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Optimization of the rotor tip seal with honeycomb land in a gas turbine

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Citation (Scopus)

Abstract

The goal of the presented work is an optimization of the tip seal with honeycomb land in order to reduce the leakage flow in the counter-rotating LP turbine of an open rotor aero engine. The goal was achieved in two ways: by means of the commercial software delivered by ANSYS with the Goal Driven Optimization tool and with the use of an in-house optimization code based on the evolutionary algorithm. A detailed study including mesh generation, computational domain simplification, geometry variants and a comparison of both methods is presented. The optimization methods give very similar optimal geometry configurations, where a significant mass flow rate reduction through the seal was obtained. Moreover, a sensitivity analysis and the results verification are presented.

Original languageEnglish
Title of host publication9th European Conference on Turbomachinery
Subtitle of host publicationFluid Dynamics and Thermodynamics, ETC 2011 - Conference Proceedings
EditorsM. Sen, G. Bois, M. Manna, T. Arts
PublisherIstanbul Technical University
Pages43-55
Number of pages13
ISBN (Electronic)9789755613901
Publication statusPublished - 2011
Event9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011 - Istanbul, Turkey
Duration: 21 Mar 201125 Mar 2011

Publication series

Name9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011 - Conference Proceedings
Volume1

Conference

Conference9th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2011
Country/TerritoryTurkey
CityIstanbul
Period21/03/1125/03/11

ASJC Scopus subject areas

  • Condensed Matter Physics
  • Automotive Engineering
  • Mechanics of Materials
  • Mechanical Engineering

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