SCIENTIFIC ABSTRACT YANKEVICH, V.F. - YANKINA, A.A.

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CIA-RDP86-00513R001962110005-6
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RIF
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S
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100
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November 2, 2016
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September 1, 2001
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5
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December 31, 1967
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SCIENTIFIC ABSTRACT
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I ' GROZIN, Boris DImitriyevich; DRAYGOR. .David Abramovich, doktor tekhn,nauk; SEMIROG-ORLIK, Vsevolod Nikolayevich, kand.tekhn.neuk; FUZANOT, Kikhoil Apollonovichq kand.tekhn.nauk; GCRB,'Katvey Wvovich. kand.tekha.nauk; YAMVICH. Vil'Yam..Fedq.s1syeTichl_~nxh.; SNYAVSKAYA, Mariya Dmitriyevas, in2h.-, V.ALICMX, Georgiy Iosi- fovich, insh.; KRAHAROV, V.S., prof., doktor tekhn.nauk, retsenzent; TY11YANYT, G.D.j red.; GORITOSTAYFOLISLAYA. H.S.. takhn.red, (Increasing operating safety of machine parts] Povyshenia ekeplu- atatuionnoi nBdezhnosti detalei mashin. Moakva, Gos.nsuchno-tekhn. izd-vo mashinostrolt,lit-ry# 1960, 292 p. (MIRA 14:1) 1. Chlen-korrespondent Ak USSR (for Grozin). (Machinery) (Mechanical wear--Testing) GROZIN, 3).D., otv.red.; DRAYGOR, D.A., 28M.otv.red.*, BARABASH9 MOL*q red.toma; KRAGELIMY, I.Y., red.; 20010 , S.Y., red.; FAMFXAN, I.D., red.; ZAMAVSXIY, B.S., red.,Prinimali uchastiye: BRAUN, M.P., prof.; VAYNM(;, M., prof.; PWRMO. I.P.. kand.tekhn.nauk-. SINYAVSKAYA9 M.D., inzh.; SMCHUK, V.A., kand.takhn.nauk; SWIROG-ORLIX, V.N., kand.tekhn.nauk;_%&NMNICE~_ .-Y.~ inzh.; GORB, H.L., kand.tokhn.nauk; RAXIM13A, N~P,g takhn.red. (Increasing the wear resistance and useful life of machinery in two volumes] Povyshenie iznosontoikosti i aroka sluzhby mashin v dvukh tomakh. Kiev, Izd-vo Akad.nauk USSR. Vol.l. 1960. 486 p. (MIRA 13:12) 1. Voesoyuznoye nauchno-tokhnichaskoye obahcheatvo mashino- stroitelinoy promyshlennosti. Kiyevskoye oblastnoye pravleniye. (Mechanical wear) (Mechanical engineering) 2?921 31123161100010 17/004/024 AGOVA101 AUTHOR: Yankevioh, V. P. TITLE: Increasing the resistance to wear-of steel.by-treatment with a high- temperature compressed gas stream PERIODICAL: Referativrjyy zhurnal, Mashinostroyeniye, no. 17, 1961, 15, abetract 17AIOV("Tr. 3-Y Vses. konferentsii po-treniyu i iznoBu v,mashinakh. V., 1". Moscow, AN SSSR, 1960, 93-98) TEXT: The author suggests a method of treat-ng metals with a compressed gas stream of high temperature to strengthen the surface layer of components, He investigated the changes in the surface layer of the 40X (40Kh) grade steel und-:-r the effect of a compressed gas stream (the combustion products of smokeless pois,~4 at a pressure on the surface of up to 600,kg/cm2 and a heating rate of up V~ 300,000 degrees/see. Under these conditions, a uniform. white layer of 75#, dept-h Is formed, in which a martansite-austenite transformation and a carb~,zn &aturat!"r). of the metal Is taking place which causes an Increaze in the reslst~ux--r- to we-ar, %I [Abstracter's note: complete translation] Card 1/1 DD AUTHORS: TITLE: PERIODICAL: M56 S/021/60/000/005/012/015 D210/0304 11rozip, R.O., Corresponding Member AS UkrSSR Nyzhnvk, S.H., and Vankevych, V,F, Structural stato of the white layer formed under the influonce of a pulse stream of high-temperature gases Akudemlya vauk ukrayin0koyi RSR* Dopovidiv, noe 5, 1960, 'VPXT! The ennifiticos t.f 1,.-.-wation of the white layer due to a stres,31 of gases are described bs ).Fo Tankevyeh (Refs 9: DAN URSR, 480 (1957))* The velGeity oi heatieg in the experiments Was 300 to 400 thousand dego per second,, taii% of cooling 80-100 thousand deg. per s6condo The velocity of the-rmal processes was determined from tht o,&- cillogrom or temperature v,tr-),AiJon on the surface. The structure of The white layer nix the X40 stiel *a,4 studied with the aid of an electron microscope; more detailed information was obtained from X-ray analyal&. Card 1/3 Structural state of th('1006 270 CV6 s/021/60/0 5/012/015 007 D210/D304. The white layer on X40 sttel- consisted of martensite; a small quantity of augtenitt was observed in the surface lgyer 10 mk thick* Initial &tructure of the steel: Temperature at 500 C after ordinary hardening. The martensite of the white layer has considerable displacement of the maximum of the (110)o(, line towards small angles in comparison with its position for the structure of the ordinary hardening; the doublet (101 i 011) (110)0~ has no splitting. At the same time the width of (110)d*, line increaseso For the (111) Y line of the thin surface layer# a considerable displacement of the maximum towards 4m;All angles in Alpo characteristice Dato on the (110)0L line are shown on FIX* 2, Local spectral analysis was made with the result that the carbon con. centration increases by 0.294 only in the thin surface layer, not in ' other*llayerse The concentration of other elements in the white layer (Mn and Cr) does not change. Theoretical explanation of experimental data is attempted* There are 2 figures and 12 referenc*a: 9 Soviet-bloc and 3 non-Soviet-bloc. The references to the English-languago publi- cations read as followa-, 1). Clayton, C. Jenkins, The Institute of Physics, London, 1, 69 (1951); F.E. Worner, B.L. Averbachl Ms Cohen% Card 2/3 Y; 27056 S/021/60/000/005/012/015 Structural state o %f the*** B210/0304 Trans* Amer* Soc, Metalsq.49, 832 (1957)o ASSOCIATION: Instytut budivellnoyi mekhanil~y AN URSR (Institute of Structural Mechan ics, AS UkrSSR) 1959 SUBMITTED: December 129 60 57# . f 20 g. 2: (1) Change o Lejends to P$ width of the-411W,~ line and so . 4t~ displacement-of"interference tp the maximum In relation 40 i , depth of the white layer. \ h f th d ( o e t 2) Wi On the left: line,, a, radians; On the (110))-~ .30 , right: (3) Double of the displace- Below: (4) 28 l B t 20 men , m= ang es ; Depth of I& er, mk. 'r,711d'U'va W0,0Y, N1((WD Card 3/3 Pwc-2. 3MfH& MHpHHjj nillij (110)a TA 3miulellf ul hl- - 'rep4)epvtq1Aiforo MaKCHMYMY 8 3anewsocTi uj ,,j r.111. 4dizorov wapy. 59 7 6 3111116010141b0010061013 D262/D301 'AUTHOR; Yankovich, V.P, TITLE: Changes in structure and composition of steel surface 0 layers caused by a stream of compressed gasen at high temnerature SOURCE: Akademiya nauk SSSR. Institut mashinovedeniyas Treniye i iznos v mashinakh, v. 14, 1960p 171 - 184 TEXT: The purpose of this article is to explain the causes of ero- sion of the surface layers of a piston ring of an aircraft engine. The following instruments and devices were used: The apparatus ~t)~;7 -3 (FLIT-3) to determine the micro-hardness of the surface layersp X---ay equipment and the installation YPC,-50 (URS-50) for radiome- tallographyp and the spectrograph KCA-1 (KSA-1 ) for spectrum analy- sis. Piston rings made of steelo; 38 Y, IN ~OA OMIMA) and Y1 2 M (Kh1 2M) and cast irons: n~iq -1 (PLCh-1 ) and ~