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Section4Lecture3Try:17.Flaretubesinagasturbineshouldbecheckedfor:
1.Thecombustionchamberofagasturbine:a.Corrosion
b.Distortion
a.Increasesthepressureofthecompressedairc.Properairflow
b.Burnsfuelwithexcessaird.Properignition
c.Islocatedbetweentheloadturbineandthe
compressorturbine8.Gasturbineunitsareused:
d.Isalwaysofthemultipleburnertype
1.Forelectricalgeneration
2.Agasturbinecombustionchamberrequires:2.Whereenergyisproducedforprocess
plants
a.Acoolingwaterjacketontheinnercanister3.Wherewastegasesfromtheprocessmay
b.Avacuumbreakerbeusedtodrive
c.Asafetypressurereliefdevicethegasturbine
d.Ahighvoltageignitionplugforinitial4.Wherehighthermalefficiencyisrequired
ignition
a.1,2,3
3.Theregeneratorofagasturbinecycleisa:b.1,3,4
c.2,3,4
a.Secondcombustord.1,2,3,4
b.Heatexchanger
c.Vesselusedtotransferheatfromtheexhaust9.Thedisadvantagesofaclosedcyclegasturbine
gastosystemare:
theworkingfluidbeforecompressionoccurs
d.Increasethepressureoftheworkingfluidin1.Morecoolingwaterisrequired
thesystem2.Morecomponentsareneeded
3.Higherinitialcost
4.Thegasturbinesystemis:4.Morespaceisrequired
a.Idealforlargegeneratorsystemsa.1,2,3
b.Idealtobeusedoverasteamturbineb.2,3,4
c.Idealtobeusedforunmannedandremotec.1,3,4
locationsd.1,2,3,4
d.Idealforallapplicationsofaprocessplant
10.Thedisadvantagesofagasturbineinclude:
5.GasturbinesoperatingontheBraytoncyclehavean
efficiencyofapproximately:1.Fuelcostsarehigh
2.Highlevelsofnoisepollutionareproduced
a.30-35%3.Lowthermalefficiency
b.35-40%4.Requiresmanyauxiliaries
c.40-45%
d.45-50%a.1,2,3
b.1,3,4
6.Inagasturbinethevolumeofairandexhaustgasesc.2,3,4
flowingthroughthecompressord.1,2,3,4
andturbine:
Section4Lecture3Try:2
a.Changeswithatmosphericpressure
b.Isalwaysthesame1.Thelowinstallationcostofagasturbineisdueto:
c.Changeswithambienttemperature
d.Changeswithloadconditiona.Cheapmaterialsinbladeconstruction
b.Lessauxiliaryequipmentneededb.1,2,4
c.Nofuelpumprequiredc.1,3,4
d.Smallfuelstoragerequiredd.1,2,3,4
2.Theregeneratorofagasturbinecycleisa:
7.Axialcompressorsusedongasturbineshavethe
a.Secondcombustorfollowingadvantages:
b.Heatexchanger
c.Vesselusedtotransferheatfromtheexhaust1.Small
gasto2.Moreefficient
theworkingfluidbeforecompressionoccurs3.Cheaper
d.Increasethepressureoftheworkingfluidin4.Runathighspeeds
thesystem
a.1,2,3
3.GasturbinesoperatingontheBraytoncyclehaveanb.1,2,4
efficiencyofapproximately:c.1,3,4
d.1,2,3,4
a.30-35%
b.35-40%8.Advantagesofgasturbinesare:
c.40-45%
d.45-50%1.Lowamountofcoolingwaterrequired
2.Lowerinitialcost
4.Wherefuelcontainingsodiumorvanadiumisbeing3.Quickstarttime
usedforagasturbine,waterwashingwill4.Highthermalefficiency
berequiredfollowedbytheadditionofchemicalsto
thefuel:a.1,2,3
b.1,3,4
a.Toreduceairpollutionc.2,3,4
b.Toreducecorrosionofexhaustductsd.1,2,3,4
c.Toreducethetemperatureoftheexhaust
gases9.Noisepollutionfromagasturbineunitcanbe
d.Toreducedepositsontheturbinebladesreducedby:
5.Gasturbinesmaybestartedremotelyby:1.Inletsilencers
2.Acousticinsulation
1.Telephone3.Byusingaxialaircompressors
2.Timedelayrelays4.Exhaustsilencers
3.Mechanicallink
4.Radiolinka.1,2
b.1,4
a.1,2c.2,3
b.1,3d.2,4
c.1,4
d.2,410.Thedisadvantagesofaclosedcyclegasturbine
systemare:
6.Gasturbinesareusedinindustryasprimemoversfor:
1.Morecoolingwaterisrequired
1.Portablegenerators2.Morecomponentsareneeded
2.Firepumps3.Higherinitialcost
3.Aircompressors4.Morespaceisrequired
4.Emergencyequipment
a.1,2,3
a.1,2,3b.2,3,4
c.1,3,4d.Isapplicabletothecompressor,turbine,
d.1,2,3,4combustorandstartingmotor
6.Amajoroverhaulisperformedonagasturbine:
a.Onanannualbasis
b.Whenperformancefallsoff
Section4Lecture3Try:3c.Duringperiodsoflightloads
d.Accordingtomanufacturer'sspecifications
1.Thecombustionchamberofagasturbine:
7.Gasturbinesareusedinlargepowerplantsto
a.Increasesthepressureofthecompressedairprovidealmost
b.Bumsfuelwithexcessairinstantemergencypowerfor
c.Islocatedbetweentheloadturbineandthe(twowords).
compressorturbine
d.Isalwaysofthemultipleburnertype
8.Advantagesofgasturbinesare:
2.Agasturbineattemptstocombine:
1.Lowamountofcoolingwaterrequired
a.Thesimplicityofthesteamturbineandthe2.Lowerinitialcost
internalcombustionengine3.Quickstarttime
b.Theadvantagesofthesteamturbineandthe4.Highthermalefficiency
internalcombustionengine
c.Theadvantagesofthesteamturbineandthea.1,2,3
simplicityoftheinternalb.1,3,4
combustionenginec.2,3,4
d.Thesimplicityofthesteamturbineandthed.1,2,3,4
advantagesoftheinternal
combustionengine9.Inagasturbinecycleusinganintercoolerthe
followingadvantagesareobtained:
3.Theregeneratorofagasturbinecyclewillrecover
aboutpercentoftheexhaustheat.1.Thespecificvolumeoftheairisreduced
2.Thecoolerairrecoversmoreheatfromthe
a.60regenerator
b.653.Thetemperatureofthesecondstage
c.70compressorwillbe
d.75increasedthusincreasingthermal
efficiency
4.Inagasturbinethevolumeofairandexhaustgases4.Moreoftheturbinepowercanbeavailable
flowingthroughthecompressorfortheoutputload
andturbine:
a.1,2,3
a.Changeswithatmosphericpressureb.1,2,4
b.Isalwaysthesamec.1,3,4
c.Changeswithambienttemperatured.2,3,4
d.Changeswithloadcondition
10.Inthetotalenergyarrangementagasturbine
5.Ingeneral,servicingcarriedoutonagasturbine:exhaustsitsfluegastoa/an:
a.Willonlybeapplicabletothecombustionunit1.Wasteheatboiler
b.Isdoneonasemi-annualbasis2.Regenerator
c.Isdoneonanannualbasis3.Exhaustheatboiler
4.Spaceheater
b.1,3,4
a.1,2c.2,3,4
b.1,3d.1,2,3,4
c.2,36.Thetotalenergyarrangementofagasturbinesystem
d.3,4isusedto:
1.Provideelectricity
2.Coolwaterfordrinking
3.Provideairconditioning
4.Provideheating
a.1,2,3
Section4Lecture3Try:4b.1,2,4
1.Thegasturbinecycleisalsoknownas:c.1,3,4
d.1,2,3,4
a.Thecurrentcycle
b.TheJoulecycle7.Aradialcompressorusedwithagasturbinehasthe
c.TheWhittlecyclefollowingadvantages:
d.TheBuchicycle
1.Simple
2.Thefreepistongasgeneratoronagasturbinecycle2.Cheap
willtaketheplaceof:3.Strong
4.Shortinlength
a.Theturbineandcombustor
b.Thecompressorandcombustora.1,2,3
c.Thecompressorandturbineb.1,3,4
d.Thecompressorandregeneratorc.2,3,4
d.1,2,3,4
3.GasturbinesoperatingontheBraytoncyclehavean8.Advantagesofgasturbinesare:
efficiencyofapproximately:
1.Lowamountofcoolingwaterrequired
a.30-35%2.Lowerinitialcost
b.35-40%3.Quickstarttime
c.40-45%4.Highthermalefficiency
d.45-50%
a.1,2,3
4.Flaretubesinagasturbineshouldbecheckedfor:b.1,3,4
c.2,3,4
a.Corrosiond.1,2,3,4
b.Distortion
c.Properairflow9.Foragasturbinetorunefficientlyyoumusthave:
d.Properignition
1.Cleanlubricatingoil
5.Gasturbineunitsareused:2.Cleangaspath
3.Cleanturbineblades
1.Forelectricalgeneration4.Cleanandgoodqualityfuel
2.Whereenergyisproducedforprocess
plantsa.1,2,3
3.Wherewastegasesfromtheprocessmayb.1,2,4
beusedtodrivethegasturbinec.2,3,4
4.Wherehighthermalefficiencyisrequiredd.1,2,3,4
a.1,2,3
10.Inagasturbinecycleusinganintercoolerthec.Thecompressorandturbine
followingadvantagesareobtained:d.Thecompressorandregenerator
1.Thespecificvolumeoftheairisreduced5.Portablegasturbinesareusedfor:
2.Thecoolerairrecoversmoreheatfromthe
regeneratora.Reducingatmosphericpressure
3.Thetemperatureofthesecondstageb.Totalenergyunits
compressorwillbec.Largeaircompressors
increasedthusincreasingthermald.Unmannedandremoteareas
efficiency
4.Moreoftheturbinepowercanbeavailable6.Thetermtotalenergyarrangement,asappliedtogas
fortheoutputloadturbinecycles,means:
a.1,2,3a.Alltheenergyisusedinthesystem
b.1,2,4b.Theturbineprovidesallthenecessaryforms
c.1,3,4ofenergy
d.2,3,4c.Thesystemisoftheclosedtypeandtherefore
Section4Lecture3Try:5lessenergyislost
d.Thehotgasesarepassedthroughaboilerto
1.Agasturbineattemptstocombine:producesteam
a.Thesimplicityofthesteamturbineandthe7.Whenagasturbineisrunningandaconditioncalled
internalcombustionenginesurgingoccursthismeans:
b.Theadvantagesofthesteamturbineandthe
internalcombustionenginea.Thespeedoftheturbineisfluctuating
c.Theadvantagesofthesteamturbineandtheb.Theturbineisrunningtoofast
simplicityoftheinternalc.Airgetschokedinthehighpressureendofthe
combustionenginecompressor
d.Thesimplicityofthesteamturbineandthed.Thefuelsupplyisfluctuating
advantagesoftheinternal
combustionengine8.Amajoroverhaulisperformedonagasturbine:
2.Thecombustionchamberofagasturbine:a.Onanannualbasis
b.Whenperformancefallsoff
a.Increasesthepressureofthecompressedairc.Duringperiodsoflightloads
b.Burnsfuelwithexcessaird.Accordingtomanufacturer'sspecifications
c.Islocatedbetweentheloadturbineandthe
compressorturbine9.Noisepollutionfromagasturbineunitcanbe
d.Isalwaysofthemultipleburnertypereducedby:
3.Theregeneratorofagasturbinecyclewillrecover1.Inletsilencers
aboutpercentoftheexhaustheat.2.Acousticinsulation
3.Byusingaxialaircompressors
60
4.Exhaustsilencers
a.b65
c7012
75a.14
d.
b.c23
24
4.Thefreepistongasgeneratoronagasturbinecycled.
willtaketheplaceof:
10.Advantagesofgasturbinesare:
a.Theturbineandcombustor
b.Thecompressorandcombustor1.Lowamountofcoolingwaterrequired
2.Lowerinitialcostd.Unmannedandremoteareas
3.Quickstarttime
4.Highthermalefficiency5.Thegasturbinesystemis:
a.1,2,3a.Idealforlargegeneratorsystems
b.1,3,4b.Idealtobeusedoverasteamturbine
c.2,3,4c.Idealtobeusedforunmannedandremote
d.1,2,3,4locations
d.Idealforallapplicationsofaprocessplant
6.Whenagasturbineisrunningandaconditioncalled
surgingoccursthismeans:
a.Thespeedoftheturbineisfluctuating
b.Theturbineisrunningtoofast
c.Airgetschokedinthehighpressureendofthe
compressor
d.Thefuelsupplyisfluctuating
7.Thebladesofanaxialcompressoronagasturbine
Section4Lecture3Try:6aremadefrom:
1.Thecompressoronagasturbine:1.Ferritesteel
2.Stainlesssteel
a.Canbedrivenbytheloadturbine3.Aluminumalloy
b.Isalwaysoftheaxialtype4.Titaniumalloy
c.Isalwaysamulti-stagecompressor
d.Canbeofthereciprocatingtypea.1,2
b.1,3
2.Theregeneratorofagasturbinecycleisa:c.2,3
d.2,4
a.Secondcombustor
b.Heatexchanger8.Inordertohavesafeandefficientoperationofagas
c.Vesselusedtotransferheatfromtheexhaustturbinetheoperatorrequires
gastoaknowledgeof:
theworkingfluidbeforecompressionoccurs
d.Increasethepressureoftheworkingfluidin1.Thelubricatingoilsystem
thesystem2.Thefueloilsystem
3.Howtocontroltheairinlettemperature
3.Thepurposeofaregeneratorinagasturbineis:4.Thefirefightingsystems
a.Tocleantheexhaustgasesa.1,2,3
b.Toimprovetheefficiencyoftheturbineb.1,2,4
c.Todecreasethetemperatureinthecombustionc.1,3,4
chamberd.2,3,4
d.Toraisetheairtemperaturebefore
compression9.Noisepollutionfromagasturbineunitcanbe
reducedby:
4.Portablegasturbinesareusedfor:
1.Inletsilencers
a.Reducingatmosphericpressure2.Acousticinsulation
b.Totalenergyunits3.Byusingaxialaircompressors
c.Largeaircompressors4.Exhaustsilencers
d.Toraisetheairtemperaturebefore
a.1,2compression
b.1,4
c.2,34.GasturbinesoperatingontheBraytoncyclehavean
d.2,4efficiencyofapproximately:
10.Thedisadvantagesofagasturbineinclude:a.30-35%
b.35-40%
1.Fuelcostsarehighc.40-45%
2.Highlevelsofnoisepollutionareproducedd.45-50%
3.Lowthermalefficiency
4.Requiresmanyauxiliaries5.Gasturbinesarefarsuperiortoothertypesof
enginesintheir:
a.1,2,3
b.1,3,4a.Fuelconsumption
c.2,3,4b.Efficiency
d.1,2,3,4c.Powerpermassratio
d.Lubricatingoilconsumption
6.Gasturbinesareusedinlargepowerplantsto
providealmost
instantemergencypowerfor
______________(twowords).
Section4Lecture3Try:77.Gasturbinesareusedinindustryasprimemoversfor:
1.Agasturbineattemptstocombine:1.Portablegenerators
2.Firepumps
a.Thesimplicityofthesteamturbineandthe3.Aircompressors
internalcombustionengine4.Emergencyequipment
b.Theadvantagesofthesteamturbineandthe
internalcombustionenginea.1,2,3
c.Theadvantagesofthesteamturbineandtheb.1,2,4
simplicityoftheinternalc.1,3,4
combustionengined.1,2,3,4
d.Thesimplicityofthesteamturbineandthe
advantagesoftheinternal8.Theadvantagesofadualshaftgasturbine
combustionenginearrangementare:
2.Agasturbineaircompressorwithanintercooler:1.Greaterflexibility
2.Itischeaper
a.Hastheintercoolerlocatedafterthe3.Smallerstartingmotormaybeused
compressor4.Highpressuresandtemperaturesmaybe
b.Increasesthevolumeofairbeingsuppliedobtained
c.Allowsmoreoutputattheturbine
d.Usedonlywithaxialtypecompressorsa.1,2
b.1,3
3.Thepurposeofaregeneratorinagasturbineis:c.2,3
d.2,4
a.Tocleantheexhaustgases
b.Toimprovetheefficiencyoftheturbine9.Noisepollutionfromagasturbineunitcanbe
c.Todecreasethetemperatureinthecombustionreducedby:
chamber
1.Inletsilencers
2.Acousticinsulationa.Idealforlargegeneratorsystems
3.Byusingaxialaircompressorsb.Idealtobeusedoverasteamturbine
4.Exhaustsilencersc.Idealtobeusedforunmannedandremote
locations
a.1,2d.Idealforallapplicationsofaprocessplant
b.1,4
c.2,35.Whenagasturbineisrunningandaconditioncalled
d.2,4surgingoccursthismeans:
10.Thelubricatingoilsystemofagasturbinemustbea.Thespeedoftheturbineisfluctuating
checkedfor:b.Theturbineisrunningtoofast
c.Airgetschokedinthehighpressureendofthe
1.Metalparticlescompressor
2.Watercontaminationd.Thefuelsupplyisfluctuating
3.Dirtcontamination
4.Leaks6.Inagasturbinethevolumeofairandexhaustgases
flowingthroughthecompressor
a.1,2,4andtur
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