New Mathematical and Software Method at Logic and Condition Monitoring System of Helicopter Turboshaft

Following a dramatic increase in the use of helicopters and increase in turboshafts to the global market,it isnecessary for these helicopters tobe tested in order toensure their engines arein good working order. Since the engine is its palpitating heart of every aircraft system,the software utilizes a thermodynamic model to assist a helicopter’s engine in stabilize and standby conditions. With the assistance of this software, it is possible to predict the effects of engine defects on the measured performance of the aircraft. A two-step process hasbeen designed to determine the maximum output power of a real turboshaft engine without requiring a motor operating at maximum power. The similar software in this field of engine design, the GSP and GasTurb10 can be named but none of them are specialized in field of turboshaft.

Keywords:

condition monitoring , gas turbine , turboshaft , performance , error detection