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Presented by: Presented by: Damon Ogden Damon Ogden 2 2 - - 13 13 - - 01 01 ME 372 Thermodynamics II Chapter 8 Gas Power Cycles ME 372 Thermodynamics II Chapter 8 Gas Power Cycles

Gas Power Cycles

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Gives Brief Description of Gas Turbine Power Cycles

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Page 1: Gas Power Cycles

Presented by:Presented by:Damon OgdenDamon Ogden

22--1313--0101

ME 372 Thermodynamics II

Chapter 8Gas Power Cycles

ME 372 Thermodynamics II

Chapter 8Gas Power Cycles

Page 2: Gas Power Cycles

Reciprocating EnginesReciprocating Engines

CH 8

Sections

8.4 - 8.6

Page 3: Gas Power Cycles

Short VideoShort Video

• 3.3 Liter• V 12• 1965 Ferrari 275• Water Brake Dynamometer • Over 300 hp

Page 4: Gas Power Cycles

Discussion TopicsDiscussion Topics

1. - History2. - General Knowledge3. - 4 Stroke Cycle4. - Otto Cycle5. - Diesel Cycle

Page 5: Gas Power Cycles

HistoryHistory• Nikolaus Otto patented the “Otto Cycle”

Engine 1876Spark ignition engines use the Otto Cycle

• Rudolf Diesel received patent for “Diesel Cycle” Engine in 1892

Compression Ignition engines use theDiesel Cycle and hence the name “diesel” engines

Page 6: Gas Power Cycles

How much do you know?How much do you know?

• What are are some differences between gasoline and diesel engines?

Page 7: Gas Power Cycles

Ways to describe an engineWays to describe an engine

• Application• Design Geometry• Working Cycle• Fuel• Method of load control• Method of ignition

Page 8: Gas Power Cycles

Piston -CylinderNomenclature

Page 9: Gas Power Cycles

Otto / Diesel Cycle DifferencesOtto / Diesel Cycle DifferencesFour Stroke Cycle

Otto Cycle Diesel Cycle

Throttle Air Load Control Meter Fuel

Fuel/Air mix Working Fluid Air During Compression

Spark Start Combustion Inject Fuel

Page 10: Gas Power Cycles

Four-Stroke CycleFour-Stroke Cycle

• Intake

http://www.howstuffworks.com/engine.htm

• Compression• Power• Exhaust

SuckSqueezeBangBlow

Page 11: Gas Power Cycles

Thermodynamic Properties

Thermodynamic Properties

• The working fluid is air, and behaves as an ideal gas.

• Combustion processes are modeled as heat addition from an external source.

• Heat reject process to the surroundings is used to restore working fluid to its initial state.

• All processes are internally reversible.

Page 12: Gas Power Cycles

Four Stroke Cycle P-V diagram

Intake Valve Opens

Combustion

Volume

Pressure Exhaust Valve Opens

Intake Valve Closes

Exhaust Valve Closes

TDC BDC

Intake

Exhaust

Power

Page 13: Gas Power Cycles

Spark Ignition, Otto Cycle Engines

Spark Ignition, Otto Cycle Engines

• From < 1 hp to > 3000 hp• Cars• Trucks• Motor Cycles• Small Engines, i.e.;

Lawn Mower, • Mems

Page 14: Gas Power Cycles

Spark Ignition Engine Characteristics

Spark Ignition Engine Characteristics

• Compression Ratio of 6 - 12=• RPM 900 - 8000• Power per unit Volume

3 - 60 kW / LiterFerrari in video @ 68 kW / liter

• Bore = .05 - .45 m

@TDC

@BDC

VV

BBDC

TDC

Page 15: Gas Power Cycles

p

v

1

2

3

4

Otto Cycle

s = constant

Page 16: Gas Power Cycles

A Quick Review of TermsA Quick Review of Terms• s = entropy, h = enthalpy, • u = internal energy• Isometric = Constant Volume• Isobaric = Constant Pressure• Isothermal = Constant Temperature• Isentropic = No irreversibilities,

Ideal process foradiabatic processes(adiabatic = no heat transfer)

Page 17: Gas Power Cycles

Otto Cycle ModelOtto Cycle Model

• Intake and exhaust strokes not modeled

• Compression modeled as isentropic• Heat input modeled as isometric,

occurring at TDC• Expansion modeled as isentropic• Heat rejection modeled as isometric,

occurring at BDC

Page 18: Gas Power Cycles

• Process 1-2: Isentropic Compression

• Apply First Lawq w u− = ∆

rvv

vv

r

r 11

2

1

2 ==

Since ∆s = 0

p

v

1

2

Otto Cycle AnalysisOtto Cycle Analysis

Page 19: Gas Power Cycles

• Process 2-3 Isometric Heating• Apply First Law

q w u− = ∆

q u uin = −3 2

but v = constant, therefore w = 0

p

v

1

2

3

Otto Cycle AnalysisOtto Cycle Analysis

Page 20: Gas Power Cycles

• Process 3-4 Isentropic Expansion• Apply First Law

q w u− = ∆

vv

vv

rr

r

4

3

4

3= =

p

v

1

2

3

4But since ∆s = 0

Otto Cycle AnalysisOtto Cycle Analysis

Page 21: Gas Power Cycles

• Process 4-1 Isometric Cooling• Apply First Law

q w u− = ∆

q u uout = −1 4

p

v

1

2

3

4but v = constant, therefore:

Otto Cycle AnalysisOtto Cycle Analysis

Page 22: Gas Power Cycles

Compression Ignition Diesel Cycle EnginesCompression Ignition Diesel Cycle Engines

• From < 50 hp to > 6000 hp• Cars• Trucks• Trains• Boats• Power Plants• Construction Equipment 1.47 L, 50 hp

Volkswagen

Page 23: Gas Power Cycles

Combustion Ignition Engine Characteristics

Combustion Ignition Engine Characteristics

• Compression Ratios, rc of 12 - 23• Power per unit volume

2 - 26 kW / Liter• Bore .075 - 1 m• RPM 110 - 5000

Caterpillar

BBDC

TDC

@TDC

@BDC

VV

=cr 8 Liter

400 hp

Page 24: Gas Power Cycles

Diesel Cycle ModelDiesel Cycle Model

• Intake and exhaust strokes not modeled

• Compression modeled as isentropic• Heat input modeled as isobaric,

occurring from TDC to appropriate volume

• Expansion modeled as isentropic• Heat rejection modeled as isometric,

occurring at BDC

Page 25: Gas Power Cycles

T

s

1

2

3

4

p=const

v=const

Diesel Cycle

p

v1

23

4s=c

s=c

Page 26: Gas Power Cycles

q w u− = ∆

rvv

vv

r

r 11

2

1

2 ==

p

v1

2

Since ∆s = 0

Diesel Cycle AnalysisDiesel Cycle Analysis• Process 1-2: Isentropic

Compression• Apply First Law

Page 27: Gas Power Cycles

p

v1

2

Diesel Cycle AnalysisDiesel Cycle Analysis

• Process 2-3 Isobaric Heating• Apply First Law• q - w = ∆u• but p = constant, • therefore w = p ∆∆∆∆v• qin = h3 - h2

• Cutoff Ratio = rc

• rc = v3 - v2• Only process where Otto and Diesel Cycle differ

Page 28: Gas Power Cycles

• Process 3-4 Isentropic Expansion

• Apply First Law• q - w = ∆u

Diesel Cycle AnalysisDiesel Cycle Analysis

p

v1

23

4•But since ∆∆∆∆s = 0

cr

r

rr

vv

vv ==

3

4

3

4

Page 29: Gas Power Cycles

q w u− = ∆

Diesel Cycle AnalysisDiesel Cycle Analysis

• Process 4-1 Isometric Cooling• Apply First Law

• but v = constant, therefore:

p

v1

23

4

q u uout = −1 4

Page 30: Gas Power Cycles

Comparison Of the Two Cycles

Comparison Of the Two Cycles

• Otto cycle utilizes an external energy source to initiate Combustion (spark plug)

• Diesel cycle relies on temp and pressure to start combustion

• Diesels only compress air, during compression stroke

• Otto cycle, spark engines compress both air and fuel during compression stroke

Page 31: Gas Power Cycles

Comparison ContinuedComparison ContinuedFuel plays major role in cycle differences

• Spark ignition engines need fuels that are resistant to (knock)

• Diesel engines require fuels that will auto ignite under proper pressure and temperature

• Diesel fuel allows for higher Comp Ratios, = higher efficiencies.

Page 32: Gas Power Cycles

Summary of Reciprocating Engines

Summary of Reciprocating Engines

• Been around for 125 years• Haven’t changed much:

Computers, Lower Emissions• Good for man, bad for the earth:• Not going anywhere soon• Future is Hydrogen, exhaust = H2O

Page 33: Gas Power Cycles

Future = Mems Engines?Future = Mems Engines?

.001 kW

Page 34: Gas Power Cycles

The EndThe End

Any Questions ?

Page 35: Gas Power Cycles

Blank SlideBlank Slide

Page 36: Gas Power Cycles

w u uon = −1 2

w u u p v vby = − + −3 4 2 3 2( )

q u uout = −1 4

q h hin = −3 2

w w w u u p v v u unet by on= + = − + − + −( ) ( ) ( )3 4 2 3 2 1 2

η thnet

in

wq

u u p v v u uh h

= = − + − + −−

3 4 2 3 2 1 2

3 2

( )

Diesel Cycle AnalysisDiesel Cycle Analysis• Combining above equations:

Page 37: Gas Power Cycles

RTpv =uwq ∆=−

For isentropic processes:

rvv

vv

r

r 1

1

2

1

2 ==

in

netth q

w=η

vwMEP net

∆=

Equations:Equations:

Page 38: Gas Power Cycles

Example: 9-2 Diesel CycleAn air-standard Diesel cycle has a compression ratio of 16 and a cutoff ratio of 2. At the beginning of compression, p1= 14.2 psi, V1 = 0.5 ft3, and T1 = 520oR. Determine:(a) the heat added, [Btu](b) the heat rejected, [Btu](c) the thermal efficiency(d) the Carnot efficiency(e) the mean effective pressure, [psi]

Page 39: Gas Power Cycles

point 1 2 3 4p - psia 14.2

T oR 520v ft3/lb

u - Btu/lbh - Btu/lb

vr

V - ft3 0.5

Summary of Conditions - Diesel Cycle

r = 16, rc = 2

Page 40: Gas Power Cycles

( )lbft

ftin

inlb

RRlb

lbftp

RTv

f

oo

f3

2

2

2

1

11

56.13

11442.14

52097.28

1545

=

==

Solution: (point 1)Solution: (point 1)

Page 41: Gas Power Cycles

(isentropic compression from point 1:

911.916

58.15812

1

2

1

2 ==⇒== rr

r vrv

vvv

from air table, T2 is between 1480 & 1520 o

563.034.10578.934.10911.9

)1480()1520(

)1480(2 =−−=

−−

=rr

rr

vvvv

fr

( )( ) RT o150214801520563.014802 =−+=

Solution cont'd (point 2)Solution cont'd (point 2)

Page 42: Gas Power Cycles

( )( )

lbBtu

u

84.266

44.26226.270563.044.2622

=

−+=

( )( )

lbBtu

h

4.369

89.36347.374563.089.3632

=

−+=

Point 2 cont'dPoint 2 cont'd

Page 43: Gas Power Cycles

( ) 222

1

21

2

1

1

212

1

11

2

22

65616520

15022.14inlb

inlb

p

rTTp

vv

TTpp

Tvp

Tvp

ff =

=

==⇒=

Point 3

( )( ) RRT

rTvv

ppTT

Tvp

Tvp

oo

c

3005215023

22

3

2

323

2

22

3

33

==

==⇒=

Point 2 cont'dPoint 2 cont'd

Page 44: Gas Power Cycles

from Air Table, T3 is between 3000 & 3050oRusing appropriate linear interpolation, determine

( )( )lb

Btuu 16.58604.58528.5961.004.5853 =−+=

( )( )lb

Btuh 15.79268.79034.8051.068.7903 =−+=

( )( ) 174.1180.1118.11.0180.13 =−+=rv

Point 3 cont'dPoint 3 cont'd

Page 45: Gas Power Cycles

Point 4Point 4Isentropic expansion from point 3

( ) 390.90625.0

5.0174.13

434 =

==

VVvv rr

from table, 1520 & 1560oR, interpolation

273.0578.9890.8578.9390.9

)1520()1560(

)1520(4 =−−=

−−

=rr

rr

vvvv

fr

( )( )( )( )

lbBtuu

RT o

4.27226.27013.178273.026.270

153115201560273.01520

4

4

=−+=

=−+=

Page 46: Gas Power Cycles

Point 1 2 3 4Start of Start of Start of Start of

Compressio Heating Expansion Cooling

p - psia 14.2 656T oR 520 1502 3005 1531

v ft3/lb 13.56u - Btu/lb 88.62 266.84 586.16 272.4h - Btu/lb 124.7 369.84 792.15

vr 158.58 9.911 9.39V - ft3 0.5 0.0313 0.0625 0.5

Summary of Conditions - Diesel Cycle

r = 16, rc = 2

Page 47: Gas Power Cycles

Calculations:Calculations:(a)

lb

lbft

ftvVm 2

3

3

1

1 1069.356.13

5.0 −×===

lbBtuhhqin 31.42284.36915.79223 =−=−=

( ) Btulb

BtulbqmQ inin 57.153.4220369.0 =

==

BtuQin 57.15=

Page 48: Gas Power Cycles

Calculations cont'dCalculations cont'd(b)

( ) ( )( )lb

BtulbuumQout 4.27262.880369.041 −=−=

BtuQout 78.6−=(c)

57.1578.611 −=−=

in

outth Q

564.0=thη

Page 49: Gas Power Cycles

w u uon = −1 2

w u uby = −3 4

q u uout = −1 4

q u uin = −3 2

w w w u u u unet by on= + = − + −( ) ( )3 4 1 2

η thnet

in

wq

u u u uu u

= = − + −−

3 4 1 2

3 2

Otto Cycle AnalysisOtto Cycle Analysis• Combining above equations:

Page 50: Gas Power Cycles

Example: 9-1At the beginning of the compression process in an air-standard Otto Cycle, p1 = 14.7 psi, T1 = 530oR. The compression ratio is 8. Determine for a maximum cycle temperature of 2000oR: thermal efficiency, Carnotefficiency, and mean effective pressure.

Page 51: Gas Power Cycles

Point 1 2 3 4start start start start

of of of ofcompression heating expansion cooling

p-psia 14.7T oR 530 2000

v-ft3/lbu-Btu/lb

vr

Summary of Conditions

r = 8

Page 52: Gas Power Cycles

Point 1 2 3 4start start start start

of of of ofcompression heating expansion cooling

p-psia 14.7T oR 530 2000

v-ft3/lbu-Btu/lb 90.3 367.61

vr 151.38 4.258

Summary of Conditions - data from air table

r = 8

Page 53: Gas Power Cycles

RTpv =uwq ∆=−

For isentropic processes:

rvv

vv

r

r 1

1

2

1

2 ==

in

netth q

w=η

vwMEP net

∆=

Equations:Equations:

Page 54: Gas Power Cycles

( )lbft

inlb

inftR

Rlblbft

pRTv

f

oo

f3

2

2

2

1

11 35.13

7.14

1441530

97.281545

=

==

lbftlbft

rvv

331

2 67.18

/35.13 ===

92.188

38.15112 ===

rvv r

r

Solution:Solution:

Page 55: Gas Power Cycles

From air tables, note that T2 is between1160 and 1200 oR.doing the interpolation:T2 = 1191 oRu2 = 207.33 Btu/lb

Solution cont'dSolution cont'd

Page 56: Gas Power Cycles

Point 1 2 3 4start start start start

of of of ofcompression heating expansion cooling

p-psia 14.7T oR 530 1191 2000 954

v-ft3/lb 13.35 1.67u-Btu/lb 90.3 207.3 367.61 164.2

vr 151.38 18.92 4.258 34.064

Summary of Conditions - calculations

r = 8

Page 57: Gas Power Cycles

( ) ( )

net

net

wlb

Btu

wwwww

=

=+−++−=+++= −−−−

4.86

02.1647.36703.2073.9014433221

( ) in

in

qlb

Btuuuqq

==−

=−== −

3.1603.2076.367

2332

Solution - cont'dSolution - cont'd

Page 58: Gas Power Cycles

thin

netth q

w ηη ==== 54.03.1604.86

Carnoth

cCarnot T

T ηη ==−=−= 74.0200053011

( )

2

2

2321

9.39

14467.135.13

7784.86

inlb

MEP

ftin

lbft

Btulbft

lbBtu

vvwMEP

f

f

net

=

=−

=

Solution - cont'dSolution - cont'd

Page 59: Gas Power Cycles

Calculations cont'dCalculations cont'd(d)

300552011 −=−=

h

cCarnot T

827.0=Carnotη(e)

=−+=

−=

2

233

2121

144

778

0313.05.078.657.15

ftinBtulbft

ftftBtuBtu

VVQQ

VVWMEP

f

outinnet

2101inlb

MEP f=

Page 60: Gas Power Cycles

Internal Combustion Engine Models

Internal Combustion Engine Models

• Spark Ignition Engine -Otto Cycle

• Compression Ignition Engine -Diesel Cycle

Page 61: Gas Power Cycles

The piston moves the length The piston moves the length of the cylinder four times for one of the cylinder four times for one complete cycle.complete cycle.

Hence the name “four stroke” orHence the name “four stroke” or“four cycle engine”.“four cycle engine”.

Page 62: Gas Power Cycles

Otto Cycle Model

Page 63: Gas Power Cycles

Diesel Cycle Model

Page 64: Gas Power Cycles

Piston-Cylinder NomenclaturePiston-Cylinder Nomenclature• Bore = B, Stroke = S• Bottom dead center = BDC• Top dead center = TDC• Mean Piston Speed = Sp = 2SN ,

N = engine speed in rev/s• Clearance volume = VTDC

• Displacement volume = VBDC - VTDC

• Compression ratio r = VBDC/VTDC

Page 65: Gas Power Cycles

Method of Load ControlMethod of Load Control

• Throttle Air • (Otto cycle, spark ignition)

• Fuel Metering• (Diesel Cycle, compression

ignition)

Page 66: Gas Power Cycles

T

s

1

2

3

4

p=const

v=const

Diesel Cycle

p

v1

23

4s=c

s=c

Page 67: Gas Power Cycles

q w u− = ∆

Diesel Cycle AnalysisDiesel Cycle Analysis• Process 3-4 Isentropic

Expansion• Apply First Law

• But since ∆∆∆∆s = 0

p

v1

23

4

Page 68: Gas Power Cycles

q w u− = ∆

cr

r

rr

vv

vv ==

3

4

3

4

p

v1

23

4

Diesel Cycle AnalysisDiesel Cycle Analysis• Process 3-4 Isentropic

Expansion• Apply First Law

• But since ∆∆∆∆s = 0

Page 69: Gas Power Cycles

q w u− = ∆

q u uout = −1 4

p

v1

23

4

Diesel Cycle AnalysisDiesel Cycle Analysis• Process 4-1 Isometric Cooling• Apply First Law

• but v = constant, therefore:

Page 70: Gas Power Cycles

Intake Stroke(Suck)

Intake Stroke(Suck)

• Intake valve open

• Exhaust valve closed

• Piston moves from TDC to BDC drawing in mixture of fuel and air (Only air for diesel cycle)

Page 71: Gas Power Cycles

Compression Stroke(Squeeze)

Compression Stroke(Squeeze)

• Intake valve closes

• Exhaust valve remains closed

• Piston moves from BDC to TDC compressing fuel/air mixture, or air only

Otto Cycle

• Near top of stroke, spark ignites fuel/air mixture, causing heat input

Diesel Cycle

• Fuel injected into compressed air, in the cylinder

Page 72: Gas Power Cycles

Power Stroke(Bang)

Power Stroke(Bang)

• Both valves closed

• Hot combustion products expand causing piston to move from TDC to BDC, producing work output

Page 73: Gas Power Cycles

Exhaust Stroke(Blow)

Exhaust Stroke(Blow)

• Exhaust valve opens

• Intake valve remains closed

• Piston moves from BDC to TDC, forcing spent combustion products out of cylinder

Page 74: Gas Power Cycles

ApplicationsApplications

• Auto• Semi-Truck• Locomotive• Marine• Aircraft• Stationary Power

Page 75: Gas Power Cycles

Design Geometry Operating CycleDesign Geometry Operating Cycle

• V• Inline• Opposed• Rotary• Radial

• 4 stroke(There are others, but

those will be for a discussion)

Page 76: Gas Power Cycles

FuelsFuels

• Gasoline• Diesel• Natural Gas• Liquid Propane• Methanol• Mixed gases