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Chemical Reaction Engineering (CRE) is the field that studies the rates and mechanisms of chemical reactions and the design of the reactors in which they take place. Lecture 19

Lecture 19

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Lecture 19. Chemical Reaction Engineering (CRE) is the field that studies the rates and mechanisms of chemical reactions and the design of the reactors in which they take place. Today’s lecture. Gas Phase Reactions Trends and Optimums. Last Lecture. - PowerPoint PPT Presentation

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Page 1: Lecture  19

Chemical Reaction Engineering (CRE) is the field that studies the rates and mechanisms of

chemical reactions and the design of the reactors in which they take place.

Lecture 19

Page 2: Lecture  19

Today’s lectureGas Phase ReactionsTrends and Optimums

2

Page 3: Lecture  19

User Friendly Equations Relate T and X or Fi

1. Adiabatic CSTR, PFR, Batch, PBR achieve this:

0CW PS

Rx

0PiEB H

TTCX i

Rx

0P

HTTC~

X A

iPi

Rx0 C

XHTT

Last Lecture

3

Page 4: Lecture  19

2. CSTR with heat exchanger, UA(Ta-T) and a large coolant flow rate

Rx

0Pia0A

EB H

TTC~TTFUA

Xi

TTa

Cm

User Friendly Equations Relate T and X or Fi

4

Page 5: Lecture  19

3. PFR/PBR with heat exchange

FA0T0

CoolantTa

User Friendly Equations Relate T and X or Fi

3A. In terms of conversion, X

XCC~F

THrTTUa

dWdT

pPi0A

RxAaB

i5

Page 6: Lecture  19

User Friendly Equations Relate T and X or Fi

3B. In terms of molar flow rates, Fi

i

ij

Pi

RxAaB

CF

THrTTUa

dWdT

4. For multiple reactions

i

ij

Pi

RxijaB

CF

HrTTUa

dVdT

5. Coolant Balance

cPc

aA

CmTTUa

dVdT

6

Page 7: Lecture  19

Reversible Reactions

endothermic reaction

exothermic reaction

KP

T

endothermic reaction

exothermic reaction

Xe

T

7

Page 8: Lecture  19

Heat ExchangeExample: Elementary liquid phase reaction carried out in a PFR

FA0FI

Tacm Heat

Exchange Fluid

A B

The feed consists of both inerts I and Species A with the ratio of inerts to the species A being 2 to 1.8

Page 9: Lecture  19

Heat Exchangea) Adiabatic. Plot X, Xe, T and the rate of

disappearance as a function of V up to V = 40 dm3.

b) Constant Ta. Plot X, Xe, T, Ta and Rate of disappearance of A when there is a heat loss to the coolant and the coolant temperature is constant at 300 K for V = 40 dm3. How do these curves differ from the adiabatic case.

9

Page 10: Lecture  19

Heat Exchangec) Variable Ta Co-Current. Plot X, Xe, T,

Ta and Rate of disappearance of A when there is a heat loss to the coolant and the coolant temperature varies along the length of the reactor for V = 40 dm3. The coolant enters at 300 K. How do these curves differ from those in the adiabatic case and part (a) and (b)?

d) Variable Ta Counter Current. Plot X, Xe, T, Ta and Rate of disappearance of A when there is a heat loss to the coolant and the coolant temperature varies along the length of the reactor for V = 20 dm3. The coolant enters at 300 K. How do these curves differ from those in the adiabatic case and part (a) and (b)?

10

Page 11: Lecture  19

Example: PBR A ↔ B

5) Parameters….

Gas Phase Heat Effects

• For adiabatic:• Constant Ta:

• Co-current: Equations as is • Counter-current:

0dWdTa

T)-T toT-T flip(or )1(dWdT

aa

0UA

11

Reversible Reactions

Page 12: Lecture  19

)1( FrdWdX

0AAMole

Balance:

0A

A

0A

BA

b

Fr

Fr

dVdX

VW

12

Reversible Reactions

Page 13: Lecture  19

)3( T1

T1

REexpkk

11

)4( T1

T1

RHexpKK

2

Rx2CC

)2( KCCkr

C

BAA

Rate Law:

13

Reversible Reactions

Page 14: Lecture  19

Stoichiometry:

5( ) CA =CA 0 1 − X( )y T0 T( )

6( ) CB =CA 0Xy T0 T( )

dydW

=αyFTFT0

TT0

⎛ ⎝ ⎜

⎞ ⎠ ⎟= −

α2y

TT0

⎛ ⎝ ⎜

⎞ ⎠ ⎟

W = ρV

dydV

= −αρ b2y

TT0

⎛ ⎝ ⎜

⎞ ⎠ ⎟

14

Reversible Reactions

Page 15: Lecture  19

b00A2Rx

2C110A

, ,T ,C ,T ,H

)15()7( ,K ,T ,R ,E ,k ,F

Parameters:

15

Reversible Reactions

Page 16: Lecture  19

Example: PBR A ↔ B

3) Stoich (gas):

v = v0 1+εX( )P0

PTT0

5( ) CA =FA 0 1 − X( )v0 1+εX( )

PP0

T0

T=CA 0 1− X( )

1+εX( )yT0

T

6( ) CB =CA 0X1+εX( )

yT0

T

7( ) dydW

=−α2y

FTFT 0

TT0

=−α2y

1+εX( )TT0

Gas Phase Heat Effects

16

Reversible Reactions

Page 17: Lecture  19

KC =CBeCAe

=CA 0X eyT0 T

CA 0 1− X e( )yT0 T

8( ) Xe =KC

1+KC

Example: PBR A ↔ B

17

Gas Phase Heat EffectsReversible Reactions

Page 18: Lecture  19

Example: PBR A ↔ B

Gas Phase Heat Effects

18

Exothermic Case: Xe

T

KC

T

KC

T T

Xe~1

Endothermic Case:

Reversible Reactions

Page 19: Lecture  19

Adibatic EquilibriumConversion on Temperature Exothermic ΔH is negativeAdiabatic Equilibrium temperature (Tadia) and conversion (Xeadia)

PA

Rx0 C

XHTT

C

Ce K1

KX

X

Xeadi

a

Tadia T19

Page 20: Lecture  19

X2

FA0 FA1 FA2 FA3

T0X1 X3T0 T0

Q1 Q2

20

Page 21: Lecture  19

X

T

X3

X2

X1

T0

Xe XEB

RX

0Pii

HTTC

X

21

Page 22: Lecture  19

Gas Phase Heat Effects

22

dTdV

=−rA( ) −ΔHRx( ) −Ua T −Ta( )

∑FiCPi

∑FiCPi = FA 0 ∑ΘiCPi + ΔCPX[ ]

Case 1: Adiabtic and ΔCP=0

T = T0 +−ΔHRx( )X∑ΘiCPi

(16A)

Additional Parameters (17A) & (17B)

T0, ∑ΘiCPi =CPA + ΘICPI

Example A ↔ B

Page 23: Lecture  19

Heat effects:

dTdW

=−ra( ) −ΔHR( ) −

Ua

ρ bT −Ta( )

FA 0 θ iCPi∑ 9( )

23

Case 2: Heat Exchange – Constant Ta

Gas Phase Heat EffectsExample A ↔ B

Page 24: Lecture  19

)C17( TT 0V , Cm

TTUadVdT

aoaP

aa

cool

Case 3. Variable Ta Co-Current

Case 4. Variable Ta Counter Current Guess ?T 0V

CmTTUa

dVdT

aP

aa

cool

Guess Ta at V = 0 to match Ta0 = Ta0 at exit, i.e., V = Vf

24

Example A ↔ B

Page 25: Lecture  19

25

Page 26: Lecture  19

26

Page 27: Lecture  19

27

Page 28: Lecture  19

28

Page 29: Lecture  19

29

Page 30: Lecture  19

Endothermic

PFR

A B

dXdV

k 1 1 1KC

X

0 , Xe

KC1KC

XEB iCPi

T T0 HRx

CPA

ICPI T T0 HRx

T0

XXEB

Xe

TT0 HRx X

CPAICPI

30

Page 31: Lecture  19

31

Effects of Inerts In The Feed

Page 32: Lecture  19

What happens when we vary

k1I

32

Endothermic

As inert flow increases the conversion will increase. However as inerts increase, reactant concentration decreases, slowing down the reaction. Therefore there is an optimal inert flow rate to maximize X.

First Order Irreversible

Page 33: Lecture  19

33

Page 34: Lecture  19

T

X

Adiabatic T and Xe

T0

exothermic

T

X

T0

endothermic

PIIPA

R0 CC

XHTT

Gas Phase Heat EffectsTrends:-Adiabatic:

34

Page 35: Lecture  19

Adiabatic:• As T0 decreases the conversion X will increase,

however the reaction will progress slower to equilibrium conversion and may not make it in the volume of reactor that you have.

• Therefore, for exothermic reactions there is an optimum inlet temperature, where X reaches Xeq right at the end of V. However, for endothermic reactions there is no temperature maximum and the X will continue to increase as T increases.

Gas Phase Heat Effects

35

X

T

Xe

T0

X

T

X

T

Page 36: Lecture  19

Adiabatic:

Gas Phase Heat Effects

36

Effect of adding Inerts

X

T

V1 V2X

TT0

I

0I

Xe

X

X =T −T0( ) CpA +θ ICpI[ ]

−ΔHRx

Page 37: Lecture  19

37

Exothermic Adiabatic

As θI increase, T decrease and

dXdV

=k

υ 0 Hθ I( )

k

θI

Page 38: Lecture  19

38

Page 39: Lecture  19

39

Page 40: Lecture  19

Adiabatic

KC

V

XeX

V

T

V

Xe

V

k

V

Xe

XFrozen

V

OR

Endothermic

T

V

KC

V

Xe

V

XeX

V

k

V

Exothermic

40

Page 41: Lecture  19

Heat Exchange

T

V

KC

V

Xe

V

XeX

V

Endothermic

T

V

KC

V

Xe

V

XeX

V

Exothermic

41

Page 42: Lecture  19

Derive the Steady State Energy Balance (w/o Work)

0HFHFdWTTUaii0i0ia

W

0 B

0dWdHFH

dWdF0TTUa i

iii

aB

Differentiating with respect to W:

42

Page 43: Lecture  19

Aii

i rrdWdF

Mole Balance on species i:

T

TPiRii

R

dTCTHH

Enthalpy for species i:

Derive the Steady State Energy Balance (w/o Work)

43

Page 44: Lecture  19

Differentiating with respect to W:

dWdTC0

dWdH

Pii

0dWdTCFHrTTUa

PiiiiAaB

Derive the Steady State Energy Balance (w/o Work)

44

Page 45: Lecture  19

0dWdTCFHrTTUa

PiiiiAaB

THH Rii

XFF ii0Ai

Final Form of the Differential Equations in Terms of Conversion:A:

45

Page 46: Lecture  19

Final Form of terms of Molar Flow Rate:

Pii

AB

CF

HrUa

dWdT

B: T,Xg

Fr

dWdX

0A

A

46

Page 47: Lecture  19

(d) Gas Phase Counter Current Heat Exchange Vf = 20 dm3

Matches

47

Page 48: Lecture  19

End of Lecture 19

48

Page 49: Lecture  19

Example: PBR A ↔ B VW b

2) Rates:

4 T1

T1

RHexpkk

3 T1

T1

REexpkk

2 kCCkr

2

R2CC

11

CBA'A

1 F

rdWdX

0A

'A1) Mole balance:

Gas Phase Heat Effects

49