DLA 116CC HF TWIN Cylinder UAV Engine

Manual Video Spare Parts DLA 116CC HF TWIN Cylinder UAV Engine Exhaust 116CC Idle speed 2000rpm Exhaust bore/stroke 46mm*35mm Actual Max.Fuel Consumption 4L/h Weight Engine: 4500g. Power Manager: 610g ECU: 175g. Pump: 265g. CDI: 233.g Staring Power Source 12S lipo battery Compression ratio 8:1 Spark Plug Iridium*4 Optional Functions Automatic start, 400W/600W Alternator Lubrication Ratio Recommend? 30:1 (trial run) 45:1 (normal flying) Fuel / Lubrication Oil Heavy Fuel / Full Synthetic 2T Oil DLA116 starter and alternaor(EFI) ?24V? propeller27*12 temperature17? Humidity36% RPM 2000 2500 3000 3500 4000 4500 5000 5500 Consumption(ml) 50 50 50 50 50 50 50 50 Time (s) 379 300 265 210 171 113 79 45 Fuel consumption (l/h) 0.47 0.60 0.68 0.86 1.05 1.59 2.28 4.00 Pulling Force (KG) 2.3 4.5 5.7 7.7 11.1 14.9 19.2 23 Touque (N.m) 1.2 2 2.48 3.4 4.6 6.1 7.6 9.4 Engine Power /KW 0.25 0.57 0.73 1.23 1.9 3 4.1 5.5 The data is just of a random engine we test, which is for reference only. In actual use, the data will fluctuate due to the influence of environmental temperature, altitude, carburetor/electric injection adjustment method and different brand propellers. Please be noted. Advantage? 1. With cowling, airflow rectifier and heat preservation at high altitude. 2. EFI system, suitable for high altitude flying. 3. Double spark plug design, better reliability andstability. 4. The cylinder head is splited and machined by CNC, the engineruns more consistently. 5. Cylinder equipped with pressure reducing valve, it makeengine start easier. 6. Electrical parts with aviation plugs, more solid andreliable. 7. Improved material and machining technology.