Product Description
Our Carbon Fiber Drone Arm Landing Gear Custom Composite Frame Component range is built to address the specific structural challenges of multi-rotor and fixed-wing UAVs. High-strength 3K or 12K carbon fiber combined with advanced epoxy resin is processed through CNC machining, compression molding, or precision lay-up to produce arms, landing gear, and related frame elements.
Key components include:
Carbon fiber drone arms designed for minimal flex and optimal motor alignment
Landing gear optimized for energy absorption and repeated rough landings
Matching center plates, connectors, and other custom composite frame parts
The result is a coherent structural system that reduces overall aircraft mass while improving flight stability, vibration control, and ground-handling safety. Mounting interfaces, tube diameters, leg geometry, and reinforcement zones can all be tailored to the customer's propulsion system, battery layout, and payload.
Having supplied international UAV projects for years, we know that arm torsional stiffness, landing-gear toughness, and precise interface matching are decisive for both flight performance and maintenance costs. Material certificates and dimensional reports are available to support quality verification and customs clearance.
Core Advantages (Export-Focused)
Targeted lightweighting: Arms and landing gear are individually optimized to cut mass without sacrificing necessary rigidity or toughness.
Balanced structural performance: High torsional stiffness in arms for precise control response; improved energy absorption in landing gear for safer touchdowns.
True component-level customization: Arms, legs, plates, and connectors can be developed as a matched set from customer CAD data.
Export-ready supply chain: Long-term experience exporting Carbon Fiber Drone Arm Landing Gear Custom Composite Frame Component. Full support for FOB/CIF terms, complete shipping documents, protective packaging, and cooperation with third-party inspections or destination compliance checks.
Customer Pain Points & Our Solutions
Pain Point 1: Arms twist or flex under load, causing unstable flight and reduced efficiency
We recognize that insufficient torsional rigidity directly harms control accuracy and power consumption.
Solution: Lay-up and cross-section are engineered for the specific motor thrust and arm length, delivering the required stiffness at minimum weight.
Pain Point 2: Landing gear fails after a few hard landings, creating recurring repair costs
Frequent breakage of stock landing gear is a common operational headache.
Solution: Geometry and reinforcement are designed for better impact distribution and fatigue life, reducing replacement frequency.
Pain Point 3: Purchased parts do not match existing interfaces, forcing extra machining
Mismatched holes, diameters, or mounting patterns waste time and introduce risk.
Solution: Every arm, leg, and plate is produced to the customer's exact drawings or sample, so interfaces fit correctly from the first delivery.
Pain Point 4: Uncertain lead times and missing export paperwork disrupt project schedules
International buyers need predictable delivery and clean documentation.
Solution: Established production planning and complete export document sets keep shipments on track.
Pain Point 5: Small trial quantities are difficult to obtain and communication is slow
Early-stage development requires fast, precise feedback.
Solution: Prototype and low-volume runs are supported, with dedicated technical and commercial contacts for clear, rapid communication.
Company Advantages
Focused expertise in carbon fiber UAV structural parts, refined through continuous customer feedback from real flight programs.
End-to-end capability covering design discussion, prototyping, and series production.
Consistent material and process control that maintains quality across batches.
Export team experienced with the expectations of international drone companies regarding communication speed and documentation accuracy.
Partnership approach with responsive after-sales support.
Customization Service
Arms, landing gear, and frame components developed directly from customer CAD files or detailed specifications
Selectable fiber type (3K / 12K), fiber orientation, and surface appearance
Prototype and pilot-batch production available
Precision CNC machining, drilling, and finishing
Single-point contact from technical clarification through final shipment
We focus on the practical requirements of UAV engineers - arm stiffness, landing-gear toughness, and interface accuracy - and deliver accordingly.
FAQ
Q1: Can arms and landing gear be fully customized from my drawings? What is the usual minimum order?
Yes, complete customization from drawings or 3D models is standard. Prototypes and small batches are accepted; series MOQ depends on part complexity.
Q2: How are arm stiffness and landing-gear impact performance controlled?
Both are achieved through appropriate fiber selection, tailored lay-up, and process discipline. Key performance points can be reviewed and validated with the customer.
Q3: Are material certificates and dimensional reports available?
Yes, both can be supplied according to the agreed requirements.
Q4: How is export packaging and documentation managed?
Full export documents are prepared. Components are protected against impact and surface damage. We regularly ship to major international destinations.
Q5: What lead times should be expected for samples and production?
Prototypes typically require 7–15 days depending on complexity. Production orders are usually 15–30 days after final confirmation. Exact dates are given with each quotation.
Q6: Is third-party inspection or a factory visit possible?
Yes, both can be arranged.
Q7: Are glossy and matte surface finishes both available?
Yes, either finish can be specified.
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Technical Parameters
| Property | Typical Value / Range | Notes |
|---|---|---|
| Material | 3K / 12K Carbon Fiber + Epoxy Resin | Structural grade |
| Density | ≈ 1.55 g/cm³ | Lightweight construction |
| Wall / Plate Thickness | 1.0 mm – 5.0 mm (custom) | Design-dependent |
| Tensile Strength | ≥ 600 MPa | Reference value |
| Flexural Strength | ≥ 500 MPa | Reference value |
| Surface Finish | Glossy or Matte | Single or double sided |
| Critical Dimension Tolerance | ±0.1 – 0.3 mm | CNC controlled |
| Service Temperature | −40°C to +120°C | Resin system dependent |
| Main Applications | FPV, Cinema, Industrial, Agricultural, Cargo Drones | Fully configurable |
Note: Figures shown are typical. Final mechanical performance is determined by lay-up schedule, geometry, and thickness. Customer-specific validation can be arranged.

