DLA32UAE

2018-03-30

This engine is mainly used for fixed-wing with take-off weights (including Gasoline) not more than 9 KGS.

DLA32 starter and alternator/EFI propeller18*10 Temperature 17℃ Humidity 50%
RPM	2000	2500	3000	3500	4000	4500	5000	5500	6000	6500	7000	7300
Voltage	0	0	0	23.58	23.57	23.58	23.56	23.57	23.58	23.575	23.576	23.577
Electric Current	0	0	0	10.65	10.66	10.65	10.64	10.66	10.67	10.675	10.683	10.691
Alternator Power	0	0	0	251.127	251.2562	251.127	250.6784	251.2562	251.5986	251.663125	251.862408	252.061707
Fuel consumption /ml	50	50	50	50	50	50	50	50	50	50	50	50
Time/ s	1426	1124	803	771	628	528	419	365	307	232	183	128
Fuel Consumption ml/s	0.04	0.04	0.06	0.06	0.08	0.09	0.12	0.14	0.16	0.22	0.27	0.39
Fuel Consumption L/h	0.13	0.16	0.22	0.23	0.29	0.34	0.43	0.49	0.59	0.78	0.98	1.41
Pulling Force/ KG	0.68	1.05	1.3	1.72	2.45	2.79	3.32	4.12	4.85	5.73	6.29	7.01
Torque N.m	0.18	0.21	0.29	0.46	0.56	0.72	0.92	0.16	1.46	1.87	2.12	2.35
Engine power /KW	0.03	0.04	0.1	0.21	0.24	0.33	0.47	0.69	0.93	1.31	1.52	1.86
*** 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.

Advantage：

1. EFI system, suitable for high altitude flying.

2. Auto-starter&alternator，2 in 1， output power400W.

5. Electrical parts with aviation plugs, more solid andreliable.

6. Improved material and machining technology.

Notice: In order to make the engine performance to the best. The fuel pulse width must be calibrated on the special test bench according to the corresponding propeller size. Please contact with us before purchase.