Parameters
This engine is mainly used for UAV with fixed-wing, Helicopter or UAV in complex environment with take-off weights (including Gasoline) not more than 50 KGS. Its crankcase, crankshaft, central screws are all made of domestic high-performance materials by CNC processing method. With beautiful appearance, light-weight, high-precision, drop resistance, fatigue resistance, good stability, strong power performance, we get good reputations from home and abroad. Our company will be grateful for your valuable guidance and advice!!
Detail
| Exhaust amount | 360cc |
| Output | 38HP |
| Cylinder Bore/ Stroke | 53MM/41MM |
| speed range | 1200-5800 RPM |
| Pulling force | 90KG/1000 Meter altitude |
| Cylinder arrangement | four boxer |
| Fuel | Gasoline + 2T synthetic oil |
| Lubrication Ratio | 25:1~30: 1(trial run) |
| Compression Ratio | 8.6:1 |
| Propeller Recommended | 36*10,38*8,34*8,34*12, 36*10,36*12 recommended |
| Spark Plug | DLA CM6,Iridium |
| Voltage | 6.6v-8.4v, 2 LiPo batteries recommended. |
| Weight | Main engine: 7280g Exhaust pipe: 240g Ignition: 180g*2 standoffs: 22*4g |
| Customization | According to Customer’s need and specifications |
| Others |
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