US2813708A - Devices to improve flow pattern and heat transfer in heat exchange zones of brick-lined furnaces - Google Patents

Description

Nov. 19, 1957 K. P. H. FREY 2,313,703

DEVICES TO IMPROVE FLOW PATTERN AND HEAT TRANSFER IN HEAT EXCHANGE ZONES OF BRICK-LINED FURNACES Filed Oct. 8, 1951 5 Sheets-Sheet 1 FIG. 4 FIG. 5 FIG. 6

INVENTOR 45 KURT PAUL HERMANN FREY BY f UM ATTORNEYS 2,813,708 TRANSFER Nov. 19, 1957 K. P. H. FREY DEVICES TO IMPROVE FLOW PATTERN AND HEAT IN HEAT EXCHANGE ZONES OF BRICK-LINEDFURNACES 5 Sheets-Sheet 2 Filed Oct. 8,

FIG" /0 FIG. .9

Y WE mm 3 v W. N M m MM F IR E H l.- m \P 2T MW 6 IK. F m H H 4 l I l a a I 6 F I! O 1F 7 ATTORNEYS Nov. 19, 1957 K P H. FREY 2,813,708

DEVICES TO IMPRO VE FLSW PATTERN AND HEAT TRANSFER IN HEAT EXCHANGE ZONES OF BRICK-LINED FURNACES Filed Oct. 8, 1951 5 Sheets-Sheet 4 2 2628V NVENTOR 62 KURT PAUL HERMANN REY wm zm, LQL -x 260 260 BY P 259 I 259 ATTORNEYS Nov. 19, 1957 K. P. H. FREY 2,813,708

DEVICES TO IMPROVE FLOW PATTERN AND HEAT TRANSFER IN HEAT EXCHANGE ZONES OF BRICK-LINED FURNACES Filed Oct. 8, 1951 5vSheets-Sheet 5 FIG. 26

' INVENTOR" KURT PAUL HERMANN FREY PWL ATTORNEY S United States Patent DEVICES TO IMPROVE FLOW PATTERN AND HEAT TRANSFER IN HEAT EXCHANGE ZONES 0F BRICK-LINED FURNACES Kurt 'Paul Hermann Frey, Goggingen, near Augsburg, Germany Application Dctober. 8, 1951, Serial No..250,362

1 Claim. (Cl. 263-51) In recuperative and also in regenerative heat transmitters or heat exchangers .of refractory brick, in industrial furnaces of refractory brick such as mufile furnaces,

enameling furnaces, open-hearth furnaces, coke furnaces or similar equipment, heat is transmitted to the-brick by encountered in most, if not all, of the conventional furnaces. The conventional brick-linedfurnaces and heat exchangers may have good flow patterns under one set of operating conditions butfrequently this set of conditions is not that which is observed in actual practice and separationof the flow with concomitant poor heat transfer and the development of hot spots occurs in actual practice to materially detract from the efificiency of the furnace and heat exchange operation.

In recuperative and regenerative heat exchangers and heattransmitters and in industrial furnaces thereresults, due to a sharp deviation of the real flow development from the assumed flow development, extremely irregular heat transitions which at many points are on the one hand extremely high and on the other hand at some points almost lacking. By means of forced convection and as a result thereof heat stresses and local overheating or insufficient heating of the brick material frequentlyresults and the consequence of this, in turn, is loss in the utilization of the thermal properties of the brick, with the-additional tendency of the brick to crack due touneven heating which introduces further hazards to'the safety of operation. The flame length is frequently impossible to control due to operations whichoccur. in the flow pattern. A further consequence is the greatly re- .duced stability of the brick material, the premature dedead-water areas in and after sudden bends or enlargements in the cross section and the accumulation of'rsla'g deposits atsuchpoints; such deposits or accumulations cause a continuing weight increase at the affected brick walls or vaults with overheating and harmfulcontrol spots developed.

The present invention provides devices for the improvement of the flow pattern in the refractorybrick-lined channels of coke furnaces, muifle furnaces and .the like 2 wherein .the combustion gases and air are subjected to changes in direction due to the connection of the inlet andoutIeLchannels Within .the furnace so as to provide .a,poorl-flowpatternin which there are formed separation .zones .in the cross section ofthe fluid stream, static and .eddy.areas-.immediatelyadjacent themainflow of the gasesand air throughthe channels, the improvement by the devices of thepresent invention. comprising providing deflecting rneansat the boundaryof the zone of separa* tion to.deflect..the gases. into thestatic zone, said deflectingmeans comprisinga staggered series of curvedvane .gui'di-ngsurfaces, the. curved vanes being eachadisposed on-.the.suction.side of thesubsequent vane, the resultant curvature of the series .beinggreater than the curvature dfanysingle vane, the amount .ofoverlap of the values withres-pect to each other being sufficienttoprovide a :substa-ntialjet directed velocity vector in adirectionsu'b .stant-ially tangential to the resultant-curvature ofv the series, .the resultant curvature of the series being defined by. the curve which joins the intersections of the.cords of. the vanes, theangle ofjattackof the first vanes beingnegative with respect .to-the .directionof the velocity vectorot the instantgas stream.

An.object.of 'thepresent invention is to overcome the drawbacks .of L prior known .devices and the invention ,provides deflecting means ..at .the boundary of .thezone of separation in the cross section of the channels-between the inlet and outlet openings of brick-lined furnaces, heat exchangers and the like .to deflect the gases into the static zouebetween the zone of separation and the brick-lined channel Wall, said deflecting means comprising a stag- .geredsseries of curved .vane guidingv surfaces, the curved vanes being each disposedon the=suction sideofthesubsequent vane, theresultant curvature of the series being greater than the curvature of any single vane, the amount of overlap ofthe vanes with respect to each other being sufficient to provide a substantial jet directed velocity vector .in .a 'direction substantially tangential .tothe resultant .curvatureof the series, .the resultant curvature of theseries being defined by the curve which joins the intersections of ,thelcordsof the vanes, the angle of. attack ofthe first vanes being'negative with respect to the .direction of ,the velocity vector ofthe instant-gas stream. I By means of the invention .pressu-re losses are reduced, whereby in. tur-n the current costs of operationeandalso the production costslbecome smaller; forexample, with "the same output the equipments may be givensmaller dimensions, :henceprovidinga better utilization of space .and at the same time more favorable possibilities .for more efficient dust-removal chambers and slag-deposit chambers in the equipments.

A further .objectof 'the invention is to make it possible ,to control the heat transition as toquantity and space by varying the heat transmitted byconvection, and by reducing the heat transmitted by radiation.

Further objects-of the invention will be apparent from the following detailed discussion .of preferred embodiments of the invention taken together with the accompanying drawings, in which:

Figs. 1 to 12are partial views of apparatus embodying "the features of the present invention and relating to a streamline principle;

"Figs. 13rto 20are views=sirnilar to' Figs. l-to 12 but embodying a resistance principle; and

'Figs.21*to. 33 are'partial views showing -the use of comb'inationsof means in varying devices and equipment.

The: invention locates deflecting means at the boundary -.of the -zoneof. separation for the improvement of *the flow, particularly for the eliminationoflarge detachments -ofthe.flowaandeforttheimprovement of the velocity disntribution of the flow through-one or more interiorcrosssections and also serves for the mutual adaptation of the velocity distributions through one or more cross-sections traversed alternately in different directions or in neighboring interior cross-sections traversed simultaneously by different media, for example, in crossing flow or in transverse flow.

Flow-influencing means which act according to a streamline principle are for example: flow-influencing stream-lined shaping of the inner channel walls at bends and enlargements in the flow path; roundings of the interior, for example with radii of curvature which are about equal to or larger than the width of the channel section ahead of the rounded part; gradual constrictions, for example in combustion chambers with the narrowest point at about the level of the starting end of the flame, for example the fuel gas outlet of the nozzle, and with gentle enlargement following in the direction of flow. To provide for streamlined shaping of the channels,

arched brick construction as is conventionally used may be employed. In one of the embodiments of the invention, the deflecting vanes may be arranged in a diagonal arrangement in the crest of the bend of a channel with such a radius of curvature of the inner bend crest and such inner radii of curvature of the partialchannels defined on opposite sides of the vanes and between the walls of the brick-lined channels so that the radius of curvature is about equal to or greater than the inlet width of the partial channel. guide bodies or walls in two or more partial diffusers may have a total enlargement angle of the partial diffuser up to degrees, and the guide surfaces of the vanes may be staggered in head-sail fashion.

Flow-influencing means acting according to a resistance principle, according to the invention, are for example: stationary grids, multiple grids, perforated plates, slotted plates and the like; closely spaced straight grids with rounded, tapered, or blunt shape of the head; straight grids, angular or rounded grids preferably in diagonal arrangement; grids of equal inlet and outlet width of the grid channels with close gn'd division; arched or rounded grids of unequal inlet and outlet widths of the grid channels; movable grids; displaceable grids, multiple grids,

The division of a large enlargement by perforated plates, slotted plates and the like; slotted. or-

perforated sliding bricks with equal or unequal subdivision of breaks such as slots or holes; grids fixed or displaceable as a unit with regulable passage cross-section, for example with shutter-like or' slidably arranged grid elements; grids with directing wall effect; subdivision of a big enlargement into partial diffusers with total enlargement angle of the individual diffuser above 10 degrees; and deflecting walls.

Combined flow-influencing means according to the invention are, for example: means connected in series in the direction of flow; means according to the resistance principle as for example grids and guide surfaces or walls; means according to the streamline principle with subsequent means according to the resistance principle as for example guide surfaces and grids or as for example guide walls and grids; combinations of grids with grids lying in another plane and/ or with guide surfaces and/ or with arcs for example in and at the housing of a regulating valve; functional spatial coordination or combination of means according to the streamline principle; guide bodies or guide walls with or without breaks and with or without arching in spatial flow-functional coordination with guide surfaces, that is, preferably guide surfaces staggered in head-sail fashion; combination of several means according to the resistance principle; guide bodies or guide walls in functional spatial coordination or combination with grids; combination of several means according to the streamline principle, e. g. parallel or series arrangement of several sets of guide surfaces staggered in head-sail fashion or of a set of guide surfaces staggered in head-sail fashion and of a set of defle blades or vice versa, etc.

31, for the purpose of substantially disturbance-free de- The drawings disclose examples of the foregoing means or individual elements according to the invention.

Figures 1 and 2 show a deflection of the flow arriving according to the arrow 1 by 180 degrees, theflow channel 2 being formed by the outer and inner masonry 3 and 4. At the deflection point the inner masonry 4 has acircular rounding 5. In the inlet thechannel width 6 is about equal to thechannel width 7 of the outlet, while thechannel width 8 at the deflection point is at least nine tenths (Fig. 1) and at most one and a half times (Fig. 2) the dimensions of thechannel width 6 or 7. With such proportions or ratios a sufficiently disturbance-free deflection is obtained in such a structural element, applicable to diversified equipment at different points and in diverse combinations especially when the radius of curvature of therounding 5 is about equal to thechannel width 7. Moreover, recuperator channels may be arranged in the inner masonry 4, about perpendicular to the plane of the drawing.

Fig. 3 shows a deflection of degrees. The inflow according to arrow 9 is deflected in thechannel 12 formed by the inner and outer masonry 1t and 11. Thecrest zone 13 slopes and the inside cross-section is subdivided at that point into twopartial channels 15 and 16 by the provision of aguide body 14, such as a shaped brick. Theflow body 14 can be variously designed, but is preferably flat inside and arched outside. This element, too, which is also suitable also for deflection angles other than 90 degrees, is applicable, like all of the elements later to be shown, in diverse equipment and combinations.

With it, flow detachments are not avoided completely but are much smaller than without such aguide body 14.

In Fig. 4 the deflection of thechannel 19 formed by inner andouter masonry 17 and 18 is provided with rounded parts at theinside crest 20 and at theoutside crest 21. It is particularly suitable when theflow 22 arrives with a velocity uniformly distributed over the cross-section of the inflow, for example according to the velocity distribution diagram 23. The deflection point has installed in it aflow body 24, the rounding of which adapts itself to thecrest curvatures 20, 21 and preferably lies closer to theinside crest 20. Such aflow body 24 may be built up ofindividual arch bricks 25 or the like. In the direction offlow 22, the distance between theinside crest 20 and theflow body 24, may advantageously decrease.

In a deflection according to Fig. 5, in which again inher andouter masonry 26 and 27 forms thechannel 28, adeflection grid 32 is provided between the rounded inside crest 30 and the preferably rounded outside crest flection of theflow 29. For each partial channel the radius of the inside are should, for disturbance-free inflow 29, be about equal to the inlet width of the partial channel. In the case of greatlydisturbed inflow 29, however, this radius should be much greater than said channel width.

Fig. 6 shows for theinflowing flow 33, an abrupt enlargement of the cross-section according tosurfaces 34 and 35 of the masonry. For the uniform spreading and possibly also for the deflection of the flow there are provided here guidesurfaces 36 of brickwork, staggered in head-sail fashion, in the zone of the crest of thewalls 34, 35. Such a design may be supplemented by mirrorsymmetry about theaxes 37 or 38.

While for the elements according to Figs. 1 to 5 the flow development is independent of the direction of flow, in Fig. 6 and various of the subsequent figures, the flow development is more favorable in the direction shown in the drawing than in the opposite direction, so that in such arrangements for alternating direction of flow more care should be taken in selecting the arrangement. Inpractice, however, examples according to Fig. 6 and to be preferred for alternating direction of flow because these arrangementsare especially-effective in one direction and" because this 'direction of flow is then decisive for' 'the purpose of heat transmission.

In. Fig. 7 there is an abrupt unilateral "enlargement, formed by themasonry walls 39,40, of the inflow'crosssection. At the transition point 41there is provided a set of guidedsurfaces 42 staggered in head s'aihfashion, and consisting of sheetmetal or cast metal. "Inthis a'rrangement the diffusorproblem occurring'in flow'direction 43 and thenozzle problemoccurringimflow direction 44 are solved in such a waythat 'n'o'essentialdis- 'turbances of the flow occur and alsoffor'exatn'plein the case of poorly distributedinflow 43, a 'goodtoi'un'iform velocity distribution exists in'the enlarged cross-section. This arrangement can be amplified by"r'nirror syrnirietry about the masonry to form a symmetrical element, naturally omitting thismasonry'wall 40. In the case of a non-uniform flow' pattern upstream'tosaidguiding "surfaces'the non-uniformity is satisfactorilyelimin'ated even when'the guiding'surfaces ofthe vanes'are'loc'ated atan entrance of the diffuser.

The unsymmetrical abrupt enlargement of theflow cross-section formed in Fig. 8bythe masonry 45 and 46 is controlled by the arrangement of two sets of guide surfaces 47, 48 staggered in head-sail fashion, which solve thedifluser problemforflow direction 49 and also still su'fliciently satisfactorily the nozzle problem "forcounterflow direction 50. If such a'difluser'is highly-asymmetrical, more partial guide. surfaces are advantageously selected on the side of the bigger enlargement than on the side of the smaller enlargement. The arrangement-according toFig. 8 may also be'sym'metri'cal, basing it 'on'the uppe'r or on the lower half of the illustration.

Fig. 9 shows a main conduit51 with alateral inflow cross-section 52 and anadditional lateralinflow crosssection 53. For the proper introduction of the "flow-54 there is provided, at theinflow cross-section 52, a set of guide surfaces 55 in spatially corresponding arrangement and staggered in head-sail fashion and which'set protrudes for example into theinside cross-section 56 of theconduit 51. In addition, adisplaceable throttle grid 57 may be arranged in the inflow cross s'ection. In theinflow cross-section 53of'the conduit 58 attached laterally or perpendicularly, a set of guidesurfacesi6 0 staggered in head-sail fashion is arranged, for 'the .p'roper introduction of theinflow 59, in'suchawaytha't itdoes not protrude into the inside cross-section "56, for only immaterially so. This arrangement gives a deflection and introduction of theflows 54, 59 into 'the'conduit 51 disturbance-free'to a very large extent. "With counter- I flow 61 in theconduit 51, 'the guide surface set 60 does not disturb theflow 61 at all and-theguide surfaceset 55 causes little disturbance of flow and'loss oftpressure, but in an immaterial and therefore harmless measure because no appreciable response acts upstreamly to the heat exchange zone so that the flowpattern is notaflected at that location.

Fig. 10 shows aninflow channel 63 formed. ofmasonry 62, the insidecroSs-section of which enlarges to amuch larger inside cross-section 64, with deflection about at a rightangle. Such a construction renders the'flow, problem especially di'flicult, above all when -theinflow 65 arrives with irregularvelocity distribution asshown by "Way of example in diagram 66. This'problem is-solved control ofthe inflow (arrows'in"solidlifies) 'occurs by means of a'guide plate 73;whi'c'h mayberourid'eti at the bottom and which cooperates with aset 74 of guide surfaces in spatial coordination and staggered in ht=.':1id=sail fashion. 'Theinflow cross-section 72 may, in "addition, have adisplaceablethrottle grid 75. Such displacea'ble throttle grids may, if desired,'be resorted'to quite generally in the inventionfor the'regulation of the quantity of flow.

According toFigj 12' there exists a sudden large crosssection enlargement, formed by the'masonry 7'6,-'for'the inflow 77. The control of the flow is achieved by arranging on both'sides at the'end of the inflow channel, but in the enlarged zone, preferably in symmetrical arrangement, two sets of guide surfaces 79, 'staggered in'head-sail fashion. Between the sets there may be provided an arched, possibly a-perforated, slotted, orbroken guide plate 81 or a corresponding guide body. This arrangement, too, permits ofcounterflow 82"and it also permits a very irregularly distributedinflow 77.

The examples describedso far relate to means and elements which operate essentially on the streamline principle. Figs. 13 to 20 show means and elements which control the flow essentially according to the resistance principle. Some of the above and the following means and elements or arrangements and applications cam-however, be combined with one another as desired and'to .goodpurpose, it being unnecessary to show suchcombinations for all needsoccurring in the practice, which are extremely varied and numerous depending on the model and nature of the equipment but if the elements are "properly employed and arranged, it will always be possible to improve or to perfect the flow conditions.

In Fig. 13 is shown an inflow and outflow withequal cross-section, a grid brick arrangement, consisting of individualflat bricks 38 which leave openpartial channels 89, arranged for theflow 83 in the diagonal line through the crest between the slopinginside crest 84 of t-he'in'side masonry 85 and the outwardlysloping outsidecrest 86 of theoutside masonry 8 7. There may be used rounded flow approaching edges 9d, pointed'and externally gently roundedflow approaching edges 91, as 'well'as blunt flow approaching edges 92.

According to Fig. 14, the chamber formed by themasonry 93 is divided by a partition 94in such a way that thereresults a deflection of the'flow 95'by 180 degrees. In the diagonals between end 9,6of the'pa'rtition 94'andthe1possibly also rounded or outwardly sloping corners97; 98of'the deflection space 99 there are, provided as flow-guiding means, cross-wise or at right angles tothe arriving flow,flat bricks 100, 101 having blunt, rounded, or pointed and rounded endfaces.

"In'Fig. 15 there are, adjacenttothe deflection space 103, and formed by themasonry 102bricklayed inflow channels 104 andoutflow channels 105 thereabove'arrangedparallel therewith. Here the sum ofthe inside cross-sections of the inflow channels'lM is often smaller than the sum of the inside cross-sections of theoutflow channels 105. Such arrangements with a partitionsuch as106 are frequently found in regenerative and recuperative equipment in refractory construction. Thedeflection space 103 contains, again in diagonal arrangement, deflectingblades 107 and 108, which may have an angular or'rounded shape. By such an arrangement theinflow 109 andcounterflow 110 are controlled sufiiciehtlydisturbance-free. This satisfies the'prerequisite of a' uniform charging (admission) or flow throughthe'channels 194,-105in both directions offlow 109, 110.

-In the model according to Fig. 16 the design cor-responds to a large extent to that shown in Fig. 15. Since here onlyone permanent direction of flow -109.is provided, it suflices to have one grid 111 of close spacing arranged diagonally in the upper portion of thedeflection chamber 103.

Figs. 17 to 20 show regulations of the inflow crosssection frequently occurring in a regenerative and -recuperative plants, with means for favorably aflecting'this regulation of the quantity of inflow. Air, for example, is to be introduced from achannel 112 in direction 113 into thechannel 115 bounded by themasonry 114. For this purpose there are arranged, at the entrance of theduct 115, a slidable grid as indicated by the double a1-row 117 and in front thereof a full brick orfull sheet 118, movable as indicated by thedouble arrow 119. According to Fig. 18, the grid is designed as a slidingbrick 120 which is provided withslots 121 according to Fig. 19 or withholes 122 or the like according to Fig. 20; the size, shape, distribution, and spacing of theseslots 121 orholes 122 may vary.

Obviously there exist different possibilities of application of the means and elements according to the invention as will be set forth hereinafter.

In Fig. 21 twoinflows 123 and 124 are to be distributed over thechannels 125 of the brick lining 126 or the like, and in such a way that as far as possible all channels carry an approximately equally large flow. Such arrangements are found in recuperative and regenerative plants, the inflow cross-section being subdivided by an angularlybent partition 127 into twochannels 128, 129 in such a way that approximately half the number ofchannels 125 are open to theinflow 123 and theinflow 124. In practiceseveral partitions 127 may be used. The masonry has astep 130. For the proper distribution of the flow there are arranged below the brick lining 126, which may also consist of grid bricks, several sets of guide surfaces 131, 132, 133 staggered in head-sail fashion in thechannel 128, and in like manner, in the recessed and higher-positionedportion 134 of thechannel 129, similar guide surface sets 135, 136. For the double deflection 137 there is again provided, between the crest 138 of thepartition 127 and the equally high, upper edge of thestep 130, a guide surface set 139 effecting the disturbance-free deflection of theflow 124 and preferably consisting of guide surfaces staggered in head-sail fashion.

In Fig. 22, aflow 141 arriving through achannel 140 is to be uniformly, or more or less uniformly, divided over a plurality ofvertical channels 125 of thebrick lining 126. Themasonry 142 bounding thechannel 140 at the bottom ascends toward its end, and in thischannel 140 guide surface sets 143, 144, 145, 146 are arranged at intervals. On the horizontal line between the upper edges of these guide surface sets, and below thechannels 125, there may be arranged additionally throttle grids or the like. The throttle grid elements may have for example a rectangular section 147,U-section 148,angular section 149, flat section 150 (bar grids, perforated plates),curved section 151, or anangular section 152 open for example toward the inflow direction. According to Fig. 23, theinflow 153 consisting, say, of fuel gas or burning or burned gas, is to flow through .a'brick lining which consists for example of brick billets 154 arranged in stage-like criss-cross superposition with passage interstices. Themasonry 155 again forms a big and abrupt enlargement of the inside cross-section, the diffuser problem occurring inflow direction 153 being solved by the arrangement of a shapedbrick 156 with or without spacing from the lowest course of the brick billets 154 in thediffuser 157. The counter-current 158 is heated air.

In Fig. 24, themasonry 159 forms a very strong diffuserlike enlargement of the inside cross-section. This is concerned with a recuperative process in which the hollow bodies arranged in superposition in the enlarged portion, such ashollow bricks 160,house channels 161 traversed crosswise to the plane of the drawing, with heat transmission through the walls of thehollow bricks 160. Theinflow 162 is distributed favorably over thevertical channels 164 located between the hollow bricks 161) by the guide surfaces 163 arranged at the beginning of the difsail fashion.

lfuser, arranged as shown for example in staggered head- According to Fig. 25,inflows 165 or 166 are to be distributed overchannels 167 with multiple deflection; thesechnnels 167 may be, for example, inlet means to combustion chambers of coke ovens. In this case alarge chamber 169 serving as a regenerating chamber is located alongside thebrick lining 168 and thechannels 167, which chamber is partly partitioned bypartitions 170, 171. The lining 168 and channels extend vertically but all start in a common horizontal plane. Theinflow 165 or 166 opening perpendicularly into theinlet conduit 172 may be deflected in a manner not shown, by guide plates or the like.Throttle grids 173 may be arranged in theinflow channel 172, there being adjacent to the inflow channel 172 abig enlargement 174 which at the inflow forms a diffuser and which, for proper distribution possesses either guide surfaces not shown or, as shown, guide plates 175 or walls in such number, length and arrangement that theenlargement 174 is divided into severalindividual diffusers 176 of smaller enlargement angle. In case ofcounterflow 177, of course, these diffusers form nozzles. For further uniformity of flow there may be arranged behind these guide plates 175, athrottle grid 178 which also has a directing wall effect and which consists of flat bricks or flat plates with many parallel, preferably narrow partial channels. The inside cross-section behind thethrottle grid 178 is lined with lining bricks and forms apartial regenerator 179. Subsequently the flow is deflected by 90 degrees and once more by 90 degrees, the inside cross-section of thefirst regenerator section 179 widening to the inside crosssection of theregenerator section 179 lying between thepartitions 170 and 171. To control this flow, knownguide walls 180 are not sufficient despite the proposals for improvement in the inlet. Additional means according to the invention in the form of deflectingwalls 181 are necessary. Appropriately also thesecond generator section 179, which lies between thepartitions 170 and 171, is additionally equipped at its two ends with such deflectingwalls 181. At thepartition 171, anend slope 183 may be built up of masonry or otherwise produced. Thepartial channels 183 and 184 resulting from theguide walls 180 can be given an outwardly increasing width. As compared with the usual system, there are thus obtained much moreeffective regenerators 179 or respectively much smaller dimensions and at the same time a uniform distribution of the total flow over thechannels 167, this leading also to a uniform flow through the subsequent combustion chambers for example of coke ovens and thus ultimately also to a still more uniform coke quality over the entire length of the coke chamber as well as resulting in smaller losses or smaller inputs per unit weight of the coke produced.

Fig. 25 shows thedevice 185 in a simplified schematic manner.Device 185 is presented in more detail in Figs. 26-29 and is shown in part in Fig. 9. Thedevice 185 controls theincoming gas 166, the incoming air 16S and theoutgoing gas 177.

In Fig. 26, adistribution chamber 186 is arranged below a standing regenerator orrecuperator 187 or the like, and a regulating device withhousing 185, which in thiscase need not necessarily be provided with guide surfaces or the like, being located in front of thedistribution chamber 186. Theair inlet opening 188 has, in this illustrated embodiment, a displaceable, for example shutter-like throttle grid 189, and is also controlled by theair damper 190. Opposite theair inflow 191 there is introduced through the conduit 193 a weak gas orother gas flow 192, while in the front portion of thehousing 183 there is arranged theoutflow valve 194 for the flow 1 95 going out in the opposite direction or leading to theoutflow conduit 197 thereof. Thedistribution chamber 186 is designed so that it distributes well even a relativelyunarranged inflow 191, 192 over all inside cross-sections of theregenerator 187 or the like. Thepartitions 198, 199 in thedistribution chamber 186 include two sets of slotted vanes 200- and 203 in steppedformationbelow regenerator 187. See the. modification and loceition'in 'Figs. '21 and 22.Partitions 198 and 199 form a sharp elbow and an'abruptly widened diffuser so that, in the case ofincoming flow 191, 192, a sharply enlarged diffuser of constant channel width is provided perpendicularly to the plane of the drawing up to the regenerator .187. It is advantageous, depending on the passages to theregenerator 187, to reduce this width in the direction of the regenerator for the purpose of as extensive as possible a reduction of the enlargement visible in the plane of .the drawing. The stepped formation provided by vanes200and'293 acts satisfactorily also when the upstream flow contains a highly irregular flowpattern. For this reason no particular features are needed to guide incoming air'191 andincoming gas 192 and both are readily mixed due to arising eddies. 3 However, the eddies are unfortunately caused at an undesirable location, namely most at the inner corner of inlet I93 resulting in an efiect that the quantities of air and weak gas which are required as maxima may not'be delivered, or may not get the favorable composition with regard to combustion. If the rate of air would be too little themanhole 196 may be used as inlet of secondary air flow, too.

In case ofreverse flow 195 coming'from the regenerator during. the heating period-this assembly ofitems 198, 199, 200 and203 acts also satisfactorily, but causes a larger drop of pressure. Actually designs of different loss of pressure are desired when said apparatus are operated inbatteries of single unitsused in parallel.

.Partitions198and 199 may be built of metal, partition 199.rnay bealternately shaped. by the upper surface ofbricksarranged in .order to diminish the .flowcross sectionof'the rearend ofchamber 186 opposite to the entrance 'of flow through device .185. The end of thepartition 198, formed for example of a bent sheetmetal wall, possesses in spatial coordination aset 200 of guide surfaces staggered in head-sailfashion, whileat the are 201 of thepartition 199 of brick or of sheetrnetal, which is made to extend to thebottom 202 of the masonry and which may in part be curved, there is arranged preferably an additional flow-regulating and flow-diffusing guide surface set 203.

In Figs. 27 to 30 are shown variants of the regulation of the inflow and outflow as necessary in arrangements according to Figs. 25 and 26 and for example in furnaces such as coke ovens.

To themasonry 204, which forms a big enlargement of the inside cross-section, there is adjacent, according to Fig. 27, thehousing 185 of the regulating organ, with packing by means of packingrings 205 or the like. The housing presents amovable damper 207 for the flow ofincoming air 208. For aiding uniformity of the flow in adjusting the required quantity of air, the inlet crosssection is here provided with adisplaceable throttle grid 209. The inlet cross-section which, in case weak gas 211 is to be used instead of air, is located diametrically opposite, possesses a set of guide surfaces 212 staggered in head-sail fashion, for deflection. In case ofinflow 208 or 211, theoutlet valve 214 movable in the direction of thedouble arrow 213 is closed. If outflow 215 is to be achieved, then, with thedamper 207 closed and at the inlet 210 closed at a point not visible, theoutflow valve 214 is more or less raised; itsstiffening plate 216 possesses guide surfaces, such as a set of guide surfaces 217 staggered in head-sail fashion, which effect a deflection of the outflow 215 previously already influenced by the guide surfaces 218, to a large extent disturbance-free.

In Fig. 28, the position of the valves and dampers is selected somewhat differently, there being arranged for the air inlet damper 219 a guide surface set 220 which is located somewhat inside thehousing 185 but without substantially disturbing thecounterflow 221 and if desired aregulatable throttle grid 234 is again additionally provided. Through this measure-at variance with the usual .237, this being sufficient for some conditions.

throttling bynteans of a full..plate-theincomingaflow 222 is'irifluenced particularly Yfavo'r'ably. The;.gas flow 224 or the like arriving from conduit- 233 is favorably deflected and distributed by ,guide surfaces 225 which are arranged in the interior of'the inletconduit and which do not protrude into the interior of the hous'ing185 and here apply without gap against theconduit 223. Theoutflow valve 214 is here shown open. It may also have flow-regulating means (not shown). In this variant, however, this merely reduces the draft requirement. Hence it is thus possible, particularly if this-is appropriately done within a draft course at several individual-points to make more powerful for example, especiallythe valves farther removed from the smoke stack, say according to the rule that the valve resistance is reduced the farther the valve is removed from the smoke stack, so that all valves or regulating organs of a complete plant ,pass about an equally largeamount of air.

According to Fig. 29, the favorable deflection of theair inflow 226 is achieved in that at theinlet cross-section 227, which can be regulated and closed by the movable damper228, there is arranged a likewiseregulable throttle grid 229 which is followed, in accordance with the deflection desired, by a gentle rounding 230 of thehousing 185 at this point. Also for thegas inflow 231 or the like a gentle rounding 232 is provided. This rounding has the advantage of an inside space, substantially free from insertions, of thehousing 185 and hence of anundisturbed outflow 233, which is controlled by theoutflow valve 214.

The embodiment according to Fig. 30 shows anair damper 219 withthrottle grid 234 in the cross-section of theair inflow 235. Herethegas inflow 236 has no special flow-regulating means; ratherfits flow regulation is here achieved according to the resistance principle by a simple, or better a double-or multiple throttle. grid The outflow valve '2l4 for the regulation of theoutflow 206 corresponds to that of Figs. 28 and 29. In all thesehousings 185 of Figs. 26 to30, there is. provided in known manner a removable front plate 196-for the purpose of repair, cleaning, control, etc. In the valve models according to Figs. 26 to 30, which are suitable for regenerators, recuperators, and other equipment, thehousings 185 may be selected smaller than previously, as their inside cross-sections are better utilized with better distribution over the regenerators and the like. This affords the operative advantage that a less intensive heat radiation takes place.

In Fig. 31, for example, ahot air flow 239 arriving through theinlet 238 and coal-distillation gas flow 241 arriving from theinlet 240 come together diametrically under deflection by degrees in the stronglyenlarged cross-section 242 for the purpose of joint combustion, as is often the case in muflle furnaces for the production of enamel ware and the like, that is, for the heating of the muffle from the outside. Themasonry 243 subsequently forms adeflection space 244 where the flow is deflected by degrees. Such deflections repeat several times. In Fig. 31, only one morerectangular deflection 245 is shown diagrammatically, these deflections being bounded by apartition 246 provided with asharp bend 249 and by astraight partition 247. In thedeflection space 244 there is provided a set of guide surfaces 248 staggered in head-sail fashion, while in thedeflection space 245 there is arranged, for example di agonally, adeflection grid 250 or the like. In this way this difficult flow can be controlled. Additionally a small partial flow may be guided from thedeflection space 244, through anopening 251 possibly provided in thewall 247 at the top, to the subsequent chambers not shown. In the example of Fig. 31 there are preferably shown means operating on the streamline principle; they disturb the flame expansion much less than the means may according to the resistance principle theoretically likewise applicable according to the invention.

Figs. 32 and 33 show the application of means of the invention in combustion chambers or respectively burners in refractory construction.

Thecombustion chamber 253, bounded in Fig. 32 by themasonry 252, contains anozzle 254 on amasonry channel 255. In thespace 256 between themasonry channel 255 or the like and theoutside wall 252 there are arranged flat shapedbricks 257, for example set on edge, which leave freepartial channels 258, so that a favorable de-eddying of theair inflow 260 arriving through thechannels 259 takes place. The result of such an arrangement is a combustion of the gas flowing out through thenozzle 254 with a longer flame. The shapedbricks 257 with the function of guide surfaces may be of difierent heights or staggered.

According to Fig. 33, theoutside wall 263 of thecombustion chamber 253 is provided in the combustion zone with constrictions or the like 264, 265, with the narrowest point preferably at the level of thenozzle 254. This, too, gives a good conveyance of the current ofair 260 to thegas 261 to be burned and an orderly, long-flame combustion, as is usually desired. Thecounter flow 262 is indicated for the sake of making it complete.

It is obvious that modifications and combinations not specifically shown and described can be utilized within the theory of the teachings of the present invention without departing from the scope thereof as defined in the appended claim.

I claim:

A heat exchanger for coke furnaces, mufile furnaces, enameling furnaces and the like having refractory or brick-lined channels for the regenerative or recuperative heating of air by the combustion gases from the furnaces, said channels being bent at an angle varying from about a right angle to about 180 degrees and in which channels the air and gases are subjected to changes in direction,

channels, thereby forming a substantially uniform cross sectional flow pattern, said deflecting means comprising a staggered series of curved vane guiding surfaces positioned in its channel to provide a suction side relative to the air and gases in the channel, the curved vanes being each disposed on the suction side of the subsequent vane, the resultant curvature of the series being greater than the curvature of any single vane, the said resultant curvature of the series being defined by the curve which passes through the intersections of the chords of the vanes, the amount of the overlap of the vanes with respect to each other being sufficient to produce a jet velocity vector of the gases flowing in the channel in a direction substantially tangential to said resultant cur vature of the series, and the angle of attack of the incident gases in said channel to the first several vanes at one end of said series being negative with respect to the direction of the velocity vector of the incident gas stream, whereby static and eddied zones of gas flow in the bends of said channels are substantially eliminated by said defleeting means.

UNITED STATES PATENTS References Cited in the file of this patent 335,558 Bissell Feb. 9, 1886 1,141,108 Diehl June 1, 1915 1,590,373 Holbeck June 29, 1926 1,676,070 Bluemel July 3, 1928 1,944,074 Forter Jan. 16, 1934 2,097,255 Saha Oct. 26, 1937 2,097,544 Ames Nov. 2, 1937 2,177,887 Huet Oct. 31, 1939 2,216,046 Peck Sept. 24, 1940 2,376,331 Abrams May 22, 1945 2,554,092 De Poray May 22, 1951 2,592,899 Hopkins Apr. 15, 1952 2,618,925 Wislicenus Nov. 25, 1952 FOREIGN PATENTS 819,028 France Oct. 8, 1937

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