TurboPropEngine

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The TurboPropEngine logic component handles the motion model for turbo prop engines.

Type: Logic Object Component
File: TurboPropEngine.slc
Version: 450.1000.355.1


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Icon properties.png Properties

NameDescriptionMaxValueMinValueDisplayNameUnitTypeUnitName
PROP_ENGINE_PARAMS_FILE_NAME  The file that defines the engine params    File System  File 
PROP_IS_STARTER_AUTO_RETURN_WHEN_STARTED  When starting the engine, is it automatically return to ON when the engine is started     Default  Default 
PROP_THRUST_MULTIPLIER  Set other than 1.0 to increase / secrease the thrust  100    Default  Default 

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Icon attributes.png Attributes

NameDescriptionParam1Param2DisplayNameUnitTypeUnitName
ATT_ENGINE_AMP  The alternator current  const int  float &    Default  Default 
ATT_ENGINE_FUEL_FLOW  The fuel flow  const int  float &    Volume Flow  Gallon Per Hour 
ATT_ENGINE_FUEL_VALVE_CMD  The engine fuel valve  const int  int &    Default  Default 
ATT_ENGINE_ITT  The engine inter turbine temperature  const int  float &    Temperature  Celsius 
ATT_ENGINE_MAX_FUEL_FLOW  The maximal engine fuel flow  float &      Volume Flow  Gallon Per Hour 
ATT_ENGINE_N1_PCT  The gas generator RPM percentage  const int  float &    Default  Default 
ATT_ENGINE_NUMBER_OF_STARTER_STAGES  The number of the starter stages  int &      Default  Default 
ATT_ENGINE_OIL_PRESS  The oil press  const int  float &    Pressure  PSI 
ATT_ENGINE_OIL_TEMP  The oil temperature  const int  float &    Temperature  Celsius 
ATT_ENGINE_PROPELLER_PITCH  The prop pitch Angle  const int  float &    Angle  Degree 
ATT_ENGINE_PROPELLER_REQUIRED_RPM  The required engine RPM for variable pitch engines  const int  float &    Angular Velocity  RPM 
ATT_ENGINE_PROPELLER_RPM  The prop RPM  const int  float &    Angular Velocity  RPM 
ATT_ENGINE_ROTOR_RPM  The fuel flow  const int  float &    Angular Velocity  RPM 
ATT_ENGINE_RPM  The attitude indicator  const int  float &    Angular Velocity  RPM 
ATT_ENGINE_RPM_FOR_SOUND  The engine RPM guage  float &      Angular Velocity  RPM 
ATT_ENGINE_STARTER_STATE  Starter state  const int  int &    Default  Default 
ATT_ENGINE_STATE  The engine state ( 0 - Off, 1 - On, 2 - Start)  const int  int &    Default  Default 
ATT_ENGINE_THRUST  The thrust produced [Nt.]  const int  float &    Force  Newton 
ATT_ENGINE_TORQUE  The torque produced by the engine shaft  const int  float &    Torque  Newton Meter 
ATT_ENGINE_VAC_PRESS  The vacum pressure  const int  float &    Pressure  PSI 
ATT_FEATHERING_CMD  Feathering cmd  const int  int &    Default  Default 
ATT_IS_MOTION_MODEL_UNIT  Is this SLC a part of the object's motion model  bool &      Default  Default 
ATT_MAGNETO_STATE  The magneto state  const int  int &    Default  Default 
ATT_PROPELLER_ADVANCED_RATIO  The propeller advanced ratio  const int  float &    Default  Default 
ATT_PROPELLER_DIAMETER  The propeller diameter  float &      Length  Meter 
ATT_PROPELLER_PITCH_CMD  The propeller pitch cmd array  const int  float &    Default  Default 
ATT_PROPELLER_POWER_COEFF  The propeller power coefficient  const int  float &    Default  Default 
ATT_PROPELLER_RPM  The prop RPM  const int  float &    Angular Velocity  RPM 
ATT_PROPELLER_THRUST_COEFF  The propeller thrust coefficient  const int  float &    Default  Default 
ATT_PROPELLER_TORQUE  The torque in the propeller shaft  const int  float &    Torque  Newton Meter 
ATT_THROTTLE_CMD  The throttle command array - value for each engine  const int  float &    Default  Default 
ATT_THROTTLE_FINE_CMD  The throttle fine command array - for the AP to use  const int  float &    Default  Default 

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Icon attributes.png Required Attributes

Name
ATT_BODY_VELOCITY 
ATT_CURRENT_MAX_FUEL_FLOW_AVAILABLE 
ATT_ENGINES_NUMBER 
ATT_IS_MOTION_MODEL_ENABLED 
ATT_IS_ON_GROUND 
ATT_IS_TO_STOP_HIGH_LEVEL_MODEL 
ATT_MANEUVERS_STACK_POINTER 
ATT_MANUEVER_ACTIVE_MANUEVER_STACK 
ATT_OUT_OF_FUEL 
ATT_POSITION 

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Icon actions.png Required Actions

Name
ACTION_ENGINE_START_STATUS_CHANGE 

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