The effect of the diffuser vane setting angle on the performance of a centrifugal compressor was experimentally investigated. Seven different vaned diffusers were tested with the same impeller. In order to evaluate the vaned diffusers under the same flow range and diffuser inlet conditions, all the diffusers were designed to have the same throat area, the same diffuser height. and the same vane inlet position. The first tests were performed by a compressor with a volute. In this case, the diffuser outlet conditions were varied along the circumferential directions due to the nonaxisymmetric geometry of the volute. In the second tests, four of the seven vaned diffusers were tested using a compressor with a collector. In this case, the diffuser outlet conditions were more uniform along the circumferential directions compared to the tests using the compressor with the volute. The effect of the vane setting angle on the stage characteristics and diffuser performance as well as the effect of the circumferential distortion caused by the volute on the stage characteristics are presented. The impact of the incidence loss on the vaned diffuser performance is discussed using 1D vaned diffuser performance modeling. Comparisons of the 1D predictions and the tests results show the incidence loss has a strong influence on vaned diffuser performance.

References

1.
Klassen
,
H. A.
, and
Wood
,
J. R.
,
1997
, “
Experimental Performance of a 16.1 Centimeter Tip Diameter Centrifugal Compressor Designed for a 6:1 Pressure Ratio
,”
Report No. NASA TM X-3552
.
2.
Yoshinaka
,
T.
,
1977
, “
Surge Responsibility and Range Characteristics of Centrifugal Compressors
,”
Joint Gas Turbine Conference
, Tokyo, Japan, May 22–27, pp.
381
390
.
3.
Tamaki
,
H.
,
Nakao
,
H.
, and
Saito
,
M.
,
1999
, “
The Experimental Study of Matching Between Centrifugal Compressor Impeller and Diffuser
,”
ASME J. Turbomach.
,
121
(
1
), pp.
113
118
.
4.
Casey
,
M. V.
, and
Rusch
,
D.
,
2014
, “
The Matching of a Vaned Diffuser With a Radial Compressor Impeller and Its Effect on the Stage Performance
,”
ASME J. Turbomach.
,
136
(
12
), p.
121004
.
5.
Ziegler
,
K. U.
,
Gallus
,
H. E.
, and
Niehuis
,
R.
,
2003
, “
A Study on Impeller-Diffuser Interaction: Part I: Influence on the Performance
,”
ASME J. Turbomach.
,
125
(
1
), pp.
173
182
.
6.
Ziegler
,
K. U.
,
Gallus
,
H. E.
, and
Niehuis
,
R.
,
2003
, “
A Study on Impeller-Diffuser Interaction—Part II: Detailed Flow Analysis
,”
ASME J. Turbomach.
,
125
(
1
), pp.
183
192
.
7.
Ubben
,
S.
, and
Niehuis
,
R.
,
2015
, “
Experimental Investigation of the Diffuser Vane Clearance Effect in a Centrifugal Compressor Stage With Adjustable Diffuser Geometry—Part I: Compressor Performance Analysis
,”
ASME J. Turbomach.
,
137
(
3
), p.
031003
.
8.
Ubben
,
S.
, and
Niehuis
,
R.
,
2015
, “
Experimental Investigation of the Diffuser Vane Clearance Effect in a Centrifugal Compressor Stage With Adjustable Diffuser Geometry—Part II: Detailed Flow Analysis
,”
ASME J. Turbomach.
,
137
(
3
), p.
031004
.
9.
Marsan
,
A.
,
Trébinjac
,
I.
,
Coste
,
S.
, and
Leroy
,
G.
,
2012
, “
Study and Control of a Radial Vaned Diffuser Stall
,”
Int. J. Rotating Mach.
,
2012
, p.
549048
.
10.
Marsan
,
A.
,
Trébinjac
,
I.
,
Coste
,
S.
, and
Leroy
,
G.
,
2015
, “
Influence of Unsteadiness on the Control of a Hub-Corner Separation Within a Radial Vaned Diffuser
,”
ASME J. Turbomach.
,
137
(
2
), p.
021008
.
11.
Kmecl
,
T.
, and
Dalbert
,
P.
,
1999
, “
Optimization of a Vaned Diffuser Geometry for Radial Compressors—Part I: Investigation of the Influence of Geometry Parameters on Performance of a Diffuser
,”
ASME
Paper No. 99-GT-437.
12.
Ribi
,
B.
, and
Dalbert
,
P.
,
1999
, “
One-Dimensional Performance Prediction of Subsonic Vaned Diffusers
,”
ASME J. Turbomach.
,
122
(
3
), pp.
494
504
.
13.
Cumpsty
,
N. A.
,
1989
,
Compressor Aerodynamics
,
Longman Science & Technical
,
Harlow, Essex, UK
, p.
293
.
14.
Tamaki
,
H.
,
Kawakubo
,
T.
,
Unno
,
M.
,
Abe
,
S.
, and
Majima
,
K.
,
2014
, “
Performance Improvement of Multistage Centrifugal Compressor With Low Flow-Rate Stages Based on Factory Acceptance Test Data
,”
ASME
Paper No. GT2014-25156.
15.
Shum
,
P. K. Y.
,
Tan
,
C. S.
, and
Cumpsty
,
N. A.
,
2000
, “
Impeller-Diffuser Interaction in a Centrifugal Compressor
,”
ASME J. Turbomach.
,
122
(
4
), pp.
777
786
.
16.
Tan
,
C. S.
,
2003
, “
Effect of Impeller-Diffuser Interaction on Centrifugal Compressor Performance
,” Gas Turbine Laboratory, Massachusetts Institute of Technology,
Report No. NAG3-2732
.
17.
Tamaki
,
H.
, and
Yamaguchi
,
S.
,
2007
, “
The Experimental Study on Matching Between Centrifugal Compressor Impeller and Vaneless Diffusers for Turbochargers
,”
ASME
Paper No. GT2007-28300.
18.
Dutta
,
S.
,
Sato
,
W.
,
Funazaki
,
K.
, and
Kakudate
,
Y.
,
2015
, “
Investigation of Impeller Exit Flow Field in a Highly Loaded Centrifugal Compressor
,”
ASME
Paper No. AJK2015-02745.
You do not currently have access to this content.