Manned drone motors stator cores are the stationary laminated magnetic structures designed for brushless motors powering human-carrying unmanned aerial vehicles — including eVTOL aircraft, heavy-lift cargo drones, and manned multirotor platforms. Unlike consumer or industrial drone motors, manned drone motors require :

• Aviation-grade reliability: Zero tolerance for in-flight failure — redundant stator designs and fault-tolerant architectures
• High torque density: Typically 80–100 N·m torque output with 20-30kW peak power
• Extended thermal stability: Sustained operation at Class H (180°C+) with advanced cooling integration
• Rigorous quality assurance: 100% inspection, batch traceability, and aviation material certifications

Reenives manufactures high-quality manned drone motors stator cores using non-grain oriented electrical steel (0.15-0.35mm) with advanced C5/C6 epoxy coating — reducing eddy current losses by up to 35% and ensuring aviation-grade thermal stability for human-carrying UAV operations .

Reenives offers manned drone motors stator cores in multiple configurations to meet diverse heavy-lift and eVTOL application requirements :

• By Power Class: 10-30kW (heavy-lift cargo), 30-50kW (eVTOL), 50kW+ (manned multirotor) — with custom configurations up to 100kg thrust per motor
• By Slot/Pole Config: 18N20P (high torque density), 24N28P (maximum torque), custom 36+ slot configurations for aviation-grade smoothness
• By Material Thickness: 0.20mm (standard high-efficiency), 0.15mm (ultra-high performance, minimum eddy loss), 0.27mm (heavy-duty industrial)
• By Insulation Coating: C5 epoxy powder coating (Class H, 180°C) with >2000V dielectric strength; C6 grade for superior thermal conductivity in high-power density applications
• By Core Architecture: Segmented stator cores (modular for fault-tolerant winding) and integrated circular laminated stacks (one-piece for maximum structural integrity)

💡 Reenives specialty: private mould development for custom manned drone stator geometries — optimized for specific eVTOL and human-carrying UAV platforms with aviation-grade reliability .

All parameters validated by Reenives R&D center (ISO 9001:2025 certified) and third-party testing per IEC 60404-2. Manned drone motor specifications benchmarked against industry leading systems like EV CRAFT's 23850 propulsion platform (24S, 20kW, 98kg thrust, 89% efficiency) .

📐 Data source: Reenives in-house quality lab, 2025–2026. SGS verification report available. Full batch traceability and material certificates .

Reenives manned drone motors stator cores power critical human-carrying UAV applications across multiple sectors :

• eVTOL & Urban Air Mobility: Aviation-grade stator cores with fault-tolerant design and redundancy for passenger-carrying electric vertical takeoff and landing aircraft .
• Heavy-Lift Cargo Drones: 18N20P / 24N28P stators for 80-180kg payload platforms with >89% peak efficiency and extended range .
• Manned Multirotor Aircraft: 24-36 slot stators with 30-50kW peak power for human-carrying drone platforms, paramotors, and paragliders .
• Search & Rescue UAVs: High-reliability stator cores for critical missions in harsh environments with IP56-ready C5 epoxy coating .
• Military & Defense Drone Platforms: Custom-designed stator cores with hardened specifications for mission-critical applications.

1. Define power, thrust, and redundancy requirements: For heavy-lift cargo (20-50kW), select 18N20P configurations. For eVTOL passenger transport (30-50kW+), consider dual-redundant stator designs with independent winding sets.
2. Choose lamination material thickness: 0.15mm for maximum efficiency and minimum eddy loss (premium); 0.20mm for standard manned drone applications; 0.35mm for cost-sensitive heavy-duty platforms .
3. Select slot/pole combination: 18N20P for high torque density, 24N28P for maximum torque, 30+ slot configurations for aviation-grade smoothness and reduced cogging torque.
4. Specify insulation, cooling, and environmental protection: C5/C6 epoxy coating for outdoor operations; oil-compatible coating for liquid-cooled eVTOL systems; aviation-grade thermal management integration.
5. Request samples and PPAP validation: Reenives delivers first-article inspection reports (FAI), material certificates, and full PPAP documentation for aviation compliance. Prototype manned drone stator samples ready in 7-10 days after design approval .

💡 Engineering support: Free DFM within 48h and FEA simulation — send your drone motor spec or drawing to linda_reenives@163.com.