In order to fully address the characteristics of the alternative recuperated cycle with divided turbine expansion, both design and off-design analyses have been performed. Two types of mechanical design are assumed: two shaft and single shaft. In particular, optimal pressure ratio division between the high- and low-pressure turbines is evaluated for the single-shaft configuration. It is predicted that the alternative recuperated cycle hardly exhibits sensible design efficiency advantage over the conventional recuperated cycle for moderate turbine inlet conditions and with usual component performances. An advantage of the alternative cycle with single-shaft design is that thermal efficiency is less sensitive to compressor pressure ratio compared to other configurations, and we can also have flexibility in the turbine division without much efficiency loss. The part load analyses have been carried out with the aid of realistic component maps and models for off-design operation. In addition to the general fuel only control, a variable speed control is assumed as the part load operating strategy of the single-shaft configuration. Obvious advantage with the alternative cycle is observed in the variable speed operation of the single-shaft design. With this strategy, the part load efficiency of the alternative cycle is far superior to the conventional cycle. Almost constant efficiency is predicted for a wide power range.

1.
McDonald
,
C. F.
, and
Rogers
,
C.
, 2005, “
Ceramic Recuperator and Turbine—The Key to Achieving a 40 Percent Efficient Microturbine
,” ASME Paper No. GT2005-68644.
2.
Farmer
,
R.
, ed., 2003, “
4.6-MW Recuperated Genset is Ready for Its Commercial Debut
,”
Gas Turbine World
,
33
(
5
), pp.
24
25
.
3.
Farmer
,
R.
, 2004, “
Recuperated Marine Gas Turbine is Rated 1800kW and 38% Efficiency
,”
Gas Turbine World
,
35
(
3
), pp.
32
35
.
4.
Facchini
,
B.
, 1993, “
New Prospects for the Use of Regeneration in Gas Turbine Cycles
,”
Proc. of ASME Cogen-Turbo
,
ASME
, New York, IGTI-Vol.
8
, pp.
263
269
.
5.
Facchini
,
B.
, and
Sguanci
,
S.
, 1994, “
RE Cycle: A System for Good Off-Design Performance
,”
Proc. of ASME Cogen-Turbo
,
ASME
, New York, IGTI-Vol.
9
, pp.
169
175
.
6.
Cardu
,
M.
, and
Baica
,
M.
, 2002, “
Gas Turbine Installations With Divided Expansion
,”
Energy Convers. Manage.
0196-8904,
43
, pp.
1747
1756
.
7.
Dellenback
,
P. A.
, 2002, “
Improved Gas Turbine Efficiency Through Alternative Regenerator Configuration
,” ASME Paper No. GT-2002-30133.
8.
Elmegaard
,
B.
, and
Qvale
,
B.
, 2004, “
Regenerative Gas Turbines With Divided Expansion
,” ASME Paper No. GT2004-54225.
9.
Cohen
,
H.
,
Rogers
,
G. F. C.
, and
Saravanamuttoo
,
H. I. H.
, 1972,
Gas Turbine Theory
, 2nd ed.,
Longman
,
London
, p.
317
.
10.
Wilson
,
D. G.
, 1984,
The Design of High-Efficiency Turbomachinery and Gas Turbines
,
MIT Press
, Cambridge, Ch. 3.
11.
Kim
,
J. H.
,
Kim
,
T. S.
,
Sohn
,
J. L.
, and
Ro
,
S. T.
, 2003, “
Comparative Analysis of Off-Design Performance Characteristics of Single and Two Shaft Industrial Gas Turbines
,”
ASME J. Eng. Gas Turbines Power
0742-4795,
125
, pp.
954
960
.
12.
Kim
,
T. S.
, and
Hwang
,
S. H.
, 2006, “
Part Load Performance Analysis of Recuperated Gas Turbines Considering Engine Configuration and Operation Strategy
,”
Energy
0360-5442,
31
, pp.
260
277
.
13.
Rodgers
,
C.
,
Watts
,
J.
,
Thoren
,
D.
,
Nichols
,
K.
, and
Brent
,
R.
, 2001, Microturbines,
Distributed Generation
,
Borbely
,
A. M.
, and
Kreider
,
J. F.
, eds.,
CRC Press
, Boca Raton, FL, pp.
119
150
.
14.
Dixon
,
S. L.
, 1978,
Fluid Mechanics, Thermodynamics of Turbomachinery
, 3rd ed.,
Pergamon Press
, New York.
15.
Aspen Technology, Inc.
, 2004, HYSYS ver. 3.2.
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