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Design and Stress Analysis of Extraterrestrial ... - The Black Vault

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At each <strong>of</strong> the points <strong>of</strong> interse-tion by a ray <strong>of</strong> exciting forces<br />

with the graph <strong>of</strong> natural frequencies resonance will occur.<br />

these modes "bursts" are observed, .i.e., sharp increase in<br />

<strong>and</strong> an increase in stresses.<br />

In<br />

amplitudes<br />

An analysis <strong>of</strong> the frequency characteristic shows which harmonies<br />

<strong>of</strong> forced vibrations will be dangerous <strong>and</strong> makes it possible to<br />

soundly implement the design <strong>of</strong> a turbine node so as to avoid<br />

dangerous resonance modes.<br />

<strong>The</strong> following practical methods <strong>of</strong> combatting resonance modes<br />

in<br />

blades exist.<br />

1. Elimination <strong>of</strong> the dangerous exciter harmonics. This can<br />

sometimes be done by a small structural alteration <strong>of</strong> the turbine<br />

unit. Let us assume that dangerous harmonic k = 4 (based on the number<br />

<strong>of</strong> racks). If we change the number <strong>of</strong> racis, increasing it, for<br />

example, to 5, then the dangercus harmonic disappears.<br />

2. To build the resonance frequency out <strong>of</strong> the blade, i.e.j to<br />

change the inherent angular velocity w.c.<br />

certain variation in<br />

This can be done by a<br />

the blade's dimensions, however, so as not to<br />

disturb the gas-dynamic characteristics <strong>of</strong> the turbine <strong>and</strong> not to<br />

make a basic alteration <strong>of</strong> the turbine stage. It is possible, for<br />

example,<br />

in<br />

webs,<br />

to use hollow blades, to cut the angle <strong>of</strong> the blade foil<br />

the periphery near the trailing edge, to use blades with b<strong>and</strong><br />

to combine blades into groups by connectors or'to cast blades<br />

with b<strong>and</strong> webs in<br />

groups.<br />

All these measures allow the redistribution <strong>of</strong> mass <strong>and</strong> the<br />

rigidity <strong>of</strong> the blade foil <strong>and</strong>, consequently, a variation in wc'<br />

3. <strong>The</strong> damping <strong>of</strong> blade vibrations. <strong>The</strong>re are several methods<br />

<strong>of</strong> damping vibrations in elastic systems based on energy dispersion<br />

<strong>of</strong> a vibrating blade. This involves primarily damping in the blade<br />

286

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