The EP-10 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. EP-10 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℃(JET Fuel),Throttle Position ≥ 25% | ||
Weight | 6.5 | Fuel Consumption | 450/kW·h |
Rated Power | 10.5kW@6500rpm | Generator | Customized |