DLA116i2UA
Exhaust amount116CC
Output12HP
Cylinder Bore/ Stroke46mm/35mm
Idel Speed 2000 RPM
Pulling force24kg/50meter altitude
Max. Comsumption4.56L/H (27*06)
FuelGasoline + 2T synthetic oil
Lubrication Ratio25:1~30: 1(trial run)
40: 1~50:1(normal flying)
Compression Ratio7.8:1
Propeller Recommended28*10, 27*10
Spark PlugDLA CM6,Iridium
AlternatorAuto-starter.             Output:24V/28V, 400W/600W
WeightMain engine assembled: 3233g, ignition:153g*2, ECU:158g, pump:272g, Power manger:391g


  
      

    DLA116 with starter and AlternatorCarburetor)  

    Pusher Propeller27*10

    (Temperature 17℃ Humidity50%)

    RPM

    2000

    2500

    3000

    3500

    4000

    4500

    5000

    5500

    6000

    Voltage

    0

    0

    0

    27.61

    27.62

    27.61

    27.64

    27.63

    27.66

    Electric  Current

    0

    0

    0

    12.55

    12.54

    12.54

    12.56

    12.57

    12.54

    Alternator Power( loaded 350W)

    0

    0

    0

    346.5055

    346.3548

    346.2294

    347.1584

    347.3091

    346.8564

    oil /ml

    50

    50

    50

    50

    50

    50

    50

    50

    50

    Time/ s

    166.8

    132

    112.4

    79.2

    69.2

    53.5

    48.9

    44.1

    39.5

    Fuel Consumption L/h

    1.08

    1.36

    1.60

    2.27

    2.60

    3.36

    3.68

    4.08

    4.56

    Pulling Force/ KG

    2.8

    4.1

    5.7

    7.9

    11.1

    13.5

    15.8

    19.3

    24

    Torque  N.m

    1

    1.4

    2.1

    3.1

    4.1

    5.1

    6.1

    7.9

    9.6

    Engine power /KW

    0.2

    0.3

    0.6

    1

    1.8

    2.4

    3.2

    4.6

    6.1

    *** 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.