Staying formula that can drop VTOL fixed wing uavs
The utility model discloses a staying formula that can drop VTOL fixed wing uavs, including fixed wing structure system, stationary vane driving system, rotor driving system, power source system, flight control carries avionics system with the machine, power source system is including power manageme...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model discloses a staying formula that can drop VTOL fixed wing uavs, including fixed wing structure system, stationary vane driving system, rotor driving system, power source system, flight control carries avionics system with the machine, power source system is including power management module, lithium battery pack, fuel tank and the disconnect -type electric connector that can drop, the disconnect -type that can drop electric connector's confession electrical output, lithium battery pack all are connected with power management module, and ground power supply system and the disconnect -type electric connector's that can drop power supply input terminal are connected. The utility model discloses a disconnect -type that can drop electric connector links to each other with theground power supply system through the staying cable taking off the in -process, directly supplies with the required electric energy of rotor driving system, and power is sufficient, and the power forthe need of the flight of |
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