| Shaft Taper Ratio | Select the taper ratio specified by the motor, rotor, coupling, or driven equipment drawing. A common machine-shaft taper is 1:10, meaning the diameter changes by 1 mm over 10 mm of axial length. | Verify the large and small diameters and the axial taper length with calibrated micrometers, a taper gauge, or a coordinate measuring machine. | Taper = (Dlarge − Dsmall) / L For a 1:10 taper, the diameter difference is 0.10 mm per 1 mm of axial length. | Do not substitute a Morse, Jacobs, or other standardized tool taper unless the mating component is designed for it. The taper ratio alone does not define the complete fit. |
| Taper Included Angle | For a 1:10 diametral taper, the included angle is approximately 5.72°; the half-angle is approximately 2.86°. | Calculate from the measured taper, or inspect directly with a calibrated optical comparator, CMM, or suitable taper measuring fixture. | Included angle = 2 × arctan(1 / 20) ≈ 5.72° | Angle tolerance, surface finish, and contact pattern must follow the equipment drawing or applicable fit specification. |
| Taper Contact Pattern | The mating hub or adapter should seat evenly over the specified taper length, without rocking, edge contact, burr interference, or visible gaps. | Apply a thin contact-checking medium, assemble without impact, rotate slightly, and inspect the transferred contact pattern. Remove all residue before final assembly. | Acceptable condition: continuous, distributed contact across the designed seating area; localized high spots are corrected before balancing. | A correct nominal diameter cannot compensate for poor contact, contamination, fretting damage, or an incorrect axial seating position. |
| Radial Runout at Taper | Use the equipment drawing as the controlling limit. For general precision rotating assemblies, a practical preliminary inspection limit is often ≤ 0.02 mm TIR at the taper surface, unless a tighter value is specified. | Support the shaft on suitable centers or precision V-blocks, establish the datum axis, and use a calibrated dial indicator or electronic probe while rotating the shaft slowly by hand. | Indicator readings: high point +0.008 mm, low point −0.007 mm TIR = 0.015 mm | TIR means total indicator reading. Measure at more than one axial location because a bent shaft and an angular taper error can produce different runout patterns. |
| Axial Face Runout | Use the drawing limit. A commonly used preliminary target for a precision mounting face is ≤ 0.02 mm TIR, subject to diameter, speed, and bearing arrangement. | Place the indicator tip on the mounting shoulder or flange face at the specified inspection radius and rotate the shaft through one complete revolution. | Indicator variation from minimum to maximum: 0.012 mm TIR | Excessive face runout can create hub wobble, axial misalignment, uneven clamping, and additional couple unbalance. |
| Runout Datum and Setup | The reference axis should represent the functional shaft axis, normally the bearing journals, centers, or specified precision datum surfaces. | Clean the journals, remove burrs, confirm support alignment, and verify indicator zero and probe preload before measurement. | Record: support condition, indicator location, rotational direction, temperature, and measured TIR at each inspection point. | Measuring directly against an unverified V-block, dirty journal, or damaged center hole can produce a false runout result. |
| Dynamic Balance Quality Grade | Balance the complete rotor assembly to ISO 21940-11 Grade G2.5, unless the machine specification requires another grade. | Use a calibrated two-plane dynamic balancing machine at the specified correction speed or a validated equivalent procedure. | Target: G2.5 The balance grade is a permissible vibration velocity value, not a direct runout tolerance. | Balance the rotor in the same configuration used in service, including the hub, key, fan, coupling, or other permanently mounted components where applicable. |
| Permissible Residual Unbalance | ISO 21940 uses the relationship: Uper = 9549 × G × m / n where Uper is in g·mm, G is in mm/s, m is in kg, and n is in r/min. | Calculate the permissible total residual unbalance for the rotor mass and operating speed, then distribute the allowable value between the correction planes according to the balancing setup. | For G = 2.5, m = 10 kg, n = 3000 r/min: Uper = 79.6 g·mm total permissible residual unbalance. | The plane-by-plane limits depend on correction-plane spacing, mass distribution, and the selected balancing convention. |
| Residual Unbalance at Other Speeds | For the same rotor mass and balance grade, permissible residual unbalance is inversely proportional to rotational speed. | Recalculate whenever the rated speed or maximum service speed changes. | For a 10 kg rotor at G2.5: 1500 r/min: 159.2 g·mm 3000 r/min: 79.6 g·mm 6000 r/min: 39.8 g·mm | Do not use the 3000 r/min value for a 6000 r/min rotor without recalculation. |
| Key and Keyway Condition | Inspect the key, keyway, retaining hardware, and any balancing plugs for burrs, looseness, fretting, or incorrect protrusion. | Verify dimensions against the shaft and hub drawings. Balance with the key configuration defined by the applicable standard or equipment specification. | Typical inspection record: key fitted, keyway clean, no rocking, no raised burrs, retaining hardware torqued to specification. | A missing, loose, or improperly represented key can change the mass distribution and invalidate the balance result. |
| Surface Finish and Damage | Taper and journal surfaces must be free from scoring, dents, corrosion, raised metal, and embedded debris. Surface roughness must meet the engineering drawing. | Perform visual inspection and measure surface roughness with a calibrated profilometer where required. Check critical diameters with calibrated instruments. | Reject or rework any damage that prevents full seating or changes the functional taper geometry. | Surface finish limits are application-specific; do not infer a roughness value solely from ISO 21940 balance grade. |
| Final Acceptance Record | Record shaft identification, rotor mass, speed, balance grade, residual unbalance by plane, runout values, instrument IDs, and inspection date. | Compare all results with the approved drawing, balancing report, and applicable safety procedure before release. | Release only when taper fit, runout, mounting condition, and dynamic balance results are all within their respective specified limits. | ISO 21940 Grade G2.5 addresses balance quality; it does not replace dimensional, fit, runout, material, or overspeed requirements. |