Exhaust amount | 232cc | Power | 22HP |
Idle Speed | 2000 rpm | Pulling Force | 40kg/50maltitude |
Exhaust bore/stroke | 53mm*41mm | Compression ratio | 9.8:1 |
Propeller· max.fuelconsumption | 32*10 / 11.6L/h | Spark Plug | double Iridium *2 |
Weight of Electrical system | motor : 870.5 g power manger :390 g | Starting Power Source | 6S/7S lipo battery |
Weight of main engine and parts | Engine: 7593g, Muffler:513g, Standoffs: 22*4g, Ignition: 191g | Lubrication Ratio | 25:1~30:1 (trial run) 40:1~50:1 (normal flying) |
Recommended propeller | 34*10、32*10 | Auto-Starting Function | Yes |
Alternator Output Voltage | 24V/28V | Alternator Output Power | 400W/600W |
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 flyingaltitude 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. | ||
DLA180 with starter and Alternator（Carburetor) Pusher Propeller32*10 (Temperature 17℃ Humidity50%) | ||||||||||
RPM | 2000 | 2500 | 3000 | 3500 | 4000 | 4500 | 5000 | 5500 | 6000 | 6500 |
Voltage | 0 | 0 | 400 | 400 | 400 | 400 | 400 | 400 | 400 | 400 |
Electric Current | 0 | 0 | 0 | 0 | 27.6 | 27.7 | 27.7 | 27.7 | 27.7 | 27.7 |
Alternator Power( loaded 250W) | 0 | 0 | 0 | 0 | 15.2 | 15.2 | 15.2 | 15.6 | 15.7 | 15.9 |
Fuel consumption /ml | 50 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | 50 | 50 |
Time/ s | 158.3 | 116.3 | 90 | 75.2 | 68.5 | 39.6 | 32.3 | 26.6 | 23.2 | 19.8 |
Fuel Consumption L/h | 1.14 | 1.55 | 2.00 | 2.39 | 2.63 | 4.55 | 5.57 | 6.77 | 7.76 | 9.09 |
Pulling Force/ KG | 4.4 | 6.9 | 10 | 12.8 | 16.8 | 20.8 | 24.8 | 30.3 | 35.6 | 41.2 |
Torque N.m | 3.5 | 3.9 | 5.1 | 5.8 | 7.8 | 9.1 | 11.2 | 13.2 | 13.9 | 16.5 |
Engine power /KW | 0.8 | 1.1 | 1.7 | 2.2 | 3.3 | 4.4 | 5.8 | 7.6 | 9.4 | 11.3 |
*** 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. | ||||||||||
