The PBS TP100
turboprop engine is suitable for small aircraft and UAVs. The system is designed for use in both pusher and tractor configuration.
Its main advantage is low weight, power of 180 kW and its capacity to achieve flight altitude of 9,000 m with a maximum starting altitude of 6,000 m. The turbine engine is able to start in cold conditions as low as - 30 °C without preheating.
The engine is equipped with autonomous oil and fuel systems, BLDC electric starter-generator and digital engine control unit (ECU). The ECU ensures automatic after-cooling of hot parts after an engine stop. The propeller governor maintains a constant propeller speed.
The engine could be controlled by the analogue interface (control voltage) or by the digital interface (based on CAN Aerospace V1.7 protocol). The engine parameters for cockpit multifunction display are available only in digital format.
: digital control system (ECU), connecting cable
ignition, electromagnetic fuel valve, boost pump, speed governor, speed limiter, oil cooler
alternator, EMS display unit, control lever, thermostatic valve, and others