FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to unmanned aerial vehicle propulsion system. Cruise engine module with internal combustion engine comprises a housing, an internal combustion engine, a fuel tank intended to be located inside the fuselage and attached to the first wall of the housing on the reverse side of the cruise engine, wherein the fuel tank is connected to the cruise engine through a first wall for transferring fuel to the cruise engine, wherein the fuel tank comprises a fuel level sensor in the tank, controller connected to cruise engine and fuel tank and configured to receive messages from external devices, receiving data on state from cruise engine and fuel tank, sending requests and commands to cruise engine and fuel tank and sending messages to external devices, besides, exchange of messages with external devices is performed via program interface.
EFFECT: simplification and acceleration of assembly/disassembly processes, transportation, refueling/charging, maintenance and preparation of UAV for operation.
11 cl, 6 dwg
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Authors
Dates
2025-02-05—Published
2024-07-03—Filed