Generator shafts connect the turbine to the generator rotor. They need a through-hole for the rotor assembly tie bolts and for cooling air circulation. The shaft is typically 4-8 meters long with a 100-300mm bore depending on the generator size. In my experience, the bore quality directly impacts rotor balance and cooling efficiency, both of which affect generator reliability over decades of service.

Material Selection and Forging Considerations

The material is usually a high-strength steel forging like 25CrMo4 or 34CrNiMo6. The shaft weight can be 10-30 tons. The bore concentricity requirement is typically within 0.5mm of the shaft centerline.

I have worked with several forging grades for generator shafts. Here is how they compare:

GradeYield Strength (MPa)Hardness (HB)WeldabilityTypical Generator Size
25CrMo4500-650200-250GoodSmall to medium (50-150 MW)
34CrNiMo6700-850250-320FairMedium to large (150-400 MW)
30Cr2Ni4MoV600-750240-290PoorLarge turbine-generators (400+ MW)
26NiCrMoV14-5650-800260-310PoorHigh-speed generators

The forging process creates directional grain structure in the shaft. I have found that the bore should be drilled parallel to the forging grain direction for best surface finish and tool life. Drilling across the grain increases tool wear by 20-30% and produces a rougher bore surface.

Drilling Parameters and Coolant Management

For a 200mm bore in a generator shaft, here are my standard parameters:

ParameterBTA DrillingNotes
Cutting speed60-80 m/minLower end for harder grades
Feed rate0.10-0.16 mm/revAdjusted based on chip form
Coolant pressure300-500 psiHigher for deeper holes
Coolant flow400-600 L/minCritical for chip evacuation
Shaft rotation20-50 RPMMatched to tool feed
Stock for finish boring0.5-1.0mmIf specified

BTA drilling is the standard process for generator shaft bores in the 100-300mm range. The BTA head uses multiple carbide inserts arranged around the cutting face, which balances the cutting forces and produces a straight bore. I use a three-insert BTA head for generator shafts because the balanced cutting forces produce the best straightness.

Coolant management is critical at these bore diameters and depths. At 400-600 L/min, the coolant carries the chips back through the annular space between the drill tube and the bore wall. If the coolant flow drops below 350 L/min, chips start accumulating and can pack around the drill head, causing tool jamming.

Workpiece Support and Steady Rest Setup

The main challenge is the length and weight. A 6-meter shaft weighing 20 tons needs careful support. I use steady rests at 1-meter intervals. The shaft rotates at 20-50 RPM during drilling to maintain concentricity.

Steady rest positioning for a 6-meter shaft:

  • Position 1: 0.5m from the drilling head
  • Position 2: 1.5m
  • Position 3: 2.5m
  • Position 4: 3.5m
  • Position 5: 4.5m
  • Position 6: 5.5m

I align each steady rest to within 0.03mm runout before drilling. The alignment process takes about 30 minutes for a 6-meter shaft but is time well spent. A misaligned steady rest will cause the bore to drift and may require scrapping the shaft.

The shaft rotation speed is set so that the surface speed at the bore wall is in the 60-80 m/min range. For a 200mm bore, this is about 95-125 RPM. However, the shaft OD might be 500-800mm, so I have to balance the bore surface speed against the OD surface speed. I keep the OD surface speed below 150 m/min to avoid vibration from the steady rest rollers.

Bore Inspection and Wall Thickness Verification

After drilling, I inspect the bore with a borescope. I also check the wall thickness with ultrasonic testing at multiple points along the length. A wall thickness variation of more than 2mm indicates the bore has drifted off-center.

My ultrasonic inspection grid for a generator shaft:

  • 4 circumferential positions (0, 90, 180, 270 degrees)
  • 8 axial positions (every 0.75m on a 6m shaft)
  • 32 total measurement points

The wall thickness data is plotted to show the bore position relative to the shaft centerline. If the bore has drifted by more than 1mm off-center at any point, I consult with the design engineer to determine whether the shaft can be salvaged with a larger finish bore.

The bore surface finish matters for rotor assembly. The tie bolts pass through the bore, and any burrs or rough spots can damage the bolts during assembly. I target Ra 1.6um as-drilled. If the finish is rougher, I run a burnishing pass to smooth any rough areas.

End Threading and Rotor Assembly Preparation

The shaft ends often have threaded holes for the rotor assembly. I drill and tap these after the main bore is finished. The thread holes need to be concentric with the main bore within 0.2mm for the rotor bolts to align properly.

The threading process:

  1. Locate the thread hole positions using the finished bore as the reference
  2. Drill pilot holes using a jig bushing aligned to the bore centerline
  3. Tap the threads with a spiral-flute tap for chip evacuation
  4. Check thread concentricity using a gauge pin in the thread and a dial indicator on the bore wall

I have found that the threading step causes more rework than any other operation. If the thread holes are misaligned by more than 0.2mm, the rotor tie bolts will bind during assembly. I always do a trial assembly of the thread gauge before sending the shaft to the customer.

Key Takeaways

  • BTA drilling with three-insert heads and 400-600 L/min coolant flow is the most reliable method for generator shaft bores
  • Steady rest alignment to 0.03mm runout at 1-meter intervals prevents bore drift in long, heavy shafts
  • Ultrasonic wall thickness measurement at 32 points confirms bore concentricity within the 0.5mm specification
  • Rotor tie bolt thread holes require a jig bushing referencing the finished bore to stay within 0.2mm concentricity
  • Material grade selection (25CrMo4 vs. 34CrNiMo6) affects tool life and requires speed adjustments of 10-15%