Detailed Description
For structural engineers developing light aircraft frames and UAV primary structures, square tube selection demands verified laminate properties and predictable long-term behavior. Our prepreg square tubes are designed with FEA-driven layup schedules-typically [0°/90°/±45°] quasi-isotropic or customized per your load case. Autoclave cure at 7bar ensures void content ≤1.0% (ASTM D3171), directly correlating to interlaminar shear strength >40MPa.
Fatigue testing per ASTM D3479 shows no strength degradation after 10⁶ tension-tension cycles at R=0.1, 60% UTS. Creep testing at 40% ULT under 1,000hr load hold shows strain growth <0.05%-critical for aircraft structures requiring dimensional stability over years of service.
We supply full mechanical property datasheets including tension, compression, shear, and bearing allowables at room and elevated temperature (+70°C). Batch consistency is enforced via statistical process control on fiber placement angle (±1°), cure temperature profile, and post-cure dimensional verification. Export documentation includes material certification, dual-use screening, and commercial export invoice.


Specification
|
Parameter |
Value |
|---|---|
|
Process |
Prepreg autoclave |
|
Fiber |
T700 / T800 |
|
Section |
15×15mm to 80×80mm |
|
Wall |
1.0mm – 5.0mm |
|
Void content |
≤1.0% |
|
ILSS |
>40MPa |
|
Fatigue |
>10⁶ cycles @ 60% UTS |
|
CTE |
0.8–1.2 ppm/°C (axial) |
|
Export |
Legal export, certified |
Custom FAQ
Q: Can you match a specific bending stiffness (EI) target for my frame design?
A: Yes, provide target EI and we iterate layup schedule and wall thickness; FEA validation included.
Q: Are bearing strength values available for bolted joint design?
A: Yes, bearing allowables per ASTM D953 at room and elevated temp provided per batch.
Q: Can tubes be supplied with pre-molded gusset attachment points?
A: Yes, integral molded gussets or bonded fittings available; designed per your load transfer requirements.
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