New Optimization Criteria for the Design of Three-Dimensional Bladings Applied to Compound Lean Nozzles of an Axial Turbine
The performance of axial turbines can be improved by the application of three-dimensionally shaped bladings. The performance improvement by three-dimensionally shaped bladings is perceptible only within a stage, leading to a time-accurate three-dimensional optimization. The paper describes two objective functions that, if applied to an isolated turbine blade row, may help to reduce the range of feasible geometries. The quality of the objective functions is tested in a parametric study, in which the stator row geometry is parameterized by only one parameter. The stage efficiency, obtained by evaluation of the time-accurate flows through turbine stages with different stator rows, is used as criterion. An optimization of compound lean nozzles parameterized by two parameters is performed with the more accurate objective function resulting in high performance compound lean nozzles.