Projects per year
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.
|Number of pages||10|
|Journal||Journal of Turbomachinery: Transactions of the ASME|
|Early online date||8 Nov 2012|
|Publication status||Published - 1 Mar 2013|
FingerprintDive into the research topics of 'Experimental measurements of ingestion through turbine rim seals. Part 1: externally induced ingress'. Together they form a unique fingerprint.
- 1 Finished
Measurement and Modelling of Ingress
Lock, G., Owen, M., Robinson, K. & Wilson, M.
Engineering and Physical Sciences Research Council
1/10/09 → 30/09/12
Project: Research council