Whileat12milesthesustainingpowerisfiguredat230pounds,at24milesitisfourtimesasgreat,or920
pounds.
SupportingAreaofBirds.
Oneofthethingswhichallproducingaviatorsseektocopyisthemotivepowerofbirds,particularlyintheirrelationtotheareaofsupport.Closeinvestigationhasestablishedthefactthatthelargerthebirdthelessistherelativeareaofsupportrequiredtosecureagivenresult.Thisisshowninthefollowingtable:
SupportingWeightSurfaceHorseareaBirdinlbs.insq.feetpowerperlb.
Pigeon1.000.70.0120.7
WildGoose9.002.650.0260.2833
Buzzard5.005.030.0151.06
Condor17.009.850.0430.57
Sofarasknownthecondoristhelargestofmodernbirds.Ithasawingstretchof10feetfromtiptotip,asupportingareaofabout10squarefeet,andweighs17
pounds.It.iscapableofexertingperhaps1—30horsepower.
(Thesefiguresare,ofcourse,approximate.)
Comparingthecondorwiththebuzzardwithawingstretchof6feet,supportingareaof5squarefeet,andalittleover1—100horsepower,itmaybeseenthat,broadlyspeaking,thelargerthebirdthelesssurfacearea(relatively)
isneededforitssupportintheair.
ComparisonWithAeroplanes.
Ifwecomparethebirdfigureswiththosemadepossiblebythedevelopmentoftheaeroplaneitwillbereadilyseenthatmanhasmadeawonderfuladvanceinimitatingtheresultsproducedbynature.Herearethefigures:
SupportingWeightSurfaceHorseareaMachineinlbs.insq.feetpowerperlb.
Santos—Dumont350110.00300.314
Bleriot700150.00250.214
Antoinette1,200538.00500.448
Curtiss700258.00600.368
Wright[4]1,100538.00250.489
Farman1,200430.00500.358
Voisin1,200538.00500.448
[4]TheWrights’newmachineweighsonly900pounds.
Whiletheaveragesupportingsurfaceisinfavoroftheaeroplane,thisismorethanoverbalancedbythegreateramountofhorsepowerrequiredfortheweightlifted.Theaveragesupportingsurfaceinbirdsisaboutthree—quartersofasquarefootperpound.Intheaverageaeroplaneitisaboutone—halfsquarefootperpound.
Ontheotherhandtheaverageaeroplanehasaliftingcapacityof24poundsperhorsepower,whilethebuzzard,forinstance,lifts5poundswith15—100ofahorsepower.
IftheWrightmachine——whichhasaliftingpowerof50
poundsperhorsepower——shouldbealoneconsideredtheshowingwouldbemuchmorefavorabletotheaeroplane,butitwouldnotbeafaircomparison.
MoreSurface,LessPower.
Broadlyspeaking,thelargerthesupportingareathelesswillbethepowerrequired.Wright,bytheuseof538squarefeetofsupportingsurface,getsalongwithanengineof25horsepower.Curtiss,whousesonly258
squarefeetofsurface,findsanengineof50horsepowerisneeded.Otherthings,suchasframe,etc.,beingequal,itstandstoreasonthatareductionintheareaofsupportingsurfacewillcorrespondinglyreducetheweightofthemachine.ThuswehavetheCurtissmachinewithits258squarefeetofsurface,weighingonly600pounds(withoutoperator),butrequiringdoublethehorsepoweroftheWrightmachinewith538squarefeetofsurfaceandweighing1,100pounds.Thisdemonstratesinaforcefulwaythepropositionthatthelargerthesurfacethelesspowerwillbeneeded.
Butthereisalimit,onaccountofitsbulkandawkwardnessinhandling,beyondwhichthesurfaceareacannotbeenlarged.Otherwiseitmightbepossibletoequipandoperateaeroplanessatisfactorilywithenginesof15horsepower,orevenless.
TheFuelConsumptionProblem.
Fuelconsumptionisaprimefactorintheproductionofenginepower.Theveriestmechanicaltyroknowsinageneralwaythatthemorepowerissecuredthemorefuelmustbeconsumed,allowingthatthereisnodifferenceinthepower—producingqualitiesofthematerialused.Butfewofusunderstandjustwhattheratioofincreaseis,orhowitiscaused.Thispropositionisoneofkeeninterestinconnectionwithaviation.
Letusciteaproblemwhichwillillustratethepointquoted:Allowingthatittakesagivenamountofgasolenetopropelaflyingmachineagivendistance,halfthewaywiththewind,andhalfagainstit,thewindblowingatone—halfthespeedofthemachine,whatwillbetheincreaseinfuelconsumption?
IncreaseofThirtyPerCent.
Onthefaceofittherewouldseemtobenocallforanincreaseastheresistancemetwhengoingagainstthewindisapparentlyoffsetbythepropulsiveforceofthewindwhenthemachineistravellingwithit.This,however,iscalledfaultyreasoning.Theincreaseinfuelconsumption,asfiguredbyMr.F.W.Lanchester,oftheRoyalSocietyofArts,willbefully30percentovertheamountrequiredforasimilaroperationofthemachineinstillair.Ifthejourneyshouldbemadeatrightanglestothewindunderthesameconditionstheincreasewouldbe15percent.
InotherwordsMr.Lanchestermaintainsthattheworkdonebythemotorinmakingheadwayagainstthewindforacertaindistancecallsformoreengineenergy,andconsequentlymorefuelby30percent,thanissavedbythehelpingforceofthewindonthereturnjourney.
CHAPTERXIV.
ABOUTWINDCURRENTS,ETC.
Oneofthefirstdifficultieswhichthenovicewillencounteristheuncertaintyofthewindcurrents.Withalowvelocitythewind,somedistanceawayfromtheground,isordinarilysteady.Asthevelocityincreases,however,thewindgenerallybecomesgustyandfitfulinitsaction.This,itshouldberemembered,doesnotrefertothevelocityofthemachine,buttothatoftheairitself.
InthisconnectionMr.ArthurT.Atherholt,presidentoftheAeroClubofPennsylvania,inaddressingtheBostonSocietyofScientificResearch,said:
"ProbablythewhirlpoolsofNiagaracontainnomoreerraticcurrentsthanthestrataofairwhichisnowimmediatelyaboveus,afacthardtorealizeonaccountofitsinvisibility."
ChangesInWindCurrents.
WhileMr.Atherholt’sexperiencehasbeenmainlywithballoonsitisallthemorevaluableonthisaccount,astheballoonswereatthemercyofthewindandtheirvaryingdirectionsaffordedanindisputableguideastothechangingcourseoftheaircurrents.Inspeakingofthishesaid:
"Inthemanytripstaken,varyingindistancetraversedfromtwenty—fiveto900miles,itwasneverpossibleexceptinoneinstancetomaintainastraightcourse.
TheseuncertaincurrentsweremostnoticeableintheGordon—BennettracefromSt.Louisin1907.Ofthenineaerostatscompetinginthatevent,eightcoveredamoreorlessdirectcoursedueeastandsoutheast,whereasthewriter,withMajorHenryB.Hersey,firststartednorthwest,thennorth,northeast,east,eastbysouth,andwhenoverthecenterofLakeEriewereagainblownnorthwestnotwithstandingthatmorefavorablewindsweresoughtforataltitudesvaryingfrom100to3,000
meters,necessitatingafinishinCanadanearlynortheastofthestartingpoint.
"Thesenineballoons,makinglandingsextendingfromLakeOntario,Canada,toVirginia,allstartedfromonepointwithinthesamehour.
"ThesingleexceptiontotheserovingcurrentsoccurredonOctober21st,oflastyear(1909)when,startingfromPhiladelphia,thewindshiftedmorethaneightdegrees,thegreatestvariationbeingatthelowestaltitudes,yetatnotimewasaheightofoveramilereached.
"Throughouttheentiredaytheskywasovercast,withathermometervaryingfromfifty—sevendegreesat300
feettoforty—fourdegrees,Fahrenheitat5,000feet,atwhichaltitudethewindhadavelocityof43milesanhour,incloudsofacirro—cumulusnature,alandingfinallybeingmadenearTannersville,NewYork,intheCatskillmountains,afteravoyageoffiveandone—halfhours.
"Ihavenoknowledgeofarecordedtripofthisdistanceandduration,maintainedinpracticallyastraightlinefromstarttofinish."
Thiswinddisturbanceismorenoticeableandmoredifficulttocontendwithinaballoonthaninaflyingmachine,owingtothebulkandunwieldycharacteroftheformer.Atthesametimeitisnotconducivetopleasant,safeorsatisfactorysky—sailinginanaeroplane.
Thisisnotstatedwiththepurposeofdiscouragingaviation,butmerelythattheoperatormayknowwhattoexpectandbepreparedtomeetit.
Notonlydoesthewindchangeitshorizontalcourseabruptlyandwithoutnotice,butitalsoshiftsinaverticaldirection,onesecondblowingup,andanotherdown.Nomanhasasyetfathomedthewhyandwhereforeofthiserraticaction;itisonlyknownthatitexists.
Themoststablecurrentswillbefoundfrom50to100
feetfromtheearth,providedthewindisnotdivertedbysuchobjectsastrees,rocks,etc.Thatthereareequallystablecurrentshigherupistrue,buttheyaregenerallytobefoundatexcessivealtitudes.
HowaBirdMeetsCurrents.
Observeabirdinactiononawindydayandyouwillfinditcontinuallychangingthepositionofitswings.
Thisisdonetomeetthevaryinggustsandeddiesoftheairsothatsustentationmaybemaintainedandheadwaymade.Onesecondthebirdisbendingitswings,alteringtheangleofincidence;thenextitisliftingordepressingonewingatatime.Stillagainitwillextendonewingtipinadvanceoftheother,orbespreadingorfolding,loweringorraisingitstail.
Allthesemotionshaveameaning,apurpose.Theyassistthebirdinpreservingitsequilibrium.Withoutthemthebirdwouldbejustashelplessintheairasahumanbeingandcouldnotremainafloat.
Whenthewindisstill,orcomparativelyso,abird,havingsecuredthedesiredaltitudebyflightatanangle,maysailorsoarwithnowingactionbeyondanoccasionalstrokewhenitdesirestoadvance.But,inagusty,uncertainwinditmustuseitswingsoralightsomewhere.
TryingtoImitatetheBird.
Writingin_Fly_,Mr.WilliamE.Whitesays:
"Thebird’sflightsuggestsanumberofwaysinwhichtheequilibriumofamechanicalbirdmaybecontrolled.
Eachofthesemethodsofcontrolmaybeeffectedbyseveraldifferentformsofmechanism.
"Placingthetwowingsofanaeroplaneatanangleofthreetofivedegreestoeachotherisperhapstheoldestwayofsecuringlateralbalance.Thiswayreadilyoccurstoanyonewhowatchesaseagullsoaring.Thetheoryofthedihedralangleisthatwhenonewingisliftedbyagustofwind,theairisspilledfromunderit;
whiletheotherwing,beingcorrespondinglydepressed,presentsagreaterresistancetothegustandisliftedrestoringthebalance.Afixedangleofthreetofivedegrees,however,willonlybesufficientforverylightpuffsofwindandtomountthewingssothatthewholewingmaybemovedtochangethedihedralanglepresentsmechanicaldifficultieswhichwouldbebetteravoided.
"Theobjectionofmechanicalimpracticabilityappliestoanyplantopreservethebalancebyshiftingweightorballast.Thecenterofgravityshouldbelowerthanthecenterofthesupportingsurfaces,butcannotbemademuchlower.Itisacommonmistaketoassumethatcompletestabilitywillbesecuredbyhangingthecenterofgravityverylowontheprincipleoftheparachute.Anaeroplanedependsuponrapidhorizontalmotionforitssupport,andifthecenterofgravitybefarbelowthecenterofsupport,everychangeofspeedorwindpressurewillcausethemachinetoturnaboutitscenterofgravity,pitchingforwardandbackwarddangerously.
PreservingLongitudinalBalance.
"Thebirdsmaintainlongitudinal,orforeandaftbalance,byelevatingordepressingtheirtails.Whetherthisactionissecuredinanaeroplanebymeansofahorizontalrudderplacedintherear,orbydeflectingplanesplacedinfrontofthemainplanes,theprincipleisevidentlythesame.AhorizontalrudderplacedwelltotherearasintheAntoinette,BleriotorSantos—Dumontmonoplanes,willbeverymuchsaferandsteadierthanthedeflectingplanesinfront,asintheWrightorCurtissbiplanes,butnotsosensitiveorpromptinaction.
"Thenaturalforeandaftstabilityisverymuchstrengthenedbyplacingtheloadwellforward.Thecenterofgravitynearthefrontandatailorrudderstreamingtotherearsecuresstabilityasanarrowisbalancedbytheheadandfeathering.Theadoptionofthisprinciplemakesitalmostimpossiblefortheaeroplanetoturnover.
TheMatterofLateralBalance.
"Allsuccessfulaeroplanesthusfarhavemaintainedlateralbalancebytheprincipleofchangingtheangleofincidenceofthewings.
"Otherwaysofmaintainingthelateralbalance,suggestedbyobservationoftheflightofbirdsare——extendingthewingtipsandspillingtheairthroughthepinions;
or,whatisthesamething,varyingtheareaofthewingsattheirextremities.
"Extendingthewingtipsseemstobeasimpleandeffectivesolutionoftheproblem.Thetipsmaybemadetoswingoutwarduponaverticalaxisplacedatthefrontedgeofthemainplanes;ortheymaybehingedtotheendsofthemainplanesoastobeelevatedordepressedthroughsuitableconnectionsbytheaviator;ortheymaybesupportedfromahorizontalaxisparallelwiththeendsofthemainplanessothattheymayswingoutward,theaviatorcontrollingbothtipsthroughoneleversothatasonetipisextendedtheotherisretracted.
"Theelasticwingpinionsofabirdbendeasilybeforethewind,permittingtheguststoglanceoff,butpresentingalwaysanevenandefficientcurvaturetothesteadycurrentsoftheair."
HighWindsThreatenStability.
Toensureperfectstability,withoutcontrol,eitherhumanorautomatic,itisassertedthattheaeroplanemustmovefasterthanthewindisblowing.Solongasthewindisblowingattherateof30milesanhour,andthemachineistraveling40ormore,therewillbelittletroubleasregardsequilibriumsofaraswinddisturbancegoes,providedthewindblowsevenlyanddoesnotcomeingustsoreddyingcurrents.Butwhenconditionsarereversed——whenthemachinetravelsonly30milesanhourandthewindblowsattherateof50,lookoutforlossofequilibrium.
Oneofthemainreasonsforthisisthathighwindsarerarelysteady;theyseldomblowforanylengthoftimeatthesamespeed.Theyareusually"gusty,"thegustsbeingamomentarymovementatahigherspeed.
Tornadicgustsarealsoformedbythemeetingoftwoopposingcurrents,causingawhirlingmotion,whichmakesstabilityuncertain.Besides,itisnotunusualforwindofhighspeedtosuddenlychangeitsdirectionwithoutwarning.
TroubleWithVerticalColumns.
Verticalcurrents——columnsofascendingair——arefrequentlyencounteredinunexpectedplacesandhavemoreorlesstendency,accordingtotheirstrength,tomakeitdifficulttokeepthemachinewithinareasonabledistancefromtheground.
Theseverticalcurrentsaremostgenerallynoticeableinthevicinityofsteepcliffs,ordeepravines.Insuchinstancestheyareusuallyofconsiderablestrength,beingcausedbythedeflectionofstrongwindsblowingagainstthefaceofthecliffs.Thisdeflectionexertsabackpressurewhichisfeltquiteadistanceawayfromthepointoforigin,sothattheverticalcurrentexertsaninfluenceinforcingthemachineupwardlongbeforethecliffisreached.
CHAPTERXV.
THEELEMENTOFDANGER.
Thatthereisanelementofdangerinaviationisundeniable,butitisnowheresogreatasthepublicimagines.Menarekilledandinjuredintheoperationofflyingmachinesjustastheyarekilledandinjuredintheoperationofrailways.Consideringthecharacterofaviationthepercentageofcasualtiesissurprisinglysmall.
Thisisbecausetheresultsfollowingacollapseintheairareverymuchdifferentfromwhatmightbeimagined.
Insteadofdroppingtothegroundlikeabulletanaeroplane,underordinaryconditionswill,whenanythinggoeswrong,sailgentlydownwardlikeaparachute,particularlyiftheoperatoriscool—headedandnervyenoughtosomanipulatetheapparatusastopreserveitsequilibriumandkeepthemachineonanevenkeel.
TwoFieldsofSafety.
Atleastoneprominentaviatorhasdeclaredthattherearetwofieldsofsafety——oneclosetotheground,andtheotherwellupintheair.Inthefirst—namedthefallwillbeaslightonewithlittlechanceoftheoperatorbeingseriouslyhurt.Fromthefieldofhighaltitudethethedescentwillbegradual,asarule,theplanesofthemachineservingtobreaktheforceofthefall.Withacool—headedoperatorincontroltheaeroplanemaybeevenguidedatanangle(about1to8)initsdescentsoastotouchthegroundwithaglidingmotionandwithaminimumofimpact.
Suchanexperience,ofcourse,isfarfrompleasant,butitisbynomeanssodangerousasmightappear.
Thereismorerealdangerinfallingfromanelevationof75or100feetthanthereisfrom1,000feet,asintheformercasethereisnochanceforthemachinetoserveasaparachute——itscontactwiththegroundcomestooquickly.
LessoninRecentAccidents.
AmongthemorerecentfatalitiesinaviationarethedeathsofAntonioFernandezandLeonDelagrange.Theformerwasthrowntothegroundbyasuddenstoppageofhismotor,theentiremachineseemingtocollapse.
Itisevidenttherewereradicaldefects,notonlyinthemotor,butintheaeroplaneframeworkaswell.AtthetimeofthestoppageitisestimatedthatFernandezwasupabout1,500feet,butthemachinegotnoopportunitytoexertaparachuteeffect,asitbrokeupimmediately.
Thiswouldindicateafatalweaknessinthestructurewhich,underpropertesting,couldprobablyhavebeendetectedbeforeitwasusedinflight.
Itishardtosayit,butDelagrangeappearstohavebeenculpabletogreatdegreeinoverloadinghismachinewithamotorequipmentmuchheavierthanitwasdesignedtosustain.Hewas65feetupintheairwhenthecollapseoccurred,resultinginhisdeath.AsinthecaseofFernandezcommon—senseprecautionwoulddoubtlesshavepreventedthefatality.
AviationNotExtraHazardous.
Alltoldtherehavebeen,uptothetimeofthiswriting(April,1910),justfivefatalitiesinthehistoryofpower—
drivenaviation.Thisissurprisinglylowwhenthenatureoftheexperiments,andthefactthatmostoftheoperatorswerefarfromhavingextendedexperience,istakenintoconsideration.MenliketheWrights,Curtiss,Bleriot,Farman,Paulhanandothers,arenowexperts,buttherewasatime,anditwasnotlongago,whentheywereunskilled.Thatthey,withnumerousotherslesswidelyknown,shouldhavecomesafelythroughtheirmanyexperimentswouldseemtodisprovetheprevailingideathataviationisanextrahazardouspursuit.
Inthehandsofcareful,quick—witted,nervymenthesailingofanairshipshouldbenomorehazardousthanthesailingofayacht.Avesselcaptainwithcommonsensewillnotgotoseainastorm,ornavigateaweak,unseaworthycraft.Neithershouldanaviatorattempttosailwhenthewindishighandgusty,norwithamachinewhichhasnotbeenthoroughlytestedandfoundtobestrongandsafe.
SaferThanRailroading.
Statisticsshowthatsome12,000peoplearekilledand72,000injuredeveryyearontherailroadsoftheUnitedStates.Cometothinkitoveritissmallwonderthatthelistoffatalitiesissolarge.Trainsarerunathighspeeds,dashingovercrossingsatwhichcollisionsareliabletooccur,andoverbridgeswhichoftencollapseoraresweptawaybyfloods.Still,whilethenumberofcasualtiesislarge,theactualpercentageissmallconsideringtheimmensenumberofpeopleinvolved.
Itissoinaviation.Thenumberofcasualtiesisremarkablysmallincomparisonwiththenumberofflightsmade.Inthehandsofcompetentmenthesailingofanairshipshouldbe,andis,freerfromriskofaccidentthantherunningofarailwaytrain.Therearenorailstospreadorbreak,nobridgestocollapse,nocrossingsatwhichcollisionsmayoccur,nochanceforsomesleepyoroverworkedemployeetomisunderstandthedispatcher’sordersandcauseawreck.
TwoMainCausesofTrouble.
Thetwomaincausesoftroubleinanairshipleadingtodisastermaybeattributedtothestoppageofthemotor,andtheaviatorbecomingrattledsothathelosescontrolofhismachine.Moderningenuityisfastdevelopingmotorsthatalmostdailybecomemoreandmorereliable,andexperienceismakingaviatorsmoreandmoreself—confidentintheirabilitytoactwiselyandpromptlyincasesofemergency.Besidesthisasatisfactorysystemofautomaticcontrolisinafairwayofbeingperfected.
Occasionallyeventhemostexperiencedandcompetentofmeninallcallingsbecomecarelessandbyfoolishactioninvitedisaster.Thisistrueofaviatorsthesameasitisofrailroaders,menwhoworkindynamitemills,etc.Butinnearlyeveryinstancetheresponsibilityrestswiththeindividual;notwiththesystem.Therearesomemenunfittedbynatureforaviation,justasthereareothersunfittedtoberailwayengineers.
CHAPTERXVI.
RADICALCHANGESBEINGMADE.
Changes,manyofthemextremelyradicalintheirnature,arecontinuallybeingmadebyprominentaviators,andparticularlythosewhohavewonthegreatestamountofsuccess.Wonderfulastheresultshavebeenfewoftheaviatorsarereallysatisfied.Theirsuccesseshavemerelyspurredthemontonewendeavors,theultimateendbeingthedevelopmentofanabsolutelyperfectaircraft.
AmongthemenwhohavebeenthusexperimentingaretheWrightBrothers,wholastyear(1909)broughtoutacrafttotallydifferentasregardsproportionsandweightfromtheoneusedtheprecedingyear.Onemarkedresultwasagainofabout31/2milesanhourinspeed.
Dimensionsof1908Machine.
The1908modelaeroplanewas40by29feetoverall.
Thecarryingsurfaces,thatis,thetwoaerocurves,were40by6feet,havingaparabolicalcurveofoneintwelve.
Withabout70squarefeetofsurfaceintherudders,thetotalsurfacegivenwasabout550squarefeet.Theengine,whichistheinventionoftheWrightbrothers,weighed,approximately,200pounds,andgaveabout25
horsepowerat1,400revolutionsperminute.Thetotalweightoftheaeroplane,exclusiveofpassenger,butinclusiveofengine,wasabout1,150pounds.Thisresultshowedaliftofafractionover21/4poundstothesquarefootofcarryingsurface.Thespeeddesiredwas40
milesanhour,butthemachinewasfoundtomakeonlyascant39milesanhour.Theuprightstrutswereabout7/8—inchthick,theskids,21/2by11/4inchesthick.
Dimensionsof1909Machine.
The1909aeroplanewasbuiltprimarilyforgreaterspeed,andrelativelyheavier;tobelessatthemercyofthewind.Thisresultwasobtainedasfollows:Theaerocurves,orcarryingsurfaces,werereducedindimensionsfrom40by6feetto36by51/2feet,thecurveremainingthesame,oneintwelve.Theuprightstrutswerecutfromseven—eighthsinchtofive—eighthsinch,andtheskidsfromtwoandone—halfbyoneandone—quartertotwoandone—quarterbyoneandthree—eighthsinches.
Thisresultshowsthatthereweresome81squarefeetofcarryingsurfacemissingoverthatoflastyear’smodel.andsome25poundslossofweight.Relatively,though,the1909modelaeroplane,whileactually25
poundslighter,isreallysome150poundsheavierintheairthanthe1908model,owingtothelessersquarefeetofcarryingsurface.
SomeoftheResultsObtained.
Reducingthecarryingsurfacesfrom6to51/2feetgavetworesults——first,lesscarryingcapacity;and,second,lesshead—onresistance,owingtothefactthattheextentoftheparaboliccurveinthecarryingsurfaceswasshortened.The"head—on"resistanceistheretardancetheaeroplanemeetsinpassingthroughtheair,andiscountedinsquarefeet.Inthe1908modelthecurvebeingoneintwelveand6feetdeep,gave6inchesofhead—onresistance.Theplanebeing40feetspread,gave6inchesby40feet,or20squarefeetofhead—onresistance.Increasingthisfigurebyalikeamountforeachplane,andaddingapproximately10squarefeetforstruts,skidsandwiring,wehaveatotalofapproximately,50squarefeetofsurfacefor"head—on"resistance.
Inthe1909aeroplane,shorteningthecurve6inchesattheparabolicendofthecurvetookoff1inchofhead—onresistance.Shorteningthespreadoftheplanestookoffbetween3and4squarefeetofhead—onresistance.
Addtothisthetotalof7squarefeet,lesscurvesurfaceandabout1squarefoot,lesswireandwoodworkresistance,andwehaveagrandtotalof,approximately,12squarefeetofless"head—on"resistanceoverthe1908model.
ChangesinEngineAction.
Theengineusedin1909wasthesameoneusedin1908,thoughsomeminorchangesweremadeasimprovements;forinstance,amakeandbreaksparkwasused,andanine—tooth,insteadofaten—toothmagnetogear—wheelwasused.Thisincreasedtheenginerevolutionsperminutefrom1,200to1,400,andthepropellerrevolutionsperminutefrom350to371,givingapropellerthrustof,approximately,170footpoundsinsteadof153,aswashadlastyear.
MoreSpeedandSameCapacity.
Oneunsatisfactoryfeatureofthe1909modeloverthatof1908,apparently,wasthelackofinherentlateralstability.Thiswascausedbythelessersurfaceandlesserextentofcurvaturesattheportionsoftheaeroplanewhichwerewarped.ThisdefectdidnotshowsoplainlyafterMr.OrvilleWrighthadbecomefullyproficientinthehandlingofthenewmachine,andwithskillfulmanagement,the1909modelaeroplanewillbejustassafeandsecureastheotherthoughitwilltakealittlemorepracticetogetthatsamedegreeofskill.
Tosumup:Theaeroplaneusedin1909was25
poundslighter,butreallyabout150poundsheavierintheair,hadlesshead—onresistance,andgreaterpropellerthrust.Thespeedwasincreasedfromabout39
milesperhourto421/2milesperhour.Theliftingcapacityremainedaboutthesame,about450poundscapacitypassenger—weight,withthe1908machine.Inthisrespect,thelossofcarryingsurfacewascompensatedforbytheincreasedspeed.
Duringthefirstfewflightsitwasplainlydemonstratedthatitwouldneedthehighestskilltoproperlyhandletheaeroplane,asfirstoneendandthentheotherwoulddipandstriketheground,andeithertearthecanvasorslewtheaeroplanearoundandbreakaskid.
WrightsAdoptWheeledGears.
InstillanotherimportantrespecttheWrights,sofarastheoutputofoneoftheircompaniesgoes,havemadearadicalchange.AlltheaeroplanesturnedoutbytheDeutschWrightGesellschaft,accordingtotheGermanpublication,_Automobil—Welt_,willhereafterbeequippedwithwheeledrunninggearsandtails.Theplanofthisnewmachineisshownintheillustrationonpage145.
Thewheelsarethreeinnumber,andareattachedonetoeachofthetwoskids,justunderthefrontedgeoftheplanes,andoneforwardofthese,attachedtoacross—
member.Itisassertedthatwiththesewheelstheteachingofpurchaserstooperatethemachinesismuchsimplified,asthebeginnerscanmakeshortflightsontheirownaccountwithoutusingthestartingderrick.
ThisisabigconcessionfortheWrightstomake,astheyhavehithertoadheredstoutlytotheskidgear.
WhileitistruetheydonotcontroltheGermancompanyproducingtheiraeroplanes,yetthenatureoftheirconnectionwiththeenterpriseissuchthatitmaybetakenforgrantednoradicalchangesinconstructionwouldbemadewithouttheirapprovalandconsent.
OnlyThreeDangerousRivals.
Officialtrialswiththe1909modelsmashedmanyrecordsandleavetheWrightbrotherswithonlythreedangerousrivalsinthefield,andwithbasicpatentswhichcoverthecurve,warpandwing—tipdevicesfoundonalltheothermakesofaeroplanes.ThesethreerivalsaretheCurtissandVoisinbiplanetypeandtheBleriotmonoplanepattern.
TheBleriotmonoplaneisprobablythemostdangerousrival,asthismakeofmachinehasarecordof54
milesperhour,hascrossedtheEnglishchannel,andhasliftedtwopassengersbesidestheoperator.Thelatesttypeofthismachineonlyweighs771.61poundscomplete,withoutpassengers,andwillliftatotalpassengerweightof462.97pounds,whichisaliftof5.21poundstothesquarefoot.ThisisabetterresultthanthosepublishedbytheWrightbrothers,thebestnotedbeing4.25poundspersquarefoot.
OtherAviatorsatWork.
TheWrights,however,arenotaloneintheireffortstopromotetheefficiencyoftheflyingmachine.Othercompetentinventiveaviators,notablyCurtiss,Voisin,BleriotandFarman,arecloseafterthem.TheWrights,asstated,haveamarkedadvantageinthepossessionofpatentscoveringsurfaceplanedeviceswhichhavethusfarbeenfoundindispensableinflyingmachineconstruction.
Numerouslawsuitsgrowingoutofallegedinfringementsofthesepatentshavebeenstarted,andothersarethreatened.Whateffecttheseactionswillhaveindeterringaviatorsingeneralfromproceedingwiththeirexperimentsremainstobeseen.
Inthemeantimethefourmennamed——Curtiss,Voisin,BleriotandFarman——aregoingaheadregardlessofconsequences,andtheinventivegeniusofeachissostrongthatitisreasonabletoexpectsomeremarkabledevelopmentsinthenearfuture.
SmallestofFlyingMachines.
ToSantosDumontmustbegiventhecreditofproducingthesmallestpracticalflyingmachineyetconstructed.
True,hehasdonenothingremarkablewithitinthelineofspeed,buthehasdemonstratedthefactthatalargesupportingsurfaceisnotanessentialfeature.
Thismachineisnamed"LaDemoiselle."Itisamonoplaneofthedihedraltype,withamainplaneoneachsideofthecenter.Thesemainplanesareof18footspread,andnearly61/2feetindepth,givingapproximately115feetofsurfacearea.Thetotalweightis242pounds,whichis358poundslessthananyothermachinewhichhasbeensuccessfullyused.Thetotaldepthfromfronttorearis26feet.
Theframeworkisofbamboo,strengthenedandheldtautwithwireguys.
HaveOneRuleinMind.
Inthisstruggleformasteryinflyingmachineefficiencyallthecontestantskeeponeruleinmind,andthisis:
"Thecarryingcapacityofanaeroplaneisgovernedbytheperipheralcurveofitscarryingsurfaces,plusthespeed;andthespeedisgovernedbythethrustofthepropellers,lessthe’head—on’resistance."
Theirideasastothepropermeansofapproachingthepropositionmay,andundoubtedlyare,atvariance,buttheoneruleinsolvingtheproblemofobtainingthegreatestcarryingcapacitycombinedwiththegreatestspeed,obtainsinallinstances.
CHAPTERXVII.
SOMEOFTHENEWDESIGNS.
Spurredonbythesuccessattainedbythemoreexperiencedandbetterknownaviatorsnumerousinventorsoflesserfamearealmostdailyproducingpracticalflyingmachinesvaryingradicallyinconstructionfromthosenowingeneraluse.
OneofthesecomparativelynewdesignsistheVanAndenbiplane,madebyFrankVanAndenofIslip,LongIsland,amemberoftheNewYorkAeronauticSociety.Whilehismachineiswhollyexperimental,manysuccessfulshortflightsweremadewithitlastfall(1909).Oneflight,madeOctober19th,1909,isofparticularinterestasshowingthepracticabilityofanautomaticstabilizingdeviceinstalledbytheinventor.Themachinewascaughtinasuddenseveregustofwindandkeeledover,butalmostimmediatelyrighteditself,thusdemonstratinginamostsatisfactorymannerthevalueofonenewattachment.
FeaturesofVanAndenModel.
Insizethesurfacesofthemainbiplaneare26feetinspread,and4feetindepthfromfronttorear.Theupperandlowerplanesare4feetapart.Silkolenecoatedwithvarnishisusedforthecoverings.Ribs(spruce)arecurvedoneinchtothefoot,thedeepestpartofthecurve(4inches)beingonefootbackfromthefrontedgeofthehorizontalbeam.Struts(alsoofspruce,asisalltheframework)areellipticalinshape.
Themainbeamsareinthreesections,nearlyhalfroundinform,andjoinedbymetalsleeves.
Thereisatwo—surfacehorizontalrudder,2x2x4feet,infront.Thisispivotedatitslateralcenter8feetfromthefrontedgeofthemainplanes.Intherearisanothertwo—surfacehorizontalrudder2x2x21/2feet,pivotedinthesamemannerasthefrontone,15feetfromtherearedgesofthemainplanes.
Hingedtotherearcentralstrutoftherearrudderisaverticalrudder2feethighby3feetinlength.
TheMethodofControl.
Intheoperationoftheserudders——bothfrontandrear——andtheelevationanddepressionofthemainplanes,theCurtisssystemisemployed.Pushingthesteering—
wheelpostoutwarddepressesthefrontedgesoftheplanes,andbringsthemachinedownward;pullingthesteering—wheelpostinwardelevatesthefrontedgesoftheplanesandcausesthemachinetoascend.
Turningthesteeringwheelitselftotherightswingsthetailruddertotheleft,andthemachine,obeyingthislikeaboat,turnsinthesamedirectionasthewheelisturned.Bylikecauseturningthewheeltotheleftturnsthemachinetotheleft.
AutomaticControlofWings.
Therearetwowingtips,eachof6feetspread(length)
and2feetfromfronttorear.Thesearehingedhalfwaybetweenthemainsurfacestothetwooutermostrearstruts.Cablesrunfromthesetoanautomaticdeviceworkingwithpowerfromtheengine,whichautomaticallyoperatesthetipswiththetiltingofthemachine.Normallythewingtipsareheldhorizontalbystiffspringsintroducedinthecablesoutsideofthedevice.
ItwasthesuccessfulworkingofthisdevicewhichrightedtheVanAndencraftwhenitwasoverturnedinthesquallofOctober19th,1909.PrevioustothatoccurrenceMr.VanAndenhadlookeduponthedeviceaspurelyexperimental,andhadadmittedthathehadgraveuncertaintyastohowitwouldoperateintimeofemergency.Heisnowquotedasbeingthoroughlysatisfiedwithitspracticability.ItisthisautomaticdevicewhichgivestheVanAndenmachineatleastonedistinctivelynewfeature.
WhileonthissubjectitwillnotbeamisstoaddthatMr.Curtissdoesnotlookkindlyonautomaticcontrol.
"Iwouldrathertrusttomyownactionthanthatofamachine,"hesays.ThisisundoubtedlygoodlogicsofarasMr.Curtissisconcerned,butallaviatorsarenotsocool—headedandresourceful.
MotivePowerofVanAnden.
A50—horsepower"H—F"watercooledmotordrivesalaminatedwoodpropeller6feetindiameter,witha17
degreepitchattheextremities,increasingtowardthehub.Therearendofthemotorisabout6inchesbackfromthereartransversebeamandtheengineshaftisinadirectlinewiththeaxesofthetwohorizontalrudders.
AnR.I.V.ballbearingcarriestheshaftatthispoint.Flying,themotorturnsatabout800revolutionsperminute,delivering180poundspull.Atestofthemotorrunningat1,200showedapullof250poundsonthescales.
StillAnotherNewAeroplane.
AnothernewaeroplaneisthatproducedbyA.M.
Herring(anold—timer)andW.S.Burgess,underthenameoftheHerring—Burgess.Thisisalsoequippedwithanautomaticstabilitydeviceformaintainingthebalancetransversely.Thecurvatureoftheplanesisalsolaidoutonnewlines.Thatthisnewplaniseffectiveisevidencedbythefactthatthemachinehasbeenelevatedtoanaltitudeof40feetbyusingone—halfthepowerofthe30—horsepowermotor.
Thesystemofrudderandelevationcontrolisverysimple.Theaviatorsitsinfrontofthelowerplane,andextendinghisarms,graspstwosupportswhichextenddowndiagonallyinfront.Ontheundersideofthesesupportsjustbeneathhisfingersarethecontrolswhichoperatetheverticalrudder,intherear.Thus,ifhewishestoturntotheright,hepressesthecontrolunderthefingersofhisrighthand;iftotheleft,thatunderthefingersofhislefthand.Theelevatingrudderisoperatedbytheaviator’srightfoot,thecontrolbeingplacedonafoot—rest.
MotorIsExtremelyLight.
Nottheleastnotablefeatureofthecraftisitsmotor.
Althoughdeveloping,underload,30—horsepower,orthatofanordinaryautomobile,itweighs,complete,hardly100pounds.Havingoccasiontomoveitalittledistanceforinspection,Mr.Burgesspickeditupandwalkedoffwithit——cylinders,pistons,crankcaseandall,eventhemagneto,beingattached.Therearenotmany30—
horsepowerengineswhichcanbesohandled.Everythingaboutitisreducedtoitslowesttermsofsimplicity,andhence,ofweight.Asinglecamshaftoperatesnotonlyalloftheinletandexhaustvalves,butthemagnetoandgearwaterpump,aswell.Themotorisplaceddirectlybehindtheoperator,andthepropellerisdirectlymountedonthecrankshaft.
Thisweightoflessthan100pounds,itmustberemembered,isnotforthemotoralone;itincludestheentirepowerplantequipment.
The"thrust"ofthepropellerisalsoextraordinary,beingbetween250and260pounds.Theforceofthewinddisplacementisstrongenoughtoknockdownagood—sizedboyasoneyoungsterascertainedwhenhegotbehindthepropellerasitwasbeingtested.Hewasnotonlyknockeddownbutdrivenforsomedistanceawayfromthemachine.Thepropellerhasfourbladeswhicharebutlittlewiderthanalath.
MachineBuiltbyStudents.
StudentsattheUniversityofPennsylvania,headedbyLaurenceJ.Lesh,aprotegeofOctaveChanute,haveconstructedapracticalaeroplaneofordinarymaximumsize,inwhichisincorporatedmanynewideas.Themostuniqueoftheseistobefoundinthesteeringgear,andtheprovisionmadefortheaccommodationofapupilwhiletakinglessonsunderanexperiencedaviator.
Immediatelybackoftheaviatorisanextraseatandanextrasteeringwheelwhichworksintandemstylewiththefrontwheel.Bythisarrangementabeginnermaybeeasilyandquicklytaughttohaveperfectcontrolofthemachine.Thesetandemwheelsarealsohandyforpassengerswhomaywishtooperatethecarindependentlyofoneanother,itbeingunderstood,ofcourse,thattherewillbenoconflictofaction.
FrameSizeandEnginePower.
Theframehas36feetspreadandmeasures35feetfromthefrontedgetotheendofthetailintherear.ItisequippedwithtworearpropellersoperatedbyaRamsey8—cylindermotorof50horsepower,placedhorizontallyacrossthelowerplane,withthecrankshaftrunningclearthroughtheengine.
The"PennsylvaniaI"isthefirsttwo—propellerbiplanechainlesscar,thisschemehavingbeenadoptedinordertoavoidthecrossingofchains.ThelateralcontrolisbyanewinventionbyOctaveChanuteandLaurenceJ.
Lesh,forwhichLeshisnowapplyingforapatent.ThedevicewasworkedoutbeforetheWrightbrothers’suitwasbegun,andissaidtobesuperiortotheWrightwarpingortheCurtissailerons.Thelandingdeviceisalsonewindesign.Thisaeroplanewillweighabout1,500pounds,andwillcarryfuelforaflightof150miles,anditisexpectedtoattainaspeedofatleast45milesanhour.
Thereareothers,lotsofthem,toonumerousinfacttoadmitofmentioninabookofthissize.
CHAPTERXVIII.
DEMANDFORFLYINGMACHINES.
Asacommercialpropositionthemanufactureandsaleofmotor—equippedaeroplanesismakingmuchmorerapidadvancethanatfirstobtainedinthesimilarhandlingoftheautomobile.Great,andevenphenomenal,aswasthecommercialdevelopmentofthemotorcar,thatoftheflyingmachineisevengreater.Thisisastartlingstatement,butitisfullywarrantedbythefacts.
Itisbarelymorethanayearago(1909)thatattentionwasseriouslyattractedtothemotor—equippedaeroplaneasavehiclepossibleofmanipulationbyothersthanprofessionalaviators.Uptothattimesuchactualflightsasweremadewerealmostexclusivelywiththesolepurposeofdemonstratingthepracticabilityofthemachine,andthemeritsoftheideasastoshape,enginepower,etc.,ofthevariousproducers.
ResultsofBleriot’sDaring.
ItwasnotuntilBleriotflewacrossthestraitsofDoveronJuly25th,1909,thatthegeneralpublicawoketoafullrealizationofthefactthatitwaspossibleforothersthanprofessionalaviatorstoindulgeinaviation.
Bleriot’sfeatwasacceptedasproofthatatlastanabsolutelynewmeansofsport,pleasureandresearch,hadbeenpracticallydeveloped,andwaswithinthereachofallwhohadtheinclination,nerveandfinancialmeanstoadoptit.
Fromthiseventmaybedatedthebirthofthemodernflyingmachineintotheworldofbusiness.Theautomobilewastakenupbythegeneralpublicfromtheverystartbecauseitwasapropositioncomparativelyeasyofdemonstration.Therewasnothingmysteriousoruncannyinthefactthatawheeledvehiclecouldbepropelledonsolid,substantialroadsbymeansofenginepower.Andyetittook(comparativelyspeaking)alongtimetoreallypopularizethemotorcar.
WonderfulResultsinaYear.
Menoflargefinancialmeansengagedinthemanufactureofautomobiles,andexpendedfortunesinattractingpublicattentiontothemthroughthemediumofadvertisements,speedandroadcontests,etc.Bythesemeansamammothbusinesshasbeenbuiltup,butbringingthisbusinesstoitspresentproportionsrequiredyearsofpatientindustryandindomitablepluck.
Atthiswriting,lessthanayearfromthedaywhenBleriotcrossedthechannel,theactualsalesofflyingmachinesoutnumbertheactualsalesofautomobilesinthefirstyearoftheircommercialdevelopment.Thismayappearincredible,butitisafactasstatisticswillshow.
Inthisconnectionweshouldtakeintoconsiderationthefactthatuptoayearagotherewasnoseriousintentionofputtingflyingmachinesonthemarket;nopreparationshadbeenmadetoproducethemonacommercialscale;nomoneyhadbeenexpendedinadvertisementswithaviewtosellingthem.
SomeoftheActualResults.
Todayflyingmachinesarebeingproducedonacommercialbasis,andthereisabigdemandforthem.Thepeoplemakingthemareovercrowdedwithorders.Someoftheproducersarealreadymakingarrangementstoenlargetheirplantsandadvertisetheirproductforsalethesameasisbeingdonewithautomobiles,whileanumberofflyingmachinemotormakersarealreadypromotingthesaleoftheirwaresinthisway.
HereareafewactualfiguresofflyingmachinesalesmadebythemoreprominentproducerssinceJuly25th,1909.
SantosDumont,90machines;Bleriot,200;Farman,130;Clemenceau—Wright,80;Voisin,100;Antoinette,100.Manyoftheseordershavebeenfilledbydeliveryofthemachines,andinotherstheconstructionworkisunderway.
Theforegoingareallofforeignmake.InthiscountryCurtissandtheWrightsareengagedinsimilarwork,butnoactualfiguresoftheiroutputareobtainable.
LargerPlantsAreNecessary.
Andthissituationexistsdespitethefactthatnoneoftheproducersarereallyequippedwithadequateplantsforturningouttheirmachinesonamodern,business—
likebasis.Thedemandwassosuddenandunexpectedthatitfoundthempoorlypreparedtomeetit.This,however,isnowbeingremediedbytheerectionofspecialplants,theenlargementofothers,andtheintroductionofnewmachineryandotherlabor—savingconveniences.
Companies,withlargecapitalization,toengageintheexclusiveproductionofairshipsarebeingorganizedinmanypartsoftheworld.Onenotableinstanceofthisnatureisworthquotingasillustrativeofthemannerinwhichtheproductionofflyingmachinesisbeingcommercialized.ThisistheformationatFrankfort,Germany,oftheFlugmaschineWright,G.m.b.H.,withacapitalof$119,000,theKrupps,ofEssen,beinginterested.
PricesatWhichMachinesSell.
Thiswonderfuldemandfromthepublichascomenotwithstandingthefactthatthemachines,owingtolackoffacilitiesforwholesaleproduction,arefarfrombeingcheap.Suchdefinitequotationsasaremadeareonthefollowingbasis:
SantosDumont——Listprice$1,000,butowingtotherushofordersagentsarereadilygettingfrom$1,300to$1,500.Thisisthesmallestmachinemade.
Bleriot——Listprice$2,500.Thisisforthecross—
channeltype,withAnzanimotor.
Antoinette——Listpricefrom$4,000to$5,000,accordingtosize.
Wright——Listprice$5,600.
Curtiss——Listprice$5,000.
Thereis,however,nostabilityinpricesaspurchasersarealmostinvariablyreadytopayaconsiderablepremiumtofacilitatedelivery.
Themotoristhemostexpensivepartoftheflyingmachine.Motorpricesrangefrom$500to$2,000,thislatteramountbeingaskedfortheCurtissengine.
SystematicInstructionofAmateurs.
Inadditiontotheproductionofflyingmachinesmanyoftheexperiencedaviatorsaremakingabusinessoftheinstructionofamateurs.CurtissandtheWrightsinthiscountryhaveanumberofpupils,ashavealsotheprominentforeigners.Schoolsofinstructionarebeingopenedinvariouspartsoftheworld,notaloneasprivatemoney—makingventures,butinconnectionwithpubliceducationalinstitutions.OneoftheselatteristobefoundattheUniversityofBarcelona,Spain.
Theflyingmachineagent,themanwhohandlesthemachinesonacommission,hasalsobecomeaknownquantity,andwillsoonbeasnumerousashisbrotheroftheautomobile.Thesign"JohnBird,agentforSkimmer’sFlyingMachine,"isnolongeracuriosity.
第4章