This invention discloses a multi-powered combined unmanned aerial vehicle (UAV) intelligent cooling
system, specifically comprising a core
control unit, a
power unit, an execution layer unit, a
perception layer unit, and a decision-making layer unit. The physical components of each unit are integrated into a frame to form a flight module. The core
control unit coordinates the operating conditions of the
power unit and the cooling actions of the execution layer unit via a data
bus. Temperature sensors in the
perception layer unit collect real-time temperature data from the engine block, radiator, and main
cooling channel. The decision-making layer unit dynamically generates drive signals based on the temperature data and the engine ECU's requirements. The
system innovatively uses hollow tubing within the frame to form the main
coolant channel, combining a liquid-cooled engine with an air-cooled radiator to form a composite cooling circuit. Intelligent flow regulation is achieved through solenoid valves and a circulating water pump, providing three
modes: basic coordination, differential
temperature control, and fuel preheating. This invention upgrades the UAV cooling
system from passive heat dissipation to active thermal management, improving the operational efficiency and reliability of multi-powered UAVs.