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contributor authorLi, Zhihui
contributor authorChristodoulou, Loizos
contributor authorJefferson-Loveday, Richard
contributor authorAmbrose, Stephen
contributor authorJackson, Richard
contributor authorLock, Gary D.
contributor authorSangan, Carl M.
contributor authorScobie, James A.
date accessioned2024-04-24T22:50:52Z
date available2024-04-24T22:50:52Z
date copyright1/29/2024 12:00:00 AM
date issued2024
identifier issn0889-504X
identifier otherturbo_146_6_061004.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295979
description abstractThe windage torque on rotational walls has a negative effect on the performance of the low-pressure turbine. In this paper, three novel flow control concepts (FCCs) were proposed to reduce the windage torque within a turbine stator well, with upstream and downstream cavities connected by an interstage labyrinth seal. The swirl and flow pattern inside a reference turbine cavity was first investigated and the potential locations for the FCCs were identified using numerical simulations. FCC1 was a circumferential row of leaned deflectors downstream of the labyrinth seal. FCC2 was a set of deflector vanes and platform to optimize the ingress swirl at high radius in the upstream cavity. FCC3 combined the two flow concepts and the superposition resulted in a stator well windage torque reduction of 70% when compared to the baseline design. The FCCs also showed performance benefits at off-design conditions and over a range of secondary flow rates to the cavity. In Part II, the numerical analysis and performance of the FCCs are validated in an experimental rig using additively manufactured components.
publisherThe American Society of Mechanical Engineers (ASME)
titleWindage Torque Reduction in Low-Pressure Turbine Cavities Part I: Concept Design and Numerical Investigations
typeJournal Paper
journal volume146
journal issue6
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4064224
journal fristpage61004-1
journal lastpage61004-9
page9
treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 006
contenttypeFulltext


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