LYSHOLM Radial Flow Turbine

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LYSHOLM Radial Flow Turbine ( lysholm-radial-flow-turbine )

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10 75 ner,itmay bedischargedwithoutsubstan tialpressuredrop,and?owfromthepoint ofdischargefromthebladesystemisas sistedduetothekineticenergyimpartedto themotive?uidinthedirectionofitsde 80 2 1,910,945 oftheturbine,sothatsteamleavingsaid aforceactingtodischargesteamfrom‘the bladeringisdirectedsoastohaveasmooth turbine. Obviously,thevalueoftheperi ?owfromitspointofdischargefromthe pheralortangentialvelocity‘representedby bladeringtotheoutlet16ofthevolutecas thevectoritvarieswithvariationsinsize ing. Theoutlet16ispreferablyarranged oftheangle7,thesizeofwhichanglemay 70 tangentially of the casing as shown, and it vary with different types of turbines and willbeapparentthat,ifdesired,steamcan mayalsovaryinliketurbines. Preferably, betakenofffromthecasingatmorethan thisanglehasavalueofatleast25°. one pointby providing additional outlets. By discharging the motive ?uid from the The exhaust conduit 17, with which the blade system in the above described man outlet 16 communicates, is preferably sup portedbymeans,suchasisindicatedat18 and19,inamannerpermittingmovement oftheexhaustconduittocompensateforex 15 pansionduetotemperaturedifferencesand thelike. In accordance with the present invention, . sired ?ow. - From theforegoing,itwillbeevidentthat theshapeandarrangementoftheblades7’ themotive?uidwill,inaccordancewiththe inthelastoroutermostbladeringissuch presentinvention,haveapressureinthedis 20 thatthemotive?uidisdischargedfromthese chargeconduit17substantiallythesameas 85 bladesinadirectionhavingacomponentin thatinthechamber8,whichis,inturn,sub the direction of discharge ?ow through the stantially the same as the pressure at the point of discharge from the last blade row. The manner in which the desired direc By arrangingthe.bladesinthelastblade 25 tion of discharge flow from the blade sys row in the above described manner, some 90 temisaccomplishedismoreclearlyillus lossmaybeincurred,ascomparedwitha tratedinthediagramofFig.3. Inthis liketurbineinwhichthedischargefromthe ?gure, the character of the discharge ?ow last’blade row is in radial direction, due to . fromthelastbladeringofaturbineofthe thegreaterdischargevelocityofthemotive 30 priorartisshowninbrokenlines,andthe ?uidwhenitisdischargedwithanappre directionofthedischarge‘?owinaccordance ciableperipheralortangentialcomponent, with the present invention is shown in full but this loss is considerably less than the lines. Reference character a designates‘ a pressure drop loss in the discharge casing ' bladearrangementfortheouterbladering whenthemotive?uidisdischargedfrom‘t-he 35whichisinaccordancewiththepriorart.lastbladerowintheusualradialdirection.'100 lVith this arrangement, the outlet angle a It is obvious that, the present invention issuchthat,withaperipheralvelocityrep maybeembodied,notonlyintheformof resentedbythevectoruandarelativedis apparatushereinshownbywayofillustra 'tion,but mayalso be embodied in other spe “,chargevelocityrepresentedbythevector'v,ci?cforms‘ofturbinesinwhichthesingle 105 the resultant or a solute discharge velocity willberepresentedbythevector0,whichis volute‘shapedexhaustchamberandoutlet, directedradiallyofthebladesystem. illustratedherein,arereplacedb aplu 45 which the motive ?uid is exhausted in this of motive uid discharged from the blade 110 manner,thebladem1isarranged,inaccordsystem. ' ' - chamber 8. In order to avoid the losses through un desirable factors inherent in a turbine in, and dischar e a portion of the total amount ancewiththepresentinvention,sothatthe outlet angle (1provides a relative discharge ‘velocityrepresentedbythevector01having 50 a value greater than the value of the vector '0, so that the resultant vector 01, represent ingtheabsolutedischarge,isdisposedatan angle )1 with respect to a radius vector. Ifthevector'c1isresolvedintoitsradial 55 and peripheral components, it will be seen WhatIclaimis: ' 1. In a radial ?ow elastic fluid turbine, a blade system for expanding motive ?uid comprising-a rotor carrying a plurality of 115 blade rings including a blade ring consti tutingtheoutermostradial?owbladering of the turbine, and a casing providing a volute shaped chamber having an outlet, ‘120 said outermost blade ring discharging mo ralityofequivalents,eachofwhic receive that,inaccordance.withthepresentinven tive?uidtosaidchamberandcomprisinga ' tion, there is provided a radial discharge pluralit of blades each arranged to simul velocityrepresentedbyaandaperipheral taneousydischargemotive?uidtherefrom 1discharevelocityrepresentedbythevec withanabsolutevelocityhavin aperiph 125 '60 torh,telatterbeingparallel,butopposite in direction, to the velocity vector u I Thisvelocityvectorhrepresentsthe'di~ ‘motionandvalueofthedischargeenergy ofthemotive?uidinthedirection-ofthe eralortangential'componentov?ow,said ?ow’being inthe directionof the ?ow‘of mo tive?uid-insaidchambertowardtheoutlet' thereof. I 2.Ina.radial?owelastic‘?uidturbine,a, outletoftheturbinecasing,andrepresents bladesystemforexpandingmotive?uid

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LYSHOLM Radial Flow Turbine

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