Velocity measurements downstream of the impellers in a multistage centrifugal blower
- Univ. di Udine (Italy). Ist. di Fisica Tecnica e di Tecnologie Industriali
- Univ. di Trieste (Italy). Dipt. di Energetica
The paper presents the results of an experimental investigation on a four-stage centrifugal blower, having the aim of obtaining an accurate description of the flow field behind the impellers in several operative conditions and for different geometric configurations. Actually, the test plant allows one to change the turbomachinery characteristics assembling one, two, three, or four stages and three different types of diffuser. In this first research step, the blower has been tested in the four-stage vaneless diffuser configuration. The unsteady flow field behind the impellers and in the diffusers has been measured by means of a hot-wire anemometer. A phase-locked ensemble-averaging technique has been utilized to obtain the relative flow field from the instantaneous signals for the stationary hot-wire probes. Several detailed measurement sets have been performed using both single and crossed hot-wire probes, to obtain the velocity vectors and turbulence trends, just behind the blower impellers and in several radial positions of the vaneless diffusers. These measurements have been done at different flow rate conditions, covering unsteady flow rate phenomena (rotating stall) also. The results obtained allowed the authors to get a detailed flow field analysis in the multistage centrifugal blower, in relation to the geometric configuration and to the differing operating conditions.
- Sponsoring Organization:
- USDOE
- OSTI ID:
- 136536
- Report Number(s):
- CONF-940626-; ISSN 0889-504X; TRN: IM9552%%78
- Journal Information:
- Journal of Turbomachinery, Vol. 117, Issue 4; Conference: 39. international gas turbine and aeroengine congress and exposition, The Hague (Netherlands), 13-16 Jun 1994; Other Information: PBD: Oct 1995
- Country of Publication:
- United States
- Language:
- English
Similar Records
The experimental study of matching between centrifugal compressor impeller and diffuser
Aerodynamically induced radial forces in a centrifugal gas compressor. Part 1: Experimental measurement