Description:
The 183CC 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. 183CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 60kg~80kg.
| Configuration | 2Cyl. Horizontally Opposed | Displacement | 183ml |
| Bore × Stroke | 54m×40m | Speed Range | 2000rpm~6700rpm |
| Compression Ratio | 10.1:1 | ||
| 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 | 6.5 | Fuel Consumption | 450/kW·h |
| Rated Power | 10.5kW@6500rpm | Generator | Customized |
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