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Preliminary Gas Turbine Design Using the Multidisciplinary Design System MOPEDS

[+] Author Affiliations
Peter Jeschke, Joachim Kurzke, Reinhold Schaber, Claus Riegler

MTU Aero Engines GmbH, Munich, Germany

Paper No. GT2002-30496, pp. 75-84; 10 pages
doi:10.1115/GT2002-30496
From:
  • ASME Turbo Expo 2002: Power for Land, Sea, and Air
  • Volume 1: Turbo Expo 2002
  • Amsterdam, The Netherlands, June 3–6, 2002
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 0-7918-3606-1 | eISBN: 0-7918-3601-0
  • Copyright © 2002 by ASME

abstract

A prototype preliminary design task for gas turbines is set up to outline the four major requirements a preliminary design program must typically meet: assessment of all major engine components and their interrelations; inclusion of all relevant disciplines; designing over several operating points; and model fidelity zooming at least for individual components. It is described how the “MOdular Performance and Engine Design System” (MOPEDS) — MTU Aero Engines’ software package for the preliminary design of airborne and stationary gas turbines — fulfills these requirements. The program structure, the graphical user interface, and the physical models are briefly presented. A typical design example is carried out emphasizing the necessity for a numerical procedure to find a solution to the many variables and constraints that the design problem comprises. Finally, some dominating multidisciplinary effects are discussed.

Copyright © 2002 by ASME
Topics: Design , Gas turbines

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