RC Micro Turbojet Engine for UAV

  YNX-400A/B Micro Turbojet Engine: Principle Empowerment and Advantage Manifestation     The micro turbojet engine operates through a closed loop of "intake compression-combustion work-exhaust energy release": air is compressed by a compressor and mixed with fuel to produce high-temperature gas, which drives the turbine to rotate and output power. Its advantage lies in high power density and quick response, and YNX-400A/B perfectly interprets this principle and advantage.   ​ The basic parameters reflect exquisite design: A/B type diameter × total length 148×319/350mm, A total weight 2.73kg (system 0.36kg), B total weight 4.87kg (system 1.18kg), total life 60h, first overhaul 25h, power supply DC28V±1.2V/650W for the power generation board, and the design point runs stably. ​       The performance parameters show the principle efficiency of micro turbofan engine: the maximum rated speed is 96500rpm, the thrust is 40kgf, and the thrust-to-weight ratio is 11.87/10.72, which proves…

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