This paper presents transient-flow component models for the prediction of the transient response of gas turbine cycles. The application is to predict the transient response of a small solar-powered regenerative gas-turbine engine with centrifugal impellers. The component sizes are similar to those under consideration for the solar-powered Space Station, but the models can easily be generalized for other applications with axial or mixed-flow turbomachinery. New component models for the prediction of the propagation of arbitrary transients in centrifugal impellers are developed. These are coupled with component models for the heat exchangers, receiver and radiator. The models are based on transient applications of the principles of conservation of mass, energy, and momentum. System transients driven by sinusoidal and double-step inputs in receiver salt temperature are presented and discussed. The new turbomachinery models and their coupling to the heat-exchanger models simulates disturbance-propagation in the components both upstream and downstream from the point of generation. This permits the study of the physical mechanisms of generation and propagation of higher-frequency contents in the response of the cycle.

1.
Moody, F. J., 1990, Introduction to Unsteady Thermofluid Mechanics, Wiley, New York.
2.
Kuhlberg, J. F., Sheppard, D. E., King, E. O., and Baker, J. R., 1969, “The Dynamic Simulation of Turbine Engine Compressors,” AIAA Paper No. 69-486.
3.
Kalnitsky
,
K. C.
, and
Kwatny
,
H. G.
,
1981
, “
A First Principles Model for Steam Turbine Control Analysis
,”
ASME J. Dyn. Syst., Meas., Control
,
103
, pp.
61
68
.
4.
Adams
,
J.
,
Clark
,
D. R.
,
Louis
,
J. R.
, and
Spanbauer
,
J. P.
,
1965
, “
Mathematical Modeling of Once-Through Boiler Dynamics
,”
Trans. IEEE, Power Apparatus Syst.
,
84
, pp.
146
156
.
5.
Corbett
,
A. G.
, and
Elder
,
R. L.
,
1974
, “
Stability of an Axial Flow Compressor With Steady Inlet Conditions
,”
J. Mech. Eng. Sci.
,
16
, pp.
377
385
.
6.
Macdougal
,
I.
, and
Elder
,
R. L.
,
1983
, “
Simulation of Centrifugal Compressor Transient Performance for Process Plant Applications
,”
ASME J. Eng. Power
,
105
, pp.
885
890
.
7.
Ray
,
A.
, and
Bowman
,
H. F.
,
1976
, “
A Nonlinear Dynamic Model of a Once-Through Subcritical Steam Generator
,”
ASME J. Dyn. Syst., Meas., Control
,
98
, pp.
332
339
.
8.
Fink
,
D. A.
,
Cumpsty
,
N. A.
, and
Greitzer
,
E. M.
,
1992
, “
Surge Dynamics in a Free-Spool Centrifugal Compressor System
,”
ASME J. Turbomach.
,
114
, pp.
321
332
.
9.
Korakianitis, T., Hochstein, J. I., and Zou, D., 1993, “Prediction of the Transient Thermodynamic Response of a Closed-Cycle Regenerative Gas Turbine,” ASME J. of Turbomach. (in press), ASME Paper No. 93-GT-136.
10.
Rocketdyne, 1986, “Space Station Work Package WP-04 Power System Preliminary Analysis and Design Document,” Rocketdyne RI/RD85-320-2, December.
11.
Rocketdyne, 1989, “Allied-Signal Interim Design Review for the CBC/PGS for the NASA Space Station Freedom,” Rocketdyne Report No. 41-9311, November.
12.
Krain, H., and Hoffmann, W., 1989, “Centrifugal Impeller Geometry and its Influence on Secondary Flows,” in AGARD Conference Proceedings CP-469 “Secondary Flows in Turbomachines.”
13.
Kays, W. M., and London, A. L., 1984, Compact Heat Exchangers, McGraw-Hill, New York.
You do not currently have access to this content.