Autoclave Prepreg Dry Carbon Fiber Plate For UAV Frames & Light Aircraft Ribs | Source Factory Legal Export

Autoclave Prepreg Dry Carbon Fiber Plate For UAV Frames & Light Aircraft Ribs | 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. This autoclave-cured prepreg dry carbon fiber plate directly replaces aluminum alloy in multi-rotor UAV frames and light aircraft wing ribs, delivering verified weight reduction of 42–48% while eliminating salt spray corrosion and vibration-induced deformation that degrade flight endurance and sensor accuracy.
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Description
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Detailed Description

Aluminum alloy airframes are the default choice for many UAV integrators-until they aren't. Field data from survey VTOL operators shows airframes exceeding 2.8kg suffer 22% shorter mission time and 15% higher motor temperature under continuous load. Worse, coastal deployments expose aluminum to salt spray, accelerating galvanic corrosion at fastener interfaces within 6–8 months.

Our solution: T700 unidirectional prepreg (UD) layup, autoclave cured at 180°C/7bar, resulting in void content ≤1.2% (ASTM D3171). Replacing 6061-T6 aluminum with this carbon plate yields a 45% mass reduction at equivalent flexural stiffness (tested to 850 GPa·mm⁴ section modulus). Surface Ra ≤0.8μm after CNC profiling eliminates delamination risk during routing-critical for thin-wall wing rib sections under ±6g maneuver loads.

Batch-to-batch fiber volume fraction is controlled at 62±2%, fully traceable via production lot records. Each shipment includes material certification and dimensional inspection report. For UAV and light fixed-wing applications requiring legal export compliance, we handle documentation including MSDS and UN transport classification.

 

Specification

Parameter

Value

Material

T700 UD prepreg / 3K twill surface option

Process

Autoclave cure, 180°C / 7bar

Thickness range

0.5mm – 12mm

Panel max size

1500×1000mm

Void content

≤1.2% (ASTM D3171)

Fiber volume fraction

62±2%

Flatness tolerance

±0.1mm / 500mm

Operating temp

-55°C to +120°C

Export docs

MSDS, CO, Material cert, Test report

 

Custom FAQ

Q: Can this plate be used for light aircraft wing ribs under EASA CS-23 structural loads?

A: Yes, the T700 UD layup meets CS-23 ultimate load factors when designed per our FEA layup schedule. We provide layup documentation and mechanical test data to support your airworthiness submission.

Q: What CNC tolerances can you hold on 3mm thick plates?

A: Standard ±0.1mm; high-precision option ±0.05mm with anti-delamination tooling paths.

Q: Is legal export clearance supported for carbon fiber plates to EU and North America?

A: Yes. We prepare full export documentation including HS code classification (6815.99), material safety data, and dual-use compliance screening.

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