Structural aerospace parts require high‑strength, fatigue‑resistant steels and alloys with certified quality. Key features include vacuum‑melted materials, full traceability, controlled heat treatment, and extensive non‑destructive testing to ensure product safety.
Structural aerospace parts such as frames, fittings, landing gear elements, and load‑bearing assemblies are subject to extreme mechanical stresses and strict safety regulations. Material requirements are driven by high static and cyclic loads, damage tolerance demands, temperature variation, and long service life. Steels and alloys used in structural aerospace applications must provide high tensile strength, excellent fatigue resistance, fracture toughness, and stable mechanical properties under dynamic loading.
Typical materials include high‑strength low‑alloy steels, vacuum‑melted steels, and martensitic or precipitation‑hardened stainless steels where corrosion resistance is required. For highly loaded structures, advanced alloy steels and selected nickel‑based alloys are used to balance strength and durability. Quality features are a key part of aerospace structural parts manufacturing and include certified material documentation, full traceability, validated heat‑treatment processes, and strict control of chemical composition and microstructure. Non‑destructive testing, dimensional verification, and surface integrity inspection ensure compliance with aerospace standards and guarantee structural reliability throughout the component lifecycle.
BÖHLER L625 is a non-magnetizable corrosion and heat resistant nickel alloy in the form of bars, forgings and semi-finished products up to max 254 mm diameter/ cross-section and oxidation resistant up to 1093°C. Best fatigue strength and resistance to stress corrosion cracking when exposed to chloride containing media. Good weldability.
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