Alternator Controller

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Presentation transcript:

Alternator Controller Exhaust amount 40cc Power 2.5KW Idle Speed 2500 rpm Pulling Force 16kg/50m altitude Exhaust bore/stroke 32mm*28mm Compression ratio 8:1 Propeller· max.fuel consumption 18*12/2.00L/h Spark Plug Iridium Weight of Electrical system motor : 245g power manger :348 g Starting Power Source 6S/7S lipo battery Weight of main engine and parts Engine: 1890g, Muffler:69g*2, Standoffs: 22*4g, Ignition: 200g Lubrication Ratio 25:1~30:1 (trial run) 40:1~50:1 (normal flying) Recommended propeller 18*12 Auto-Starting Function Yes Alternator Output Voltage 24V Output Power 400W Advantage of Carburetor Stable performance, Strong power and low price. Easy to use, long service life, convenient maintenance. Simple and compact structure, small size. Suitable for flying altitude below 3000m. Notes When test engine on the ground test, it shall be equipped with air filter; Take care to prevent dust and impurities from being sucked into the carburetor; Do not adjust the mixing ratio screw. If you need to adjust, please contact with us. Ignition Spark plug Alternator Controller

DLA40 with starter and Alternator（Carburetor) Pusher Propeller18*12 (Temperature 17℃ Humidity50%) RPM 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 7500 Voltage 23.98 24 24.01 空载 Electric Current 16.9 16.89 16.87 16.88 Alternator Power 405.262 405.36 405.0487 405.12 Fuel consumption /ml 50 Time/ s 216 180 150 116 97 90 Fuel Consumption ml/s 0.23 0.28 0.33 0.43 0.52 0.56 Fuel Consumption L/h 0.83 1.00 1.20 1.55 1.86 2.00 Pulling Force/ KG 3.1 4 4.5 5.7 7.1 8.2 9.7 11.1 Torque N.m 0.9 1.1 1.2 1.7 2.1 2.43 2.7 Engine power /KW 0.25 0.5 0.7 0.84 1.68 2 2.5 *** 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 even the different brand propellers. Please be noted.