TY - JOUR
T1 - Prediction of ingestion through turbine rim seals-part I
T2 - rotationally induced ingress
AU - Owen, J Michael
PY - 2011/11/12
Y1 - 2011/11/12
N2 - The mainstream flow past the stationary nozzle guide vanes and rotating turbine blades in a gas turbine creates an unsteady nonaxisymmetric variation in pressure in the annulus, radially outward of the rim seal. The ingress and egress occur through those parts of the seal clearance where the external pressure is higher and lower, respectively, than that in the wheel-space; this nonaxisymmetric type of ingestion is referred to here as externally induced (EI) ingress. Another cause of ingress is that the rotating air inside the wheel-space creates a radial gradient of pressure so that the pressure inside the wheel-space can be less than that outside; this creates rotationally induced (RI) ingress, which-unlike EI ingress-can occur, even if the flow in the annulus is axisymmetric. Although the EI ingress is usually dominant in a turbine, there are conditions under which both EI and RI ingress are significant, these cases are referred to as combined ingress. In Part I of this two-part paper, the so-called orifice equations are derived for compressible and incompressible swirling flows, and the incompressible equations are solved analytically for the RI ingress. The resulting algebraic expressions show how the nondimensional ingress and egress vary with 0, which is the ratio of the flow rate of sealing air to the flow rate necessary to prevent ingress. It is shown that , the sealing effectiveness, depends principally on 0, and the predicted values of are in mainly in good agreement with the available experimental data.
AB - The mainstream flow past the stationary nozzle guide vanes and rotating turbine blades in a gas turbine creates an unsteady nonaxisymmetric variation in pressure in the annulus, radially outward of the rim seal. The ingress and egress occur through those parts of the seal clearance where the external pressure is higher and lower, respectively, than that in the wheel-space; this nonaxisymmetric type of ingestion is referred to here as externally induced (EI) ingress. Another cause of ingress is that the rotating air inside the wheel-space creates a radial gradient of pressure so that the pressure inside the wheel-space can be less than that outside; this creates rotationally induced (RI) ingress, which-unlike EI ingress-can occur, even if the flow in the annulus is axisymmetric. Although the EI ingress is usually dominant in a turbine, there are conditions under which both EI and RI ingress are significant, these cases are referred to as combined ingress. In Part I of this two-part paper, the so-called orifice equations are derived for compressible and incompressible swirling flows, and the incompressible equations are solved analytically for the RI ingress. The resulting algebraic expressions show how the nondimensional ingress and egress vary with 0, which is the ratio of the flow rate of sealing air to the flow rate necessary to prevent ingress. It is shown that , the sealing effectiveness, depends principally on 0, and the predicted values of are in mainly in good agreement with the available experimental data.
UR - http://www.scopus.com/inward/record.url?scp=78449239271&partnerID=8YFLogxK
UR - http://dx.doi.org/10.1115/1.4001177
U2 - 10.1115/1.4001177
DO - 10.1115/1.4001177
M3 - Article
SN - 0889-504X
VL - 133
SP - 1
EP - 9
JO - Journal of Turbomachinery: Transactions of the ASME
JF - Journal of Turbomachinery: Transactions of the ASME
IS - 3
M1 - 031005
ER -