TECHNICAL PAPERS: Gas Turbines: Aircraft Engines

Thermomechanical Design of a Heat Exchanger for a Recuperative Aeroengine

[+] Author and Article Information
Harald Schoenenborn, Ernst Ebert, Burkhard Simon, Paul Storm

MTU Aero Engines, Dachauer Str. 665, Muenchen 80995, Germany

J. Eng. Gas Turbines Power 128(4), 736-744 (Sep 18, 2006) (9 pages) doi:10.1115/1.1850510 History: Received October 01, 2003; Revised March 01, 2004; Online September 18, 2006
Copyright © 2006 by ASME
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Broichhausen, K., Scheugenpflug, H., Mari, Ch., Barbot, A., 2000, “CLEAN The European Initiative Towards Ultra Low Emission Engines,” ICAS 2000, Harrogate, UK.
Wilfert, G., and Massé, B., 2001, “Technology Integration in a Low Emission Heat Exchanger Engine,” Proceedings of the 8th CEAS European Propulsion Forum, Nottingham, UK.
Scheugenpflug,  H., Wilfert,  G., and Simon,  B., 2001, “Erfüllung zukünftiger Umweltanforderungen durch den Einsatz eines Wärmetauschertriebwerks,” DGLR-Jahrbuch, 3, pp. 1647–1654.
Pellischek, G., and Reile, E., 1992, “Compact Energy Recovery Units for Vehicular Gas Turbines,” SAE Paper 920151.
Pellischek, G., and Kumpf, B., 1991, “Compact Heat Exchanger Technology for Aero Engines,” ISABE Paper 91-7019.
Eggebrecht, R., and Schlosser, W., 1986, “Kompakter Hochtemperatur-Wärmetauscher für Wellenleistungsturbinen,” MTZ Motortechnische Zeitschrift, 47 , pp. 235–241.
Duffy, R. J., and Hower, G. K., 1987, “Turbine Propulsion for Heavy Armored Vehicles,” AIAA Paper 87-1911.
Brockett, W., and Koschier, A. V., 1992, “LV100 AIPS Technology-for Future Army Propulsion,” ASME Paper 92-GT-391.
Koschier, A. V., and Mauch, H. R., 1999, “Advantages of the LV100 as a Power Producer in a Hybrid Propulsion System for Future Fighting Vehicles,” ASME Paper 99-GT-416.
Goulas,  A., Katheder,  K., Palikaras,  A., and Yakinthos,  K., 2003, “Flow Measurements and Investigations in a Staggered Tube Matrix of a Heat Exchanger,” Int. J. of Heat & Technology, 21(2).


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IRA—intercooled recuperative aeroengine concept
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Profile tube matrix cross section
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Advective flow network of the thermal model
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Interaction between advective flow network and material mesh at a profile tube
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Nondimensional transient behavior of boundary conditions during acceleration
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Temperature distribution at takeoff conditions
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Transient temperature response at selected profile tube locations during minicycle
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FE model structure mechanics
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Static Mises stress during takeoff
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Mission temperature and pressure
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Example evaluation creep calculation
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Stress response at 1 g excitation at location of maximum stress (Mises)
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Vibration stress distribution



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