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GSP 10 Components

Gas Path Component Library (standard)

inlet fan compressor duct combustor turbine flow mixer exhaust nozzle heat exchanger (recuperator) link

Control Component Library (standard)

manual fuel control exhaust nozzle control load control bleed control gas generator governor fuel control power turbine control (turboshaft)

Supplementary Component Library (licensed)

custom gas composition inlet    define the medium that enters the gas turbine multi reactor combustor    divide the combustor in segments flow splitter    splits the flow into two separate flows heat exchanger with dynamic effects    heat soakage and heat capacity are taken into account pressure vessel back pressure exhaust    model the back pressure as a result of a boiler in the exhaust intercooler    cools the (compressed) medium propeller    fixed pitch propeller, constant speed propeller flow splitter controller    controls the splitting of the flow splitter pressure/temperature vessel control    controls the pressure and temperature of the pressure vessel intercooler control    controls the amount of coolant in the intercooler component fuel mixer    mixes two types of user specified composition fuels back pressure exhaust control    controls the pressure at the end of the back pressure exhaust component PLA controlled exhaust nozzle control rotor speed control    the free state fuel flow can be calculated since the rotor speed is set thrust control    the free state fuel flow can be calculated since the thrust is set bleed scheduler    schedule the bleed air as function of corrected rotor speed flight scheduler    creates a set of ambient conditions to represent the flight envelope of a certain engine design point sweep component    calculate design point sweeps for selected parameters equation schedule control    control engine based on user specified equation (output parameter or component    property parameter) 1-D table look-up schedule control    control engine based on user specified equation using a 1-D look-up table map schedule control    control engine based on user specified equation using a map generic schedule control    This powerfull schedule control component contains functionality of last 3 schedule    control components. Generic Power Control    generic engine power control component simple After Burner Control    revision of PLA controlled after burner control now containg many more options to control AB limiter    define limits to limit certain engine parameters property control    directly modify engine parameters during calculation design point equation control    incorporate design point iteration in your engine model installation effects    incorporate installation effects in your engine model

STOVL Component Library (licensed)

lift fan inlet lift fan clutch lift fan exhaust convergent exhaust nozzle control FADEC fuel control

Additional Components / Libraries

More components have been developed over the years to assist in gas turbine modeling of specific applications, e.g.: F100-PW-220 control component library F100-PW-229 control component library adaptive model component custom output (to file) components ABCD matrix generator components (for control system design) load/life usage component gasifier components library adaptive modeling library