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

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at which the blade obtained the initial<br />

crack) has a characteristic<br />

flat polished surface.<br />

In the cross section where the blade was<br />

broken <strong>and</strong> the crack has not yet developed, the fracture surface<br />

is<br />

crystalline.<br />

<strong>The</strong> breakdown <strong>of</strong> one blade usually leads to the failure <strong>of</strong> the<br />

remaining blades <strong>and</strong> the turbine as a whole.<br />

To prevent vibration breakage <strong>and</strong> control it<br />

successfully when<br />

it does appear, it is necessary to correctly evaluate the possible<br />

sources <strong>of</strong> the onset <strong>of</strong> the defect. For this purp% 4t is necessary<br />

to determine the natural frequencies <strong>of</strong> blade vibration; to determine<br />

the disturbing forces <strong>and</strong> to produce their wave analysis; to construct<br />

a frequency diagram <strong>and</strong> reveal the possible resonant frequenciez<br />

over the range <strong>of</strong> operating revolutions <strong>of</strong> the motor <strong>and</strong> find which are<br />

the most dangerous. <strong>The</strong> various vibrational modes follow: flexural,<br />

torsional, flexural-torsional, <strong>and</strong> edge vibration (when almost tne<br />

entire surface <strong>of</strong> the blade is fixed <strong>and</strong> only individual poiits<br />

on the edge, sometimes the closed areas <strong>of</strong> the blade, vibrate).<br />

Edge vibrations have very high-frequencies <strong>and</strong> appear in fineý<br />

blades.<br />

Flexural vibrations are the most dangerous because their<br />

frequency can be within the range <strong>of</strong> the working rpm. <strong>The</strong> other<br />

wave forms o! turbine blades have a high frequency <strong>and</strong> do not always<br />

fall within the range <strong>of</strong> working rpm's.<br />

Edge vibrations have a frequency on the order <strong>of</strong> 10,000 vibrations<br />

per second <strong>and</strong> can be excited with a certain combination <strong>of</strong><br />

nozzle <strong>and</strong> rotor blade quantities during vibrational combustion in<br />

the combustion chambers. <strong>The</strong>se vibrations as yet have not been<br />

generalized.<br />

blades.<br />

Figure 3.22 shows the types <strong>of</strong> vibration cracks in<br />

turbine<br />

Let us examine only the flexural vibrations <strong>of</strong> blades.<br />

259

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