Diagnostics of steam turbine blades

Inspection is carried out on the convex surface of the blade on the side of steam inlet and outlet. Fig.1 shows the scheme of the blades inspection.

Scanning with the TSC-type instrument sensor is performed in the direction from the blade root section to the peripheral section or conversely.

It is recommended to execute all the blades inspection operations step-by-step for the blades of a specific stage.

In the course of the inspection the TSC-type instrument’s screen displays the graphs of the?Hp?leakage field distribution along the blade length. The inspection results are stored to the instrument’s ROM for their further processing on the IBM-compatible computer.

The blades operating in the most stressed conditions are determined based on the inspection results. These are the blades with the stress and strain concentration lines (SC lines) located transverse to the blade wing and having the maximum?Hpfield gradient:?Kin=dHp/dx. The value of the filed gradient?Kin, characterizing the level of residual stresses in the blade, is determined automatically and displayed on the screen by the operator’s command. The technique for blades inspection, submitted to the Customer, specifies the limiting values of the field gradient, which precede the crack formation.

Fig.1.?The scheme of turbine blades inspection using the TSC-type instrument and the Type 2 scanning device: 1, 2 – flux-gate transducers; 3 – length meter; 4 – connecting cable; 5 – TSC-type instrument; 6 – blades.

Fig.2 shows the results of blades #31, 32 and 33 inspection of stage #33 of the K-300-240 steam turbine low-pressure rotor (LPR) at Konakovo TPS using the metal magnetic memory method. The distribution of the?Hp?field and, accordingly, of the field gradient (dHp/dx) recorded on the blade #31 (see fig.2,?a) characterizes its satisfactory state. It is seen in figures 2,?b?and 2,?c?that the abrupt variation of the?Hp?field and, accordingly, of the field gradient?Kin?was recorded on the blades #32 and #33 at the distance of 180-200 mm from the root. Based on the available experience, such?Kin?values are close to limiting values. It should be noted that the numerical values of?Kin?also depend to some extent on the sensitivity of the inspection instruments used.

Fig.2a.?The distribution of the?Hp?field. Blade #31.

Fig.2b.?The distribution of the?Hp?field. Blade #32.

Fig.2c.?The distribution of the?Hp?field. Blade #33.

Fig.3 shows the lines of the field gradient?Kin?sign alternation, detected during the more detailed measurement of the field on the surface of the blades #32 and #33. As it was pointed out above, according to the technique, these lines correspond to the SC lines, and exactly in these zones occurrence of the blades damaging should be expected. The blades #32 and #33 were replaced, and the metallographic investigation was carried out along the SC lines.

Fig.3.?SC lines detected on the surface of the blades #32 and #33: 1 – SC lines.

The pronounced corrosion-fatigue damaging of the metal, corresponding to the pre-failure state of the blades #32 and #33, can be seen on the structure fragments (magnification ×500) shown in fig.4,a?and 4,b.

It should be noted that the maximum damaging of the metal’s structure was detected in the course of investigations exactly in the zones of the maximum?Hp?field gradient recorded during the inspection near the SC line. The metal’s structure is satisfactory at a distance of just 100 micrometers from the SC line (for example, see the structure fragment shown in fig.4,?c?for the blade #33).

Fig.4a.	Fig.4b.	Fig.4c.

Of the total number of more than 800 LPR blades, inspected using the metal magnetic memory method, only three blades in the pre-failure state were detected. The non-failure operating time of these blades was ~ 200000 hours at the date of inspection.

In the course of the industrial verification of the considered inspection method Energodiagnostika Co. Ltd. accumulated the data bank of the numerical?Kin?values for the blades in the pre-failure state for the last stages of the PT-60-130, K-100, K-200 and K-300 turbines.