Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall

A. A. Thrift, K. A. Thole, S. Hada

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

10 Citations (Scopus)

Abstract

First stage, nozzle guide vanes and accompanying endwalls are extensively cooled by the use of film cooling through discrete holes and leakage flow from the combustor-turbine interface gap. While there are cooling benefits from the interface gap, it is generally not considered as part of the cooling scheme. This paper reports on the effects of the position and orientation of a two-dimensional slot on the cooling performance of a nozzle guide vane endwall. Inaddition to surface thermal measurements, time-resolved, digital particle image velocimetry (TRDPIV) measurements were performed at the vane stagnation plane. Two slot orientations, 90° and 45°, and three stream wise positions were studied. Effectiveness results indicate a significant increase in area averaged effectiveness for the 45° slot relative to the 90°orientation. Flowfield measurements show dramatic differences in the horseshoe vortex formation.

Original languageEnglish (US)
Title of host publicationASME 2011 Turbo Expo
Subtitle of host publicationTurbine Technical Conference and Exposition, GT2011
Pages291-301
Number of pages11
EditionPARTS A AND B
DOIs
StatePublished - Dec 1 2011
EventASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011 - Vancouver, BC, Canada
Duration: Jun 6 2011Jun 10 2011

Publication series

NameProceedings of the ASME Turbo Expo
NumberPARTS A AND B
Volume5

Other

OtherASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011
CountryCanada
CityVancouver, BC
Period6/6/116/10/11

Fingerprint

Combustors
Turbines
Cooling
Nozzles
Time measurement
Velocity measurement
Vortex flow

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Thrift, A. A., Thole, K. A., & Hada, S. (2011). Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall. In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011 (PARTS A AND B ed., pp. 291-301). (Proceedings of the ASME Turbo Expo; Vol. 5, No. PARTS A AND B). https://doi.org/10.1115/GT2011-45507
Thrift, A. A. ; Thole, K. A. ; Hada, S. / Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall. ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011. PARTS A AND B. ed. 2011. pp. 291-301 (Proceedings of the ASME Turbo Expo; PARTS A AND B).
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abstract = "First stage, nozzle guide vanes and accompanying endwalls are extensively cooled by the use of film cooling through discrete holes and leakage flow from the combustor-turbine interface gap. While there are cooling benefits from the interface gap, it is generally not considered as part of the cooling scheme. This paper reports on the effects of the position and orientation of a two-dimensional slot on the cooling performance of a nozzle guide vane endwall. Inaddition to surface thermal measurements, time-resolved, digital particle image velocimetry (TRDPIV) measurements were performed at the vane stagnation plane. Two slot orientations, 90° and 45°, and three stream wise positions were studied. Effectiveness results indicate a significant increase in area averaged effectiveness for the 45° slot relative to the 90°orientation. Flowfield measurements show dramatic differences in the horseshoe vortex formation.",
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Thrift, AA, Thole, KA & Hada, S 2011, Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall. in ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011. PARTS A AND B edn, Proceedings of the ASME Turbo Expo, no. PARTS A AND B, vol. 5, pp. 291-301, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011, Vancouver, BC, Canada, 6/6/11. https://doi.org/10.1115/GT2011-45507

Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall. / Thrift, A. A.; Thole, K. A.; Hada, S.

ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011. PARTS A AND B. ed. 2011. p. 291-301 (Proceedings of the ASME Turbo Expo; Vol. 5, No. PARTS A AND B).

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

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Thrift AA, Thole KA, Hada S. Effects of orientation and position of the combustor-turbine interface on the cooling of a vane endwall. In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011. PARTS A AND B ed. 2011. p. 291-301. (Proceedings of the ASME Turbo Expo; PARTS A AND B). https://doi.org/10.1115/GT2011-45507