The discrepancy between manufactured and design geometry of turbomachinery blades has a detrimental effect on the performance variability. In this work, the authors propose a methodology to reduce the impact of the randomness induced by the manufacturing process: a tolerance optimization is carried out by resorting to an efficient robust optimization method based on quantile regression. Its application to a typical two-dimensional supersonic nozzle cascade for ORC showcases promising preliminary results.

Tolerance Optimization of Supersonic ORC Turbine Stator

Persico G.;
2021-01-01

Abstract

The discrepancy between manufactured and design geometry of turbomachinery blades has a detrimental effect on the performance variability. In this work, the authors propose a methodology to reduce the impact of the randomness induced by the manufacturing process: a tolerance optimization is carried out by resorting to an efficient robust optimization method based on quantile regression. Its application to a typical two-dimensional supersonic nozzle cascade for ORC showcases promising preliminary results.
2021
ERCOFTAC Series
978-3-030-69305-3
978-3-030-69306-0
Geometric uncertainty
NICFD
ORC Stator
Quantile regression
Random field
Robust optimization
File in questo prodotto:
File Dimensione Formato  
151-BookNICFD20.pdf

Accesso riservato

Descrizione: Articolo principale
: Publisher’s version
Dimensione 4.85 MB
Formato Adobe PDF
4.85 MB Adobe PDF   Visualizza/Apri

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1167379
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 0
  • ???jsp.display-item.citation.isi??? ND
social impact