SCAIR 30HP 1.2MPa Oil-Free Compressor for Aerospace Hydraulic Test Benches & NDT Systems
SCAIR 30HP 1.2MPa Oil-Free Compressor: Flight-Critical Air for Aerospace Manufacturing
SCAIR's 30HP compressor delivers 3.1 m³/min at 1.2MPa with zero hydrocarbon risk, preventing $500k/month scrapped landing gear assemblies where oil contamination causes hydraulic fluid degradation per AMS 2641 standards.
Featuring ASME B40.2 calibrated pressure control, this 22kW system maintains ±0.01MPa stability during 150% proof pressure testing - critical for wing spar certification where 0.1% deviation causes test invalidation. The FOD-free design achieves NAS 1638 Class 4 cleanliness for composite NDT applications.
Air Delivery: 3.1 m³/min @ 1.2MPa (2.6m³/min @ 1.5MPa for cryogenic valve testing)
Pressure Accuracy: ±0.01MPa with NIST-traceable calibration
Particle Control: Class 100 cleanroom equivalent air (ISO 14644-1)
Response Time: 0.4s ramp from 0-1.2MPa for burst testing
Proof Pressure Mode: Automated 200% overpressure safety lockout per ISO 10770-3
FOD Prevention: Magnetic particle traps capture 0.5μm ferrous contaminants
Cryogenic Compatibility: Operates at -50°C for space component testing
Data Integrity: 21 CFR Part 11 compliant electronic records
Landing Gear Testing: Supplies hydraulic test rigs for 5,000psi cyclic endurance testing (meets MIL-L-87107)
Composite Inspection: Powers laser shearography systems detecting 0.005mm delaminations
Fuel System Certification: Tests aircraft fuel valves at 1.2MPa simulating 50,000ft altitude
Engine Nacelle Assembly: Provides contamination-free air for pneumatic riveters in FOD-controlled zones
Certifications: AS9100D, FAA AC 20-193, EASA Part 21G
Material Traceability: EN 10204 3.1 certificates with batch-specific DNA marking
Calibration: ISO/IEC 17025 accredited pressure calibration
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Q: How to prevent hydraulic fluid degradation?
A: ISO 8573-1 Class 0 air prevents additive breakdown in Skydrol LD-4 fluid.
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Q: Solution for false positives in composite NDT?
A: Pulse-free airflow eliminates 0.02mm measurement artifacts in laser shearography.
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Q: Temperature compensation for high-altitude simulation?
A: Real-time PVT algorithm adjusts for adiabatic cooling during rapid decompression tests.
Technical Differentiation:
Pioneering 1.2MPa aerospace testing focus
Industry-first proof pressure lockout and FOD trapping
Applications in laser shearography and cryogenic testing
Compliance with FAA AC 20-193 and MIL-L-87107
Solved hydraulic fluid degradation and NDT artifacts
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