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AGE RADIAL FLOW TURBINE

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AGE RADIAL FLOW TURBINE ( age-radial-flow-turbine )

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to outlets such as 2|. There will be a slight amount of leakage of the set being closed at one end and the other set being closed at the other end, the said surface of the other of said members having a cooperat ing set of link channels closed at both ends 2,417,6007 producing at each crossing point an impulse thrust in thedirection of rotation. The ?uid between inlet 18 and a crossing point such as 31,. and between crossing points 32 and 33, in the rotor channels produces reaction thrust additive totheimpulsethrustsatthecrossingpoints. array 28. .The broken line 3--3 in Fig. 2 and Fig. 3 show one of the various paths for ?uid from inlet 18 15 of direct communication with the other set, one ‘To take care of the expansion‘ of ?uid as it approaches the outlet 21, the various rotor and stator channels may increase in number or size or both as the outlet 2| is approached. Fig. 2 10 sh0ws'12channelsineachofthearraysHand ingarotormemberandastatormemberhaving 21, 16 channels in array 23, and 24 channels in fluid due to the fact that rotor 19 is ?oating on anextremelythin?lmofthe?uidandsuchleak age will, in general, do useful work on the rotor 20 crossing and opening into each of said separated l3 because if such leakage as indicated ?nds its way into a stator groove, such as 21 or 28, all elastic ?uid, including the leakage, expands in that groove, performing work on each of the rotor grooves, 22, 23 as they communicate therewith. The composite channel provided partly by the separated rotor grooves, 22, 23, and the remainder by the separated stator grooves, 21,‘ 28, effects a substantially continuous, uninterrupted expan sion of elastic ?uid such as steam. The ?uid pressure on the under side of rotor l9 may serve to ?oat the rotor and the thrust imposed on it by its work whereby the rotor 2 sets at points which progress radially as said rotor member rotates to provide ?uid communi cation from one of said two spaced sets to the other through said link channels at the crossing points of said link channels with said separated sets of channels. 2. A machine for ?uids and having two rela tively rotatable coaxial adjacent members hav ing opposed surfaces in close face to face rela , tion, the said surface of one of said members having inner and outer spaced arrays of chan-. nels, and the said adjacent opposed surface of the other of said members having a,cooperating array of link channels, said link channels of one serves as a thrust bearing. Instead of having all of the arrays of channel-s 35 of said members intersecting the channels of curved, one or more of such arrays may be straight, to cheapen the cost of manufacture as it is cheaper to machine a straight groove than a curved groove. In the modi?cation shown in Fig. 4, the stator channels 36, 31 are straight 40 at their outer ends and communicating with said whiletherotorchannels34,35arecurve-d. The inner rotor link channels 34 are closed at their opposite ends while the outer rotor channels 35 are closed at their inner ends and open at their outer ends to exhaust into the outlets l5. The channels 34 and 35 are convex in the direction of rotation, which is counterclockwise, and cooper ating therewith is an inner array 35 and an outer array 31 of stator channels, both of which are straight, that is, their central line is straight 50 of channels at the progressive crossing points whereasthesidesthereofmaytaperasindicated. thereof. _ The channels 36 are closed at their outer ends and their inner ends open into inlet 38. The channels 31 are link channels closed at both ends. 3. A machine according to claim 2 wherein the channels of said outer array are closed at their outer ends, said other member having an outer Thechannels36arehereshownastangentialto. arrayofchannelsclosedattheirinnerendsand the inlet 38, although these channels may be radial. Thearray36crossesapluralityofchan nels in the array 34; each channel in array 34 crosses a plurality of channels in the array 31; crossing at points progressing radially along outer portion of said last mentioned outer array of channels. 4. A multi-stage turbine comprising relatively and each channel 31 is crossed, at times, by a 60 rotatable coaxial stator and rotor members hav plurality of the outlet channels 35. The opera tion is substantially as described in connection with Fig. 2, the ?uid in inlet 38 passing to the various stator channels 36 to the points where they cross the rotor channels 34, thence, along channels 34 to the points where the latter cross the stator channels 31 and along them to the points where they cross the outlet channels 35 and, thence, out the channels 35 to the outlets 15. ing adjacent surfaces in close face to face rela tion, said surface of one of said members having . a set of link channels closed at both ends, the said surface of said other member having (a) an inner array of channels closed at their outer ends and crossing inner portions of said link channels‘ and (b) an outer array of channels closed at their inner ends and crossing outer‘ portions of said link channels, said crossings Inthemodi?cationshowninFig.5allchan 70progressingradiallyassaidrotorrotates. nels are illustrated as being straight, that is their median line is straight, the stator channels being shown in dotted lines, the rotor channels in full lines,asinother?gures. Oneofthepathsfor ?uid is shown by the broken lines 6-6 and by 75 angularly related radially spaced arrays of dead Figure 6, wherein fluid in inlet 33 passes into a statorgroove40toacrossingpoint41thenalong a rotor groove 42 to a crossing point 43 then along a stator groove 44 to a, crossing point 45then along a rotor groove 46 to one of the outlets I5 showninFig.1. Theoperationissubstantially the same as that described in connection with Fig. 2. I claim: . 1. A multi-stage radial ?ow machine compris opposed surfaces in close face to face relation, the said surface of one of said members having two spaced sets of channels each set being out both arrays of the other member at points progressing radially during relative rotation of said members, a ?uid passage, the channels of the inner one of said spaced arrays being closed ?uidpassageattheirinnerends,thechannelsof the outer spaced array being closed at their inner ends, and having ?uid passages at their outer ends, and said link channels being closed at both ends, whereby the path for ?uid between said ?rst mentioned ?uid passage and the outer ends of said outer array of channels shifts from said inner array of channels to said link channels and from said link channels to said outer array 5. A machine comprising a rotor member and a stator member having surface in close face to face relation, an inlet and an outlet therefor, said rotor and stator surfaces having more than two

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