Product Description
ZS12H is a family of two-stroke, two-cylinder horizontally opposed, engines designed for It can be small drones, long-duration drones, forest fire drones, and vertical takeoff and landing drones. , Fixed wings. It has the characteristics of low fuel consumption and high power-to-weight ratio, it’s reliability and stability.
Provide professional maintenance and technical support services.
Applications:
Small long endurance UAV, Shipborne UAV etc.
Product Advantages
Low fuel consumption rate: The lowest fuel consumption rate of the engine’s universal characteristics is <280g / kW.h.
High power-to-weight ratio: The dry weight of the engine is 5kg, and the power-to-weight ratio is 2.2kW / kg.
Excellent low-pressure startability: meets 5000 meters altitude starting.
Excellent low temperature startability: no auxiliary heating measures at room temperature, starting time <2s, no auxiliary heating measures at -20 ° C, no starting heating time of 2.7s, no auxiliary heating measures at -30°C, no starting heating time of 4.5s.
Convenient and efficient after-sales support: 24-hour service response system, providing professional product maintenance, repair services and training, and technical support services.
Customized development support: Designed development can be carried out according to customer needs to make the product more in line with customer needs.
High power-to-weight ratio: The dry weight of the engine is 5kg, and the power-to-weight ratio is 2.2kW / kg.
Excellent low-pressure startability: meets 5000 meters altitude starting.
Excellent low temperature startability: no auxiliary heating measures at room temperature, starting time <2s, no auxiliary heating measures at -20 ° C, no starting heating time of 2.7s, no auxiliary heating measures at -30°C, no starting heating time of 4.5s.
Convenient and efficient after-sales support: 24-hour service response system, providing professional product maintenance, repair services and training, and technical support services.
Customized development support: Designed development can be carried out according to customer needs to make the product more in line with customer needs.
Technical Parameters
WEIGHT |
KG |
|
| Engine with propeller speed reduction drive | 5 | |
| Exhaust system | – | |
| PERFORMANCE | ||
| 11 kW | 15 hp | 7500 RPM |
| MAX RPM | 7500 RPM | |
| BORE | STROKE | |
| 52 mm | 40 mm | |
| DISPLACEMENT | FUEL | |
| 170 cm³ | RP-3 aviation kerosene, 95 # gasoline, diesel | |
External characteristic curve
Height characteristic curve
