NNR IN RAPIDLY ROTATED METALS By - Nottingham eTheses ...
NNR IN RAPIDLY ROTATED METALS By - Nottingham eTheses ...
NNR IN RAPIDLY ROTATED METALS By - Nottingham eTheses ...
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- 47 -<br />
The problem may also be overcome by using a propelling gas in<br />
which the velocity of sound is much higher. The maximum velocity<br />
of the rotor is then determined by other factors - usually<br />
mechanical - before the sonic limit is reached.<br />
4.3 THE CONICAL ROTOR SYSTEM<br />
4.3.1 DESCRIPTION<br />
This rotor system is based on the type originally described<br />
(54)<br />
by Henriot and Huguenard and by Beams ý55,56),<br />
The conical-<br />
shaped rotor base sits in a stator in which there are a series of<br />
jets. The gas passing through these jets serves both to lift<br />
the rotor off the base stator and to drive it round. Because of<br />
the Bernoulli forces the rotor does not fly out of the stator,<br />
but is supported by a cushion of air.<br />
The present system, shown in Figure 4.1, is a compromise bet-<br />
ween sample size and the higher rotation speeds possible with<br />
smaller diameter rotors. The rotors have a series of 20 flutes<br />
cut to a depth of 0.030" at an angle of approximately 300 to<br />
the vertical axis. In the past much effort has gone into optimiz-<br />
ing the number, position and size of the jets in the stator(57,58).<br />
The most efficient combination of rotor and stator has been found<br />
to vary with each individual rotor. Generally the best results<br />
were achieved here using stators with 23 0.015" diameter jets set<br />
in a single ring. Each jet was drilled at an angle of 600 to a<br />
vertical line through the-apex of the stator and in a plane tangent-<br />
ial to the rotor flutes at each point.<br />
I