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Custom Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear
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  • Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear
  • Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear
  • Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear
  • Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear

Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear

The landing gear is a key component for drones when landing and needs to withstand huge impact loads. Carbon fiber composite materials, through reasonable structural design, such as the use of honeycomb sandwich structures, not only reduce weight, but also improve energy absorption and shock absorption capabilities, which can protect the safety of drones when landing.

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Parameter
AEROSPACE GRADE · VACUUM BAGGED
Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear
The Carbon Fiber UAV Landing Gear is a structural component engineered for multi-rotor and fixed-wing unmanned aircraft systems. Constructed from 3K twill weave carbon fiber and reinforced with epoxy resin, this landing system utilizes a high strength-to-weight ratio to minimize the aircraft's maximum take-off weight (MTOW). The landing gear is manufactured through a vacuum bagging or autoclave process, ensuring a consistent wall thickness and internal structural integrity. Its streamlined profile is designed to reduce aerodynamic drag during flight, while the inherent vibration-damping properties of carbon fiber composites protect onboard sensors and gimbal payloads during touchdown sequences.
40-60%Lighter than aluminum
5-100kg+Load capacity (MTOW)
-40 to 80°COperational range
Technical Specifications
Material CompositionToray Carbon Fiber / Epoxy Resin Matrix
Surface Finish3K Matte / Glossy Twill or Plain Weave
Weight Reduction40% - 60% lighter than aluminum alloy alternatives
Load CapacityScalable from 5kg to 100kg+ MTOW
Thermal StabilityOperational range from -40°C to 80°C
Core Advantages
High Tensile Strength Corrosion Resistance Fatigue Endurance Vibration Absorption EMC Compatible
The composite matrix dissipates kinetic energy upon impact, reducing mechanical stress transferred to the fuselage.
01
High Tensile Strength
Provides rigid support for heavy-lift UAVs, maintaining structural geometry under maximum payload conditions.
02
Corrosion Resistance
Unlike metallic components, carbon fiber does not oxidize, making it suitable for maritime and coastal operations.
03
Fatigue Endurance
Resists structural softening over repeated landing cycles, extending the operational lifecycle of the airframe.
04
Vibration Absorption
The composite matrix dissipates kinetic energy upon impact, reducing the mechanical stress transferred to the fuselage.
05
Electromagnetic Compatibility
Designed with clearances that minimize interference with bottom-mounted GPS antennas or transmission modules.
[A]
Agricultural Spraying Drones
Supports the heavy weight of liquid tanks and spraying hardware. The chemical resistance of the carbon fiber ensures the gear does not degrade when exposed to fertilizers or pesticides.
[G]
Geospatial Mapping and Surveying
Provides a stable, lightweight platform for LiDAR scanners and multispectral cameras. The weight savings directly translate into increased flight endurance for large-area mapping missions.
[S]
Search and Rescue (SAR) Operations
Enables rapid deployment in diverse environments. The rugged construction allows for landings on uneven or unprepared terrain without permanent deformation of the struts.
Maintenance and Operational Guidelines
Installation Precautions
1 Use torque-limiting drivers when securing mounting bolts to prevent crushing the composite laminate.
2 Install rubber dampening grommets between the landing gear mount and the carbon fiber plate to further isolate high-frequency motor vibrations.
Inspection and Storage
I Impact Inspection: After any hard landing, inspect the surface for delamination or hairline fractures. Damaged carbon fiber components should be replaced immediately as they cannot be straightened or welded.
II UV Exposure: While treated with UV-resistant coatings, long-term storage should be in a shaded area to prevent resin degradation over years of service.
III Cleaning: Use non-abrasive detergents; avoid solvent-based cleaners that may affect the epoxy resin finish.
i Certified for UAV applications up to 25kg per landing strut (static load). Custom geometry available for specific airframes. Batch inspection includes ultrasonic testing for internal voids.
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About Us
Jiangyin Dongli New Materials Technology Co., Ltd.
Founded in 2018, Jiangyin Dongli New Materials Technology Co., Ltd. specializes in the comprehensive development and manufacturing of high-performance fiber composite materials. We are China Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear Manufacturers and Custom Carbon Fiber Unmanned Aerial Vehicle (UAV) Landing Gear Factory. Located in a 32,000-square-meter industrial complex, the company features precision-controlled production environments, including climate-regulated workshops and 100,000-grade purification zones.
As a one-stop factory with full process control, we integrate material innovation with engineering expertise to serve industries such as aerospace, automotive and sports equipment development. Our capabilities include the R&D and production of high-performance fiber fabrics through weaving and prepreg processes, as well as composite products utilizing autoclave, RTM, RMCP, PCM, WCM, and spraying technologies.
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