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VGB POWERTECH 10 (2019)

VGB PowerTech - International Journal for Generation and Storage of Electricity and Heat. Issue 10 (2019). Technical Journal of the VGB PowerTech Association. Energy is us! Cyber security. Power generation. Environment. Flexibility.

VGB PowerTech - International Journal for Generation and Storage of Electricity and Heat. Issue 10 (2019).
Technical Journal of the VGB PowerTech Association. Energy is us!
Cyber security. Power generation. Environment. Flexibility.

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Flexible steam turbine operation in combined cycle power plants <strong>VGB</strong> PowerTech <strong>10</strong> l <strong>2019</strong><br />

Fig. <strong>10</strong>. Application areas of THS’ heating blankets indicated in yellow.<br />

heat transfer coefficients on outer casing)<br />

is applied in the simulation of the 3D model<br />

without blades. The adapted boundary<br />

conditions improve the results, as shown in<br />

F i g u r e 7 c . The differences between the<br />

3D model without blades and the 2D model<br />

without blades originate on the one<br />

hand from the different boundary conditions.<br />

On the other hand, different view<br />

factors due to included flanges in the 3D<br />

model influence the results. The distances<br />

between the inner and outer casing are also<br />

smaller in the 3D model without blades a<br />

fact that influences the heat transfer. Including<br />

the flanges increases the component<br />

volume hence leading to a higher<br />

stored energy. This results in a reduced rate<br />

of cooling in the 3D model without blades.<br />

Comparison of models<br />

All models are able to capture the most important<br />

effects during cool down. The 3D<br />

model without blades performs better due<br />

to the more exact representation of the turbine<br />

geometry. 3D effects should not be<br />

neglected for a detailed analysis. For large<br />

scale optimization approaches, using a 2D<br />

model will be sufficiently accurate. No<br />

model is able to capture the effects at the<br />

beginning of the simulation very accurately,<br />

which is acceptable as the long term<br />

temperature distribution is the main point<br />

of interest.<br />

Application of the HSM<br />

The validated 3D model without blades is<br />

enhanced to additionally include the THS.<br />

The enhanced model is used to investigate<br />

the performance of the HSM.<br />

A load case for the analysis of the warmkeeping<br />

mode is constructed based on the<br />

cool-down load case. The turbine is turned<br />

off and left to cool down. The THS is activated<br />

once the outer casing temperature<br />

reaches a threshold temperature T t .<br />

Different locations of the THS “heating<br />

blankets” are possible. The positioning of<br />

the heating blankets has been exemplarily<br />

investigated for the location shown in F i g -<br />

u r e <strong>10</strong> , where the heating blanket is<br />

mounted on the whole outer casing.<br />

The heating blankets are modeled by including<br />

their respective heat fluxes in the<br />

turbine model. The heat flux does not exceed<br />

a maximum value and the temperature<br />

of the outer casing is defined to be at<br />

maximum 5 K above T t . A PID controller<br />

with temperature feedback loop regulates<br />

the magnitude of the heat flux. It is included<br />

via a user subroutine in Abaqus CAE.<br />

The rotor temperature is the limiting factor<br />

for warm start-up conditions and is hence<br />

chosen as the process variable. F i g u r e 4<br />

shows the location of the considered HP rotor<br />

notch and IP rotor notch. The analysis<br />

of the results shows that the IP rotor notch<br />

temperature is lower than the HP rotor<br />

notch temperature wherefore effectively<br />

the IP rotor notch temperature is the limiting<br />

factor.<br />

The heat flux is the control variable u(t) for<br />

the PID controller, which is computed by<br />

[14]<br />

<br />

(<strong>10</strong>)<br />

where the error value e(t) is the difference<br />

between the actual and the set point temperature<br />

at the IP rotor notch.<br />

F i g u r e 11 shows the temperatures at the<br />

HP rotor notch and IP rotor notch. The temperatures<br />

are normalized by the starting<br />

temperature at the HP rotor notch while<br />

the time is normalized by the time of the<br />

heating blanket activation. The results<br />

show that it is possible to maintain conditions<br />

for warm start-up conditions within<br />

the turbine.<br />

T [-]<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

Cool Down HP<br />

HSM HP<br />

Cool Down IP<br />

HSM IP<br />

0.2<br />

0 0.5 1 1.5 2 2.5 3<br />

<br />

Fig. 11. Temperature profiles during cool down<br />

(Cool Down) and in warm-keeping<br />

mode (HSM) at the HP and IP rotor<br />

notches. Temperatures are normalized<br />

by the starting temperature at the high<br />

pressure notch.<br />

Conclusions<br />

The heat transfer throughout the complex<br />

turbine topology has been investigated using<br />

three models with different degrees of<br />

geometry simplification. The analysis<br />

shows that it is possible to capture the most<br />

important aspects using two-dimensional<br />

models with simplified topology. Further<br />

geometry simplifications can be realized by<br />

adapting the thermal behavior of the FEMmodel.<br />

A large part of the heat transfer in the turbine<br />

is realized by radiation. Without modelling<br />

this type of heat transfer, it is not<br />

possible to make an accurate prognosis of<br />

the temperature load and distribution. The<br />

simplified CAE model “2D model without<br />

blades” is able to perform the calculations<br />

faster than models with more geometrical<br />

detail. The negligible change of the accuracy,<br />

with regard to the shortening of the<br />

calculation duration, is therefore fully justifiable.<br />

A controller was further developed<br />

which makes it possible to specify the power<br />

of the HSM within the CAE simulation.<br />

A simulation of the HSM shows that it can<br />

maintain the temperature of the turbine at<br />

a high level. The warm-keeping allows the<br />

customer to preserve the steam turbine<br />

warm start conditions without seal steam<br />

depending on their own commercial targets.<br />

As a result the energy consumption<br />

for long standstill times can be minimized.<br />

Nomenclature<br />

A<br />

F c<br />

r<br />

T<br />

t<br />

<br />

<br />

<br />

<br />

<br />

<br />

<br />

<br />

cond<br />

conv<br />

real<br />

rad<br />

sub<br />

References<br />

Area<br />

factor for alpha substitution<br />

heat flow<br />

specific heat flow<br />

distance between surfaces<br />

absolute temperature<br />

time<br />

heat transfer coefficient<br />

angle with respect to normal to<br />

the surface<br />

emissivity<br />

thermal conductivity<br />

density<br />

Stefan-Boltzmann constant<br />

normalized time<br />

view factor<br />

conduction<br />

convection<br />

physical value<br />

radiation<br />

substitute value<br />

[1] T. Eisfeld, A. Feldmüller, and F. Roehr,<br />

“CCPP improvements in a business environment<br />

of intermittent power generation,” in<br />

Power-Gen Europe 2017.<br />

[2] A. Feldmüller, T. Zimmerer, and F. Roehr,<br />

“From Base to Cycling Operation – Innovative<br />

Operational Concepts for CCPPs,” in<br />

Power-Gen Europe 2015.<br />

[3] D. Toebben et al., “Numerical Investigation<br />

of the Heat Transferand Flow Phenomena in<br />

an IP Steam Turbine in Warm-Keeping Operation<br />

with Hot Air (GT2017-63555),”<br />

Proceedings ASME Turbo Expo, 2017.<br />

48

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