ROTO 35 FS AL
Single cylinder four-stroke air-cooled petrol internal combustion engine
ROTO 35 FS AL is suitable for UAV projects within the range of 4 meters and weight up to 25 kg.
Properties of ROTO 35 FS AL
| Engine capacity | 34,3 ccm |
| Fuel consumption | 400-600 g/h |
|
Power |
1,5 kW |
| Engine weight | from 1740 g |
| Arrangement of the engine | single cylinder |
| Cooling | air-cooled |
| Lubrication | petrol 95 oct. + 2% oil |
| Speed | 1400 – 6500 rpm |
| Speed with alternator | 2200 – 6500 rpm (limiter) |
| Ceiling | 5000 metres above sea level |
| Fuel system | Carburettor (+Altimeter unit) |
| Flight modes (lifetime) | 200 hours if TBO is kept |
Engine ROTO 35 FS AL can be fitted with:
ROTO E-Control Remote Control Management
Roto E-control is an electronic system designed to control the motor generator, which allows the start of the internal combustion engine, charging batteries and hybrid operation, increasing the power of the internal combustion engine (so-called afterburning).
| Operating temperature: | -20°C to +80°C |
| Non-operational voltage: | 9 - 60V DC |
| Charging current: | 45A |
| Peak power (10 sec): | 4300W |
| Peak current (10 sec): | 100A |
| Safe voltage: | 11 - 55V DC |
| Operating voltage: | 12 - 51V DC |
| Battery conguration: | 12 S |
| Battery nominal voltage: | 43.2V DC |
| PWM frequency: | 20 kHz |
Controller thermally connected to infinite heat sink which does not exceed 60°C.
| Maximal power dissipation: | 20W |
| Nominal power (60 min): | 2200W |
| Nominal current (60 min): | 51A |
Controller placed in still air of temperature 25°C.
| Maximal power dissipation: | 10W |
| Nominal power (60 min): | 1500W |
| Nominal current (60 min): | 35A |
Engine Fuel Injection
The Engine Management is designed to manage and control petrol engines from one central Injector to four sequential Injectors.
The Engine Management does not need to be connected to a PC, which is often difficult when running petrol engines in the given environment.
Engine Management - Main Unit
-
sequence control of 1 to 4 Injectors
- one Injector – one, two, four-cylinder engine
- two Injectors – two-cylinder engine with sequential control, or
-
four-cylinder engine – one pair = one Injector
- four Injectors – four-cylinder engine with sequential control
-
6x temperature input
- CHT, EGT, water, oil sensors
- fuel level sensor – capacitance fuel sensor
- fuel consumption measurement
-
2x voltage measurement
- Main power supply
- Servomotor power supply
-
fuel pressure measurement with possibility Fuel Pump regulation
- constant (adjustable) power Fuel Pump – mechanical press. regulator
- automatic Fuel Pump – adjustable fuel pressure
- wideband oxygen sensor
- ECO and MAX Power mode
- timers
- choice litter or gallon
- choice °C or °F
- Export data to flight computer
Control Module
Alternator
| Alternator 300W | Alternator 600W | |
|---|---|---|
| PMG ( Permanent Magnet Generator) | 3 phase output | |
| NdFeB magnets | ||
| Voltage curve | 14V/1000RPM (possibility of rewinding according to client) | |
| Diameter | 101mm | |
| Thickness | 22mm | 25mm |
| Weight | 450g | 550g |
| Out. Power at 3000RPM | 300W | 430W |
| Out. Power at 6000RPM | 600W | 960W |
| Cooling | forced by air flow | |
| Resistance | to fuel, oil, water, mechanical stress | |
| Operating temperature | -30°C to 120°C | |
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