3K Twill Dry Carbon Fiber Sheet Autoclave Cured For FPV Drone Fuselage & Small Plane Skin | Source Factory Legal Export

3K Twill Dry Carbon Fiber Sheet Autoclave Cured For FPV Drone Fuselage & Small Plane Skin | Source Factory Legal Export
Details:
Guangdong Shenyang New Material, ISO9001 & CE certified dry carbon composite manufacturer based in Huizhou, China. Equipped with autoclave, 4.0m×2.0m large-format CNC router and prepreg cold storage. Products for legal export, prototype & mass production available, batch performance traceable. 3K 2×2 twill dry carbon fiber sheets autoclave cured for FPV racing drone fuselages and small aircraft skin panels, replacing dent-prone aluminum with 50% lighter pseudo-isotropic plate that absorbs crash energy via controlled fiber break rather than permanent deformation.
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Description
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Detailed Description

FPV and light aircraft builders report aluminum panels dent on hard landing (>5J impact) and crack under motor vibration (80–120Hz). 5052-H32 also corrodes in humid fields within a season.

Feature: T300 3K twill prepreg, autoclave 6–7bar, pseudo-isotropic in-plane stiffness.

Advantage: Density 1.55g/cm³, bending modulus 60–65GPa, Charpy impact 26J/mm, Ra≤0.8μm after CNC.

Benefit: 50% lighter than 5052 aluminum → extends flight time 10–15%; impact energy dissipates via fiber break not permanent dent → airframe reusable after minor crashes; zero galvanic corrosion; matte/gloss/peel-ply finishes available.

CNC compression-cut prevents edge fuzz. Batch void ≤1.2%, FVF 60±2%. Lot-traceable with test coupon. Legal export pack included.

 

Specification

Parameter

Value

Weave

3K 2×2 twill / plain opt.

Fiber

T300 / T700 opt.

Process

Autoclave prepreg

Size

400×500 to 1500×1000mm

Thickness

0.3–15.0mm

Density

1.55g/cm³

Impact

26J/mm (Charpy)

Void

≤1.2%

Export

Legal export full docs

 

Certifications

Hot Pressed Custom Carbon Fiber Exoskeleton Joint Support Component

FAQ

Q: Minimum bend radius for 1mm sheet?

A: Cold form min R15×t; heated form at 110–120°C allows tighter radii without fiber damage.

Q: Peel-ply for bonding to airframe frames?

A: Std on request-no surface abrasion needed before secondary bonding.

Q: Damping vs aluminum?

A: Loss factor 0.016–0.02 vs Al 0.006 → 2.5–3× vibration attenuation, improves FPV video.

Q: Lead time prototype?

A: 7–10 days; batch 15–20 days incl. NDT.

Q: Export clearance?

A: HS 6815.99, MSDS, CO, cert, ITAR-free dual-use screening.

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