Description:
The 312CC engine is an air cooled horizontally opposed piston engine with dual-redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 312CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 80kg~ 100kg.
| Configuration | 2Cyl. Horizontally Opposed | Displacement | 312ml |
| Bore × Stroke | 65mm×47mm | Speed Range | 1600rpm~7000rpm |
| Compression Ratio | 10.6:1 | ||
| Lubrication | Oil Gas Lubrication | Fuel Delivery | Electronic Fuel Injection |
| Fuel Type | 3# JET Fuel (or 92# Gasoline and Above, Aviation Gasoline) | ||
| Starting Method | External Starter Starting, Integrated Starter Starting | ||
| Starting Conditions | Cylinder Temperature ≥ 85 Celsius (JET Fuel),Throttle Position ≥ 25% | ||
| Weight | 10.8kg | Fuel Consumption | 410g/kW·h |
| Rated Power | 4.1kW@8000rpm | Generator | Customized |
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