SCIENTIFIC ABSTRACT ZOZULYA, N.V. - ZRAYCHENKO. V.A.

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP86-00513R002065510013-8
Release Decision: 
RIF
Original Classification: 
S
Document Page Count: 
100
Document Creation Date: 
November 2, 2016
Document Release Date: 
September 26, 2002
Sequence Number: 
13
Case Number: 
Publication Date: 
December 31, 1967
Content Type: 
SCIENTIFIC ABSTRACT
File: 
AttachmentSize
PDF icon CIA-RDP86-00513R002065510013-8.pdf2.88 MB
Body: 
:i/ H.11/6 1/0()o/oo I/ oo:2/ool) I., 1.,) 4 / ~, -3 r ri Tubular Surf aces with Long r t ij~"v,~ I Ri b b 1_n(t for Regune I at or s and Water Heaters of Gas~ tut t, tn~, Sei s are arranged to flow countvi- Io one anoLher so as to make the best use of the temperature differeziLe between them. The longitudinal ribbing increases the vigiditv ol the tubes and makes them stronger, so that with relatively smatl i.ncrease in resistance a heat-exchanger --an be constructed for higher gas speeds, The ribbing is not partic:ularly !3ubject to contamination and is convenient for rleaxii.ng: Accordingly, the Khar;kov TUrbiiie Work,-4 was vecommended to use such tubes for theirmgenerator for Xas turbine type jo-80U~ By agreement with the works, the In6titute of' Aiermal Power of the AS Ukrainian SSR ma&t invest igat ions of 1he heat transfer and resistance of lt)Tk,%I.A 'Utdilvil Iy -r ibbed ttibes of' 16 itun diameter, with ri.h!; I"' mni highi :ovvenlent :or use in the regeneratcr The i)bject of' the investigation was to obtain more accurate dosi-vit Uormulae on heat transfer and hydraulic resistancp of' ribb i tjibi~s wilh -,-ar:tc-us numbars.~: round the tube perimeter. s/114/61/000/001/002/00!) E19VE355 Tubular Surfaces with Longitudinal Ribbing for Regenerators and Water Heaters of Gas-turbine Sets Simultaneously, the Institut elektrosva.-ki imeni Ye,O.Patona AN UkrSSR (Electric Welding Institute imeni. Ye.0, I)aton of the AS Ukrainian SSR) developed automatic equipment for manufacturing longitudinally-ribbed tubes by ;sreld;ng the ribs to the plain tubes. Aluminium tubes may be made by pressing or drawing from molten metal. Heat-transfer investigations for a single ribbed tube were made in an open-circuit wind tunnel of cylindrical shape, a sketch of which is given in Fig, 2, In the test rig the tube consisted of measuring, stabilising, experimental and tail-end sections. Comprest5ed air was ' obtained from a compressor and tould be passed at rates from 5 to 30 m/sec. The seamless tubes and ribs were made of steel, grade 20, The tubes were electrically heated and the power input measured. The instrumentation and experimental procedures are described., The accuracy of' the experimenti4 depends very much on the correct measurement of the mean Card 3/7 EPA/E%:' Tubular Surfaces with Longitudinal Ribbing ft)r Regenerators and Water Heaters of Gas-turbine Sets temperature of the tube surface and so partitialar atteintion must be paid to this point, An assessment of the accuracy of determination of the heat.-t.ransfer coefficient ine-ludmg heat lost by radiation showed that the maximum relative error is 8 .. 10%. Heat-transfer coefficients were determined and for comparison and generalisation the results were expressed as relationship.41 between the Nusselt and Reynolds criteri.a, the resistance being also plotted as a function of the Reynolds number, The tube dimensions are tabulated,, The tests ware made with air-flow rates of 7 , 26 ni/sec. which ccorresj)ondli to Reynolds number range of 3 000 to 20 000 with a difference of 30 - 75 0C and with the 9ppcific thermal loadl_nz in the range 11 000 to 36 000 kcal./an hour., Experimental heat -transfer re,sults are plotted it, Flgs~ 3 and 4 and it will be seen Lhat the Points tend to lie highor Card 4/7 i .. I I"... I 1 1. -1 1 ~ - .1 S/ll4/6l/oOO/OOl/oo2jooq Eiq4/E!5i Tubular Surfaces with Longitudinal Ribbing fo.r Ragenerator.s and Water Heaters of Gas-turbine Sets as the ratio of length to equivalent diameter 1.3 decreased, For all tubes investigated the heat-transfer rasults are satisfactorily described by expression (1). Resistance tests were made under isothernial conditions, The test results plotted in Fig. 5 show that within the limits of experimental error the msistance follows the usual relation- ship for smooth tubes given by expression (3), Comparison between ribbed and smooth tubes shows that. tho r[bbad tubcs have considerable advantages in weight, volumn and heat- transfer characteristics., This is partizu.1avly noticeable when the thermal resistance of the heat-tranitfer medium flowing within the tube is small compared with the resistance to gas flowing over the outside of the ribbed surface, O~omparative data were obtained by building up bundles of tubes, some smooth with longitudinal gas flow., others smooth with c;ross-flow of gas, and longitudinally-ribbed tubes with gas flowing along the ribbing, In each :;ase the bundles were made Card 5/7 S/114/6.1/ooo/ool./oo2/oo9 E194/E355 Tubular Surfaces with Longitudinal Ribbing for Regenerators and Water Heaters of Gas-turbine SetH equal in volume and in active section for pasisage oC gika~ The comparison is made in Fig. 6 and c;onsidering iis uuity g. 'i a the heat-transfer coefficient of smooth tijbes with lon itudn I flow, smooth tubes with a cross-flow havo a :.nefficient of .1.2 and the longittidinally-ribbed tubes have a coeffi4ienl of 2.2, In gas-turbine regenerators the longitudinally-ribbed tubes will not give all of this improvement but the redu:.tion is leiti when the heat-transfer coefficient from the air side is highs Thus, even with the present ~_imple fc.-rin of ribbing an the gas side it is necessary to intensify the heat -tt'ansftr pro-ess on the air side, A simple way LS to raist, the air cij).qed by reducing the active sertion of the tube ivith Ii.ght i ns or t 5 Internal ribbing could be used but would he rather difticuLt to make, Thus, the use of tubps with kongitudinal ribbinA has improved the pro,:.ess of heat exzhangc, I'lip use of these tubts for gas-turbine regenerators witli high cnwpr,~,sqion ratios and, for gas water heaters makes 3-1. pos!-ihle Lo preserve thf~ Card 6/7 S/lI/I/(,I/OOo/OOl/oO2/00q r. 1911/E3'- Tubular Surfaces with Longitudinal Ribbing for Regenerators and Water Heaters of Gas-turbine Sets advantages of the tubular construction. At. the iame time, the amount of metal used in manufacturing heat-exchangers, their size and the consumption of' seamless tubes are all reduced, Acknowledgment is made to senior tpchni~;xan V.I, Kosov for his assistance in the experunental work, There are 6 figures, 2 tables and 2 Sovxet references, Card 7/7 ZOZULYA, N.V.[Zozulia, M.Y.); rJIAVIN, A.A.[Khavin., 0.0,11 KA01111., B.L. Heat transfer and 17draulic: resistance of pipes jr1th spirally winding fins. Zbir. prats' Inst. topl. Ali IMR no.22331,40 161. (KIRA 1.6t 6) (Heat-Transmission) (Hydrodynamics) KREWEEV, O.A. (Kremnlov, O.C.); ZOZIJLYA. N.V..__[ZoZulia, M.V.1 Int,ansification of heat losses in longitudinal flow past trans- versely perforated plates. Dop. AN URSR no.41484-1,,36 162. (MIRA 15:5) 1. Institut teploenergetiki AN USSR. Predstavlano akademikom All USSR I.T.Shvetsom j3hvets', I.T.). (ilea t--Conve c tion) (Hydrodyneumics) KREWEVp O.A., doktor tekhn.nauk; ZOZU..LYA-,_.N,.V..,....-kand.teklinnauk; 101AVIN, A.A., inzh. Heat transfer of tubes with loop-wiref~ibbinc in case of longitudinal flow around them. Energomashinostrocnie 8 no-5:30-31 My 162. (MMil 15: 5) (Heat-Tranamission) III 'I It ;till: I;; :j!1;1II.!;A1II1jlII ZOZULYAI N.V. LrZo=lia', M-V.1; KHAVINY A.A. [Kbavln, 0.0.1; RUB, Yu-I- Layout diagrams of heat exchangers made from longitudinally finned tubes. Mr. pratst Inst. tepl. AN UfSR no.24:24-32 162p (mlFj, lb-.J) (Heat exchangers) S/021/62/OUO/004/011/012 D299/D302 AUTHORS: -Kremnlovt 0.0., and Zozulya,, MT,V- TITLE: Intensification of heat transfer by naeans of vertical perforation of Plates in a horinxiti-Lal flaw P_1,,'[iIODICAL: Alcademiya nauk UkrRSR. Dopovidit no. 4, 1962, 484-4s6 TEXT: The thickness of the lainin-ir boundary-iayer, ai, viell a,-, the formation of this layerf depend on the length of the heat trun.9fer 0 element. A shortening of these elements leadO to intensification of heat transfer. This can be achieved by perforation of the plates ,,,ihich constitute the heat-transfer elerient4 Exporime-ats were cariled out at the Institute of Ifeat and Pot-;er Engineering of the AS UlcrIM with various types of perforated plateaq having, following ratios of length a of surface element, to size b of perforation.- Vb _~ 5/1 ; 5/1.5; 7/1.5; 10/1; 10/1.5; 10/2; 15/1.5; 20/2, It was found that the intensity of the heat transfer is conaidereably affected by a decrease in the length a, and to a much lesser extent by the size b, The best results were obtained with smallest a (a = 5). A comparati- ve study was made of heat transfer in perforatod- oid in wiperfora- Card 1/2 S/021,/'62/000/004/011/012 Intensification of heat transfer D299/D302 ted plates. It waa found that the pQrforations increase the heat transi-er by a factor of 1.75 (with a = 5 n1m). By procesoing- the ob- ' 4 U'ained data, the heat-transfer coefficient was determined by means of the function Nu = f(Re). This function has th,'.~ form Nu = 0.038 100.8 for tubes with perforated plates (a = 5 mm, b = 1.5 rL11). It is no- ted that the size b shouid equal 1 to 1.5 Mm. A Turther reduction in size is hardly possible from technological coit.s;-ide-rations. The above type of surface can be used for heat-transfer ele-mentst if the heat carrier does not form precipitates on the sixrface of the heat-exchanger. There are 4 figures and 3 Soviet-bloc, vefereneac. ASSOCIATION: Instytut teploenerhetyky AN URSR (Institute of Heat and Power Engineering of the As UkrRSR) PRESE11TED: by Academician I.T. Shvets', As UkrRSR SUBMITTED: July 27, 1961 ,Card 2/2 k;ind.tokhn.nauk; Wld~'f 3, V.A., im~-,- Heat transfar and hydraulic rumiotmca In a buril: ol,* tulms IwIth b. 6 lontritudinal ribbing W. vys. u('114 119 A(:,, 163. 1. Institut teploonurgo'lliki A" UkrSSR i Kliaxlkovskiy birbinn, Yy %,^",rod Kirova. "I Tli- T-1111"ll 11 ilk Z024,11 LYA )J[.V [Zozulil, I.f.V.]; DAHTAFY, S.A. Z'.,".,! Analytical ip.,(~thod for detorminin(!, tho .511"tJ111 th'l~-Akrios:~ or a .Ilcj%,~d layer durirg boiling in a downward flowbij-, fi'm. 1) r). .;A" C).I: .1 oz '- n , 342-344 '65. MINI, i8:3) 1. institut tpkhnicheskoy tel).Ic)fi,,,,Iki AN Is L 4005--66 E',,,-r (d )/EE1,'1T( I )/EP= (c)1F*-';TF qn)--._/_-1U,,m, 1;/0'G0/015/0125/01 26 ACCESSION 1411, AF5021JW WIS A. S. UTH i A 11M6 j' tj 14 t; 0 g ur I Z r- -3 n -n 1,f i:~eato tieat A,,,- 11,13 AlItnCr ',,3rt pro -ort-ri a tdlb-l lar i i a. r,. e r s i, r p1_- P- L r Tw!] c, f !,utii: t--, Ir 5oe Fig. 1 orl e f~ f i c- 0 s u _r e ---reas,~ 111`i~i A' frontal J,;-~cruave its c 0 c ff - -~ ~-j ",. 1;:,;n -w1jacoln ~.~r Flutes 17 Unif 1"~Us 0j, %lbo-a o1- ploltoa a~-- pjat,.L~a an:j -tr,~s ua f I., I ccI'larm iteSuoers, IV 'La r I g n as i I et jj