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Balancing in one or two planes: how to choose the number of correction planes

A fan starts humming after the impeller is cleaned. You've arrived with the instrument, fitted the sensors, and the first real question comes up: balance in one plane, or two? The answer decides how many runs you'll make and whether you get a result at all. Below: the L/D rule, an explanation of couple imbalance, and the signs that tell you one weight won't be enough.

Updated 27 August 2026 · by AXILINE · Vila Nova de Gaia

In short: Work out the L/D ratio. L is the rotor's working length — more precisely, the distance between the available correction planes (the cross-sections of the rotor where a weight can be fitted). D is the diameter in the zone where the weight is mounted. At L/D below 0.5, the rotor behaves like a disc, and one plane is usually enough. At L/D above 0.5, use two, or the couple component of the imbalance will remain and the second bearing will keep shaking. Make the final call not from the formula but from the two 1x vectors at both bearings. 1x is the vibration at the rotor's rotation frequency; the instrument shows its amplitude and phase — the angle at which the vibration peak arrives within each revolution. Similar phases at both bearings point to a static imbalance, a difference of around 180° points to a couple.

Static and couple imbalance: why one mass sometimes can't do the job

Imbalance is classified by how the extra mass sits along the rotor's axis. This isn't an academic distinction. It's exactly what decides whether you fit one mass or two.

You'll see static imbalance on a stopped machine. The center of mass is offset from the rotation axis, and a rotor placed on knife-edges will turn itself until the heavy spot settles at the bottom. When it spins, one uncompensated centrifugal force appears. One weight in one plane cancels it out.

Couple imbalance doesn't show up at rest. Picture two equal masses sitting in different planes along the rotor's length, on opposite sides of the axis. Gravity balances them out, and the rotor sits still on the knife-edges. Spin it up, and the centrifugal forces from these masses turn out equal in magnitude and opposite in direction, but applied at different points along the shaft. They don't lie on the same line, so they don't cancel each other out. Instead they form a couple — a moment. That moment rocks the rotor around its center of mass: bearing 1 moves up while bearing 2 moves down at the same instant.

From there it's simple mechanics. Only a pair of forces creates a moment. A single weight produces one force, not a pair. Fit it to calm the first bearing, and the second one gets worse. You've simply pushed the vibration from one end of the rotor to the other. A moment is cancelled by a moment: two weights, spaced along the rotor's length and pointed in different directions.

In real life, two unbalanced masses are rarely equal, so you almost always end up with a mix of static and couple imbalance. That's what's called dynamic imbalance. For a rotor that stays rigid at operating speed, it's a proven fact: two weights in two spaced-apart planes are always sufficient. One plane is just the special case where there's practically no couple component.

Static

The center of mass is offset from the axis. Shows up at rest. One force, one weight, one plane. Typical of narrow disc-shaped rotors: a grinding wheel, a thin pulley, a brake disc.

Couple (paired)

A pair of equal masses in different planes, on opposite sides of the axis. Not visible at rest. Produces a moment that rocks the rotor. Only removed with two weights in two planes.

Dynamic

A mix of the first two — the usual real-world case. Requires two correction planes. The instrument calculates both weights at once, solving a system of equations with a 2x2 matrix of influence coefficients — the sensitivity of each bearing to a weight in each plane.

How this looks on the screen. A typical picture of a dominant couple: the bearing on the coupling side shows 7.8 mm/s at a phase of 32°, the opposite bearing 6.9 mm/s at a phase of 211°. The amplitudes are close, the phases are almost 180° apart. If the phases are close and the amplitudes comparable instead, you're looking at a static imbalance. The numbers here are illustrative, but the phase relationship works as a reliable indicator.

The L/D rule: a one-minute calculation

The rotor's shape tells you whether a moment even has a lever arm to work with. A moment is a force multiplied by a distance. A thin disc has almost no distance, so the resulting moment is small. An elongated rotor has a lever arm, and a moment appears from any asymmetry along its length.

Determine two values. L is the rotor's working length — more precisely, the distance between the two planes where you can actually fit a weight. D is the diameter in the zone where the weight is mounted, at the correction radius. Not the shaft diameter. Not the machine housing's overall size. The diameter where the mass will actually sit.

Then divide one by the other and check the table.

L/DRotor shapePlanesTypical examples
up to 0.3thin disconegrinding wheel, clutch disc, thin pulley, circular saw blade
0.3-0.5short, disc-likeusually one, but check the second bearingimpeller of a narrow fan, flywheel, brake disc
0.5-2elongated rotortwowide impeller, electric-motor rotor, drum, pump impeller on a shaft
over 2long shafttwo; separately check whether the rotor stays rigid at operating speedscrew conveyor, crusher shaft, driveshaft, long shafting

The 0.5 threshold is a working guide, not a figure from a standard. ISO 21940 classifies rotors by their behavior and by operating speed relative to critical speeds, not by a single geometric ratio. Check the applicable part and edition of the standard for your machine. Use L/D as a first filter, and make the actual decision from the measured vectors.

Between-bearing and overhung rotors: where to put the planes

The mounting geometry determines where the weight can physically go and how strongly the planes interact with each other.

Between-bearing (symmetric) rotor

The rotor's mass sits between two bearing housings. Take the correction planes near the ends of the rotor: at the disc near bearing 1, and at the disc near bearing 2. The farther apart the planes are spaced, the smaller the weight mass needed for the same compensating moment. The planes' influence on each other is moderate.

Overhung (cantilevered) rotor

The wheel is mounted outboard of the bearings, with both bearings on the same side. That's how single-inlet centrifugal fans and overhung pumps are built. Take the planes at the front and back disc of the wheel. The mutual influence is strong: a weight in one plane noticeably changes the readings at both bearings. You can't work this one out in your head — the instrument does the calculation.

When to use two planes regardless of L/D

The reverse situation happens too. The second plane isn't accessible: it's covered by a guard, potted in, or simply out of reach without a strip-down. In that case, work in one plane, reduce what can be reduced, and record honestly in the report that the couple component remains. Sometimes it helps to recalculate the correction weights onto other, accessible planes — the software has that function. But a recalculation doesn't create a lever arm where none exists.

The cost of the question: runs, stoppages, and time

Two-plane balancing follows the three-run method. First you take the baseline vibration reading. Then you fit a trial weight of known mass in plane 1 and make a second run. Then you move the trial weight to plane 2 and make a third run. After that, the software calculates the masses and angles for both planes.

One plane takes just two runs before the calculation. The difference of one run looks small on paper, but on site it's measured not in calculation time but in stoppages: coast-down, lockout, removing the guard, repositioning the weight, reassembly, clearance to start. On a machine with a long coast-down, each cycle can easily eat up 20-30 minutes. That's where the cost of the second plane actually hides.

What's being comparedOne planeTwo planes
Trial runs12
Total runs before calculation2 (baseline and trial)3 (baseline and two trials)
Repositioning the trial weightnot neededneeded, from plane 1 to plane 2
Vibration sensorsone is enough, but two give more informationtwo required
What you're reducingthe static componentthe static and couple components
What you riskthe couple imbalance goes unnoticedone extra stoppage, if there was no couple to begin with

If you service a fleet of identical machines, the three runs are only needed once. The instrument stores the influence coefficients, and on the next identical machine you balance from the saved coefficients with no trial runs at all. Always do a verification run after fitting the weights, and add trim weights (small fine-tuning weights) to the ones already fitted if needed.

How to tell the choice was right

A rough guide for a typical fan on a rigid foundation: a starting level of around 12 mm/s comes down to around 1.5-2 mm/s once the right number of planes has been chosen. This is an expectation, not a guarantee. On a machine with resonance, worn bearings, or a drifting phase, you won't get that result no matter how many planes you use.

If the second bearing got worse after a single-plane correction, don't add a weight at random and don't try to guess an angle. Take fresh baseline vectors at both bearings and move to a full two-plane calculation. Otherwise you'll just be chasing the vibration around the rotor blind.

Where the choice of plane count won't solve anything

Balancing removes vibration caused by an asymmetric mass distribution. It removes nothing else, no matter how many planes you use. Here are the cases where you need to stop and deal with something else instead.

Sources: ISO 21940-11:2016 · ISO 21940-12:2016 · ISO 20816-1:2016 · ISO 13373-3:2015 · ISO 13373-5:2020 · ISO 281:2007

What this looks like on site with AXILINE

The procedure is straightforward. We come to the machine, mount two vibration sensors on the bearing housings, aim the laser tachometer at the mark, and take the baseline picture: speed, overall vibration, the amplitude and phase of 1x at both bearings, and the FFT spectrum (vibration broken down by frequency). We decide one plane or two from the phase difference and the L/D ratio. Then come the trial runs, the correction, the verification run, and, if needed, a small trim-weight top-up.

The Balanset-1A handles both one and two planes. It tells you whether the trial weight was adequate, splits the correction mass across fixed positions (blades or holes), calculates drilling when mass is being removed, displays a polar diagram, recalculates weights onto other correction planes, and stores the results in an archive for the report. The kit fits in a case: two accelerometers, a laser phase sensor, a two-channel USB module with preamplifiers and an ADC, and Windows software.

If you balance regularly, it makes sense to keep the instrument on hand rather than booking a site visit every time. If the case is a one-off or unclear, we'll come and do it ourselves. Balanset instruments are designed and manufactured by engineers who use them themselves on site visits, so on choosing planes, mounting sensors, and troubleshooting a failed run, you get consulting support.

Sources: Balanset-1A manufacturer specification · Balanset-1A operation manual

Frequently asked questions

Can a long rotor be balanced in one plane?

You can try, and you'll reduce the static component. The couple component will remain, because a single weight produces a force, not a pair of forces. You'll see the tell right away: one bearing housing comes into normal range, the other stays where it was or gets worse. At that point, don't guess at an angle — take fresh baseline vectors at both bearings and calculate a two-plane solution.

How do I measure L and D if the rotor has a complex shape?

Take L as the distance between the two planes where you can actually fit a weight, not as the assembly's overall length. Take D as the diameter in the zone where the weight is mounted — roughly twice the correction radius. The shaft diameter and the housing's overall size have nothing to do with this calculation.

How many runs does two-plane balancing take?

Three runs before the calculation: baseline, trial weight in plane 1, trial weight in plane 2. Plus a verification run after fitting the correction weights. If you don't hit tolerance the first time, the instrument will suggest small trim weights on top of what's already fitted — that's one more run. Usually 4-5 runs in total.

Do I need two vibration sensors if I'm balancing in one plane?

For the calculation itself, one is enough. With a second channel you can immediately see what's happening at the far bearing, and catch a couple component before you fit any weight. The Balanset-1A records both channels at once, so the second sensor doesn't cost you any extra runs.

How do I tell couple imbalance from static imbalance using the instrument?

Compare the two 1x vectors from both bearings. Close phases with comparable amplitudes point to a dominant static component. A phase difference of around 120-180° points to a dominant couple. An additional sign of a couple: noticeable axial vibration from the frame twisting. Before drawing a conclusion, check that the three runs repeat. With a drifting phase, this kind of comparison is meaningless.

What do you do if the second correction plane isn't accessible?

Work in one plane, reduce what can be reduced, and note in the report that the couple component remains. Sometimes it helps to recalculate the correction weights onto the accessible planes — the software has that function. But if there's no lever arm between the accessible points, a recalculation won't create one, and the issue becomes a design one: access to a second plane will need to be arranged at the next repair.

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