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Battery & touch Springs

battery springs

Shapes & Sizes

Common Types

Common Materials

Technical Specification for Battery Spring Material Selection

1. Electrical Conductivity Classification

  • Premium Conductivity Group‌ (σ > 20 MS/m):

    • Gold-plated Beryllium Copper (C17200): Contact resistance <5mΩ, for precision instruments
    • Silver-Nickel Alloy (AgNi10): Current-carrying capacity up to 15A/mm²
  • Economy Conductivity Group‌ (σ 10-20 MS/m):

    • Phosphor Bronze (C51000): 15% IACS conductivity, 30% cost reduction
    • Tin-plated Brass (C26000): Non-corrosive environments only

2. Mechanical Properties Matrix

MaterialElastic Modulus (GPa)Fatigue Limit (MPa)Temperature Range
17-7PH Stainless196620-70~300℃
Inconel 718200550-250~700℃
Beryllium Cu (C17200)131690-200~150℃

3. Electrochemical Compatibility

  • Li-ion Batteries‌: Mandatory Ni/Au plating; prohibit direct copper exposure to electrolyte
  • Alkaline Batteries‌: 316L stainless steel recommended (KOH corrosion resistance)
  • Lead-Acid Batteries‌: Requires Pb-Sn alloy plating

4. Surface Treatment Solutions

  • Standard Treatments‌:

    • Nickel Plating (5-8μm): Salt spray resistance >96h
    • Gold Plating (0.5-1μm): 40% contact resistance reduction
  • Advanced Treatments‌:

    • PTFE Coating: Coefficient of friction <0.1 (sliding contacts)
    • Graphene Coating: 300% thermal dissipation improvement

5. Failure Mode Analysis

  • Stress Relaxation‌:

    • Phosphor bronze: 15% force loss after 1,000h @60℃
    • Beryllium copper: Only 3% force loss under same conditions
  • Fretting Wear‌:

    • Gold plating >0.8μm withstands 50,000 mating cycles

6. Cost Optimization Strategies

  • Bimaterial Design‌: 0.1mm Au layer on contact surface + phosphor bronze substrate
  • Selective Plating‌: Precious metal coating only on critical contact zones

Compliance & Validation

  • Critical applications (aerospace/medical implants) require ‌DOE (Design of Experiments)‌ validation
  • Accelerated aging tests:
    • 85℃/85% RH for 1,000h (JEDEC JESD22-A101)
    • Thermal shock (-55℃⇄125℃, 50 cycles) per MIL-STD-883

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