Fossil Fuel - Compressor and turbine work

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    FACULTY OF ENGINEERING AND APPLIED SCIENCE

    MECE4410U Fossil Fuel Energy Conversion

    LABORATORY REPORT

    Course Instructor: Dr. Bale Redd

    La! Instructor: Dr. "u# S$#

    LAB REPORT %: &

    LAB GROUP NU'BER %:

    LAB GROUP 'E'BERS

    % Surna(e Na(e ID S#)nature

    * +u(ara,elaut$a( -#not$ */&&0&1

    2

    /

    &

    Remarks:

    I3 one #n )rou4 c$eats5 t$e ent#re )rou4 6#ll !e res4ons#!le 3or #t.

    Pla)#ar#s( and d#s$onest 6#ll not !e tolerated. T$e )rou4 (e(!er7s85 6$o don9t s#)n t$e re4ort5 6#ll !e cons#dered not contr#!uted; and )#,en

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    Table of Conens

    Pa)e %

    Introduct#on>>>>>>>>>>>>>>>..................................................*

    T$eoret#cal Bac=)round>>>>>>>>>>>>>>>...............................*

    E?4er#(ental Un#t and Procedure>>>>>>>>>>>>>>>>>........2

    Results and D#scuss#on>>>>>>>.................................................................&

    Conclus#ons>>>>>>>>>>>>>>>>>>>...................................

    Ac=no6led)e(ent 7#3 a44l#ca!le8>>>>>>>>.............................................

    No(enclature>>>>>>>>>>>>..........................................................

    Re3erences>>>>>>>>>>>>>>>>>>>>>>>>>>>

    A44end#? 7#3 a44l#ca!le8>>>>>>>>>>>>>>>>>>>>>>.

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    Introduct#on

    In t$#s e?4er#(ent5 t$e o!@ect#,e #s to o!ser,e and anal

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    2/: Re,ers#!le constant 4ressure $eat add#t#on Fuel and a#r #s (#?ed at constant 4ressure to

    )enerate $ot )asses

    /&: Isentro4#c E?4ans#on $ot )ases are e?4anded t$rou)$ tur!#ne at constant entro4&*: Re,ers#!le Constant Pressure Heat Re@ect#on: E?$aust and #nta=e #n t$e ccle

    T$ese tur!#nes are co(4act and $a,e a $#)$ 4o6er to 6e#)$t rat#o5 t$ere3ore t$e are 4re3erredo,er t$e stea(6ater tur!#nes. It #s #deal 3or a#rcra3ts5 and ot$er a44l#cat#ons 6$ere t$e 6e#)$t o3

    t$e eu#4(ent #s #(4ortant 3or t$e e33#c#enc o3 t$e sste(. For e?a(4le5 a#rcra3t tur!#nes

    o4erates on a @et 4ro4uls#on ccle. In #deal @et 4ro4uls#on ccles t$e )ases are not e?4anded toa(!#ent 4ressure5 !ecause t$e tur!#ne 4o6er #s onl needed to 4o6er t$e co(4ressor and ot$er

    eu#4(ent 7Net 6or= out4ut 8. T$e )ases are released a3ter tur!#ne #n a#rcra3ts and s#(#lar

    a44l#cat#ons $a,e a no

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    Figure .! Turbo&e engine/ s$'e(ai$ of 'e syse( an) lo$aion of ea$' sages

    Alt$ou)$ t$e e?4er#(ent 6as conducted ! t$e teac$#n) ass#stant5 so(e sa3et 4rocedure 6as3ollo6ed. Students 6ere to stand at a sa3e d#stance 3ro( t$e e?$aust o3 t$e tur!#ne5 and 6eres4ons#!le 3or 6ear#n) sa3et )o))les. Re3er to La!orator (anual & 3or e?act sa3et 4rocedure

    3ollo6ed ! teac$#n) ass#stant *.

    Results and D#scuss#ons

    *.

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    Table 1! Resuls for urbine roaion s"ee) of a""roi(aely 000 r"(

    E"eri(en 2ae ****2*& Ti(e &J.1&

    A(os"'eri$ Pressure

    P0

    **./21 =Pa A(os"'eri$

    Te("eraure/ T0

    2

    Co("ressor 3nle

    Pressure/ P1

    2.&& Co("ressor 3nle

    Te("eraure/ T1

    *2.*K

    Co("ressor Ei

    Pressure/ P2

    KJ.1/ Co("ressor Ei

    Te("eraure/ T2

    .K

    Turbine 3nle

    Pressure/ P3

    KJ. Turbine 3nle

    Te("eraure/ T3

    &K0.&

    Turbine Ei Pressure/P

    4

    J.*0 Turbine Ei

    Te("eraure/ T4

    JK.22

    E'aus as Pressure/P

    5

    &.* E'aus as

    Te("eraure/ T5

    &*K./

    Fuel Flo5 6L7'8 *./J Turbine Roaion9"ee) 6RPM8

    110&

    T'rus 6:8 &1.2J

    Table %! Resuls for urbine roaion s"ee) of a""roi(aely ; 000 r"(

    E"eri(en 2ae ****2*& Ti(e 2./&

    A(os"'eri$ PressureP

    0

    **./21 =Pa A(os"'eri$

    Te("eraure/ T0

    2

    Co("ressor 3nle

    Pressure/ P1

    /.01 Co("ressor 3nle

    Te("eraure/ T1

    **.11

    Co("ressor Ei

    Pressure/ P2

    *&J.2J Co("ressor Ei

    Te("eraure/ T2

    *&.12

    Turbine 3nle

    Pressure/ P3

    *&1.K Turbine 3nle

    Te("eraure/ T3

    1&.&

    Turbine Ei Pressure/P

    4

    *1.*J Turbine Ei

    Te("eraure/ T4

    J*K.J

    E'aus as Pressure/P

    5

    *.J1& E'aus as

    Te("eraure/ T5

    &J*.2

    Fuel Flo5 6L7'8 *1.1 Turbine Roaion

    9"ee) 6RPM8

    J10

    T'rus 6:8 1J./2

    Table 1! Resuls for urbine roaion s"ee) of a""roi(aely

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    E"eri(en 2ae ****2*& Ti(e 0*.1&

    A(os"'eri$ PressureP

    0

    **./21=Pa A(os"'eri$

    Te("eraure/ T0

    2

    Co("ressor 3nle

    Pressure/ P1

    J.12 Co("ressor 3nle

    Te("eraure/ T1

    **.

    Co("ressor Ei

    Pressure/ P2

    2*&.1 Co("ressor Ei

    Te("eraure/ T2

    *&/.0

    Turbine 3nle

    Pressure/ P3

    2*&.2 Turbine 3nle

    Te("eraure/ T3

    J/0.0

    Turbine Ei Pressure/P

    4

    2./0 Turbine Ei

    Te("eraure/ T4

    J&/.K

    E'aus as Pressure/P

    5

    *.K* E'aus as

    Te("eraure/ T5

    1K.2

    Fuel Flo5 6L7'8 2*./ Turbine Roaion

    9"ee) 6RPM8

    1/K

    T'rus 6:8 K&.21

    2.

    0 50 100 1500

    50

    100

    150

    200

    250

    Compressor Exit/Inlet Pressure vs Time

    Inlet Compressor

    Pressure vs time

    Compressor Exit

    Pressure vs time

    Time (s

    Pressure! "P#

    Figure .a! Co("ressor Ei73nle Pressure vs Ti(e

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    0 50 100 1500

    20

    40

    60

    80

    100

    120

    140

    160

    180

    Compressor Inlet/Exit Temper#ture vs time

    Inlet Compressor

    Temper#ture vs time

    Exit Compressor

    Temper#ture vs time

    Time (s

    Temper#ture! C

    Figure .b! Co("ressor 3nle7Ei Te("eraure vs Ti(e

    0 50 100 1500

    100

    200

    300

    400

    500

    600

    700

    800

    Tur$ine Exit/Inlet Temper#ture vs Time

    Tur$ine Exit

    Temper#ture vs TimeTur$ine Inlet

    Temper#ture vs Time

    Time (s

    Temper#ture! C

    Figure .$! Turbine Ei73nle vs Ti(e

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    0 50 100 150

    %50

    0

    50

    100

    150

    200

    250

    Tur$ine Inlet/Exit Pressure vs Time

    Tur$ine Inlet Pressure

    vs Time

    Tur$ine Exit Pressure

    vs Time

    Time (s

    Pressure! "P#

    s

    F#)ure /d: Tur!#ne InletE?#t Pressure ,s T#(e

    0 20 40 60 80 100 120 1400

    5

    10

    15

    20

    25

    &uel &lo' s Time

    Time (s

    &uel &lo' )/*r

    s

    F#)ure /e: Fuel Flo6 ,s T#(e

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    0 20 40 60 80 100 120 1400

    10

    20

    30

    40

    50

    60

    70

    80

    90

    T*rust vs Time

    Time! (s

    T*rust! +

    s

    Figure .f! T'rus vs Ti(e

    iscussion

    Bot$ co(4ressor outlet 4ressure and te(4erature r#ses cont#nuousl unt#l #t 4ea=s at a!out*s t$en #t dro4s sl#)$tl 7F#)ure /a and /!8. T$e 4ressure dro4s (uc$ 3aster t$an t$e

    te(4erature. In t$e e?#t 4ressure read#n)s5 t$e 4ressure dro4s a l#ttle d#33erent t#(es5 $o6e,er t$e

    o,erall 4lot s$o6s )radual #ncrease 7F#)ure /a8. Tur!#ne #nlete?#t te(4erature 4lot 4ea=s ,eru#c=l 7F#)ure /c8. T$en #t 3luctuate !ut t$e 4ea= ,alue re(a#ns constant. As 3or 4ressure at #nlet

    #s sa(e as co(4ressor e?#t 4ressure5 t$ere3ore #t loo=s s#(#lar to t$at 4lot5 6$ere #t #ncreases 6#t$

    t#(e 7F#)ure /d8. Ho6e,er t$e tur!#ne e?#t 4ressure #s ,er lo65 (uc$ l#=e t$e #nlet co(4ressor4ressure 4ro3#le5 !ut #t st#ll #ncreases ,er slo6l. Bot$ t$rust ,s t#(e and 3uel 3lo6 ,s t#(e s$o6

    s#(#lar relat#ons as t$e !ot$ #ncrease unt#l 4ea= co(4ressor e?#t 4ressure 4o#nt at a!out 0Ks5

    7F#)ure /e and F#)ure /38. T$e 3uel 3lo6 4lot s$o6s a sudden dro4 #n 3uel 3lo6 r#)$t a3ter t$e

    start5 !ut t$en #t u#c=l #ncreases at nor(al rate.

    .- 9"e$ifi$ En'al"y for ea$' s"ee) a ea$' sage/ $al$ulae) using EE9 sof5are-

    At 11r4(5

    h1=285.8 kj

    kg, h2=781.6 kj

    kg, h3=912.7 kj

    kg, h4=704.3 kj /kg

    At J1 r4(5

    h1=285.2

    kj

    kg, h

    2=378.6

    kj

    kg,h

    3=844.8

    kj

    kg,h

    4=924.5 kj /kg

    At 1 r4(5

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    h1=284.7

    kj

    kg, h

    2=418.5

    kj

    kg, h

    3=948.3

    kj

    kg, h

    4=952.5 kj /kg

    4- 9"e$ifi$ 5or= )one by 'e $o("ressor 61#%8 an) urbine 6.#48!

    S#nce T/ ,alue #s less t$an T& ,alue unt#l a!out 1 r4(5 6e 6#ll onl calculate 6or= 3or

    1/K r4( as s$o6n #n Ta!le /.

    Co("ressor:

    W=(h2h1 ) W=418.5284.7W=133.8 kj/kg

    T$ere3ore t$e co(4ressor 6or= #s *//.K =@=).

    Turbine:

    Wout=(h3h4 ) Wout=952.5948.3Wout=4.2 kj /kg

    T$ere3ore t$e tur!#ne 6or= out4ut #s &.2 =@=)

    - 9"e$ifi$ energy a))e) by 'e fuel is/

    For 11 r4(5

    Q=h3h2=912.7 kj

    kg781.6 kj

    kg=131.1 kj

    kg

    For J1 r4(5

    Q=h

    3h

    2=844.8

    kj

    kg378.6

    kj

    kg=466.2

    kj

    kg

    For 1 r4(5

    Q=h

    3h

    2=948.3

    kj

    kg418.5

    kj

    kg=529.8

    kj

    kg

    ;- 9"e$ifi$ >or= an) Effi$ien$y of 'e $y$le

    S4ec#3#c 6or= done ! t$e ccle #s5

    Wnet=Wc+Wt=133.8 kj

    kg+4.2

    kj

    kg=138kj/kg

    E33#c#enc o3 t$e ccle 3or 1r4(5

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    n=Wt+WCQin

    =

    4.2kj

    kg+133.8

    kj

    kg

    529.8kj

    kg

    =0.2626 ,

    Thereforetheefficiency of the cycle is about26

    . T$rust S4ec#3#c Fuel Consu(4t#on 7TSFC85 6#t$ FuelA#r rat#o o3 **&. D#esel dens#t o3

    .K2l=)l

    At 11r4(5

    TSFC=(FuelFlowrate)

    Thrust =(10.36

    l

    hr0.82 kg /L

    3600 s

    45.26N )=5105kg /s

    At J1r4(5 5TSFC=

    (Fuel Flowrate )Thrust

    =(15.57

    l

    hr

    0.82kg /L

    3600 s

    56.32N )=6.3105kg /s

    At 1r4(5 5

    TSFC=(FuelFlowrate)

    Thrust =(21.37

    l

    hr0.82 kg /L

    3600 s

    84.25N )=6.6105kg /s

    Conclus#on

    In conclus#on5 t$#s e?4er#(ent 6as conducted to !etter understand t$e Braton ccle !

    o!ser,#n) and anal

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    Re3erences

    * La!orator 'anual &: Tur!oet En)#ne. 'ECE&&*U: Foss#l Fuel Ener) Con,ers#on.

    La!oroator FEAS. UOIT. Fall 2*&.

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