Title page for ETD etd-07082003-080311

Type of Document Master's Thesis
Author Couch, Eric L.
Author's Email Address ecouch@vt.edu
URN etd-07082003-080311
Title Measurements of Cooling Effectiveness Along the Tip of a Turbine Blade
Degree Master of Science
Department Mechanical Engineering
Advisory Committee
Advisor Name Title
Thole, Karen A. Committee Chair
Dancey, Clinton L. Committee Member
King, Peter S. Committee Member
  • microcircuit
  • blade heat transfer
  • film-cooling
  • gas turbines
  • tip gap
Date of Defense 2003-06-20
Availability unrestricted
In a gas turbine engine, turbine blades are exposed to temperatures above their melting point. Film-cooling and internal cooling techniques can prolong blade life and allow for higher engine temperatures. This study examines a novel cooling technique called a microcircuit, which combines internal convection and pressure side injection on a turbine blade tip. Holes on the tip called dirt purge holes expel dirt from the blade, so other holes are not clogged. Wind tunnel tests are used to observe how effectively dirt purge and microcircuit designs cool the tip. Tip gap size and blowing ratio are varied for different tip cooling configurations.

Results show that the dirt purge holes provide significant film cooling on the leading edge with a small tip gap. Coolant injected from these holes impacts the shroud and floods the tip gap reducing tip leakage flow.

With the addition of a microcircuit, coolant is delivered to a larger area of the tip. In all cases, cooling levels are higher for a small tip gap than a large tip gap. Increased blowing ratio does not have a dramatic effect on microcircuit film-cooling at the midchord but does improve internal cooling from the microcircuit. While the combined dirt purge holes and microcircuit cool the leading edge and midchord areas, there remains a small portion of the trailing edge that is not cooled. Also, results suggest that blowing from the microcircuit diminishes the tip leakage vortex. Overall, the microcircuit appears to be a feasible method for prolonging blade life.

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  Appendix.pdf 7.49 Mb 00:34:41 00:17:50 00:15:36 00:07:48 00:00:39
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