

= xMJ,<br />

2( 33,000)<br />

(4- 143)<br />

The torque at the optimum speed M, is one-half the stall torque. Thus<br />

M, M, = - 2<br />

(4-144)

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