G360 Gasoline Piston Engine

The G360 is an aviation derivative of a V8 four-stroke gasoline engine producing 367 kW take-off and 280 kW continuous power. Aviation-suitability modifications optimize weight, reliability and emissions. Drives the propeller through a reduction gearbox for heavy UAV and light aircraft applications.

The G360 gasoline piston engine is an aviation derivative of an automotive V8 cylinder four-stroke gasoline engine. Building on the compact design of the original engine, modifications have been made to external accessories and internal components to enhance aviation suitability, thereby further meeting the requirements for lightweight and reliability in aviation. The intake, exhaust, and combustion systems have been optimized, and an aviation-standard electronic control system has been implemented to achieve stable high-power output. The engine drives the propeller through a reduction gearbox, providing propulsion for the aircraft. It delivers 367 kW take-off power and 280 kW continuous output from dimensions of 930 × 685 × 640 mm at a dry weight of 250 kg, with a power-to-weight ratio of 1.4 kW/kg. Minimum specific fuel consumption is 0.35 kg/kWh with a displacement of 6.2 L. Maximum usage height is 4,000 m and time between overhaul is 1,000 hours, with high durability and high reliability.

Key specifications: Dimensions: 930 × 685 × 640 mm; Take-off Power: 367 kW; Continuous Power Output: 280 kW; Dry Weight: 250 kg; Power-to-Weight Ratio: 1.4 kW/kg; Minimum Specific Fuel Consumption: 0.35 kg/kWh.

Specifications

All specifications are taken from the manufacturer’s current datasheet.