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Question 9.13: A 2,400 MW(t) plutonium sodium-cooled fast reactor has the f......

A 2,400 MW(t) plutonium sodium-cooled fast reactor has the following characteristics:

W = 14,000 kg /s                      τ = 4.0 s                                     c_p = 1,250~J/(kg °C)

M_ƒc_ƒ = 13.5 × 10^6  J/°C        M_cc_p = 1.90 × 10^6  J/°C      T_i = 360  °C

Λ = 0.5 × 10^{-6}  s                      α_ƒ = -1.8 × 10 ^{-5} /°C            α_c = +0.45 × 10 ^{-5} /°C

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The reactor undergoes a loss of flow transient with { W}(t)={ W}(0)/(1+t/t_{o}) where t_{o}=5.0\,\mathrm{s}\,. Employ appropriate software to Eqs. (8.36) through (9.40) to analyze the transient: Make plots of the reactor power, fuel and coolant outlet temperatures for 0 < t < 20 s ( Hint, note that \tilde τ cannot be approximated by τ in this problem.)

β1 := 0.00021          \operatorname{c1}:=\mathbb{\beta 1}\cdot {\frac{\operatorname{P0}}{(\lambda1\cdot\Lambda)}}     \mathrm{c}2:=\beta 2.{\frac{\mathrm{P}0}{(\lambda2\cdot\Lambda)}}

β2 := 0.00142            \operatorname{c3}:=\mathbb{\beta 3}\cdot {\frac{\operatorname{P0}}{(\lambda3\cdot\Lambda)}}    \mathrm{c}4:=\beta 4.{\frac{\mathrm{P}0}{(\lambda4\cdot\Lambda)}}

β3 := 0.00128             \operatorname{c3}:=\mathbb{\beta 3}\cdot {\frac{\operatorname{P0}}{(\lambda3\cdot\Lambda)}}    \mathrm{c}4:=\beta 4.{\frac{\mathrm{P}0}{(\lambda4\cdot\Lambda)}}

β5 := 0.0007            \operatorname{c5}:=\mathbb{\beta 5}\cdot {\frac{\operatorname{P0}}{(\lambda5\cdot\Lambda)}}    \mathrm{c}6:=\beta 6.{\frac{\mathrm{P}0}{(\lambda6\cdot\Lambda)}}

β6 := 0.00027

Sample calculations shown for $0.10 below using the stiff differential equations solver Radau (Mathcad) to obtain the vector Y.

\mathrm{Rf}:={\frac{\tau}{\mathrm{MfCf}}}=0.296         \alpha_{\mathrm f}:=-1.8\cdot10^{-5}

\mathrm{Tf0}:=\mathrm{Rf.P0}+\mathrm{Ti}=1.071\times10^{3}     \alpha_{\mathrm c}:=0.45\cdot 10^{-5}

C=({2 \cdot \operatorname{Rf}\cdot{{W}}_{0}\cdot{{C}}{{p}})}^{-1}

C = 0.096

\mathrm y := \begin{pmatrix}P0 \\ c1 \\ c2 \\ c3 \\ c4 \\ c5 \\c6 \\ \mathrm {Tf0} \end{pmatrix}

 

\mathrm{DD(t,y)} := \begin{bmatrix}\frac{\bigg[\alpha_{\mathrm{f}}.\left(\mathrm{y_7} -\mathrm{Tf0}\bigg )+\alpha_{\mathrm{{c}}}.\mathrm{C}.\bigg [ \bigg (1+{\frac{\mathrm{t}}{\mathrm{t}_{0}}}\bigg).\mathrm{y_7} -\mathrm{Tf0}\right]-\beta \bigg ]}{\Lambda} \cdot y_0 + \lambda1 \cdot y_1 + \lambda2 \cdot y_2 + \lambda3 \cdot y_3 + \lambda4 \cdot y_4 + \lambda5 \cdot y_5 + \lambda6 \cdot y_6 \\ \begin{matrix}\left({\frac{\beta1}{\Lambda}}\right)\mathbf{y}_0-\lambda1.\mathrm{y_1} \\ \left({\frac{\beta2}{\Lambda}}\right)\mathbf{y}_0-\lambda2.\mathrm{y_2} \\ \left({\frac{\beta3}{\Lambda}}\right)\mathbf{y}_0-\lambda3.\mathrm{y_3}\\ \left({\frac{\beta4}{\Lambda}}\right)\mathbf{y}_0-\lambda4.\mathrm{y_4} \\ \left({\frac{\beta5}{\Lambda}}\right)\mathbf{y}_0-\lambda5.\mathrm{y_5} \\ \left({\frac{\beta6}{\Lambda}}\right)\mathbf{y}_0-\lambda6.\mathrm{y_6} \\ \frac{y_0}{\mathrm{MfCf}} – \frac{(y_7 – \mathrm{Tf0})\cdot \bigg [1 + C \cdot \bigg (1 + \frac{t}{t_0}\bigg)\bigg]}{\tau}\end{matrix} \end{bmatrix}

Y := Radau (y , 0 , 100 , 10000 , DD)

n := 0 .. 10000

Below is an algebraic equation to obtain the coolant outlet temperature using the fuel temperature and the inlet temperature.

\mathrm{Y_{n,9}} :=\mathrm{Ti}+\mathrm{C} \cdot\bigg (1 + \frac{Y_{n,0}}{t_0}\bigg) \cdot Y_{n ,8}

 

27 d
28 d
29 d

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