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Statically equivalent vector distribution

Correction-Unbalance Decomposition

Distribute one supplied add-mass correction-unbalance vector at the CG between two planes while conserving the resultant vector and its axial first moment.

Input U in g·mmKnown plane radiiStatic component only

Applicabilita: the supplied vector is an add-mass correction vector acting at the CG, which lies between the two planes. Both output vectors therefore use the same angle. This does not derive a dynamic two-plane correction from vibration data and does not represent a couple component or a CG outside the planes.

Equivalent plane corrections

Plane 1 correction
Plane 2 correction
U₁
U₂
Resultant check U₁+U₂
CG moment residual −U₁L₁+U₂L₂

U₁+U₂=U;   −U₁L₁+U₂L₂=0
U₁=U L₂/(L₁+L₂);   U₂=U L₁/(L₁+L₂)
m₁=U₁/R₁;   m₂=U₂/R₂

The first two equations conserve the correction-unbalance resultant and the axial first moment about the CG. Dividing g·mm by mm gives correction mass in grams. The angle is normalized to [0°,360°).

These equilibrium equations are general mechanics, not a formula claimed from ISO. ISO 21940-11:2016 con Amd 1:2022 addresses procedures/tolerances for rotors with rigid behaviour, including correction-plane requirements and tolerance allocation; flexible rotors are excluded. ISO 21940-13:2012 addresses criteria/safeguards for in-situ balancing and explicitly does not provide methods for calculating correction masses from vibration data.

Do not substitute this split for influence-coefficient balancing: measured bearing response, cross-effect, rotor flexibility and couple unbalance require the appropriate one-/two-plane balancing procedure and safe trial-weight practice.

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Equivalent static-vector distribution only. Scientific review: July 2026.

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