The Dynamics of Rotating Machines with Cracks ... - Michael I Friswell
The Dynamics of Rotating Machines with Cracks ... - Michael I Friswell
The Dynamics of Rotating Machines with Cracks ... - Michael I Friswell
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312<br />
Modern Practice in Stress and Vibration Analysis<br />
2 Title <strong>of</strong> Publication (to be inserted by the publisher)<br />
2 <strong>The</strong> Mayes model for an opening and closing crack<br />
This model is defined, in rotating coordinates, by<br />
and<br />
k<br />
k<br />
<br />
<br />
<br />
kM<br />
kDC1<br />
(1a)<br />
<br />
kM<br />
kDC1<br />
(1b)<br />
where k<br />
1<br />
M k0<br />
k<br />
, k<br />
1<br />
D<br />
k0<br />
k<br />
, etc., and C<br />
2<br />
2<br />
1 cos . When <br />
closed and kk k0<br />
. When cos 1<br />
k k .<br />
<br />
<br />
the crack is fully open and<br />
cos 1 the crack is<br />
k<br />
<br />
<br />
k ,<br />
<strong>The</strong> stiffnesses in fixed coordinates can be determined by transforming from rotating coordinates so<br />
that<br />
T<br />
K F T K RT<br />
(2)<br />
<br />
where<br />
C1<br />
S1<br />
<br />
T . (3)<br />
<br />
S1<br />
C1<br />
<br />
<br />
In (3), S1 sin<br />
. Carrying out the matrix multiplications <strong>of</strong> (2) and expanding the trigonometric<br />
expressions in multiple angles gives<br />
1<br />
K<br />
<br />
1<br />
k<br />
k S<br />
k<br />
k S<br />
<br />
F 12 2 M M<br />
2 4 D<br />
D<br />
1 S3<br />
or<br />
K 1<br />
k k S S S <br />
<br />
<br />
1<br />
F <br />
12 4 2 <br />
2 1 3<br />
(4)<br />
where S <br />
and<br />
3 sin 3 , etc. Similarly<br />
1 1<br />
1<br />
F D D D D 3<br />
D D D D<br />
<br />
K k 11 0 k k k k C<br />
2 2 2 k k C<br />
4<br />
1 k k C3<br />
(5)<br />
1 1<br />
1<br />
F D D D D 3<br />
D D D D<br />
<br />
K k 22 0 k k k k C<br />
2 2 2 k k C<br />
4<br />
1 k k C3<br />
. (6)<br />
Now, if t , where is the rotor angular velocity, then in fixed coordinates the Mayes model<br />
generates a constant term plus 1X, 2X and 3X rotor angular velocity components in the diagonal<br />
stiffness terms and 1X, 2X and 3X rotor angular velocity components in the <strong>of</strong>f-diagonal stiffness<br />
terms.<br />
3. Approximating the Equations <strong>of</strong> motion<br />
<strong>The</strong> analysis may be performed in fixed or rotating coordinates. If the bearings and foundations are<br />
axi-symmetric then the stator dynamic stiffness will appear constant in the rotating frame, and there<br />
is some benefit in analysing the machine in rotating coordinates. Typically foundations will be