The heat transfer in rotating cavities, as found in the internal air system of gas turbines, is mainly governed by the flow passing through these specific machine structures. The core rotation ratio represents the circumferential velocity, and is thought to be an influential flow parameter for heat transfer in rotating cavities with radial flow-through. Therefore, this paper focuses on deducing the core rotation ratio and the estimation of its local distribution using telemetric pressure measurements. The local core rotation ratio depends on the radial pressure distribution in a rotating cavity system. Thus, an integral core rotation ratio can be determined from pressure measurements in the rotating cavity system. A flow structure-based approximation of the measurements allows an estimation of the radial distribution of the core rotation ratio in the rotating cavity. The results of the measurements with varied flow rates and revolving speeds are presented, as well as a discussion of the fit parameters and their dependency on the operation mode of the test rig.

References

1.
Günther
,
A.
,
Uffrecht
,
W.
, and
Odenbach
,
S.
, 2010, “
Local Measurements of Disc Heat Transfer in Heated Rotating Cavities for Several Flow Regimes
,” ASME Paper No. GT2010-22544.
2.
Owen
,
J. M.
, and
Rogers
,
R. H.
, 1995,
Flow and Heat Transfer in Rotating-Disc Systems
, Vol.
2
,
Wiley
,
New York
.
3.
Xiao
,
Y.
,
Luo
,
X.
,
Xu
,
G. Q.
, and
Sun
,
J. N.
, 2009, “
PIV Measurements of the Flow in a Rotating Cavity With a Radial Inflow
,”
Int. Symp. on Heat Transfer in Gas Turbine Systems
, Aug. 9–14, Antalya, Turkey
4.
Kaiser
,
E.
, 2003, “
Surface Temperature Measurement With Liquid Crystals for Flow Visualization
,”
Tech. Mess.
,
70
, pp.
279
285
.
5.
Uffrecht
,
W.
, and
Kaiser
,
E.
, 2005, “
Stray Light Measurement for the Visualization of Air Flow in Rotating Cavities
,”
Tech. Mess.
,
72
, pp.
671
678
.
6.
Johnson
,
B. V.
,
Daniels
,
W. A.
,
Kawecki
,
E. J.
, and
Martin
,
R. J.
, 1991, “
Compressor Drum Aerodynamic Experiments and Analysis With Coolant Injected at Selected Locations
,”
ASME J. Turbomach.
,
113
, pp.
272
280
.
7.
Regnery
,
D.
,
Hoeppner
,
U.
,
Vortmeyer
,
N.
, and
Nitsche
,
K.
, 1999, “
Measurements of Complex Air Flow Phenomena Inside the Rotor of an Operating Industrial Gas Turbine
,” Report No. C557/073/99.
8.
Uffrecht
,
W.
, and
Kaiser
,
E.
, 2008, “
Influence of Force Field Direction on Pressure Sensors Calibrated at up to 12000g
,”
ASME J. Eng. Gas Turbines Power
,
130
, p.
061602
.
9.
Chew
,
J. W.
, and
Snell
,
R. J.
, 1988, “
Prediction of Pressure Distribution for Radial Inflow Between Co-Rotating Discs
,” ASME Paper No. 88-GT-127.
10.
Günther
,
A.
,
Uffrecht
,
W.
,
Kaiser
,
E.
, and
Odenbach
,
S.
, 2008, “
Experimental Analysis of Varied Vortex Reducer Configurations for the Internal Air System of Jet Engine Gas Turbines
,” ASME Paper No. GT2008-50738.
11.
Bernhard
,
F.
, 2004,
Technische Temperaturmessung
,
Springer
,
Berlin
.
12.
Pfleiderer
,
C.
, and
Petermann
,
H.
, 1991,
Strömungsmaschinen
, Vol.
6
,
Springer
,
Berlin
.
13.
Albring
,
W.
, 1961,
Angewandte Strömungslehre
,
Theodor Steinkopff
,
Dresden
.
14.
Nikuradse
,
J.
, 1933,
Strömungsgesetze in Rauhen Rohren
,
VDI-Verlag
,
Berlin
.
15.
VDI
, 2006,
VDI-Wärmeatlas
, Vol.
10
, Berlin.
You do not currently have access to this content.