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Bearing and shaft misalignments in large turbomachinery: |
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Whereas flexible couplings somewhat allow subsequent bearing
motions after cold alignment, rigid couplings are mere extensions of shafts.
Hot misalignment causing bearing relative motion results in alternate stresses
developing at the surface of shaft ends
In the following discussion, one assumes that shaft radial alignment
is always perfect. With rigid couplings, this is mandatory to avoid vibrations
due to the crankshaft syndrome, as shown left and introduces unbalances.
This can be observed with pairs of eddy probes targeting coupling rims.
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When a single horizontal shaft rests on its two bearings, it bends.
As a result its shaft ends are no longer horizontal and the coupling faces
are no longer vertical. If one neglects their own weight including the
coupling halves belonging to them, they are straight. This assumption is
almost true in turbomachinery where the shaft weight is concentrated between
bearings.
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Bearings pedestals may or may not move after cold alignment. The thickness of oil films in sleeve bearings will vary anyway. As a result, shaft ends will normally undergo some bending. The issue of hot misalignment can best be treated via the basic theory of material strength applied to beams. Surprisingly textbooks dealing over shaft alignment never mention this evidence. Yet this tremendously helps design devices to measure angular shaft misalignment directly. Beam material strength and hot misalignment. The left-hand side figure represents the shaft ends on its two nearest bearings A and B, first when aligned in cold condition (upper part) and then misaligned in cold condition (lower part). L is the distance between bearings When aligned, shaft ends are oriented along aa’. Their center line is straight. Bearing B was raised by ya(L) to bring coupling faces to be parallel, where is the axial distance between the bearings A and B nearest to the couplings on either side. The positions of the centers of the shaft cross-sections in a Cartesian system (x, y(x)) of coordinate whose origin coincides with the center of the cross-section containing bearing A. Another system used to described the motion of bearings is obtained by shifting the previous system by -r vertically, where 2r is the diameter of the shaft ends. Without impairing the generality of the reasoning, one assumes that cross-sections do not vary over the span of shaft ends. In cold aligned condition, y(x) = ya(x) = (slope of aa’) . x, expressing that shaft ends are straight. Reactions of bearings A and B are both w/2. Distance ya(L) in the bearing system coordinates is the amount by which bearing B was raised to obtain a good cold alignment. In hot misalignment, let bearing B rise Dy(L) while bearing remains in the same position. The center line of shaft ends bends. Bearing A unloads by Dw which is transferred to bearing B. A shear force transits through the shaft ends which undergo a linearly varying bending moment. The center line of shaft ends bends. The center line is characterized by y(x) = ya(x) + Dy(x) · what is the amount of the load exchange Dw · what is the amount Dy(L) by which one should misalign shaft in cold condition so that they would be aligned in hot conditions. |
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Extensometry and hot misalignment: Shaft alternate stresses.
Shaft alternate stresses may not be a safety issue but
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etc. |
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There a shaft line is composed of various rotors linked with rigid couplings rests on multiple bearings b1 to b10. When aligning shaft ends, one loosens couplings. Then one lowers the heaviest rotor on its bearings. It sags. Its shaft ends are no longer horizontal. At mid span, gravity causes a typically 20MPa surface stress. The neighboring rotor is then laid down. Its bearings are displaced to bring its coupling rims to be concentric with those of the former rotor. If one also brings faces to be parallel, one ends up with a shaft line bending like the aa’ catenary. In practice, one anticipates the action of vacuum that tends to lower the bearings belonging to the L(ow) P(ressure) rotors LP1, LP2 and LP3. One lifts the catenary from aa’ to cc’ to allow it to descend to hh’ in nominal operation at maximum vacuum, not far away from the ideal catenary aa’ characterized by zero alternate stresses in shaft ends between rotors and no load transfer DW between (selfish) neighboring bearings. In the process, bearing self-alignment should operate properly from cc’ to hh’ (ask manufacturers about it, you are in for a big surprise) . With faces bolted together, a subsequent motion of the bearings supporting the shafts is opposed (or favored in case of misalignment anticipation) by the rigid coupling. Bending moments vary in shaft ends. One can track them with shaft plane stresses and strains (b) to (c). Alternate strains e(x) and -e(x) can be measured with a strain gauge S on the surface of shaft ends. They bring along a heavy and costly instrumentation. Thus, bearing misalignments get cast as a problem of beam (shafts are rotating beams) material strength. This has been all along in the minds of shaft designers who consider bearing alignment to be good provided alternate stresses do not exceed 20MPa in shaft ends (40 in stress concentration zones like fillets). And yet nobody measures these alternate stresses in practice relying on some kind of model of thermal growth to anticipate bearing motions from a cold start to full operation! What about if this model fails??? |