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NADCAP Process — AMS 2430 / AMS 2432 — Worldwide Operations

Shot
Peening

Processes — Shot Peening

Controlled shot peening using calibrated media (steel, ceramic, glass) under high pressure or wheel blast. Induces residual compressive stresses that delay fatigue crack initiation and propagation. Our processes are NADCAP qualified and compliant with AMS 2430 / AMS 2432 / OEM specifications.

Applicable standards

AMS 2430AMS 2432Mil-S-13165BAC 5730

How it works

How it works

Shot peening consists of bombarding the surface of a metal part with calibrated media (steel, ceramic, glass) projected at high velocity by a centrifugal wheel or compressed air jet. Each impact causes highly localized plastic deformation at the surface: the underlying material resists, and the end result is a residual compressive stress field that impregnates the first 150 to 400 microns of the part.

These compressive stresses delay the initiation of fatigue cracks (which preferentially start in tension) and slow their propagation. The fatigue life gain is typically ×2 to ×5 depending on the material, geometry and loading mode. Shot peening does not consume material, does not significantly alter dimensions, and applies equally to new parts and to parts under maintenance.

The master parameters — Almen intensity (transferred energy), coverage (percentage of surface impacted) and media selection — are monitored and documented at every intervention per AMS 2430 (automated process), AMS 2432 (manual process) or AMS 2546 (ultrasonic peening).

Typical applications

Typical applications

Engine turbine disks and blades

LCF (Low Cycle Fatigue) life extension on Inconel 718 and Ti-6Al-4V disks. Typical intensities 12-18A.

Aircraft landing gears

High-strength steel structures (300M, 4340). Fatigue prevention on lugs and clevises. Intensities 10-16A.

Transmission gears and pinions

Case-hardened steels, shot-peened at tooth root. Automotive, railway and wind applications. Intensities 8-14A.

Suspension and helical springs

Two-stage process (high energy + finish) for performance automotive and railway springs.

Aircraft fastener holes

Life extension after cold working, or alternative to cold working for large-diameter holes.

Naval and offshore welds

Shot peening or HFMI (preferred) on critical welds — wind-turbine jackets, marine structures.

High-performance fastener components

Titanium and Inconel bolts — thread/head junction zones, typical fatigue initiation points.

Forming tools and dies

Surface fatigue resistance improvement on forging, stamping and injection tooling.

Parameters by material

Parameters by material

MaterialAlmen intensityMedia typeCoverage
Aluminum 2024-T3 / 7075-T66-10AGlass or ZrO₂ ceramic100-200%
Titanium Ti-6Al-4V8-14AZrO₂ ceramic200%
Inconel 71812-20AConditioned steel S330/S460200%
Aerospace steels 300M / 434010-16AConditioned steel100-200%
Case-hardened steels (gears)8-14ASteel S170/S280100%

Media selection is critical: conditioned steel for classic steels and hard alloys, ZrO₂ ceramic for titanium and applications where metallic embedment is prohibited, glass for light alloys and cosmetic applications. Media hardness must be greater than or equal to the treated material's hardness to deliver efficient energy transfer.

Frequently asked questions

Frequently asked questions

What is the difference between shot peening and shot blasting?+
Shot peening is a controlled mechanical process aimed at generating residual compressive stresses. Shot blasting is a cleaning or surface-preparation process — energy, media and controls differ. Shot peening = fatigue function; shot blasting = cleanliness/roughness function.
How long does a typical shot peening treatment take?+
For a medium-sized aerospace part (e.g. landing gear), between 30 minutes and 3 hours of net treatment, plus preparation (masking), intensity/coverage checks and documentation. Allow 1 to 2 days for a full workshop batch.
Does shot peening alter the part dimensions?+
Dimensional variation is small but non-zero. On thin parts, shot peening produces plastic deformation that may result in slight bowing. Our procedures include post-peening dimensional checks and, if needed, compensating peen-forming.
What certifications are required to operate?+
NADCAP Heat Treatment for aerospace, EN 9100 / AS9100 for quality management, SAE J2277 operator level 2 minimum, and specific OEM qualifications (Airbus, Boeing, Safran, GE, Rolls-Royce) depending on the parts processed.
Can shot peening be performed on an already assembled part?+
Yes, for accessible zones and with adequate protection of non-concerned zones. Manual flapper peening is particularly suited to interventions on assembled parts or on whole aircraft. Our 24/7 AOG team operates on-wing worldwide.
What is the typical fatigue life gain?+
×2 to ×5 depending on material and loading mode. On aluminum aerospace parts under variable loading, the typical factor is ×3 to ×5. On nickel-base superalloys, ×2 to ×3 is common. Justification calculations are performed by our structures engineering office.

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