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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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ductility and poor toughness, since as the creep-rupture strength increases,<br />

so does the fracture appearance transition temperature (FATT). More<br />

recently, toughness has been improved through changes in steel-making<br />

practices, alloy content, heat treatment, and increased steel purity.<br />

Maximizing creep-rupture strength has been relaxed in favor <strong>of</strong> improving<br />

creep ductility. However, creep cracking at the blade attachment areas<br />

continues to be a problem for many operators.<br />

The range <strong>of</strong> service conditions <strong>of</strong> rotors has changed over the years.<br />

Under continuous service at temperatures up to 565 8C (1050 8F), creep<br />

damage was the primary threat to integrity, and considerable long-term<br />

(100,000 hr) creep data have been generated. However, as rotors have<br />

become increasingly subject to cyclic service conditions (load cycling and<br />

full startup/shutdown cycles), other potential damage mechanisms such as<br />

low cycle fatigue and creep-fatigue have been introduced. Startup and<br />

shutdown induce thermal stresses that become a maximum at temperatures<br />

substantially lower than those that occur at steady state. Fracture toughness<br />

becomes the dominant property in the resistance <strong>of</strong> the steel to brittle<br />

fracture.<br />

Fossil and nuclear Lp rotors. Typical damage mechanisms for LP rotors are<br />

(1) low cycle fatigue cracking in the rotor bore, (2) high cycle fatigue<br />

cracking <strong>of</strong> the shaft, (3) stress corrosion cracking <strong>of</strong> discs in areas <strong>of</strong><br />

condensation, especially in shrunk-on disks, and (4) stress corrosion<br />

cracking <strong>of</strong> the blade attachment areas.<br />

Most <strong>of</strong> the potential problem areas on the LP rotor are in regions<br />

where stress concentrations are present. These stress concentrations may be<br />

further aggravated by erosion and/or pitting. Corrosion caused by chemical<br />

pitting at the surface <strong>of</strong> the rotor can lead to crack initiation and subsequent<br />

propagation by rotating bending fatigue (transverse cracking). High levels<br />

<strong>of</strong> concentrated bending stress can exist in the shaft beneath certain disks,<br />

during conditions <strong>of</strong> journal bearing misalignment.<br />

The disk and shaft assembly <strong>of</strong> large LP rotors includes either keys or<br />

locking pins at each shrink-fit interface to prevent rotation <strong>of</strong> the disk<br />

relative to the shaft. Keyways are stress concentrators and provide<br />

interstices for deposition <strong>of</strong> chemical contaminants from the steam. Both<br />

<strong>of</strong> these factors are important in assessing the problems associated with disk<br />

cracking.<br />

As with HP and IP rotors, the LP bores are highly stressed largely by<br />

thermal transients that can lead to low cycle fatigue damage. Unlike the<br />

high-temperature rotors, creep is not a factor because the maximum<br />

temperature <strong>of</strong> operation is below the creep regime, which simplifies<br />

evaluation. However, the older NiMoV and newer NiCrMoV steels are<br />

Copyright © 2003 Marcel Dekker, Inc.

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