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Balance Quality Grade (G-Grade)

📌 Canonical Reference Article — vibromera.eu

The international standard for rotor balancing precision — how ISO 1940-1 and ISO 21940-11 G-grades define permissible residual unbalance, why they matter for bearing life and machine reliability, and how to calculate tolerances for any rotor.

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Calculate permissible residual unbalance per ISO 21940-11 / ISO 1940-1

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Permissible residual unbalance and balancing targets

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Balance Quality Grades at a Glance

From ultra-precision gyroscopes (G 0.4) to coarse reciprocating engines (G 4000) — the complete ISO classification

G 0.4
≤ 0.4 mm/s
Ultra-precision: Gyroscopes, precision spindles, HDD platters, satellite components, microelectronics manufacturing equipment
G 1.0
≤ 1.0 mm/s
Precision: Grinding machine drives, audio and video drives, small high-speed motors, dental/medical equipment spindles
G 2.5
≤ 2.5 mm/s
High-quality: Gas/steam turbines, turbocompressors, high-speed electric motors, machine tool drives, centrifuge rotors
G 6.3
≤ 6.3 mm/s
Standard: Pump impellers, fans, blowers, general electric motors, turbochargers, flywheels, process machinery — the most commonly specified grade
G 16
≤ 16 mm/s
Medium: Drive shafts (cardan), crushers, agricultural machinery, parts of process plant with moderate requirements
G 40
≤ 40 mm/s
General: Car wheels, wheel rims, wheel sets, drive shafts; inherently balanced, elastically mounted crankshaft drives
G 100
≤ 100 mm/s
Coarse: Complete reciprocating engines for cars, trucks and locomotives
G 630+
≤ 630–4000 mm/s
Very coarse: Crankshaft drives, inherently unbalanced, elastically mounted (G 630); crankshaft drives of large, slow marine diesel engines (G 1600–G 4000)
📋 Complete ISO 21940-11 / ISO 1940-1 — Balance Quality Grade Table
G-Grade e·ω (mm/s) Precision Class Typical Rotor Types / Applications
G 40004000Very CoarseCrankshaft drives for large, slow marine diesel engines (piston speed below 9 m/s), inherently unbalanced
G 16001600Very CoarseCrankshaft drives for large, slow marine diesel engines (piston speed below 9 m/s), inherently balanced
G 630630CoarseCrankshaft drives, inherently unbalanced, elastically mounted
G 250250CoarseCrankshaft drives, inherently unbalanced, rigidly mounted
G 100100GeneralComplete reciprocating engines for cars, trucks and locomotives
G 4040GeneralCars: wheels, wheel rims, wheel sets, drive shafts; crankshaft drives, inherently balanced, elastically mounted
G 1616StandardAgricultural machinery; crushing machines; drive shafts (cardan shafts, propeller shafts); crankshaft drives, inherently balanced, rigidly mounted
G 6.36.3StandardAircraft gas turbines; centrifuges (separators, decanters); electric motors and generators (shaft height ≥ 80 mm) of maximum rated speeds up to 950 r/min; electric motors of shaft heights smaller than 80 mm; fans; gears; machinery, general; machine tools; paper machines; process plant machines; pumps; turbochargers; water turbines
G 2.52.5PrecisionCompressors; computer drives; electric motors and generators (shaft height ≥ 80 mm) of maximum rated speeds above 950 r/min; gas turbines and steam turbines; machine-tool drives; textile machines
G 1.01.0PrecisionAudio and video drives; grinding machine drives
G 0.40.4Ultra-precisionGyroscopes; spindles and drives of high-precision systems
📊 Quick-Reference — Pre-Calculated Tolerances for Common Scenarios
Rotor Type Mass (kg) Speed (RPM) Grade Uper Total (g·mm) Uper per Plane (g·mm) eper (µm)
Small electric motor82900G 6.31668320.7
Pump impeller122950G 6.324512220.4
Industrial fan851480G 6.33459173040.7
Large motor rotor3501500G 2.55578278915.9
Steam turbine12003600G 2.5795839796.6
Turbocharger (OEM spec; ISO default is G 6.3)0.890000G 1.00.0850.0420.11
Grinding spindle512000G 1.03.981.990.80
Crusher flywheel500600G 16127,32063,660254.6
Drive shaft (cardan)154500G 1650925533.9
HVAC blower451750G 6.3154677334.4
Car wheel assembly20900G 4084884244424.4
Centrifuge306000G 2.5119603.98
📚 Balancing Standards Comparison — ISO vs. API vs. ANSI vs. VDI
Standard Scope G-Grade System? Key Difference Status
ISO 21940-11:2016All rigid rotors — general proceduresYes (primary)Current international standard; replaces ISO 1940-1Current
ISO 1940-1:2003All rigid rotorsYes (original)Established the G-grade system; still widely referencedSuperseded
ISO 21940-12Balancing procedures and tolerancesYes (references Part 11)Practical balancing procedures, correction plane allocationCurrent
API 610 / 617 / 611Pumps / compressors / turbines (petroleum industry)References ISO; adds stricter limitsOften specifies Uper = 4W/N oz·in (W in lb; equivalent to 6350·W/N g·mm with W in kg, ≈ G 0.67) for API 617 rotors; more conservativeCurrent
ANSI S2.19US-adopted version of ISO 1940Yes (identical)Direct adoption of ISO G-grade system for US marketCurrent
VDI 2060German standard (pre-ISO)Equivalent systemHistorical predecessor to ISO 1940; still referenced in German industrySuperseded by ISO
MIL-STD-167-1US military — shipboard equipmentNo (vibration limits)Specifies vibration amplitude limits, not unbalance tolerancesActive

What is a Balance Quality Grade (G-Grade)?

Quick Answer

A Balance Quality Grade (G-Grade) is an international standard classification per ISO 21940-11 (formerly ISO 1940-1) that defines the maximum permissible residual unbalance for a rigid rotor. The G number represents the maximum velocity of the rotor's center-of-gravity displacement in mm/s. Common grades: G 6.3 for general machinery (pumps, fans, motors), G 2.5 for turbines, compressors and precision equipment, G 1.0 for grinding machine drives and audio/video drives (turbochargers fall under G 6.3 in the ISO table, though OEMs often specify tighter). The formula for permissible unbalance: Uper = 9549 × G × m / n (g·mm), where m = mass (kg), n = speed (RPM).

A Balance Quality Grade, commonly called a "G-Grade," is a standardized classification defined in ISO 21940-11 (which superseded ISO 1940-1) that specifies the maximum permissible residual unbalance for a rigid rotor. The G-grade defines how precisely a rotor must be balanced — not a vibration measurement in the installed machine, but a quality specification for the rotor itself based on its mass and maximum service speed.

The number following the letter "G" represents the maximum permissible velocity of the rotor's center-of-mass displacement, expressed in millimeters per second (mm/s). For example, G 6.3 means the product of the specific eccentricity (eper) and the angular velocity (ω) must not exceed 6.3 mm/s. G 2.5 limits this velocity to 2.5 mm/s. The lower the G number, the tighter the balancing tolerance — meaning higher precision and less permissible residual unbalance.

What the G Number Physically Means

The G value represents the maximum permissible velocity of the rotor's center of gravity relative to the geometric rotation axis, at the maximum service speed. G 6.3 means the center of gravity may move at no more than 6.3 mm/s relative to the spin axis. Since centrifugal force is proportional to this velocity squared, even small reductions in G-grade produce significant reductions in dynamic bearing loads.

The Purpose of the G-Grade System

Before the G-grade system was established, balancing specifications were vague — "balance as well as possible" or "balance until smooth." The ISO G-grade system replaced this ambiguity with a universal, verifiable standard. It provides a common language for manufacturers, service engineers, and end users worldwide. The main objectives are:

1. Limiting Unbalance-Induced Vibration to Acceptable Levels

Unbalance produces centrifugal forces that increase with the square of rotational speed. These forces cause vibration, noise, fatigue loading, and ultimately mechanical failure. By specifying a G-grade, the engineer limits these forces to levels the machine's bearings, seals, and structure can safely tolerate throughout the intended service life.

2. Minimizing Dynamic Loads on Bearings

Bearings are the components most directly affected by unbalance. The cyclic radial load from residual unbalance acts as a fatigue load on rolling elements and raceways. Bearing life (L10) is inversely proportional to the cube of the applied load — so even a modest reduction in unbalance force can dramatically extend bearing service life. Balancing a motor rotor from G 16 to G 6.3 typically doubles bearing L10 life; balancing to G 2.5 can quadruple it.

3. Ensuring Safe Operation at Maximum Design Speed

Centrifugal force from unbalance is proportional to ω² — doubling the speed quadruples the force from the same unbalance. A rotor that is acceptably balanced at 1500 RPM may produce dangerous vibration at 3000 RPM. The G-grade system accounts for this by incorporating speed into the tolerance calculation, ensuring the rotor is safe at its maximum rated speed.

4. Providing a Clear, Measurable Acceptance Criterion

The G-grade converts "balance quality" from a subjective judgment into an objective, measurable pass/fail criterion. After balancing, the residual unbalance is compared against the calculated tolerance. If the measured value is below the limit, the rotor passes. This is essential for manufacturing quality control, contractual specifications, warranty claims, and regulatory compliance.

Calculating Permissible Residual Unbalance

The core of the G-grade system is the ability to calculate a specific, numerical unbalance tolerance for any rotor. Two key quantities are derived from the G-grade:

Specific Unbalance (Permissible Eccentricity)

Permissible Specific Unbalance (Eccentricity)
eper = (9549 × G) / n
eper in µm (micrometers), G in mm/s, n in RPM. Constant 9549 = 60×1000/(2π)

The specific unbalance (eper) represents the maximum permissible displacement of the rotor's center of gravity from the rotation axis, in micrometers. It depends only on the G-grade and the speed — not on the rotor mass. This makes it useful for comparing the balance quality of rotors of different sizes.

Total Permissible Residual Unbalance

Total Permissible Residual Unbalance
Uper = eper × m = (9549 × G × m) / n
Uper in g·mm, G in mm/s, m in kg, n in RPM

The total permissible residual unbalance (Uper) is the actual target the balancing technician must achieve. It is expressed in g·mm (gram-millimeters) — the product of the residual unbalance mass times its distance from the rotation axis. This is the number displayed on the balancing machine and compared against the tolerance.

Centrifugal Force from Residual Unbalance

Centrifugal Force at Tolerance Limit
F = m × eper × ω² = Uper × ω² / 10⁶
F in Newtons, eper in meters, ω = 2π×n/60 in rad/s. Divide by 10⁶ when Uper in g·mm

This formula shows the actual dynamic force the bearings must withstand from the permissible residual unbalance at operating speed. It is useful for verifying that the bearing load rating is adequate and for understanding the real-world impact of the G-grade specification.

Variables Reference

SymbolNameUnitDescription
GBalance quality grademm/sProduct eper·ω; defines the ISO grade (e.g. 6.3, 2.5, 1.0)
eperPermissible specific unbalanceµmMaximum CG offset from rotation axis
UperPermissible residual unbalanceg·mmTotal unbalance tolerance = eper × mass
mRotor masskgTotal mass of the rotor being balanced
nMaximum service speedRPMHighest speed at which the rotor will operate
ωAngular velocityrad/s= 2π × n / 60
FCentrifugal forceNDynamic force from residual unbalance at speed

How to Select the Right G-Grade

The ISO standard provides recommendations for hundreds of rotor types, but in practice the selection depends on several interrelated factors:

Machine Type and Application

The standard groups rotors by application and recommends a G-grade for each group (see the ISO table above). A high-speed turbine needs much tighter balance (G 2.5 or G 1.0) than a slow-speed agricultural mechanism (G 16 or G 40). The designer considers how sensitive the machine is to vibration and what the consequences of unbalance-induced failure would be.

Rotor Speed

Speed is the single most important factor. For the same G-grade, permissible unbalance (Uper) decreases linearly with speed. A rotor at 6000 RPM has half the tolerance of the same rotor at 3000 RPM. For high-speed rotors (turbines, turbochargers, grinding spindles), the tolerance becomes extremely small, requiring specialized balancing equipment and procedures.

Bearing Type and Support Stiffness

A rotor on a rigid foundation typically requires tighter balance than one on flexible (elastic) supports, because soft mounts transmit less of the unbalance force to the structure. ISO 21940-11 reflects this: the same inherently balanced crankshaft drive is assigned G 16 when rigidly mounted but G 40 when elastically mounted. Similarly, rotors on fluid-film bearings may tolerate more unbalance than those on rolling-element bearings due to the damping effect of the oil film.

Environmental and Safety Requirements

Equipment operating near personnel (HVAC, medical devices), in noise-sensitive environments, or in safety-critical applications (power generation, aviation, offshore) may require tighter balance than the standard recommends for the rotor type. Some industries (petrochemical, power generation) have their own standards (API, IEEE) that specify tighter limits than ISO.

Industry-Specific Recommendations

Industry / ApplicationTypical G-GradeNotes
Power generation (turbines)G 1.0 – G 2.5API 612/617 often specifies even tighter than ISO
Petroleum / chemical (pumps, compressors)G 2.5 – G 6.3API 610 pumps often G 2.5 or tighter
HVAC (fans, blowers, AHU)G 6.3Noise-sensitive installations may require G 2.5
Pulp & paper (rollers, dryers)G 6.3 – G 16Large slow rollers; high mass compensates for lower precision
Mining & minerals (crushers, screens)G 16 – G 40Harsh environment; moderate precision acceptable
Automotive (wheels, driveshafts)G 16 – G 40NVH requirements may tighten beyond ISO minimum
Machine tools (spindles, drives)G 1.0 – G 2.5Surface finish quality depends on spindle balance
Marine (propeller shafts, engines)G 6.3 – G 40Classification society rules (DNV, Lloyd's, ABS) apply
Wind energy (rotor hubs, generators)G 6.3Blade pitch imbalance handled separately from hub balance
Aerospace (turbofan, gyros)G 0.4 – G 2.5Extremely tight; military standards (MIL-STD) may override ISO

Two-Plane Balancing — Distributing the Tolerance

The total permissible unbalance Uper calculated from the G-grade formula is for the entire rotor. In practice, most rotors are balanced in two correction planes (dynamic balancing), so the tolerance must be apportioned between the planes.

ISO Guidance for Tolerance Distribution

  • Symmetric rotors (CG approximately at midspan): Divide Uper equally between the two planes. Each plane gets Uper/2.
  • Asymmetric rotors (CG offset toward one end): Distribute proportionally to the bearing distances from the CG. The plane closest to the CG receives the larger share of the tolerance.
  • Single-plane balancing: The entire Uper applies to the single correction plane. This is appropriate for narrow disc-shaped rotors (L/D < 0.5) where couple unbalance is negligible.
Important: Don't Double the Tolerance

A common error is to calculate Uper and then apply this value to each plane, effectively doubling the total tolerance. The correct approach: Uper is the total; divide it between planes. Each plane receives Uper/2 for a symmetric rotor.

Worked Examples

Example 1: Centrifugal Pump Impeller

Given: Pump impeller, mass = 12 kg, operating speed = 2950 RPM, required grade G 6.3.

Step 1 — Specific unbalance: eper = 9549 × 6.3 / 2950 = 20.4 µm

Step 2 — Total tolerance: Uper = 20.4 × 12 = 245 g·mm

Step 3 — Per plane (symmetric): 245 / 2 = 122 g·mm per plane

Step 4 — Correction weight: At correction radius R = 100 mm: weight = 122 / 100 = 1.22 grams per plane maximum

Step 5 — Centrifugal force: ω = 2π × 2950/60 = 308.9 rad/s. F = 245 × 10⁻⁶ × 308.9² = 23.4 N — well within bearing capacity.

Example 2: Large Industrial Fan

Given: Fan rotor, mass = 85 kg, operating speed = 1480 RPM, required grade G 6.3.

Step 1 — Specific unbalance: eper = 9549 × 6.3 / 1480 = 40.6 µm

Step 2 — Total tolerance: Uper = 40.6 × 85 = 3,455 g·mm

Step 3 — Per plane: 3,455 / 2 = 1,728 g·mm per plane

Step 4 — Correction weight: At R = 400 mm: weight = 1728 / 400 = 4.3 grams per plane maximum.

Practical note: This fan can be balanced in the field using a Balanset-1A portable balancer with the rotor installed. The device automatically calculates the G 6.3 tolerance based on rotor mass and speed.

Example 3: Automotive Turbocharger

Given: Turbine wheel, mass = 0.8 kg, max speed = 90,000 RPM, required grade G 1.0 (typical OEM specification for high-speed turbochargers — tighter than the ISO 21940-11 default of G 6.3).

Step 1 — Specific unbalance: eper = 9549 × 1.0 / 90000 = 0.106 µm — about 100 nanometers!

Step 2 — Total tolerance: Uper = 0.106 × 0.8 = 0.085 g·mm

Step 3 — Correction weight: At R = 20 mm: weight = 0.085 / 20 = 0.004 grams (4 milligrams!) per plane maximum.

Practical note: This extremely tight tolerance requires specialized high-speed balancing machines with sub-milligram resolution. Material removal (grinding/drilling) is typically used rather than adding weights at this precision level.

Historical Context — ISO 1940-1 to ISO 21940-11

The G-grade system has evolved through several iterations:

  • VDI 2060 (1966): The original German standard that established the concept of balance quality grades. Developed by the Verein Deutscher Ingenieure (Association of German Engineers).
  • ISO 1940 (1973, rev. 1986, 2003): International adoption of the VDI 2060 concept. ISO 1940-1:2003 "Mechanical vibration — Balance quality requirements for rotors in a constant (rigid) state" became the worldwide reference for G-grades.
  • ISO 21940-11:2016: The current standard. Part of the comprehensive ISO 21940 series covering all aspects of rotor balancing. Part 11 specifically covers balance quality requirements and replaces ISO 1940-1. The G-grade values and application tables remain essentially the same; the main changes are editorial and structural.

Despite the formal supersession, "ISO 1940" remains the most commonly used reference in industry conversations, purchase specifications, and equipment manuals. Both designations refer to the same G-grade system.

Common Mistakes in Applying G-Grades

Mistake 1: Using Balancing Speed Instead of Service Speed

The G-grade tolerance must be calculated using the maximum service speed (operating speed), not the balancing machine speed. Many rotors are balanced at a lower RPM than their service speed. Using the balancing speed in the formula produces a tolerance that is too loose for the actual operating conditions. The Balanset-1A software allows you to enter the service speed separately from the balancing speed to avoid this error.

Mistake 2: Confusing G-Grade with Vibration Level

G 6.3 does NOT mean the installed machine will vibrate at 6.3 mm/s. The G value is a property of the rotor alone, measured or calculated as a free-body tolerance. The vibration of the installed machine depends on many additional factors: bearing condition, alignment, structural natural frequencies, damping, and more. A rotor balanced to G 6.3 may produce 1 mm/s vibration in one machine and 4 mm/s in another, depending on the installation.

Mistake 3: Over-Specifying the Grade

Specifying G 1.0 for a slow-speed fan that only needs G 6.3 wastes time and money. Tighter grades require more balancing iterations, more precise equipment, and longer balancing times. Specify the grade appropriate to the application — better balance than needed provides diminishing returns while increasing cost.

Mistake 4: Applying Total Tolerance to Each Plane

As noted above, Uper is the total tolerance for the rotor. For two-plane balancing, divide by 2 (or distribute proportionally for asymmetric rotors). Applying Uper to each plane doubles the actual total tolerance, potentially exceeding the intended grade.

Mistake 5: Ignoring Temperature and Assembly Changes

Some rotors change balance state between cold (ambient) and hot (operating) conditions due to thermal distortion, centrifugal growth, or fit changes. A rotor that meets G 2.5 on the balancing machine at room temperature may exceed this tolerance at operating temperature. For critical rotors, high-speed balancing at or near operating conditions is recommended.

Mistake 6: Neglecting Key and Keyway Convention

ISO 21940-11 specifies that the half-key convention should be used when balancing a rotor with a keyway (add a half-key to the keyway during balancing to approximate the installed condition). Using a full key, no key, or ignoring this convention introduces an initial unbalance error that may be significant for tight G-grades.

Why G-Grades Matter — The Business Case

Proper application of G-grades delivers measurable benefits:

  • Bearing life: Bearing L10 life is proportional to (C/P)³ where P includes the unbalance force. Reducing unbalance by half can increase bearing life by up to 8× (2³ = 8). This translates directly to reduced maintenance costs and downtime.
  • Energy efficiency: Unbalance-induced vibration dissipates energy as heat in bearings, seals, and dampers. Well-balanced rotors run cooler and consume less power — typically 1–3% energy savings on industrial motors.
  • Noise reduction: Vibration from unbalance transmits through the structure and radiates as noise. Meeting the correct G-grade is often the most cost-effective way to comply with workplace noise regulations.
  • Standardization and interoperability: The G-grade system ensures that a rotor balanced by Manufacturer A meets the same quality standard as one balanced by Manufacturer B — essential for global supply chains and interchangeable components.
  • Regulatory compliance: Many industries require documented evidence of balance quality for insurance, warranty, and safety certification. The G-grade provides a universally recognized documentation standard.
Practical Balancing Equipment for G-Grade Compliance

The Balanset-1A portable balancer includes a built-in ISO 1940 / ISO 21940-11 tolerance calculator. Enter the rotor mass, service speed, and desired G-grade — the software automatically calculates Uper, distributes the tolerance between planes, and provides a clear pass/fail indication after each balancing run. The Balanset-4 extends this capability to four-channel measurement for complex balancing setups.


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Frequently Asked Questions — Balance Quality Grades

Common questions about G-grades, ISO 1940, and balancing tolerances

What is the most commonly used Balance Quality Grade?
G 6.3 is by far the most widely specified grade worldwide. It applies to the majority of general industrial machinery: electric motors, pump impellers, fans, blowers, flywheels, and process plant equipment. It provides a practical balance between manufacturing cost and vibration performance for equipment operating at typical industrial speeds (750–3600 RPM).
What is the difference between ISO 1940-1 and ISO 21940-11?
ISO 21940-11:2016 supersedes ISO 1940-1:2003. Both define exactly the same G-grade system — the G values and application tables are identical. ISO 21940-11 is part of the comprehensive ISO 21940 series covering all aspects of rotor balancing (terminology, procedures, tolerances, machines, instrumentation). The change is primarily organizational and editorial, not technical. In practice, most engineers still say "ISO 1940" when referring to G-grades, and both references are universally understood.
Does the G-Grade equal machine vibration level?
No. This is one of the most common misconceptions. The G value is a property of the rotor alone — it defines the permissible unbalance of the free rotor, not the vibration of the installed machine. G 6.3 does NOT mean the machine will vibrate at 6.3 mm/s. The actual installed vibration depends on bearing condition, alignment, structural natural frequencies, foundation stiffness, and damping. A rotor balanced to G 6.3 might produce anywhere from 0.5 to 5 mm/s in different machines.
How do you calculate permissible residual unbalance?
Use the formula: Uper (g·mm) = (9549 × G × m) / n, where G is the grade (mm/s), m is rotor mass (kg), and n is maximum service speed (RPM). Example: a 25 kg rotor at 3000 RPM, grade G 6.3 → Uper = (9549 × 6.3 × 25) / 3000 = 502 g·mm total. For two-plane balancing, each plane gets 502 / 2 = 251 g·mm. The Balanset-1A software performs this calculation automatically.
What G-Grade for pumps, fans, and electric motors?
ISO 21940-11 recommends G 6.3 for standard industrial pumps, fans, blowers, and general electric motors. Critical service pumps per API 610 often require G 2.5. HVAC fans in noise-sensitive locations (hospitals, offices) may also warrant G 2.5. Large, slow fans (<600 RPM) can sometimes use G 16. Turbine-driven pumps and high-speed compressors: G 2.5 or G 1.0.
Should I use balancing speed or operating speed in the formula?
Always use the maximum operating (service) speed — the highest speed at which the rotor will run in actual service. This is a common and dangerous mistake: many rotors are balanced on machines at lower speeds than they will operate in the field. Using the balancing speed produces a tolerance that is too loose. For example, if a rotor operates at 3600 RPM but is balanced at 600 RPM, the tolerance calculated at 600 RPM would be 6× too generous.
Can I balance in the field to an ISO G-Grade?
Yes. Modern portable balancing equipment like the Balanset-1A enables field balancing to ISO G-grade standards without removing the rotor from the machine. The device measures vibration amplitude and phase, and its built-in software calculates the required correction weights for single-plane or two-plane dynamic balancing. It includes an automatic ISO 1940 / ISO 21940-11 tolerance calculator with pass/fail indication.
What about balancing quality for flexible rotors?
The G-grade system (ISO 21940-11, formerly ISO 1940-1) applies specifically to rigid rotors — rotors that operate well below their first critical speed. Flexible rotors (those operating above or near their first critical speed, such as large turbogenerators) require modal balancing techniques covered by ISO 21940-12. The G-grade can still be applied as an initial low-speed balance target, but additional high-speed balancing runs at or near operating speed are necessary.

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