B2B manufacturer of precision carbon fiber assemblies with custom CNC aluminum integration for robotics, industrial automation, and UAV structural applications. Toray T700 & T800 grade materials.
Each assembly is engineered for structural performance, dimensional accuracy, and seamless integration with CNC-machined metal components.
Precision carbon fiber structural links for 6-axis and collaborative robots. Combines high stiffness-to-weight with CNC 7075-T6 aluminum end fittings for bolt-on integration.
High-speed carbon fiber rollers for printing, packaging, and web-handling lines. 60–80% lighter than steel; reduces drive motor load and extends bearing life.
Wing spars and booms for fixed-wing UAVs and multi-rotor frames. Optimized layup schedules via Classical Laminate Theory (CLT) for maximum stiffness at minimum weight.
Flat and contoured CFRP plates, machined to net shape with routed pockets, drilled holes, and counter-bores. Ideal for structural brackets and chassis panels.
Multi-material assemblies joining CFRP tubes or plates with precision CNC-machined aluminum 7075-T6 brackets using aerospace-grade adhesive bonding and mechanical fastening.
Full design-to-delivery service for specialized carbon fiber components. From DFM review through tooling, lay-up, cure, and CNC finishing — one source of supply.
Our vertically integrated facility in Dongguan covers filament winding, autoclave/oven curing, 5-axis CNC machining, and quality inspection — eliminating handoff risk and compressing lead times.
CNC-controlled winding with fiber placement angle ±0.5°. Autoclave cure at 135°C for Vf >62% and near-zero porosity.
DMG Mori 5-axis machining centres. Tolerances to ±0.02mm. PCD (polycrystalline diamond) tooling avoids delamination on all cut edges.
Zeiss Contura CMM with CALYPSO software. 100% inspection on critical dimensions; statistical process control (SPC) on production runs.
Controlled-environment bonding room. Fixtures ensure ±0.1mm alignment of CF-to-metal joints. Peel and lap-shear testing on each batch.
We source from Toray (Japan), SGL Carbon (Germany), and HEXCEL (USA) — providing traceability and consistent mechanical properties for every production run.
Standard-modulus carbon fiber. Best balance of tensile strength, stiffness, and cost for structural assemblies.
Intermediate-modulus fiber. Preferred for UAV spars and robotic links demanding high stiffness-to-weight.
Aerospace-grade aluminum for CNC-machined end fittings, flanges, and inserts. Anodized for corrosion resistance.
Toray E250 / Hexcel 8552 epoxy resin systems. Tg >190°C for post-cure stability in high-temperature operating environments.
A structured 5-stage manufacturing workflow ensures quality is built in at every step, not inspected in at the end.
We analyze your drawing for carbon fiber-specific design-for-manufacture issues: fiber orientation, wall thickness, tooling radius, and insert geometry.
Mandrel or cavity tooling fabricated in-house. Prepreg layers cut and placed to engineered fiber angle schedules using CLT-optimized laminate design.
Vacuum-bagged parts cured at controlled pressure (6 bar) and temperature (135°C). Post-cure free-stand cycles improve Tg and dimensional stability.
5-axis machining with PCD tooling. Adaptive feed-rate control prevents delamination. All critical features verified against first article inspection plan.
CMM inspection, visual and dimensional checks. Conformance data package included. Parts packed in custom foam for zero-damage transit.
Practical guidance on designing carbon fiber assemblies for performance, manufacturability, and long-term reliability.
Learn how to perform tolerance stack-up analysis for carbon fiber tube and aluminum end-fitting assemblies. Includes worked example with Toray T700S, MIL-HDBK-17 references, and best practices for ±0.05mm assemblies.
Explore the carbon fiber opportunity for humanoid robot structural components. Technical analysis with material properties, stiffness/weight comparisons, and a worked example for robotic arm links.
Learn how to optimize CNC machining parameters for CFRP UAV propellers to achieve ±0.02mm profile tolerance. Includes worked example, toolpath strategies, and material-specific feeds/speeds for carbon fiber composites.
Send us your drawings, specifications, or rough requirements. Our engineering team will review and respond within 24 hours with a technical feasibility note and indicative pricing.
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