Effect of turbine inlet temperature on blade tip leakage flow and heat transfer

Sung In Kim, Md Hamidur Rahman, Ibrahim Hassan

Research output: Chapter in Book/Report/Conference proceedingConference contribution

6 Citations (Scopus)

Abstract

One of the most critical gas turbine engine components, rotor blade tip and casing, are exposed to high thermal load. It becomes a significant design challenge to protect the turbine materials from this severe situation. As a result of geometric complexity and experimental limitations, Computational Fluid Dynamics (CFD) tools have been used to predict blade tip leakage flow aerodynamics and heat transfer at typical engine operating conditions. In this paper, the effect of turbine inlet temperature on the tip leakage flow structure and heat transfer has been studied numerically. Uniform low (LTIT: 444 K) and high (HTIT: 800 K) turbine inlet temperature have been considered. The results showed the higher turbine inlet temperature yields the higher velocity and temperature variations in the leakage flow aerodynamics and heat transfer. For a given turbine geometry and on-design operating conditions, the turbine power output can be increased by 1.48 times, when the turbine inlet temperature increases 1.80 times. Whereas the averaged heat fluxes on the casing and the blade tip become 2.71 and 2.82 times larger, respectively. Therefore, about 2.8 times larger cooling capacity is required to keep the same turbine material temperature. Furthermore, the maximum heat flux on the blade tip of high turbine inlet temperature case reaches up to 3.348 times larger than that of LTIT case. The effect of the interaction of stator and rotor on heat transfer features is also explored using unsteady simulations.

Original languageEnglish
Title of host publicationProceedings of the ASME Turbo Expo 2009: Power for Land, Sea and Air
Pages1773-1782
Number of pages10
Volume7
EditionPART B
DOIs
Publication statusPublished - 2009
Externally publishedYes
Event2009 ASME Turbo Expo - Orlando, FL, United States
Duration: 8 Jun 200912 Jun 2009

Other

Other2009 ASME Turbo Expo
CountryUnited States
CityOrlando, FL
Period8/6/0912/6/09

Fingerprint

Intake systems
Turbomachine blades
Turbines
Heat transfer
Temperature
Heat flux
Aerodynamics
Rotors
Flow structure
Thermal load
Stators
Gas turbines
Computational fluid dynamics
Engines
Cooling

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Kim, S. I., Rahman, M. H., & Hassan, I. (2009). Effect of turbine inlet temperature on blade tip leakage flow and heat transfer. In Proceedings of the ASME Turbo Expo 2009: Power for Land, Sea and Air (PART B ed., Vol. 7, pp. 1773-1782) https://doi.org/10.1115/GT2009-60143

Effect of turbine inlet temperature on blade tip leakage flow and heat transfer. / Kim, Sung In; Rahman, Md Hamidur; Hassan, Ibrahim.

Proceedings of the ASME Turbo Expo 2009: Power for Land, Sea and Air. Vol. 7 PART B. ed. 2009. p. 1773-1782.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Kim, SI, Rahman, MH & Hassan, I 2009, Effect of turbine inlet temperature on blade tip leakage flow and heat transfer. in Proceedings of the ASME Turbo Expo 2009: Power for Land, Sea and Air. PART B edn, vol. 7, pp. 1773-1782, 2009 ASME Turbo Expo, Orlando, FL, United States, 8/6/09. https://doi.org/10.1115/GT2009-60143
Kim SI, Rahman MH, Hassan I. Effect of turbine inlet temperature on blade tip leakage flow and heat transfer. In Proceedings of the ASME Turbo Expo 2009: Power for Land, Sea and Air. PART B ed. Vol. 7. 2009. p. 1773-1782 https://doi.org/10.1115/GT2009-60143
Kim, Sung In ; Rahman, Md Hamidur ; Hassan, Ibrahim. / Effect of turbine inlet temperature on blade tip leakage flow and heat transfer. Proceedings of the ASME Turbo Expo 2009: Power for Land, Sea and Air. Vol. 7 PART B. ed. 2009. pp. 1773-1782
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