Surface compression.
Fatigue life 2–5× better.
AMS 2430.
Shot peening creates beneficial compressive residual stress in the surface layer of metal parts by bombarding the surface with small hardened beads. Dramatically improves fatigue life — standard for aerospace springs, landing gear, compressor blades, and fatigue-critical components.
How Shot Peening works.
Shot peening is a cold-working process that bombards a metal surface with small hardened steel, ceramic, or glass beads at high velocity (50–100 m/s). Each bead impact plastically deforms a small area of the surface, creating a thin layer of compressive residual stress. Because fatigue cracks initiate at surface tensile stresses, this compressive surface layer dramatically increases fatigue life — typically 2–5× improvement.
The process is fundamentally different from shot blasting: shot blasting cleans and roughens the surface (high-velocity coarse shot), while shot peening creates controlled residual stress with specific Almen intensity measurement. Shot peening is a specified engineering process with documented parameters — shot size, velocity, coverage, Almen intensity — not just surface cleaning.
Aerospace specification AMS 2430 governs shot peening for aerospace components. Each batch is process-verified using Almen test strips measuring peening intensity. Documented records traceable to specification are standard for aerospace Tier-2/3 suppliers.
Capability specs.
Standard specification for shot peening aerospace components
Typical improvement in fatigue life for peened vs unpeened components
Depth of beneficial residual stress depending on Almen intensity
Almen intensity measured on "A" strips. Higher = deeper residual stress
Standard target — surface completely peened with 2× overlap
Steel shot sizes from small (0.3 mm) to large (0.8 mm)
Ceramic beads for aluminum (no iron contamination), glass for delicate
All metal alloys. Different shot media selected per material
Where Shot Peening excels.
Aerospace springs
Coil springs, leaf springs — fatigue life improvement critical for safety
Landing gear components
High-cycle fatigue aerospace parts — peening required per AMS 2430
Compressor & turbine blades
Jet engine blades — fatigue life + cleaning
Gears
Transmission gears, differential gears — peened tooth flanks for fatigue life
Automotive springs
Coil springs, leaf springs for automotive — peening standard practice
Aircraft structural
Aircraft structural hardware — fatigue improvement for flight-critical parts
Firearm components
Gun components, springs, slides — extended service life
Helicopter rotor
Helicopter rotor components — high-cycle fatigue critical
Torsion bars
Automotive and industrial torsion bars — peened for fatigue resistance
Not suitable for:
Every process has its limits. Being honest about where Shot Peening isn\'t the right answer saves time and money.
- Parts where surface texture matters (cosmetic parts) — peening leaves dimpled texture
- Parts where tight tolerances already achieved — peening alters surface dimensions slightly
- Very thin material — peening intensity can cause warping on thin sections
- Soft materials (annealed aluminum, copper) — compressive layer benefit minimal
- Parts not subject to fatigue loading — no benefit, wasted process cost
Shot Peening questions.
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