Stainless steel offers an excellent combination of mechanical strength, corrosion resistance, and temperature stability, making it a reliable material for structural and functional components in aerospace and aviation applications. Additive manufacturing enables the production of lightweight, high-performance stainless steel parts with complex geometries, integrated features, and reduced lead times.
At Neway Aerotech, our stainless steel 3D printing services support the fabrication of custom aerospace-grade brackets, housings, fasteners, and internal components using SLM and DMLS processes.
Technology | Layer Thickness (μm) | Accuracy (mm) | Surface Roughness (Ra, μm) | Suitable Components |
|---|---|---|---|---|
SLM | 30–50 | ±0.05 | 6–12 | Brackets, mounts, clips, fuel system covers |
DMLS | 40–60 | ±0.08 | 8–15 | Avionics housings, fasteners, structural parts |
SLM is preferred for thin-walled parts with critical tolerances; DMLS for bulkier components and assemblies.
Grade | UTS (MPa) | Hardness (HV) | Temperature Limit (°C) | Main Benefits |
|---|---|---|---|---|
316L Stainless Steel | 480–680 | 160–190 | ~870 | Excellent corrosion resistance, weldable |
17-4PH Stainless Steel | 900–1150 | 300–380 | ~600 | High strength, precipitation hardened |
304 Stainless Steel | 500–700 | 170–200 | ~800 | Cost-effective with general corrosion protection |
Corrosion Resistance: Suitable for exposure to jet fuel, hydraulic fluids, and moisture in variable environments.
Dimensional Stability: Maintains tolerances across wide temperature fluctuations typical in aerospace operations.
Mechanical Integrity: High tensile strength and fatigue resistance make stainless steel ideal for load-bearing components.
Weldability and Post-Processing: Compatible with CNC machining, passivation, and joining techniques for hybrid assemblies.
A Tier 1 aviation supplier required a lightweight avionics mounting bracket with integrated wire routing features, designed for vibration isolation and resistance to corrosion from hydraulic fluid exposure. The traditional approach involved multi-part assemblies and brazing.
Design: Lattice-filled hollow structure with two integral mounting bosses.
Material: 17-4PH stainless steel chosen for high strength and fatigue resistance.
Printing Process: SLM at 40 μm layer thickness; argon atmosphere, 350 W laser.
Post-Processing:
HIP + H900 heat treatment.
Surface blasted to Ra ≤ 6 μm.
CNC machining on all mounting surfaces.
Inspection: CMM and tensile testing performed to validate conformance.
The final part achieved a 40% weight reduction over the machined aluminum baseline while meeting strength and vibration standards. Fatigue testing exceeded 10⁷ cycles at 500 MPa, and dimensional tolerances were held within ±0.02 mm across all datum planes.
What types of stainless steel are best for aerospace 3D printing applications?
Are stainless steel printed parts suitable for high-vibration environments?
How does heat treatment affect 17-4PH stainless steel after printing?
Can stainless steel printed components be welded or brazed to others?
What is the largest part size available for stainless steel 3D printing?