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Robust Design of a Gas Turbine Engine Secondary Flow System

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Two turbine blades from the same engine. Note the difference in condition. ... Blade Oxidation Life ... roughly 15% of the blades will fail before 2800 hours! ... – PowerPoint PPT presentation

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Title: Robust Design of a Gas Turbine Engine Secondary Flow System


1
Robust Design of a Gas Turbine Engine Secondary
Flow System
Vince Sidwell, Prof. Dave Darmofal
  • Motivation
  • Gas turbine engine performance and durability
    relies on the performance of the secondary flow
    system.
  • The variability in the performance of the
    secondary flow system appears to be linked to
    shortfalls in engine durability.
  • Research Objectives
  • Determine a method to peform robust design on gas
    turbine engine secondary flow systems.
  • Determine the characteristics of a robust
    secondary flow system.

Two turbine blades from the same engine. Note
the difference in condition.
2
Robust Design of a Gas Turbine Engine Secondary
Flow System
Secondary Flow System
Region of Interest
Combustor
Minidisk
Turbine Disk
3
Robust Design of a Gas Turbine Engine Secondary
Flow System
Example of Variability
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