Features:
1. The cylinder head and cylinders are fully water-cooled, with better cooling and better reliability performance, while the benchmark product uses cylinder head with water cooling & cylinder block in air cooling;
2. Carburetor and EFI versions are optional;
3. Maximum ceiling Up to 10,000 meters (MIL version is optional), while the others has a maximum ceiling of 7,000 meters;
4. Integrated 6 or 9kw one key starter options available to meet up wide range of airborne applications, while the others only has a 250w generator;
5. Helicopter version optional;
6. Short leading time in 1-2 months, while the others is 3-12 months;
7. It has integrated propeller-engine matching Technology, self-developed ZP3VELD1920/1900 variable-pitch propeller (compared to fixed-pitch propellers, it can improve ground static thrust, fuel economy and high-altitude efficiency are higher);
8. Cost advantage, the procurement cost is 15-20% lower than the others
The 700-1600kg fixed-wing manned/unmanned aircraft and the 600kg unmanned helicopter/rotorcraft
The engine body (need to check with the customer whether there is an overload clutch) also includes: fuel pump (2), overflow bottle (1), fuel filter
(1), air filter (1), exhaust system kit (1), oil temperature sensor (1), liquid temperature sensor (4)