.ClaRa.Components.TurboMachines.Turbines.TurbineGas_L1_stageStacked

Information

Model description: A multi stage compressor model based on the stage stacking method of Gasparovic able to calculate off-design behaviour according to nominal values

FEATURES

• This model uses TILMedia
• Stationary mass and energy balances are used
• Modeled according to the stage stacking method of Gasparovic
• Supports multi stage VIGV's
• Calculation of surge and choke margins (assert triggers when crossed)

NOTE: If the design point is not known please determine all needed values with simplier compressor models to ensure the model to run.

For detailed model documentation please consult the html-documentation shipped with ClaRa.

Authorship and Copyright Statement for original (initial) Contribution

Author:

References:

For references please consult the html-documentation shipped with ClaRa.

Remarks:

This component was developed by ClaRa development team under the 3-clause BSD License.

ClaRa originated from the collaborative research projects DYNCAP and DYNSTART. Both research projects were supported by the German Federal Ministry for Economic Affairs and Energy (FKZ 03ET2009 and FKZ 03ET7060).

CLA:

The author(s) have agreed to ClaRa CLA, version 1.0. See https://claralib.com/pdf/CLA.pdf

By agreeing to ClaRa CLA, version 1.0 the author has granted the ClaRa development team a permanent right to use and modify his initial contribution as well as to publish it or its modified versions under the 3-clause BSD License.

The ClaRa development team consists of the following partners:

TLK-Thermo GmbH (Braunschweig, Germany)

XRG Simulation GmbH (Hamburg, Germany).

Contents

Name	Description
Outline
Summary

Revisions

For revisions please consult the html-documentation shipped with ClaRa.