modelStep7BootStrapCycle

Extends from Modelica.Icons.Example (Icon for runnable examples).

Information

In a seventh step, compressor1 and turbine are connected via energy flow connectors, meaning the turbine drives the compressor. The pressurized air used to operate the air cycle can be supplied either by an electric compressor or directly by the aircraft engine.

The compressor outlet pressure depends on the turbine power, which in turn depends on the compressor outlet pressure, forming an implicit nonlinear equation loop. A suitable start value is required for this equation to be solvable.

Further documentation is available in the AirCycle package.

Components

TypeNameDefaultDescription
ThermofluidStream.DropOfCommonsdropOfCommons
ThermofluidStream.Idealized.Processes.Adiabaticcompressor
ThermofluidStream.Boundaries.SourceairSource
ThermofluidStream.Idealized.Processes.Isobariccooler
ThermofluidStream.Utilities.showRealValuecoefficientOfPerformance
.ThermofluidStream.Boundaries.Sink_mairSink
ThermofluidStream.Idealized.Processes.Isenthalpicvalve
Boundaries.MassFlowRatemassFlowRateSource
Modelica.Blocks.Sources.RampmassFlowRate
Modelica.Blocks.Sources.RampmassFlowRateValve
Topology.JunctionT1junctionT1_1
ThermofluidStream.Topology.SplitterT1splitter
ThermofluidStream.Idealized.Processes.Isobariccooler2
ThermofluidStream.Idealized.Processes.Adiabaticturbine
ThermofluidStream.Idealized.Processes.Adiabaticcompressor1

Contents

NameDescription
Medium

Revisions

  • 2026, by Raphael Gebhart (raphael.gebhart@dlr.de):
    Initial version.