PMP360S 4 is a 2 cylinder opposed, 4 stroke water-cooled gasoline piston engine.
Equipped with high-efficiency alternator and self-starting motor, the fuel injection ignition adopts EFI control mode. Has good performance characteristics: Long life, low fuel consumption, high power-to-weight ratio, low noise, etc.
Suitable for small Long-endurance UAV,small unmanned helicopters, small fixed-wing unmanned aerial vehicles and power parachutes.
PMP360S 4 stroke piston engine consists of an engine system and a generating unit (optional).
The engine system consists of crankcase assembly, crankshaft connecting rod assembly, piston assembly, cylinder block, cylinder head assembly, intake and exhaust system, timing system, etc.
Type: 2 cylinder opposed, 4 stroke water-cooled, ignition piston engine
Dimension: 580mm×340mm×400mm
Bore: 63mm
Stroke: 58mm
Displacement: 362ml
Net weight: ≯26kg
Max. power: 26kW@8250rpm
Min. fuel consumption rate: ≯300g/ kW.h
Limited altitude: 4000m
Feeding mode: EFI
Ambient temperature: -20℃~+50℃
TBO: ≮1000 h
Generation Unit and Technical Parameters
Power generation unit including efficient generators and ACDC modules,which can provide power for UAV airborne equipment. (Optional)
Type: coaxial generator with outer rotor
Generator weight: 900g
ACDC weight: 950g
Working temperature: -30℃~65℃
Power: output power 300W≥at 6500rpm
Out put voltage:at 6500rpm, three-phase on-load output voltage≥35V.
PMP360S 型四冲程活塞发动机由发动机系统和发电单元组成,
发电单元为选配件,可根据用户要求进行选配。
发动机系统及技术参数
PMP360S 型四冲程活塞发动机由曲轴箱组件、曲轴连杆组件、
活塞组件、缸体、缸头组件、进排气系统、正时系统等组成。
型式: 双缸对置、四冲程水冷、点燃式活塞发动机
尺寸: 580mm×340mm×400mm
缸径: 63mm
行程: 58mm
排量: 362ml
本体干量: ≯26kg
最大功率: 26kW@8250rpm
最低燃油消耗率: ≯300g/ kW.h
最大使用高度: 4000m
供油方式: 电喷
环境工作温度: -20℃~+50℃
发动机寿命: ≮1000 小时
发电单元及技术参数
发电单元包含高效率发电机和 ACDC 模块,为无人机机载设备
提供用电,可根据用户要求进行选配。
电机类型: 外转子同轴发电机
发电机重量: 900g
ACDC 模块重量: 950g
使用温度: -30℃~65℃
发电功率: 发动机转速6500rpm 时,输出功率不低于
300W
输出电压: 发动机转速6500rpm 时,三相带载输出电压
不低于35V