Chapter 9

Gas Power Cycles

Study Guide in PowerPoint

to accompany

Thermodynamics: An Engineering Approach, 8th editionby Yunus A. Çengel and Michael A. Boles

1

2

Our study of gas power cycles will involve the study of those heat engines in which the working fluid remains in the gaseous state throughout the cycle. We often study the ideal cycle in which internal irreversibilities and complexities (the actual intake of air and fuel, the actual combustion process, and the exhaust of products of combustion among others) are removed.

We will be concerned with how the major parameters of the cycle affect the performance of heat engines. The performance is often measured in terms of the cycle efficiency.

thnet

in

W

Q

3

Carnot Cycle

The Carnot cycle was introduced in Chapter 5 as the most efficient heat engine that can operate between two fixed temperatures TH and TL. The Carnot cycle is described by the following four processes.

Carnot CycleProcess Description 1-2 Isothermal heat

addition 2-3 Isentropic expansion 3-4 Isothermal heat

rejection 4-1 Isentropic

compression

4

Note the processes on both the P-v and T-s diagrams. The areas under the process curves on the P-v diagram represent the work done for closed systems. The net cycle work done is the area enclosed by the cycle on the P-v diagram. The areas under the process curves on the T-s diagram represent the heat transfer for the processes. The net heat added to the cycle is the area that is enclosed by the cycle on the T-s diagram. For a cycle we know Wnet = Qnet; therefore, the areas enclosed on the P-v and T-s diagrams are equal.

th CarnotL

H

T

T, 1

We often use the Carnot efficiency as a means to think about ways to improve the cycle efficiency of other cycles. One of the observations about the efficiency of both ideal and actual cycles comes from the Carnot efficiency: Thermal efficiency increases with an increase in the average temperature at which heat is supplied to the system or with a decrease in the average temperature at which heat is rejected from the system.

5

Air-Standard Assumptions

In our study of gas power cycles, we assume that the working fluid is air, and the air undergoes a thermodynamic cycle even though the working fluid in the actual power system does not undergo a cycle.

To simplify the analysis, we approximate the cycles with the following assumptions:

•The air continuously circulates in a closed loop and always behaves as an ideal gas.

•All the processes that make up the cycle are internally reversible.

•The combustion process is replaced by a heat-addition process from an external source.

•A heat rejection process that restores the working fluid to its initial state replaces the exhaust process.

•The cold-air-standard assumptions apply when the working fluid is air and has constant specific heat evaluated at room temperature (25oC or 77oF).

6

Terminology for Reciprocating Devices

The following is some terminology we need to understand for reciprocating engines—typically piston-cylinder devices. Let’s look at the following figures for the definitions of top dead center (TDC), bottom dead center (BDC), stroke, bore, intake valve, exhaust valve, clearance volume, displacement volume, compression ratio, and mean effective pressure.

7

The compression ratio r of an engine is the ratio of the maximum volume to the minimum volume formed in the cylinder.

rV

V

V

VBDC

TDC

max

min

The mean effective pressure (MEP) is a fictitious pressure that, if it operated on the piston during the entire power stroke, would produce the same amount of net work as that produced during the actual cycle.

MEPW

V V

w

v vnet net

max min max min

8

Internal Combustion Engine

Below is an eight-cylinder, four stroke internal combustion engine.

Photo by M. Boles

9

Otto Cycle: The Ideal Cycle for Spark-Ignition Engines

Consider the automotive spark-ignition power cycle.

ProcessesIntake stroke Compression stroke Power (expansion) stroke Exhaust stroke

Often the ignition and combustion process begins before the completion of the compression stroke. The number of crank angle degrees before the piston reaches TDC on the number one piston at which the spark occurs is called the engine timing. What are the compression ratio and timing of your engine in your car, truck, or motorcycle?

10

The air-standard Otto cycle is the ideal cycle that approximates the spark-ignition combustion engine.

Process Description 1-2 Isentropic compression 2-3 Constant volume heat addition 3-4 Isentropic expansion 4-1 Constant volume heat rejection

11

The P-v and T-s diagrams are

12

Thermal Efficiency of the Otto cycle:

thnet

in

net

in

in out

in

out

in

W

Q

Q

Q

Q Q

Q

Q

Q

1

Now to find Qin and Qout.

Apply first law closed system to process 2-3, V = constant.

Thus, for constant specific heats,

Q U

Q Q mC T T

net

net in v

,

, ( )

23 23

23 3 2

13

Apply first law closed system to process 4-1, V = constant.

Thus, for constant specific heats,

Q U

Q Q mC T T

Q mC T T mC T T

net

net out v

out v v

,

, ( )

( ) ( )

41 41

41 1 4

1 4 4 1

The thermal efficiency becomes

th Ottoout

in

v

v

Q

Q

mC T T

mC T T

,

( )

( )

1

1 4 1

3 2

14

th Otto

T T

T T

T T T

T T T

,

( )

( )

( / )

( / )

1

11

1

4 1

3 2

1 4 1

2 3 2Recall processes 1-2 and 3-4 are isentropic, so

Since V3 = V2 and V4 = V1, we see that

T

T

T

T

or

T

T

T

T

2

1

3

4

4

1

3

2

15

The Otto cycle efficiency becomes

th Otto

T

T, 1 1

2Is this the same as the Carnot cycle efficiency? Since process 1-2 is isentropic,

where the compression ratio is r = V1/V2 and

th Otto kr, 11

1

16

We see that increasing the compression ratio increases the thermal efficiency. However, there is a limit on r depending upon the fuel. Fuels under high temperature resulting from high compression ratios will prematurely ignite, causing knock.

17

Example 9-1

An Otto cycle having a compression ratio of 9:1 uses air as the working fluid. Initially P1 = 95 kPa, T1 = 17oC, and V1 = 3.8 liters. During the heat addition process, 7.5 kJ of heat are added. Determine all T's, P's, th, the back work ratio, and the mean effective pressure. Process Diagrams: Review the P-v and T-s diagrams given above for the Otto

cycle.

Assume constant specific heats with Cv = 0.718 kJ/kg K, k = 1.4. (Use the 300 K data from Table A-2)

Process 1-2 is isentropic; therefore, recalling that r = V1/V2 = 9,

18

The first law closed system for process 2-3 was shown to reduce to (your homework solutions must be complete; that is, develop your equations from the application of the first law for each process as we did in obtaining the Otto cycle efficiency equation)

Q mC T Tin v ( )3 2

Let qin = Qin / m and m = V1/v1

vRT

P

kJkg K

K

kPa

m kPa

kJ

m

kg

11

1

3

3

0 287 290

95

0 875

. ( )

.

19

qQ

mQ

v

V

kJ

mkgm

kJ

kg

inin

in

1

1

3

3 37 5

0 875

38 10

1727

..

.

Then,T T

q

C

K

kJkgkJ

kg K

K

in

v3 2

698 41727

0 718

31037

..

.

20

Using the combined gas law (V3 = V2)

P PT

TMPa3 2

3

2

9 15 .

Process 3-4 is isentropic; therefore,

1 1 1.4 1

34 3 3

4

1 1(3103.7)

9

1288.8

k kV

T T T KV r

K

21

Process 4-1 is constant volume. So the first law for the closed system gives, on a mass basis,

Q mC T T

qQ

mC T T

kJ

kg KK

kJ

kg

out v

outout

v

( )

( )

. ( . )

.

4 1

4 1

0 718 12888 290

7171

The first law applied to the cycle gives (Recall ucycle = 0)

w q q q

kJ

kg

kJ

kg

net net in out

( . )

.

1727 717 4

1009 6

22

The thermal efficiency is

th Ottonet

in

w

q

kJkgkJkg

or

,

.

. .

1009 6

1727

0585 585%

The mean effective pressure is

max min max min

1 2 1 2 1 1

3

3

(1 / ) (1 1/ )

1009.61298

10.875 (1 )

9

net net

net net net

W wMEP

V V v v

w w w

v v v v v v r

kJm kPakg

kPam kJkg

23

The back work ratio is (can you show that this is true?)

2 112 2 1

exp 34 3 4 3 4

( ) ( )

( ) ( )

0.225 22.5%

comp v

v

w C T Tu T TBWR

w u C T T T T

or

Air-Standard Diesel Cycle

The air-standard Diesel cycle is the ideal cycle that approximates the Diesel combustion engine

Process Description 1-2 Isentropic compression 2-3 Constant pressure heat addition 3-4 Isentropic expansion 4-1 Constant volume heat rejection

The P-v and T-s diagrams are

24

25

Thermal efficiency of the Diesel cycle

th Dieselnet

in

out

in

W

Q

Q

Q, 1Now to find Qin and Qout. Apply the first law closed system to process 2-3, P = constant.

Thus, for constant specific heats

Q U P V V

Q Q mC T T mR T T

Q mC T T

net

net in v

in p

,

,

( )

( ) ( )

( )

23 23 2 3 2

23 3 2 3 2

3 2

26

Apply the first law closed system to process 4-1, V = constant (just as we did for the Otto cycle)

Thus, for constant specific heats

Q U

Q Q mC T T

Q mC T T mC T T

net

net out v

out v v

,

, ( )

( ) ( )

41 41

41 1 4

1 4 4 1

The thermal efficiency becomes

th Dieselout

in

v

p

Q

Q

mC T T

mC T T

,

( )

( )

1

1 4 1

3 2

27

th Dieselv

p

C T T

C T T

k

T T T

T T T

,

( )

( )

( / )

( / )

1

11 1

1

4 1

3 2

1 4 1

2 3 2What is T3/T2 ?

PV

T

PV

TP P

T

T

V

Vrc

3 3

3

2 2

23 2

3

2

3

2

where

where rc is called the cutoff ratio, defined as V3 /V2, and is a measure of the duration of the heat addition at constant pressure. Since the fuel is injected directly into the cylinder, the cutoff ratio can be related to the number of degrees that the crank rotated during the fuel injection into the cylinder.

28

What is T4/T1 ? PV

T

PV

TV V

T

T

P

P

4 4

4

1 1

14 1

4

1

4

1

where

Recall processes 1-2 and 3-4 are isentropic, so

PV PV PV PVk k k k1 1 2 2 4 4 3 3 and

Since V4 = V1 and P3 = P2, we divide the second equation by the first equation and obtain

29

th Diesel

ck

c

kck

c

k

T T T

T T T

k

T

T

r

r

r

r

k r

,

( / )

( / )

( )

( )

11 1

1

11 1

1

11 1

1

1 4 1

2 3 2

1

2

1

What happens as rc goes to 1? Sketch the P-v diagram for the Diesel cycle and show rc approaching 1 in the limit.

P

v

Therefore,

When rc > 1 for a fixed r, .

But, since , .

30

th Diesel th Otto, ,

r rDiesel Otto th Diesel th Otto, ,

31

Brayton Cycle

The Brayton cycle is the air-standard ideal cycle approximation for the gas-turbine engine. This cycle differs from the Otto and Diesel cycles in that the processes making the cycle occur in open systems or control volumes. Therefore, an open system, steady-flow analysis is used to determine the heat transfer and work for the cycle.

Search the web for information on new gas turbine technologies. One site that gives a link to the GE 7FA group of gas turbines that operate on natural gas ishttp://www.webshots.com/explains/sports/gas-turbine.html

A second link gives an overview of the applications of gas turbines.http://www.energysolutionscenter.org/DistGen/Tutorial/CombTurbine.htm#Heat_Recovery

Brayton Cycle Analysis

We assume the working fluid is air and the specific heats are constant and will consider the cold-air-standard cycle.

32

The closed cycle gas-turbine engine

33

The T-s and P-v diagrams for the Closed Brayton Cycle

Process Description 1-2 Isentropic compression (in a

compressor)2-3 Constant pressure heat addition 3-4 Isentropic expansion (in a turbine)4-1 Constant pressure heat rejection

34

Thermal efficiency of the Brayton cycle

th Braytonnet

in

out

in

W

Q

Q

Q, 1

Now to find Qin and Qout.

Apply the conservation of energy to process 2-3 for P = constant (no work), steady-flow, and neglect changes in kinetic and potential energies.

E E

m h Q m hin out

in

2 2 3 3

The conservation of mass gives

m m

m m min out

2 3

For constant specific heats, the heat added per unit mass flow is

( ) ( )

( )

Q m h h

Q mC T T

qQ

mC T T

in

in p

inin

p

3 2

3 2

3 2

35

The conservation of energy for process 4-1 yields for constant specific heats (let’s take a minute for you to get the following result)

( ) ( )

( )

Q m h h

Q mC T T

qQ

mC T T

out

out p

outout

p

4 1

4 1

4 1

The thermal efficiency becomes

th Braytonout

in

out

in

p

p

Q

Q

q

q

C T T

C T T

,

( )

( )

1 1

1 4 1

3 2

th Brayton

T T

T T

T T T

T T T

,

( )

( )

( / )

( / )

1

11

1

4 1

3 2

1 4 1

2 3 2

36

Recall processes 1-2 and 3-4 are isentropic, so

Since P3 = P2 and P4 = P1, we see that

3 32 4

1 4 1 2

orT TT T

T T T T

The Brayton cycle efficiency becomes

th Brayton

T

T, 1 1

2

Is this the same as the Carnot cycle efficiency?

Since process 1-2 is isentropic,

37

where the pressure ratio is rp = P2/P1 and

th Brayton

pk kr

, ( )/ 11

1

Extra Assignment

Evaluate the Brayton cycle efficiency by determining the net work directly from the turbine work and the compressor work. Compare your result with the above expression. Note that this approach does not require the closed cycle assumption.

38

Example 9-2

The ideal air-standard Brayton cycle operates with air entering the compressor at 95 kPa, 22oC. The pressure ratio rp is 6:1 and the air leaves the heat addition process at 1100 K. Determine the compressor work and the turbine work per unit mass flow, the cycle efficiency, the back work ratio, and compare the compressor exit temperature to the turbine exit temperature. Assume constant properties.

Apply the conservation of energy for steady-flow and neglect changes in kinetic and potential energies to process 1-2 for the compressor. Note that the compressor is isentropic.

E E

m h W m hin out

comp

1 1 2 2

The conservation of mass gives

m m

m m min out 1 2

39

For constant specific heats, the compressor work per unit mass flow is

( )

( )

( )

W m h h

W mC T T

wW

mC T T

comp

comp p

compcomp

p

2 1

2 1

2 1

Since the compressor is isentropic

40

w C T T

kJ

kg KK

kJ

kg

comp p

( )

. ( . )

.

2 1

1005 492 5 295

19815

The conservation of energy for the turbine, process 3-4, yields for constant specific heats (let’s take a minute for you to get the following result)

( ) ( )

( )

W m h h

W mC T T

wW

mC T T

turb

turb p

turbturb

p

3 4

3 4

3 4

Since process 3-4 is isentropic

41

Since P3 = P2 and P4 = P1, we see that( 1) /

4

3

( 1) / (1.4 1) /1.4

4 3

1

1 11100 659.1

6

k k

p

k k

p

T

T r

T T K Kr

w C T TkJ

kg KK

kJ

kg

turb p

( ) . ( . )

.

3 4 1005 1100 659 1

442 5

We have already shown the heat supplied to the cycle per unit mass flow in process 2-3 is

( ) . ( . )

.

m m m

m h Q m h

qQ

mh h

C T TkJ

kg KK

kJ

kg

in

inin

p

2 3

2 2 3 3

3 2

3 2 1005 1100 492 5

609 6

42

The net work done by the cycle is

w w w

kJ

kg

kJ

kg

net turb comp

( . . )

.

442 5 19815

244 3

The cycle efficiency becomes

th Braytonnet

in

w

q

kJkgkJkg

or

,

.

..

244 3

609 60 40 40%

43

The back work ratio is defined as

BWRw

w

w

w

kJkgkJkg

in

out

comp

turb

19815

442 50 448

.

..

Note that T4 = 659.1 K > T2 = 492.5 K, or the turbine outlet temperature is greater than the compressor exit temperature. Can this result be used to improve the cycle efficiency?

What happens to th, win /wout, and wnet as the pressure ratio rp is increased? Consider the T-s diagram for the cycle and note that the area enclosed by the cycle is the net heat added to the cycle. By the first law applied to the cycle, the net heat added to the cycle is equal to the net work done by the cycle. Thus, the area enclosed by the cycle on the T-s diagram also represents the net work done by the cycle.

44

Let's take a closer look at the effect of the pressure ratio on the net work done.

w w w

C T T C T T

C T T T C T T T

C Tr

C T r

net turb comp

p p

p p

pp

k k p pk k

( ) ( )

( / ) ( / )

( ) ( )( )/( )/

3 4 2 1

3 4 3 1 2 1

3 1 11

1 1

11

1

45

Note that the net work is zero when/( 1)

3

1

1k k

p p

Tr and r

T

For fixed T3 and T1, the pressure ratio that makes the work a maximum is obtained from:

dw

drnet

p

0

This is easier to do if we let X = rp(k-1)/k

w C TX

C T Xnet p p 3 111

1( ) ( )

dw

dXC T X C Tnet

p p 3

210 1 1 0 0[ ( ) ] [ ]

Solving for X

46

Then, the rp that makes the work a maximum for the constant property case and fixed T3 and T1 is

For the ideal Brayton cycle, show that the following results are true.•When rp = rp, max work, T4 = T2

•When rp < rp, max work, T4 > T2

•When rp > rp, max work, T4 < T2

The following is a plot of net work per unit mass and the efficiency for the above example as a function of the pressure ratio.

0 2 4 6 8 10 12 14 16 18 20 22120

140

160

180

200

220

240

260

280

0.15

0.20

0.25

0.30

0.35

0.40

0.45

0.50

0.55

0.60

Pratio

wnet

kJ/k

g

th,B

rayt

on

T1 = 22C

P1 = 95 kPa

T3 = 1100 K

t = c = 100%

rp,max

47

Regenerative Brayton Cycle

For the Brayton cycle, the turbine exhaust temperature is greater than the compressor exit temperature. Therefore, a heat exchanger can be placed between the hot gases leaving the turbine and the cooler gases leaving the compressor. This heat exchanger is called a regenerator or recuperator. The sketch of the regenerative Brayton cycle is shown below.

48

We define the regenerator effectiveness regen as the ratio of the heat transferred to the compressor gases in the regenerator to the maximum possible heat transfer to the compressor gases.

q h h

q h h h h

q

q

h h

h h

regen act

regen

regenregen act

regen

,

, max '

,

, max

5 2

5 2 4 2

5 2

4 2

49

For ideal gases using the cold-air-standard assumption with constant specific heats, the regenerator effectiveness becomes

5 2

4 2regen

T T

T T

Using the closed cycle analysis and treating the heat addition and heat rejection as steady-flow processes, the regenerative cycle thermal efficiency is

th regenout

in

q

q

h h

h h

,

1

1 6 1

3 5

Notice that the heat transfer occurring within the regenerator is not included in the efficiency calculation because this energy is not heat transferred across the cycle boundary.

Assuming an ideal regenerator regen = 1 and constant specific heats, the thermal efficiency becomes (take the time to show this on your own)

50

When does the efficiency of the air-standard Brayton cycle equal the efficiency of the air-standard regenerative Brayton cycle? If we set th,Brayton = th,regen then

Recall that this is the pressure ratio that maximizes the net work for the simple Brayton cycle and makes T4 = T2. What happens if the regenerative Brayton cycle operates at a pressure ratio larger than this value?

51

For fixed T3 and T1, pressure ratios greater than this value cause T4 to be less than T2, and the regenerator is not effective.

What happens to the net work when a regenerator is added?

What happens to the heat supplied when a regenerator is added?

The following shows a plot of the regenerative Brayton cycle efficiency as a function of the pressure ratio and minimum to maximum temperature ratio, T1/T3.

52

Example 9-3: Regenerative Brayton Cycle

Air enters the compressor of a regenerative gas-turbine engine at 100 kPa and 300 K and is compressed to 800 kPa. The regenerator has an effectiveness of 65 percent, and the air enters the turbine at 1200 K. For a compressor efficiency of 75 percent and a turbine efficiency of 86 percent, determine

(a) The heat transfer in the regenerator.(b) The back work ratio.(c) The cycle thermal efficiency.

Compare the results for the above cycle with the ones listed below that have the same common data as required. The actual cycles are those for which the turbine and compressor isentropic efficiencies are less than one.

(a) The actual cycle with no regeneration, = 0.(b) The actual cycle with ideal regeneration, = 1.0.(c) The ideal cycle with regeneration, = 0.65.(d) The ideal cycle with no regeneration, = 0.(e) The ideal cycle with ideal regeneration, = 1.0.

We assume air is an ideal gas with constant specific heats, that is, we use the cold-air-standard assumption.

53

The cycle schematic is the same as above and the T-s diagram showing the effects of compressor and turbine efficiencies is below.

s

T 100 kPa

800 kPa

T-s Diagram for Gas Turbine with Regeneration

1

2s

2a5

3

4s

4a

6

54

Summary of Results

Cycle type Actual Actual Actual Ideal Ideal Ideal

regen 0.00 0.65 1.00 0.00 0.65 1.00

comp 0.75 0.75 0.75 1.00 1.00 1.00

turb 0.86 0.86 0.86 1.00 1.00 1.00

qin kJ/kg 578.3 504.4 464.6 659.9 582.2 540.2

wcomp kJ/kg 326.2 326.2 326.2 244.6 244.6 244.6

wturb kJ/kg 464.6 464.6 464.6 540.2 540.2 540.2

wcomp/wturb 0.70 0.70 0.70 0.453 0.453 0.453

th 24.0% 27.5% 29.8% 44.8% 50.8% 54.7%

55

Compressor analysis

The isentropic temperature at compressor exit is( 1) /

2 2

1 1

( 1) /

(1.4 1) /1.422 1

1

800300 ( ) 543.4

100

k k

s

k k

s

T P

T P

P kPaT T K K

P kPa

To find the actual temperature at compressor exit, T2a, we apply the compressor efficiency

compisen comp

act comp

s

a

s

a

acomp

s

w

w

h h

h h

T T

T T

T T T T

K K

K

,

,

( )

.(543. )

.

2 1

2 1

2 1

2 1

2 1 2 1

1

3001

0 754 300

624 6

56

Since the compressor is adiabatic and has steady-flow

2 1 2 1( )

1.005 (624.6 300) 326.2

comp a p aw h h C T T

kJ kJK

kg K kg

Turbine analysis

The conservation of energy for the turbine, process 3-4, yields for constant specific heats (let’s take a minute for you to get the following result)

( ) ( )

( )

W m h h

W mC T T

wW

mC T T

turb a

turb p a

turbturb

p a

3 4

3 4

3 4

57

Since P3 = P2 and P4 = P1, we can find the isentropic temperature at the turbine exit. ( 1) /

4 4

3 3

( 1) /

(1.4 1) /1.444 3

3

1001200 ( ) 662.5

800

k k

s

k k

s

T P

T P

P kPaT T K K

P kPa

To find the actual temperature at turbine exit, T4a, we apply the turbine efficiency.

turbact turb

isen turb

a

s

a

s

a turb s

a

w

w

h h

h h

T T

T T

T T T T

K K

K T

,

,

( )

. ( . )

.

3 4

3 4

3 4

3 4

4 3 3 4

2

1200 086 1200 662 5

737 7

58

The turbine work becomesw h h C T T

kJ

kg KK

kJ

kg

turb a p a

3 4 3 4

1005 1200 737 7

464 6

( )

. ( . )

.

The back work ratio is defined as

BWRw

w

w

w

kJkgkJkg

in

out

comp

turb

326 2

464 60 70

.

..

59

Regenerator analysis

To find T5, we apply the regenerator effectiveness.

regena

a a

a regen a a

T T

T T

T T T T

K K

K

5 2

4 2

5 2 4 2

624 6 0 65 737 7 624 6

6981

( )

. . ( . . )

.

60

( )

. ( . . )

.

m h Q m h

m m m

qQ

mh h

C T T

kJ

kg KK

kJ

kg

a a regen

a

regenregen

a

p a

2 2 5 5

2 5

5 2

5 2

1005 6981 624 6

739

To find the heat transferred from the turbine exhaust gas to the compressor exit gas, apply the steady-flow conservation of energy to the compressor gas side of the regenerator.

61

4 4 6 6

4 6

4 6 4 6

6 4

( )

73.9737.7

1.005

664.2

a a regen

a

regenregen a p a

regena

p

m h Q m h

m m m

Qq h h C T T

mkJ

q kgT T K

kJCkg K

K

Using qregen, we can determine the turbine exhaust gas temperature at the regenerator exit.

62

Heat supplied to cycle

Apply the steady-flow conservation of energy to the heat exchanger for process 5-3. We obtain a result similar to that for the simple Brayton cycle.

q h h C T T

kJ

kg KK

kJ

kg

in p

3 5 3 5

1005 1200 6981

504 4

( )

. ( . )

.

Cycle thermal efficiency

The net work done by the cycle is

(464.6 326.2) 138.4

net turb compw w w

kJ kJ

kg kg

63

The cycle efficiency becomes

th Braytonnet

in

w

q

kJkgkJkg

or

,

.

.. .

138 4

504 40 274 27 4%

You are encouraged to complete the calculations for the other values found in the summary table.

64

Other Ways to Improve Brayton Cycle Performance

Intercooling and reheating are two important ways to improve the performance of the Brayton cycle with regeneration.

65

The T-s diagram for this cycle is shown below. Sketch the P-v diagram.

v

P

66

Intercooling

When using multistage compression, cooling the working fluid between the stages will reduce the amount of compressor work required. The compressor work is reduced because cooling the working fluid reduces the average specific volume of the fluid and thus reduces the amount of work on the fluid to achieve the given pressure rise.

To determine the intermediate pressure at which intercooling should take place to minimize the compressor work, we follow the approach shown in Chapter 7.

For the adiabatic, steady-flow compression process, the work input to the compressor per unit mass is

4 32 4

1 31 2

= = compw v dP vdP v dP v dP 0

67

For the isentropic compression process

2 2 1 1 4 4 3 3

2 1 4 3

1 2 1 3 4 3

( 1) /( 1) /

2 41 3

1 3

= ( ) ( )-1 -1

( ) ( )-1 -1

( / 1) ( / 1)-1

1 1-1

comp

k kk k

k kw P v Pv P v Pv

k kk kR

R T T T Tk kk

R T T T T T Tk

k P PR T T

k P P

Notice that the fraction kR/(k-1) = Cp.

Can you obtain this relation another way? Hint: apply the first law to processes 1-4.

68

For two-stage compression, let’s assume that intercooling takes place at constant pressure and the gases can be cooled to the inlet temperature for the compressor, such that P3 = P2 and T3 = T1.

The total work supplied to the compressor becomes

To find the unknown pressure P2 that gives the minimum work input for fixed compressor inlet conditions T1, P1, and exit pressure P4, we set

dw P

dPcomp ( )2

2

0

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This yields

P PP2 1 4

or, the pressure ratios across the two compressors are equal.

P

P

P

P

P

P2

1

4

2

4

3

Intercooling is almost always used with regeneration. During intercooling the compressor final exit temperature is reduced; therefore, more energy must be supplied in the heat addition process to achieve the maximum temperature of the cycle. Regeneration can make up part of the required heat transfer.

To supply only compressed air, using intercooling requires less work input. The next time you go to a home supply store where air compressors are sold, check the larger air compressors to see if intercooling is used. For the larger air compressors, the compressors are made of two piston-cylinder chambers. The intercooling heat exchanger is often a pipe with a attached fins that connects the large piston-cylinder chamber with the smaller piston-cylinder chamber. Often the fly wheel used to drive the compressor has spokes shaped like fan blades that are used to increase air flow across the compressor and heat exchanger pipe to improve the intercooling effect.

70

Shown here is a two-stage, 7.5 hp air compressor with intercooling.

Photo by M. Boles

71

Extra Assignment

Obtain the expression for the compressor total work by applying conservation of energy directly to the low- and high-pressure compressors.

Reheating

When using multistage expansion through two or more turbines, reheating between stages will increase the net work done (it also increases therequired heat input). The regenerative Brayton cycle with reheating was shown above.

The optimum intermediate pressure for reheating is the one that maximizes the turbine work. Following the development given above for intercooling and assuming reheating to the high-pressure turbine inlet temperature in a constant pressure steady-flow process, we can show the optimum reheat pressure to be

P P P7 6 9or the pressure ratios across the two turbines are equal.

P

P

P

P

P

P6

7

7

9

8

9