The application of improved blade tip geometries is studied with the aim of identifying an effective design concept for industrial fan passive noise control. The concept developed optimizes a datum blade by means of profiled endplates at the tip, reducing fan noise by changing the tip leakage flow behaviour. Experimental and computational investigations have been carried out on a family of axial fans, in fully ducted configuration, to establish the aerodynamic merits of the proposed blade tip design concept. The flow mechanisms in the fan tip region are correlated to specific blade design features that promote a reduction of the fan aero-acoustic signature in both tonal and broadband noise components. The tip vortical flow structures are characterized, and their role in creation of overall stage acoustic emissions clarified. The reported research identifies modification of tip geometry as markedly affecting the multiple vortex behaviour of blade tip leakage flow by altering the near-wall fluid flow paths on both blade surfaces. Blade tip endplates were also demonstrated to influence the rotor loss behaviour in the blade tip region. Improvement of rotor efficiency was correlated to the control of tip leakage flows.

Development of improved blade tip endplate concepts for low-noise operation in industrial fans / Corsini, Alessandro; Rispoli, Franco; A. G., Sheard. - In: PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS. PART A, JOURNAL OF POWER AND ENERGY. - ISSN 0957-6509. - STAMPA. - 221:5(2007), pp. 669-681. (Intervento presentato al convegno International Conference on Modelling Fluid Flow (CMFF 06) tenutosi a Budapest, HUNGARY nel SEP 06-09, 2006) [10.1243/09576509jpe386].

Development of improved blade tip endplate concepts for low-noise operation in industrial fans

CORSINI, Alessandro;RISPOLI, Franco;
2007

Abstract

The application of improved blade tip geometries is studied with the aim of identifying an effective design concept for industrial fan passive noise control. The concept developed optimizes a datum blade by means of profiled endplates at the tip, reducing fan noise by changing the tip leakage flow behaviour. Experimental and computational investigations have been carried out on a family of axial fans, in fully ducted configuration, to establish the aerodynamic merits of the proposed blade tip design concept. The flow mechanisms in the fan tip region are correlated to specific blade design features that promote a reduction of the fan aero-acoustic signature in both tonal and broadband noise components. The tip vortical flow structures are characterized, and their role in creation of overall stage acoustic emissions clarified. The reported research identifies modification of tip geometry as markedly affecting the multiple vortex behaviour of blade tip leakage flow by altering the near-wall fluid flow paths on both blade surfaces. Blade tip endplates were also demonstrated to influence the rotor loss behaviour in the blade tip region. Improvement of rotor efficiency was correlated to the control of tip leakage flows.
2007
endplates; industrial fans; passive noise control; tip leakage flow
01 Pubblicazione su rivista::01a Articolo in rivista
Development of improved blade tip endplate concepts for low-noise operation in industrial fans / Corsini, Alessandro; Rispoli, Franco; A. G., Sheard. - In: PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS. PART A, JOURNAL OF POWER AND ENERGY. - ISSN 0957-6509. - STAMPA. - 221:5(2007), pp. 669-681. (Intervento presentato al convegno International Conference on Modelling Fluid Flow (CMFF 06) tenutosi a Budapest, HUNGARY nel SEP 06-09, 2006) [10.1243/09576509jpe386].
File allegati a questo prodotto
Non ci sono file associati a questo prodotto.

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/11573/69739
 Attenzione

Attenzione! I dati visualizzati non sono stati sottoposti a validazione da parte dell'ateneo

Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 55
  • ???jsp.display-item.citation.isi??? 37
social impact