Experimental measurements of ingestion through turbine rim seals. Part 1 : externally induced ingress
Sangan, C. M., Pountney, O., Zhou, K., Wilson, M., Owen, J. M. and Lock, G., 2013. Experimental measurements of ingestion through turbine rim seals. Part 1 : externally induced ingress. Journal of Turbomachinery: Transactions of the ASME, 135 (2), 021012.
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This paper describes a new research facility which experimentally models hot gas ingestion into the wheel-space of an axial turbine stage. Measurements of the CO2 gas concentration in the rim-seal region and inside the cavity are used to assess the performance of two generic (though engine-representative) rim-seal geometries in terms of the variation of concentration effectiveness with sealing flow rate. The variation of pressure in the turbine annulus, which governs this externally-induced (EI) ingestion, was obtained from steady pressure measurements downstream of the vanes and near the rim seal upstream of the rotating blades. Although the ingestion through the rim seal is a consequence of an unsteady, three-dimensional flow field and the cause-effect relationship between the pressure and the sealing effectiveness is complex, the experimental data is shown to be successfully calculated by simple effectiveness equations developed from a previously published orifice model. The data illustrate that, for similar turbine-stage velocity triangles, the effectiveness can be correlated using a nondimensional sealing parameter, phio. In principle, and within the limits of dimensional similitude, these correlations should apply to a geometrically-similar engine at the same operating conditions. Part II of this paper describes an experimental investigation of rotationally-induced (RI) ingress, where there is no mainstream flow and consequently no circumferential variation of external pressure.
|Creators||Sangan, C. M., Pountney, O., Zhou, K., Wilson, M., Owen, J. M. and Lock, G.|
|Departments||Faculty of Engineering & Design > Mechanical Engineering|
|Research Centres||Aerospace Engineering Research Centre|
|Additional Information||Best Paper award from the Heat Transfer Committee of the ASME International Gas Turbine Institute.|
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