Journal of Power and Energy Engineering, 2014, 2, 729-734
Published Online April 2014 in SciRes. http://www.scirp.org/journal/jpee
http://dx.doi.org/10.4236/jpee.2014.24097
How to cite this paper: Liu, W.Y., et al. (2014) Thermo-Dynamical Analysis on Electricity-Generation Subsystem of CAES
Power Plant. Journal of Power and Energy Engineering, 2, 729-734. http://dx.doi.org/10.4236/jpee.2014.24097
Thermo-Dynamical Analysis on
Electricity-Generation Subsystem of CAES
Power Plant
Wenyi Liu, Gang Xu, Yongping Yang
Key Lab of Education Ministry for Power Plant Equipments Conditions Monitoring and Fault Diagnosis, North
China Electric Power University, Beijing, China
Email: lwy @ncepu.edu.cn, xg2008@ncepu.edu.cn, yyp@ncepu.edu.cn
Received January 2014
Abstract
Besides pumped hydropower, Compressed Air Energy Storage (CAES) is the other solution for
large energy storage capacity. It can balance fluctuations in supply and demand of electricity. CAES
is essential part of smart power grids. Linked with the flow structure and dynamic characteristic
of electricity generation subsystem and its components, a simulation model is proposed. The r-
mo-dynamical performance on off-design conditions have been analyzed with constant air mass
flux and constant gas combustion temperature. Some simulation diagrams of curve are plotted t oo.
The contrast of varied operation mode thermal performance is made between CAES power plant
and simple gas turbine power plant.
Keywords
Electricity Generation Sub-System; CAES Power Plant; Thermal Performance; Simulation Analysis;
Off-Design Conditions
1. Introduction
With the development of renewable energy, the grid load regulation problem is becoming more and more se-
rious. Its performance is dependent on energy storage system because of the load fluctuation. Some problems
can be solved by electrical energy storage system, for example the peak & off-peak demand of power generation,
the improvement of reliability and steadiness of power supply [1] [2].
In CAES technology, air is compressed with a motor/generator using low cost, off-peak electricity and stored
underground in caverns or porous media. This is called energy storage subsystem. This pressurized air is re-
leased from the ground and then be mixed and burned with gas in a combustor. The hot expanding gases drive a
turbo expander and run a motor/generator which, in turn, produces electricity during peak demand periods. This
is the other subsystem, electricity generation subsystem. The electricity generation subsystem of CAES includes
[3]: isobaric heating process in burner, adiabatic expanding process in turbo expander and isobaric heat release
process. Main influence factors of practical thermo-dynamic processes including burning efficiency of burner
η
b,
expansion efficiency of turbo expander and some performance parameters of flowing loss processes. Combined
W. Y. Liu et al.
730
with the characteristics of this subsystem and its components, an off-design condition simulation model is pro-
posed based on unit’s modeling system. Equipments selection and their off-design condition characteristics are
analyzed.
2. Simulation Modeling [4] [5]
Turbo expander is key equipment of electricity generation subsystem for CAES. For the sake of utilizing high
pressure air released from air storage dome, the air expander can be added before gas expander. At the same
time, the re-heater and recuperator can be used in this subsystem. Figure 1 is the conceptual diagram of electric-
ity generation subsystem. M/G is motor/generator, Air EXP is air expander, Gas EXP is gas expander, REC is
recuperator and AS is air storage dome.
The electricity generation subsystem can be divided to some modeling parts, as Figure 2.
Model based on assumptions as follows: 1) air and gas is ideal air, 2) the specific heat of air is constant, 3) the
flowing of air and heat transfer between air and wall is steady process, 4)
η
b is constant.
The equations of these typical parts can be formulated. They include 6 differential equations. With considera-
tion of practical conditions, the heat content of air and gas can be ignored, the compressibility of air and gas in
recuperator can be ignored too.
The equation for metal heat storage is Equation (1):
()( )
m
wpggmam a
dT
cTT TT
d
ρδ αα
τ
⋅⋅=− −−
(1)
δthe thickness of recuperator wall
αg, αahot end and cold end convection heat transfer coefficients
,
ag
TT
average temperature of air part and gas part
ρw,Awdensity of wall and heat transfer area
Based on
QKA t= ∆
, Δt = 75 K and K0 = 100 W/(m2·K) on design condition.
The density of recuperator material is 7800 kg/ m3, specific heat cp = 460 J/(kg·K), αg = αa = α, so the time
constant can be derived as Equation (2) on design condition:
3588000
ww pc
w
Vca
A
ρτδ
α
= =
(2)
Figure 1. The conceptual diagram of electricity gen-
eration subsystem.
Figure 2. Typical modeling parts of electricity generation subsystem.
W. Y. Liu et al.
731
The burning efficiency of burner can be expressed as Equation (3).
1.75 300
max max
()
T
ba
pADe
fG
η
=
(3)
P, Tinlet pressure and inlet temperature of burner
Amax, Dmaxmaximum cross-section area and its diameter
The off-design equations of recuperator is Equation (4)
(4)
Heat transfer coefficient K is associated with recuperator type and air flux, so the off-design formula can be
expressed as Equation (5)
0
0.8 0.060.16
000
()( )())
g
aa
aag
T
KG T
KG TT
=
(5)
3. Off-Design Conditions Operation Simulation [4]
PG9171E (GE) can be taken as simulation object, main parameters as Table 1. Some values are as follows: 1)
Relative internal efficiency of gas expander is 0.905 (k = 1.33) and air expander is 0.88. 2) The pressure losses
in burner, cold end of recuperate and hot end of recuperator are 3%, 1% and 3% respectively. LHV of fuel is
41,960 kJ/kg, working consuming for compressing air
c
P
= 617.65 kJ/kg [4], outlet air pressure of air storage
dome is 61bar, temperature is 30˚C.
The additional formulations are as follows (6)-(9):
1
1
1
11211 1
0()(273)(1)
k
k
pa paa
cGtt cGt
πη
=⋅ ⋅− −⋅⋅+−⋅
(6)
23 12
0 ()
bfa fppa
LHV GGGctcGt
η
= ⋅⋅−+⋅⋅+⋅⋅
(7)
2
2
1
234232
0() ()() (273)(1)
k
k
p afpaft
c GG ttc GG t
πη
=⋅+⋅−− ⋅+⋅+−⋅
(8)
1
4
30
0 0.85
30
t
t
= −
(9)
t1, t2, —inlet T and outlet T of air expander.
0.85the heat transfer efficiency of recuperator.
A) Simulation calculations on design air flux, additional equation are as follows (10)-(12) [6] [7]:
234 112
[() ()()]
epafp amg
P cGGttcGtt
ηη
=⋅+⋅−+⋅ ⋅−⋅
(10)
00
0
(2 )
a asas
a asas
hh
hh
η
η
= −
(11)
00
0
(2 )
t tsts
t tsts
hh
hh
η
η
= −
(12)
The calculation results are shown as Figures 3-5. Some conclusions can be drawn from figures. With the load
lowered, the internal efficiency of air expander and gas expander is lowered obviously, heat rate of generating
Table 1. Main performance parameters of gas turbine.
Ty pe Pe (kW )
η
e (%) Pressure rati o Ga (kg/s) Initial T/t3 (˚C) Leakage T/t4 (˚C) Leakage air flus G4 (kg/s)
PG9171E 123400 33.8 12.3 403.7 1124 538 412.4
W. Y. Liu et al.
732
Figure 3. t1, t2, t4 varying with load rate on design
air flux.
Figure 4. t3, ηa, ηt varying with load
rate on design air flux.
Figure 5. HR, ER, ξ varying with load rate on design air
flu x.
electricity is lowered, electricity rate of generating electricity is improved obviously, the energy transformation
coefficient is lowered obviously too.
B) Simulation calculations on design inlet temperature of gas expander.
Some results are seen as Figures 6-8. Some conclusions are: with the load lowered, the internal efficiency of
air expander and gas expander is constant approximately, heat rate and electricity rate of generating electricity
are improved, the energy transformation coefficient is lowered a little.
Some results are seen as Figures 6-8. Some conclusions are: with the load lowered, the internal efficiency of
air expander and gas expander is constant approximately, heat rate and electricity rate of generating electricity
are improved, the energy transformation coefficient is lowered a little.
C) Contrast with off-design gas turbine performance.
On the basis of off-design performance of gas turbine, using former selected gas turbine, the performance
contrast diagram of gas turbine and electricity generation subsystem is shown in Figure 9 with the load scope
100% - 40%.
W. Y. Liu et al.
733
Figure 6. t1, t2, t4 varying design inlet temperature.
Figure 7. t3, ηa, ηt varying with load rate on design
inlet temperature.
Figure 8. HR, ER, ξ varying with load rate on design
inlet temperature.
It is obvious that thermal efficiency is varying from 33.8% to 0% of gas turbine power plant when load rate
varying among 100% - 40%. But energy transform coefficient varies from 53.6% to 34.3% on design air flux,
from 53.6% to 49.5% on design inlet temperature.
4. Conclusions
1) The electricity generation subsystem of CAES is divided into three processes, the difference between prac-
tical process and ideal process is described and analyzed in this paper.
2) Combined with the characteristic of electricity generation subsystem and its components, a subsystem si-
mulation model is proposed based on unit’s modeling system.
p
q
q
p
p
W. Y. Liu et al.
734
Figure 9. η, ξ1, ξ2 varying with load rate. Ηthermal effi-
ciency of gas turbine; ξ1energy transform coefficient on de-
sign air flux; ξ2energy transform coefficient on design inlet
temperatu re.
3) The simulation diagrams of off-design condition are plotted. The conclusion is that thermal efficiency is
varying from 33.8% to 0% of gas turbine power plant when load rate varying among 100% - 40%. But energy
transform coefficient varies from 53.6% to 34.3% on design air flux, from 53.6% to 49.5% on design inlet tem-
perature.
Acknowledgements
The paper is supported by National Nature Science Fund of China (No. 51276059).
Funding
This work was supported by the Fundamental Research Funds for the Central Universities (No. 10MG11).
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