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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

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