Light aircraft electric propulsion system 45KW
for ULM40 kW...60 kWhybrid

light aircraft electric propulsion system
light aircraft electric propulsion system
light aircraft electric propulsion system
light aircraft electric propulsion system
light aircraft electric propulsion system
light aircraft electric propulsion system
light aircraft electric propulsion system
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Characteristics

Application
for light aircraft, for ULM
Engine power
40 kW...60 kW
Type
hybrid, brushless

Description

We have done HUNDREDS OF HOURS of testing the setups that helped us to find OPTIMAL SOLUTIONS for our customers. We always recommend combinations of products based on our EXPERTISE and EXPERIENCE from laboratory testing as well as testing in REAL APPLICATIONS. Our solutions are successfully used in many CHALLENGING PROJECTS in AVIATION, MARINE, and GROUND VEHICLES. max continuous power1 100 kW voltage 400 V max continuous current1 400 A peak current 560 A cooling1 air/fluid monitoring complex data monitoring COMMUNICATION CAN | RS232 | RS485 MOTOR SENSORS 3 Hall sensors CONTROL SIGNALS PWM | potentiometer | voltage | data | log.signal VARIOUS ADJUSTABLE PARAMETERS VERY HIGH EFFICIENCY 98-99% EMERGENCY DISCONNECTION Safe to disconnect during the operation. COMPLETE GALVANIC INSULATION INTERNAL DATA LOGGING (BLACKBOX) Reports 22 parametres. SUPPORT OF EXTERNAL DISPLAY UNITS Real time monitoring of important values. torque 250 Nm max power1 60 kW rpm2 4000 max continuous power1 35-45 kW diameter 271 mm voltage 400-800 V motor sensors sensored / sensorless cooling air/hybrid (fluid+air)

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.