A spring spec sheet that lists free length, diameter, wire size, and rate tells you whether the part fits and produces the right force on day one. It tells you nothing about whether that spring still produces the right force at cycle 500,000, and in a facility that runs continuously, cycle 500,000 can arrive inside the first two years of service. Few catalog sheets show fatigue testing data at all, which leaves the engineer to assume the spring holds up or find out the hard way.
Fatigue life is the spec most often left undefined on a spring drawing, because calculating it needs information a standard load-and-deflection datasheet doesn't carry. This guide covers what fatigue life means, how to calculate the stress that drives it, how to turn "24/7 operation" into a real cycle number, and what to put in front of a manufacturer so the rating you get back means something.
Why a Load Rating Isn't a Fatigue Rating
A static load test answers one question: does the spring produce the specified force at the specified deflection? It takes seconds, and a spring can pass it and still fail in service. Fatigue failure is a different mechanism, the progressive growth of a crack under repeated stress cycling, usually starting at a surface flaw or stress concentration, until the part fractures. The spring isn't overloaded; it's loaded within its rated range, repeatedly, until cumulative damage adds up to failure. That's how a compression spring rated for 80 lbs at 0.5" can perform exactly to spec on a bench and still fracture at cycle 120,000 in a rack door opening 40 times a day.
What Determines Whether a Spring Reaches Its Cycle Target
Five variables control fatigue life, and all five belong in the spec rather than left to assumption.
Operating stress range. Fatigue is driven by stress amplitude, the swing between minimum and maximum operating load, not peak load. A spring cycling 20% to 80% of rated load sees a smaller range than one cycling 0% to 100% at the same peak, and smaller range generally means longer life.
Material selection. Different materials behave very differently under repeated stress (see table). The detail engineers most often miss: not every material has an endurance limit. Music wire and some ferrous alloys do; stainless steels, beryllium copper, and most non-ferrous materials don't, so their fatigue life is a finite cycle count at a given stress that has to be designed with margin.
| Material | Typical Application | Fatigue Behavior | Trade-off |
|---|---|---|---|
| Music wire (ASTM A228) | High-cycle, non-corrosive, room temp | Defined endurance limit, effectively unlimited cycles below it | Highest fatigue strength; not for corrosive or hot environments |
| Stainless 302/304 | Humid, corrosive, washdown | No true endurance limit, finite life at any stress | Corrosion resistance outweighs lower fatigue strength |
| 17-7 PH stainless | Combined heat and corrosion | Better than 302/304 after precipitation hardening | Higher material and processing cost |
| Beryllium copper | EMI fingerstock, contact springs | Good for a conductive non-ferrous material | Cost and machinability trade-offs |
| Phosphor bronze | Lower-stress contact springs | Moderate | Lower cost than BeCu |
Spring index (D/d). The ratio of mean coil diameter to wire diameter controls how much coil curvature concentrates stress at the inside of the bend. A lower index raises that concentration and reduces fatigue life, one reason a custom spring can outperform a catalog one of similar rate. Industry practice keeps the index between roughly 4 and 12, because values below 4 produce severe stress concentration at the inner coil and tend to fail early under cyclic loading.
Surface condition. Cracks start at surface imperfections. Shot peening induces residual compressive stress that closes microscopic flaws, and ground ends remove stress risers. Skipping surface treatment to save cost is the most common reason a fatigue-rated spring underperforms.
Operating environment. Heat lowers elastic modulus and accelerates relaxation; corrosion pitting acts as a stress site, and corrosion fatigue can cut cycle life well below clean-room data. HVAC condensation, humidity swings, and cleaning chemicals are exactly those conditions.
Calculating the Stress That Drives Fatigue
Fatigue is evaluated against stress, not load, so the first step is converting operating load into the stress the material experiences. For helical compression and extension springs, the value is torsional shear stress at the inside of the coil:
τ = 8FDK_c / (πd³)
where F is operating load, D is mean coil diameter, d is wire diameter, and K_c is the Wahl correction factor for curvature and direct shear. The correction matters more than it looks: for a typical spring index it raises the true peak stress on the inner coil by roughly 25% above the basic torsional value, and neglecting it in high-cycle work is a direct path to premature failure. For torsion springs, the comparable value is bending stress:
σ = 32MK_b / (πd³)
where M is the applied moment and K_b the bending correction factor. Once stress is known at the minimum and maximum points of the cycle, the amplitude is compared against the material's fatigue strength at the target cycle count, adjusted for mean stress with a Goodman or Soderberg relationship. That comparison, not the static rating, determines whether the spring reaches its cycle target with margin, and it's the calculation a manufacturer should run before quoting, not after the first prototype fails.
Translating "24/7 Operation" Into a Cycle Count
"24/7 operation" describes a duty pattern, not a number, and fatigue life has to be designed against cycles. Take a bracket spring under continuous cooling-fan vibration. A fan at 1,800 RPM produces about 30 cycles per second:
30 × 60 × 60 × 24 = 2,592,000 cycles/day
Over a year that's roughly 946 million cycles, solidly high-cycle, where the only realistic approach is a stress at or below the endurance limit (if the material has one) or a documented finite-life target with substantial margin. Compare a rack access door at 40 cycles/day: over a 10-year life, 40 × 365 × 10 = 146,000 cycles. Two applications, two orders of magnitude apart, and a spring engineered for one is not automatically adequate for the other, which is why a "rated for high-cycle applications" claim alone doesn't tell you what you need.
How to Specify Fatigue Requirements in an RFQ
State the duty cycle in cycles, not adjectives. Convert frequency, hours per day, days per year, and product life into a target cycle count.
Provide the full load and deflection range, not just the peak. Fatigue depends on stress amplitude across the cycle; 20 to 80 lbs is a different problem than 0 to 80 lbs at the same peak.
Describe the environment in numbers. "65 to 85°F, 40 to 60% RH, periodic isopropyl alcohol contact" is something a material selection can be made against.
Define the failure criteria before testing. Fracture, or a set percentage of load loss? The two can produce very different cycle numbers for the same part.
Ask what the cycle rating is based on. Dynamic testing of the actual geometry and load range is a documented result; extrapolation from general material data is an estimate. This distinction is widely flagged in spring engineering practice, since surface flaws like pits, seams, or tool marks can severely reduce fatigue life in ways general material data won't capture. Know which one you're getting.
Talk to Katy Spring
Katy Spring & Mfg designs and manufactures custom compression, extension, torsion, and flat springs for data center equipment that has to perform through millions of cycles, not just pass an initial load check. Our engineering team works through the duty cycle, material selection, stress calculations, and surface treatment with you before tooling starts, and we'll tell you honestly when a material or geometry change is the difference between a 150,000-cycle spring and a 1.5-million-cycle spring.
If you're specifying a spring for continuous-duty equipment, request an engineering consultation or send us your fatigue life requirements for a custom quote.
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