Case study

Vibration Isolator Resonance Transmissibility Case Study

Mechanical engineering case study on rotating equipment vibration isolation, mount stiffness, natural frequency, transmissibility, floor vibration, static deflection, flexible connections, and validation evidence.

This case study follows a supply fan skid that made the supporting floor vibrate after a mount replacement. The fan rotor was balanced, the bearings were healthy, and the motor current was normal. The hidden problem was that the replacement isolators were selected mainly by static load capacity, not by dynamic stiffness. Their natural frequency landed close to the fan running speed, so the mounts amplified transmitted vibration instead of isolating it.

The case teaches a practical mechanical engineering lesson: vibration isolation is not the same as putting a machine on soft-looking pads. The supported mass, mount stiffness, damping, forcing frequency, static deflection, pipe connections, frame flexibility, and validation measurements must work together.

Case Summary

ItemEngineering relevance
MachineBelt-driven supply fan on a skid, installed above occupied technical space.
Operating speed900\ \text{rpm} during normal duty.
SymptomFloor vibration exceeded the site limit while fan casing vibration was moderate.
Initial suspicionRotor imbalance after maintenance.
Actual root causeIsolator natural frequency was close to 1x running speed.
Hidden contributorRigid duct and pipe connections partly short-circuited the isolator system.
Corrective actionLower mount stiffness, add flexible connectors, verify static deflection and operating transmissibility.

The central engineering question was:

Is the floor vibrating because the fan is generating excessive force, or because the support system is amplifying ordinary 1x force?

The evidence pointed to support-system amplification.

Initial Data

Use these simplified investigation values.

QuantitySymbolValue
supported fan skid massm1600\ \text{kg}
number of mounts4
installed stiffness per mountk_m3.2\ \text{MN/m}
total vertical stiffnessk12.8\ \text{MN/m}
estimated damping ratio\zeta0.08
operating speed900\ \text{rpm}
floor vibration limit2.0\ \text{mm/s RMS}
measured floor vibration4.8\ \text{mm/s RMS}
measured fan casing vibration5.5\ \text{mm/s RMS}

The vibration spectrum showed a dominant 1x component at the operating speed. Phase was stable. Bearing fault bands and blade-passing components were not dominant. That made imbalance possible, but the high floor response relative to casing response suggested a support transmissibility problem.

Step 1: Forcing Frequency

Convert running speed to forcing frequency:

\displaystyle f=\frac{900}{60}=15.0\ \text{Hz}

For a rotating machine, a 1x force at shaft speed is common. It can come from residual imbalance, eccentricity, pulley runout, aerodynamic asymmetry, or rotating assembly tolerances. The engineering question is whether the support system attenuates or amplifies that force.

Step 2: Installed Natural Frequency

For a simplified single-degree-of-freedom mounted skid:

\displaystyle f_n=\frac{1}{2\pi}\sqrt{\frac{k}{m}}

Substitute:

\displaystyle f_n=\frac{1}{2\pi}\sqrt{\frac{12.8\times 10^6}{1600}}
\displaystyle f_n=\frac{1}{2\pi}\sqrt{8000}=14.2\ \text{Hz}

The operating forcing frequency was:

15.0\ \text{Hz}

So the speed ratio was:

\displaystyle r=\frac{f}{f_n}=\frac{15.0}{14.2}=1.06

Engineering Comment

This is too close to resonance. For isolation, the forcing frequency should normally be well above the mounted natural frequency. If r is near 1, the isolator system can amplify motion and transmitted force.

Step 3: Force Transmissibility

For a damped single-degree-of-freedom isolator, a common force transmissibility estimate is:

\displaystyle T_R=\frac{\sqrt{1+(2\zeta r)^2}}{\sqrt{(1-r^2)^2+(2\zeta r)^2}}

Using:

\zeta=0.08,\quad r=1.06

gives:

2\zeta r=2(0.08)(1.06)=0.170

Numerator:

\sqrt{1+0.170^2}=1.014

Denominator:

\sqrt{(1-1.06^2)^2+0.170^2}=0.211

Therefore:

\displaystyle T_R=\frac{1.014}{0.211}=4.8

The installed mounts were not isolating the 1x force. They were amplifying transmitted force by roughly a factor of five in the simplified model.

Engineering Comment

The number should not be treated as exact, because real skids have frame modes, uneven mount loads, lateral stiffness, duct connections, and floor flexibility. It is still decisive: the selected mount stiffness placed the system in the amplification region.

Step 4: Static Deflection Check

Static deflection is:

\displaystyle \delta=\frac{mg}{k}

Substitute:

\displaystyle \delta=\frac{1600(9.81)}{12.8\times 10^6}=0.00123\ \text{m}

So:

\delta=1.23\ \text{mm}

That deflection is small for a machine expected to be isolated at 15\ \text{Hz}. Stiff mounts can carry the load, but load capacity alone does not imply isolation performance.

Step 5: Corrected Mount Target

A practical target was to move the mounted natural frequency below:

5.0\ \text{Hz}

That gives a speed ratio:

\displaystyle r_{new}=\frac{15.0}{5.0}=3.0

Required total stiffness:

k_{new}=(2\pi f_n)^2m
k_{new}=(2\pi\cdot 5.0)^2(1600)=1.58\times 10^6\ \text{N/m}

Required stiffness per mount:

\displaystyle k_{m,new}=\frac{1.58\times 10^6}{4}=0.395\ \text{MN/m}

This is much softer than the installed:

3.2\ \text{MN/m}

mounts.

New static deflection:

\displaystyle \delta_{new}=\frac{1600(9.81)}{1.58\times 10^6}=0.0099\ \text{m}

So:

\delta_{new}\approx 9.9\ \text{mm}

Engineering Comment

The corrected design requires more static deflection. That is not a flaw by itself, but it must be checked against alignment, belt tension, guards, seismic restraints, pipe flexibility, startup motion, and maintenance clearance.

Step 6: Corrected Transmissibility Estimate

With:

r=3.0,\quad \zeta=0.08

the transmissibility is:

2\zeta r=0.48
\displaystyle T_R=\frac{\sqrt{1+0.48^2}}{\sqrt{(1-3^2)^2+0.48^2}}
\displaystyle T_R=\frac{1.109}{8.014}=0.138

So the corrected mount selection should transmit only about:

14\%

of the dynamic force in the simplified model.

The improvement ratio compared with the installed condition is:

\displaystyle \frac{0.138}{4.8}=0.029

In an ideal single-degree-of-freedom model, transmitted 1x force would fall to about 3% of the previous value. In the real installation, parallel paths through ductwork, pipework, electrical conduit, frame flexibility, and floor modes limit the achievable reduction.

Step 7: Short-Circuit Path Check

The investigation found that a rigid discharge duct and a tightly clamped drain line were bypassing part of the isolator motion. This matters because a vibration isolator works only if the machine can move slightly relative to the receiver structure.

The corrective package therefore included:

  • flexible duct connector with correct slack and no hard contact at the frame;
  • flexible drain section with strain relief;
  • conduit loop with clearance through the expected static and dynamic motion;
  • snubbers adjusted with clearance so they do not preload the skid in normal operation;
  • alignment check after the new static deflection settled.

Without these checks, softer mounts could still fail because another stiff path would carry force into the floor.

Validation Results

After installing the corrected mounts and flexible connections, the team repeated startup, steady operation, and shutdown measurements.

MetricBefore correctionAfter correctionAcceptance
mounted natural frequency from bump test14.2\ \text{Hz}5.3\ \text{Hz}below 5.5\ \text{Hz}
static deflection1.2\ \text{mm}9.4\ \text{mm}within clearance plan
floor vibration at 900 rpm4.8\ \text{mm/s RMS}0.9\ \text{mm/s RMS}below 2.0\ \text{mm/s RMS}
fan casing 1x vibration5.5\ \text{mm/s RMS}4.7\ \text{mm/s RMS}no new machine fault indicated
duct connector contactintermittent hard contactnone observedpass
startup resonance dwellstrong floor responsebrief controlled passagepass

The measured reduction was smaller than the ideal transmissibility ratio because the real structure had residual parallel paths and floor response. It still met the engineering requirement.

Failure Mode Diagnosis

EvidenceInterpretation
dominant 1x frequencyrotating force was exciting the support system
stable phaseconsistent forcing, not random looseness
natural frequency near running speedmount system was near resonance
low static deflectioninstalled mounts were too stiff for isolation
floor vibration high relative to casing vibrationtransmitted force, not only machine health, controlled the complaint
improvement after softer mounts and flexible connectionssupport transmissibility was the root cause

The diagnosis did not clear the machine forever. It showed that this event was primarily an isolation design and installation problem rather than a bearing or balance failure.

Risk and Maintenance Controls

The team updated the maintenance plan:

  1. replacement mounts must be specified by stiffness, load range, static deflection, damping, temperature, and chemical compatibility;
  2. speed changes must be checked against mounted natural frequency;
  3. flexible connectors must be inspected after maintenance;
  4. vibration acceptance must include both machine casing and receiver structure measurements;
  5. bump-test natural frequency must be recorded after mount replacement or skid modification.

The simplified RPN changed from:

RPN_{before}=6\times 5\times 4=120

to:

RPN_{after}=6\times 2\times 2=24

Severity did not change because excessive floor vibration could still affect occupants, instruments, and fatigue-sensitive supports. Occurrence and detection improved because the new specification and validation checks directly target the failure mode.

Engineering Lessons

  1. A mount selected only by static load can put the machine near resonance.
  2. Isolation requires a speed ratio well above the mounted natural frequency, not simply a compliant material.
  3. Static deflection is a useful quick check because it reflects stiffness.
  4. Ducts, pipes, conduits, snubbers, and frames can short-circuit isolators.
  5. Validation should measure source vibration and receiver vibration; one number cannot diagnose the path.

The transferable lesson is that vibration isolation is a system property. The mount, machine, forcing frequency, floor, attached services, and acceptance measurement must be reviewed together.

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