During extreme low volume flow conditions, the last stages of a low pressure steam turbine operate in ventilation conditions that can cause a significant temperature increase of critical regions of the last stage moving blade (LSB). Under some conditions, the blade temperature may rise above a safe operating temperature, requiring the machine to be shut down. Limiting the heating effect on the LSB increases the allowable operating range of the low pressure turbine. One common method is to spray water droplets into the low pressure exhaust. As the length of LSBs continues to increase, this method reaches its limit of practical operating effectiveness due to the amount of water required and its impact on the erosion of the LSB. An investigation into complimentary solutions to limit the temperature increase was conducted using CFD. An appropriate CFD setup was chosen from a sensitivity study on the effects from geometry, mesh density, turbulence model, and time dependency. The CFD results were verified against steam turbine data from a scaled test facility. The proposed solutions include low temperature steam extraction, targeted for critical regions of the moving blade. From the test turbine and CFD results, the drivers of the temperature increase during ventilation conditions are identified and described.

References

1.
Troyanovskii
,
B.
,
Lagun
,
V.
,
Maiorskii
,
E.
,
Noiman
,
K.
, and
Simoyu
,
L.
,
1970
, “
Designing Steam Turbine Last Stages
,”
Teploenergetika
,
17
, pp.
16
20
.
2.
Lagun
,
V.
,
Simoyu
,
Z.
,
Frumin
,
Y.
,
Povolotskii
,
L.
, and
Sukharev
,
F.
,
1971
, “
Features of Operation of a Turbine Stage With Low DML Ratio Under Conditions of Low Loads
,”
Teploenergetika
,
18
, pp.
21
24
.
3.
Shnee
,
Y.
,
Ponomarev
,
F.
,
Fedorov
,
M.
, and
Bystritskii
,
L.
,
1971
, “
Features of Operation of a Turbine Stage With Low DML Ratio Under Conditions of Low Loads
,”
Teploenergetika
,
18
, pp.
39
42
.
4.
Teufelberger
,
A.
,
1980
, “
Ventilation von Dampfturbinen bei Schwachlast, Leerlauf und Leistungsaufnahme
,”
VDI Ber.
,
361
, pp.
145
152
.
5.
Sigg
,
R.
,
Heinz
,
C.
,
Casey
,
M. V.
, and
Sürken
,
N.
,
2009
, “
Numerical and Experimental Investigation of a Low-Pressure Steam Turbine During Windage
,”
Proc. Inst. Mech. Eng., Part A
,
223
(
6
), pp.
697
708
.
6.
Gloger
,
M.
,
Neumann
,
K.
, and
Termuehlen
,
H.
,
1986
, “
Design Criteria for Reliable Low-Pressure Blading
,” ASME Paper No. 86-JPGC-Pwr-42.
7.
Megerle
,
B.
,
Rice
,
S.
,
McBean
,
I.
, and
Ott
,
P.
,
2013
, “
Numerical and Experimental Investigation of the Aerodynamic Excitation of a Model Low-Pressure Steam Turbine Stage Operating Under Low Volume Flow
,”
ASME J. Eng. Gas Turbines Power
,
135
(
1
), p.
012602
.
8.
Usachev
,
I.
,
Efimenko
,
E.
,
Il'inikh
,
V.
,
Kolyasnikov
,
V.
, and
Neuimim
,
V.
,
1981
, “
Excitation of Axial Oscillations of Steam Turbine Rotors Under Operating Conditions
,”
Energomashinostroenie
,
3
, pp.
5
9
.
9.
Truckenmüller
,
F.
,
2002
, “
Untersuchung zur Aerodynamisch Induzierten Schwingungsanregung von Niederdruck-Laufschaufeln bei Extremer Teillast
,” Dr.-Ing., ITSM, Universität Stuttgart, Stuttgart, Germany.
10.
Gerschütz
,
W.
,
2006
,
Experimentelle Untersuchung von Rotierenden Strömungsinstabilitäten im Betriebsbereich der Ventiation Einer Niederdruck-Dampfturbine
,
VDI Verlag
,
Düsseldorf, Germany
.
11.
Queune
,
O.
, and
He
,
L.
,
2001
, “
Experimental Study of 3D Unsteady Flow Around Oscillating Blade With Part-Span Separation
,”
ASME J. Turbomach.
,
123
(
3
), pp.
519
525
.
12.
Filippenko
,
V.
,
Frolov
,
B.
,
Chernobrovkin
,
A.
,
Zhou
,
B.
,
Mujezinovic
,
A.
, and
Slepski
,
J.
,
2011
, “
Analyses of Temperature Distribution on Steam Turbone Last Stage Low Pressure Buckets at Low Flow Operations
,”
ASME
Paper No. GT2011-46858.
13.
Traupel
,
W.
,
1977
,
Thermische Turbomaschinen, Bd. 1
, 3rd ed.,
Springer Verlag
,
Berlin
.
14.
Bergmann
,
D.
,
Gloger
,
M.
,
Gartner
,
G.
, and
May
,
G.
,
1985
, “
High Temperature Control in High Backpressure LP Turbines
,”
47th American Power Conference
, Chicago, IL, Apr. 22–24, pp.
219
229
.
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