SCIENTIFIC ABSTRACT BROJEWSKI, M. - BROKHOVICH, A. I.

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP86-00513R000307010010-9
Release Decision: 
RIF
Original Classification: 
S
Document Page Count: 
100
Document Creation Date: 
November 2, 2016
Document Release Date: 
August 22, 2000
Sequence Number: 
10
Case Number: 
Publication Date: 
December 31, 1967
Content Type: 
SCIENCEAB
File: 
AttachmentSize
PDF icon CIA-RDP86-00513R000307010010-9.pdf5.96 MB
Body: 
t-.cnds of 1-.rm,,actio-,- tcchr)4qni~-~ the -Iot'-L L;r, 1!-liz.-itionrl cal -robicnn:3. u. 5. "iol - Lo6z, Pol:-nd. SOITICE: &5t E~rorc&n Acce3-.ionz Liat (LE. L-, -701. 5, :--:D. BROJBVSKI, 14aksYmilian - --- -J ' or social insuranc-le aTt, -- Assessment of rates f f v jvq-t--) hand i crapt - I rP eL insur&nco bene-fi-tv, for workers o r zai)--zp spol 3. irlo,.8/9.93,=~0/5-~ E61, BROJEWSKI, Maksymilian . Maternity insurance allowances during maternity vacations. Praca ZAbeZp spol 3 no.12:53-56 '(-I. BROJEkSYLI j I-Wwymilian --- --l-I.. . - -1. - Compensation and.the right to a health-or-maternity insurance &Uowance. Praca zabezp GPOI 3 no.11:42-44 161. BRORWSUI-~~k-symiMerl Pay periods of sickness allowances. Praca i zabezp sTCl 4 no. 5:52-55. My 162 BROJEWSKI, Maksymilian -Forms of 6mployme.nt and social insurance of employees of the Agricultural Circles. Praca zabezp spol 5 no-3:57-61 Mr 163, BROJEWSKI, Maksymilian Types of wages constituting the bases for the calculation of benefits in cases of health and maternity insurance. Praca zabesp SPQ1 5 no.8/9:SM2 Ag-S 163. BROJEWSKI, Maksymilian Method of computing sicImess allowances. Praca saberp spol 5 no.12s40-43 D163. BROJEWSKZ, Makaymilian' New principles of supervising employee~;,.on sick leave ordered by a physician. Praca zabeap spol 6 no.3-.32-35 Mr 164. BhUJhWShI, MaksymJlian Subsidies because of contagious diseases. PracmL zabezp spol 6 no.6:30- , 33 Je 164, .1 ~!l 4 BROJEWSHY Maksymillan Periods of suspending and reinstatini- tlv~ title to socinl security pensions. Praca zabezp spol 6 no.12:29-32 D 164. BROJEWSKI, Maksymilian Decisions concerningAthparAzy work disability for past periods. Praoa zabazp spol 7 no.1:39-42 A 165. - BROJEWsKI, MaksYmilian Social Security funeral allOwancG and the obligation to pay the funeral costs. Praca zabesp sPol 5 no.7:45-48 JI 163. I'll ~Ok ~_rbw_9Yi_uh,,-__ZAU&AYLOV, Boris Aleksoyevich; STEPANOV, Nikolay Grigorlyevich; KOLTUNOVIA, M.P., red.; BOBROVA, Te.N., tekhn.red. [Fundamentals of safety engineering and fire prevention measures in railroad transportation] 08novy tekhniki bes- opsenosti i protivopozbarnoi tekhniki na thel02nodorozhnom transports. Xoakva, VOSS.i2datellsko-poligr.ob"edinaniog-va putei soobahcheniia. 1960. 234 p. (MIRA 14:4) (Railroaas--Safety measures) (Railroads--Fires and fire prevention) BROK, V. A. "Tem-zerature Anoiralies of Sprint-, and the Beginning of Surz.-,er in the South- eastern FRrt of Western Siberia." Cand Geog Eel, Chait of ClimatoloV and Meteorologr, Tomsk State U imeni V. V. Kuybyshev, Tomsk, 1955. M, No 15, APr 55, SO: Sum. ".0. 704, 2 Nov 55 - Suarvey of Scientific and Technical Dissertations Defended at USSR Higher Educational Institutions (16). BROK,-j,A-, kand.googr.nauk; KOYALSTA, T.Te., inzh.; MICHMUTA, L.S., starshiy inzhener; IMAIRSKATA, I.A., starBhiy inzhener; KUKHARSKAU, Y.L.; PAXMMICH, K.P., inzh.; DYNOTICH, Tu.L.. inzh.-, TOROBINTA, T.P., insh.: FAKHMIGH. S.Ta., otv.red.; LEONTOTICH, B.T., nauchno-takhn.red.-, USMOTA, T.Y., red.; WMGNYZY, A.N., tekhn.red. (Agroclimatic reference book on Kemerovo Province] Agroklima- ticheakii Bpravochnik po, Kemarovskol oblasti. Leningrad, Gidro- mateor.izd-vo. 1959o 135 P. (KIRA 13:2) 1. Novosibirsk. Gidrometeorologichaskaya observatoriya. 2. Novosibirskays gidrometeorologichaskaya observatoriya (for Brok, Kovaleva. Kellchavgkaya. Iznairskaya, Kukharskaya, K.Po Pakhnevich, Dynovich, Toroblyeve). 3. Direktor Novosibirskoy gidrometeorologichookoy observatorli (for Leontovich)o (Kemerovo Province-Crops and climate) BROK V. A. Climatological characteristics of temperature anomalies in the southh.- egatern part of Western S~lbqria. Trudy TGU 147-136-1" 157, (MIRA 16 M (Siberia., Western-Atmosphedo temperature) 17 (2) ,.-,Golldfarb, D. M.9 SOV20-129-6-61/69 AUTHORS: Bass, 1. A., Gorlenkol Zh. M., Illyashanko, B. N., Hankinap V. P., Khesin, R. B. TITLE: Infectious Properties of Injured Phages PERIODICAL: Doklady Akademii nauk SSSR, 1959, Vol 129, Nr 6, Pp 1421 - 1423 (USSR) ABSTRACT: D. Fraser and co-workers (Ref 12) concluded from their investiga- tions that the infectious activity of the destroyed preparations of phage T2 is related to the desoxyribonucleic acid (DITA) which was liberated from the protein covers of the phage particles by the effect of urea. The results obtained by the authors, how- ever, were rather divergent. Therefore, they thoroughly investi- gated the preparations formed from bacteriophages by treatment with urea. The following dysentery phages were used; T4r, DILI (isolated from the soil by T. 11. Broker), an& N-2 (obtained by F. I. Yershov, 2-y 111oakovskiy gosudaretvennyy meditainakiy institut, Second Moscow State Medical Institute). The effect of the phages was tested on protoplasts (bacteria without cell walls). The authors obtained them from cells of the following Card 1/4 bacterial strains by means of lysozyme according to R. Repaska Infectious Properties of Injured Phages SOV120-1291-6-6il6q Ref 13): E. coli B (sensitive to phage TO and DMI); E. coli 600 resistant to all three phages mentioned); and Sh. dys. New- ~ castle (obtained by F. 1. Yershov, sensitive to N-2). Suspen- sions of phages, concentrated to 10 12 particles in 1 ml, were treated with an 8 M urea solution. Thereafter, the action of phages on intact cells was completely eliminated. They showed an activity of 0.00001 to 0.0011%, on protoplasta. This effect concerns bacteria strains sensitive to phages as well as those-- resistant to phages. Thus, this remaining activity cannot be due to the preservation of a few phage particles. Further ex-. periments showed that the above residual infectivity is not re- lated to the free DNA which has left the virus particles. Thus, it could be assumed that only the part of the DNA is active which is protected against the used desoxyribonuclease by other components of the phage (probably by proteins). In order to -he pro- check this assumption, the proteins were separated from 4. parations by phenol or chlorqform. The preparations were com- pletely inactivated in spite of the proved extensive separation Card 2/4 of the proteins from the DNA. This proved again that, after Infectious Properties of Injured Phagee SOV/20-129-6-61/69 treatment with urea, infectious activity is not due to free DNA. On the other hands it has been known that the protein com- ponent isolated from the phage cannot cause phage reproduction in the bacteria. The only assumption is that one complex of the DNA with the protein has infectious activity. It was serologi- cally proved that the proteins of the active complexes mention- ed are similar to the antigenea of normal phage particles. The transition of 80-90,06 of activity into the precipitate could be achieved by centrifugation of virus preparations treated with urea as well as by suspensions of intact phages. The electron microscope showed that the above complex has corpuscular struc- ture and that it is of about the same size as the intact phage. Figures 1 and 2 show that, apparently, urea destroys only the distal parts of the processes. Thus, the phage particles become incapable of depositing on normal bacteria. The inner part of the process axis which consists of protein is uncovered by the urea effect. Further experiments with trypsin, which destroyed the uncovered part, brought about complete suppression of ac- tivity. Thus, the protein in the axis of the phage particle is necessary for the occurrence of the infectious activity of the Card 3/4 preparationsmentioned. There are 1 figure and 13 references. Infectious Properties of Injured Phages SOV/20-129-6-61/69 ASSOCIATION: Institut biofiziki kkademii nauk SSSR (Institute of Biophysics of the Academy of Sciences, USSR). Institut epidemiologii i mikrobiologii im. N. F. Gamaleya Ak-ademii meditsinskikh nauk SSSR (Institute of Epidemiology and Microbiology imeni N. F. Gamaley of the Academy of Medical Sciences, USSR) PRESENTED: June 10, 1959, by I. L. Knunyants, Academician v SUBMITTED: May 29, 1959 Card 4/4 VLASOVp V.V., kand, ned. nauk (Novosibirsk); BROKHES, L.I. (Novosibirsk); ~, SHTERNSHIS) Yu.S. (Novosibirsk) Effective anticoagulant treatment in thromboambolism of the pulmonary artery. Xhirurgiia 40 no.11:121-122 N 165. (MIRA 1817) BROKSH, M.M.; GVOZDEV, B.P.; ZAYTSEV, V.I.; ESTRlNA, A.A.; SALTYKOVI A.L. Investigating a full-Beale model ofaspherical scrubber, a ball-shaped dust collector. Trudy VNIIGAZ no.21/29:222 2 164. .(M 17:9) 0 BROKSIII M.M.; YERMOSH1NA, H.S.; SALTYKOV, A'.L.; ESTR1NA, A.A. Ghecking the liquid content in gas flow. Trudy VNIIGAZ no.21/~9:183-195 '64. (MIRA 17:9) GVOZDEV, B.P.; KVASHUK, V.S.; HOSHELEV, V.A. Using cermet filters to remove solid impurities from natural gas. Trudy VNIIGAZ no.21/29,-205-217 164. (MIRA 17-9) VNI BASS, I.A:;_2~~T ~N.- GOLII)FARB., D.M.; GORLENKO) Zh.M.; ILIYASHENKO, B N.;~ KANKINA, V.P.J. KHESIN, R.B. Significance of proteins for the Jnfectivity of bacteriophages treated with urea...Biokhimiia. 25 no.2':360-367 Mr-Ap 169.' (MIRA 14:5) 1, Institut biofiz:Ud Akademii nauk SSSR i Institut epidemiologii j mi iologii im. N.F.Gamaleya Akademij m9ditsinskikh nauk SSSR 149-skva. (BACTERIOPHAGE) (UREA) (PROTEINS) BROKERp T.N. Mechanism of antiphage activity of antit=or preparations. Zhur. mikrobiol. epid. i '-min. 31 no.2:84,89 D 160. (MM 14:6) 1. Iz Instituta epidemiologii i mikrobiologii imeni Gamalei AMN SSSR. (BACTERIOPHkGE) (TUCIL) (DIETHYLAKM) (AUNINE) BROKAR 0, lonstantin Kuzlmich; IGNATOV. Viktor Nikolayevich: PITROV. _-l-, - - ~ Nor~s rvanovich-,-MIETSIM. D.M.. red.; XHITROV, P.A., tekhn.red. [Technological training for students specializing in railroad transportation; organization and wthods) Professionalino- tokhnichmakoe obuchenle na zhelesnodoroshnom transports; organizataiia i mtodika. Noskya, Goo.transp.shol-dor.isd-yo, 1959. 25.5 p. (KM 12:6) (Railroads) GOLIDFARB, D.M.; BROM, T.N. Airti~hage properties of certain antibiotics, antiaeptics, amino acids and antitumor drugB. Vop. virus. 4 no.1:103-108 Ja-F '59. (NIRA 12:4) 1. Inboratoriya izmen chivosti mikrobov i otdel epidemiologii Instituta epid.emiologil i mikroblolopil imeni N.F. Gamalei. AKN SSSR, Moskva. (BACTIBUOPUAGN, effect of drugs on. repeat title (Phs)) I . , IAESTROVAYA, BIjOKEIj. T.11. ILIRDASHEV, S.R.; I-MGORDA. Airdno aeld decarboxylases in bacteria of the intestilial group. Zh. m1kroblol. 4.0 no-7t25-29 J1163 (MIRA 17--l) 1. Iz Instituta bioloalcheskoy i meditsinskoy khLrrdi ANN SSSR i Instituta epidemiologil i mikrobiologii imeni Ganrdei AN! SSSR. PETROV, V. I. .. GOELEVSKAYA, M.V.; SYRKASHEVA, A.V.; RAYKHSHTAT, G.N.; SJIAPIRO~ A.A.; BERLOVICH, E.A.; KARASEVA, MU.; RYURIVA, M.G. LEYKINA, R.S.; -BRO04,-T,,N.; GITARIN, D.Yu.; MOSKOVENKO, D.F.; STASIlXVICH, Z.K.; REUT, A.I., ALIYEVA, S.G. Aimotations. Zhur. mikrobiol., epid. i immun. 40 no.2:109-112 F t63. (MIRA 17:2) 1. Iz Dnepropetrovskoy gorodskoy sanitarno-epidemiologicheakoy stantsii (for Petrov). 2. Iz Saratovskogo meditsinskogo institute. i Saratovskoy gorodskoy sanitarno epidemiologicheskoy stantsii (for Godlevskaya, Syrkasheva)- 3- Iz sanitarno-epidemiologicheskoy stantsii Sverdlovakogo rayona Moskovy (for Raykhshtat, Shapiro,, Berlovic~, Karaseva, Ryumina, Leykina, Broker). 4. Iz Instituta eksperimentallnoy patologii i terapii klN SSSR (for Stasilevich). 5. Iz Belorusskogo sanutarni-gigiyenicheskogo imstituta (for Rout). 6. Iz Uzbekskogo nauchno-issledovatellskogo kozhno-venerologicheskogo instituta (for Aliyeva). RAYKHSHTAT, G.N.; SHAPIRO, A.A.; LEYKINA, R.F.; UJUSEVA, M.F.; BERLOVICH, E.A.; T.N.; KNINEETSWA, N.S. RYLNINA) M.G.LB~ Epidemiological effectiveness of preventive bacteriophage treatment against dysentery in pediatric institutions. Zhur. mikrobiol., epid i immun. 42 no.8:139-141 Ag 165. (MIRA 18:9i 1. Sanitdrno-epi-demiol_og-~clieskaya stantsiya Sverdlovskogo rayona Moskvy. I'The Influence of Hardening With High Frequency Heated Currents on the Resilience of Steel," p. 43 of the book "Problems on Strength and Deformation of IM1.3tals and Alloys", releasel by the Moscow Engineer-Physics Inst., Mashgiz, 1954. TABCON D-342613, 24 Oct 1955 -BROKHES, L.I.; NISNMCH, Ya.G. (Novosibirsk) Migrating source of ventriculer excitation in Fredericq's syndrome. Terap. arkh. 35 no.92109-114 S963 (MIRA 17:10 BROMES,L.I. (Novosibirsk) Negative coronary TLelactrocardiog?'am as- a- mgnifersta-tion of heart abnormality. z. med. zhur. n'0.6t47-50 N-D 163. (,%a.-A 17-10) 1. D'71,11,~F . I. I. P-t! a. f o -1 t - . I : . : , ~ -11 ~- ., i 1, 1.!~' , ~', -1.1p t I, lkmll, a ~~ - 1 (;) k -7 * -I . - _ I. e. ~ . .. ... , 1. - Ll:-::f . ~' D= - ) , -ospitallra.,~-r. , -.-. A Il L D A J 6 111 L L Q V A I I "t L( OD (t I 0 'Hgfd aUDY- VV PIlluftKOV. 1. 8 Jim-'Xillm aod I A I'vit ikwi N u.. 0 1. )'Wo 24. 1 lKl IA hard alhy rciiMZ",ii NTIN u,. I%- Io ~N,. JA L#tt"f,.( ' ' it %A v 4) 1% " , Ot 0 0 00 ee* 00 0 0 0 0 0 0-0 0 0 0 0 0 0 OMOW1. _1111 (at, IM t 00090090008000T 000 11 u 34 J i-00 -00 Ay 11141111111116"m d ihi 2whiin of 6 SkesWrW dvmmm, .00 Mdhods fur tbecirteTutination of I he hanInrom of the itArklual minscluml rumiummts of Strilde anti ximitar 00 vys in wbich nickel is ribetituted for cobalt (Sormite; Smena).-D. N. S. VID Ilk- 00 z 00 Hi of 0* as jr A kil - I L A MITALLUKICAL LITCRAILSE CLASSIFICAMIN LL 0 .10 C. tr C, 1, 0 91 ~ a, IN, KF I'If no I A :*I 9a Opw a a a I w Im 2 a a 3 1 IF 0 0 e 0 0 a 0 0 0 0 0 coo V a Ago to* to z,;z7z-,: 11G., ".Inv .11111 CIA 19, So A 4 of be it SO SO I .2 00 a ,3 vtj: 9 U It U 6 b - 170 0 a x a A 11 V 0 bd a It 9 a M 4 .1 4 43 a axe ff IF - ffluj._AW"~ -1 a A tp '!to swuiw Type. 1. S. uxi V. 1. liumorkin "rat_q. )"it.sa v,ku~ t-ne"grad MOIRA. Ve" 1a4 Mdala. 1"impral). IM (12). WS-113- rhromium on Sormite was studird. and a metbod ftw welklisw an the haM allosm Was devvlaprd. Moon &bDve 4-5% inciesom Uw bwdnnw wW irsistancr it) -90 sear, but n*W&a in irvegular val;9 for semporary nsitumv to rupture aml rvsis~ to b"Kholt. Tbm is a deciftse in ourra4m with a high silinni see nmirat. 1U nichd coobent can be redutvd to 3". witbout affecting thr nx-chani=pertim or ckw*ing tbo microptructurp. Cartxm intimas the ' hardneva W A 0 roa anmtowrar. "Uono(3V, ,orawmchtutniumgrt-atly ' in tb roo creases a cerfusion-maidow, Tbe bpA lion for Sormite is chromium Z&-29 i k l 3 6 b =M - c e on 2-7-3-31, . n . oar .5, MAIW&FWW oil to borus mW ~Wpbjw IMIA not Inure Ilian "7"~, Two harx! alloy nv 7_3 m) ahould be 11 m oul W th f h on, w e sone o over eating slx)ukl tw s u *b*ied to bardealn. noreWiting, ~sW quesebing In oil. Such beat. tre t e t ill t ff U ee a m n w no ect A 0 structure WA propertito of the primary cast alloy. 0 -8. G. M 0 wee &SO-ILA METALLURGICAL L"FRATWI CLAUrcat" goo Ito" 9"-Inv woo MCI/ td1loss -4 1 IVI083 wit amw 909 ad 0q. III r I i1b i- All; 'a ; t,9 Vo a i Ira 01:f: 00 0 0 0 0 0 e 9 4 0 0 *10 a 0 0 0000 00 * 0 0 0 0 0 0 0 O_S_AjL0_S_S_L"_O 0-0 0 0 0 0 0 0 V 00 0 0 0 0-0-0 sio 0 0 0 0 0 0 0 0 0 0 0-~*" 0 0 0 0 0 9 0 0 0 a 0 9 9 9 v we *Wof 0000 0 0 S` 40 0 -o- 0 e 0 eit"l-4-7,04--o -*-*To * 0 6 0 00 00 0 o 00 09 0 0 1 6 4 W3 It if 11 tits% It If "39111z: n-342s it v .4 jv L 11 1, 11 u r, m 1, P - ti 1, 00 A #**C(Sgfs -t 00 - ------ -.00 00.1 -00 GO Albom 00, &W S. Ys. Ar'ei&jMiWiwp (MfiWlvr&). 19M,-]V . 11). C. Abe., IM Sk an)).-fln Jtt,,j,,) AHqm Ml7MjKWXiLW III caml.W. 00 90 Nomille wm nbjtdW to mkiOKi)0C MA V,.My cj&Mjn&tjUn. ewbicke we" famw to have Ow mmPromm (t'r'r)rhv 1(*r.yr),(;. as ruhtdir am Wrnfiral-\'71 1. V, so i-00 0001 0 0 00- 00 002 pro* C:O U06 A S jl~ VLA OETALLUCCOCAL 1.11FRAT1,41 CLAIWIC678014 Z-- u*o U Is AV so a n' -1W -0 0 n toll'll UP69 Nil It.11 Iftt; It V 0000 00*000000000000041000ooo**O#)OOOOOOOOI.,, 00000 00000 '_O_o 0 o-0 0 0 0 0 a 00 0000000 U:O 00000000000001 a 0 a 0 a . 6 7 a 1 4 It 11 11 1 -1 It --L a It j of A so a 0 a :0 1 of 09 00 68 00 .4 0 a 0 Is 1$ 11 Is Is allin bills ~nn r,'rli v 11 k n is it a IV 8, j i3 are 0 A I I V v I P-J - I I AA 10 U SP t I I 1 0 1. 1401.1 -00 I The pblisical-ervilcUaltal PrOP"Is Of 1110AL11-011FOMIC -00 alkys at elevated tompentuirts. I. S. firokIrin. -00 lik Mriallpfrom. 16, No. 14, &1-71. N lepilt. 1937, 1. -'K'4I--S1WCimft15 (If Imil+,dite tvnig. allonit 6.31*~ C. III W-o Vii, W.4% .9 W, ,;I .%--I It, V~ -- 1-6,1 It.. Wall at 10-1111" 1,- -00 'I"-f .-Ii'vill.lit til."I Imalil" I.. t.mf Nkf-. I t.v birlidult strength of ",!i kil.i0q. Itlill, at tatfillsiv trull.l. .00 9 decres" between 5W* and MX)' to about NO kg./sq. turn. At ordinary temps. the elasticity of compression was s about 200 kg./sq. tnm,. the breaking suength about W-W kg./oq. mm. At 900* the letter was '2N) kg./sq. too mm. Tic impact resistance was slight but changed very little upon heating. According to ditatorritter messure- ment-, a transition orcurs, at &W-750* accompanied by a change in vol., which is obviously the restdt of a change 0 in phase of the Co. No change in fbe inkrostructure could be detected inctallographically tip to 9W'. Upon .0 0 heating in the air at 450-&W an oxide layer formed which "-schr4 a thkknm of 1-1.5 min, It was soft and could IN easily removed. M. G. Afoure M-ILA 111,11TALLURCKAL LITIFIAT OF CLAISOKATPON too., I a 1 -7.; I M IS AV so I P KW a I 0 0 0 tPe ib, 0 Z- - Roo ?FW-j-j i--&7-o a a I W I 0 0 0 a 0 0 0 0 0 a 411, 0 00 so -ii ~09 0 0000 0 41-0 0 - J~Apijf 0 0 0 a a 0 v 0 Ofo 0-0 GOOD* 0 0 0 0 a *3~ I I as tp it to it it n n jo Y5 x is 2% r 11 v u t7 u I , I G r I I it 1: is Lit b oT A a 00 I v 1_1 IF I AA L. I I l A ~ -09 0 .1 0 : 11! -90 :-Do -66 i-09 a l SMORCIP I"Wtis* birtsir"m Soft itran and mrsolten alloy 1 .84 oraw a m d mantairsts of momwow larfors, I ~S li"Ali... v:1 A 1. /virm,i lr.t*ik metalb.p.-at , 1 11- 16 14 13 I W 1 .00 I - . 1 . . - 1. Its- Aqe, I .I lilt. m%. ~lliej . as arm. 1'. ah-l it". V11-11 l h i k 00 ~ j, am v-~ v tanK., ti ing p W~ .01 list- -411(mv 4-1 .40 lliml "Mille. , - N .1 slim. 1 i N f 41.1 I I'll, . 1 ' it, t 11N Assisi S I I I Ilivil I t I its billiki millillilr .011111. 0 ~N :V0. Sl 4.;1-, t' N, I lit, zoo oo ~ili VINI slid V 11,117"j, Iss., Zoo 00 01mr: 41) pufliol fil-i'm W list purv iffma of sit, mill- 6thl 01 difitt'isin .4 tits. Clawiluills. .,f tile ."11111t, lilt., go 0 0 U 1., .41 iloll~ fist. '218141 inf,xv%, C%Iti 014-1 1114. Ahl Go it witlishavitt l Sig ASM.ItA fissm thr tswinisir Ismilt stiol it too mm"I 1.1 equal. Xlkliwtmpls~ m4 xl%* 11 of vm- Ism% S. 1 :0 0 :-~OO ts CLAS woo m4y&LLURGKAL Llyfrof IT at o 0 0 slip 6 6 0 0 0 0 e G~q 0 0 0 0 0 Ott cat T-11--v`11 An i t 0 v o- n jig at f9ft ICIFK=4 I tK4 0 0 0 0 0 0 0 0 0;0 0 0 0 0 0 0 0 0 0 0 0 0 0 6~16 0 q 0 0 0 0 0 - - - - - - - - - - w W wj~ W-111, Ar _v v~ v wl 1, Iv v w v v v v v v w 9 Q v v 0 0 0 0 9 9 0 0 0 6 0 90 6 0 a of* 0 0 0 a 0 * a 0 0 0 a 0 4 ; go z I A 1 6 7 a A a -U 1y 15 - 4 11 Ij 4 15 23 - -xv n n 1, IN it a ii 34 x x v a P a - 41 r-A-2-1 11 1!1.1 Ig a M - 4 E 4 1.0 (111rot POCICIIII& ..0".50t.t4l '~M. ~ 7 0 The chemical composition and structure of stalinite -00 : in, At4ef"PO'N. Velo 1039, No. ;.1 :1, :.'A ". 0 1 Zhu?. 1939, No. 9. 77.- *I'll,- hindne- -00 a . t-nilin. anti wemins; proixtite. t.f II, ~l 11111 t 1 ot , '14,411till 11Y tile uqual are ItIvillod jilt] I.%. I 41011, 1. g 0 al 11441t-I were invCN11calvd. Stalinite. 4 1 zoo so Mit 1:1 17. C 8 10, Si -~;I. 1, too I-114111C.111 front lerv (Will onle. 0 .3 : 'having.. IWIrollenol coke and tuola%" a. binding uh. ZOO 0u slanrv~. hirialfic virctrodes produced a inch which Aa% l r ,00 I-,- alloyed and whov hardrim was ctrreqxmilingiv 6 11F a t10wer. The wear rrsistarlm of he poducls I 1*"amrding ago 0 0 to Swin) of the elec. are and of ro'.. J.C VICCU(MICS W(TC '00 M AM ;ON) anti 3:10. reqP. W. R. Ih-on zoo ,low. IN, =00 tie 0 too v I It N 9 a a v X4 UNA,%," ROVIVION ad it a R a 40000 000000000000, OOCO*ooooooooooooo* *000 :::o1:::i 0 IT44 -001000000000090 0000000000009000000 9 9 Le 0 0 0 0 0 0 e 0 0 e 04 - - - l - - 1 14 It is it x it I, n 1, n AA (A I it 0 weld Electrodes with alloy coatings for wear-resistAn S Ilt,V.1kill. Prb, 1040, -N-- 6 1 pittal . . "I the 01,111 Ali !14 .1metuTv glid luir-lin. of cr, %III all'i 't.dimlv ~1 00 1 I,,. li, MCM14 for the f-p. dertrode, wilh ~11"v V-m ' ; . , 41). %1n Cr-.Nin chvirode wIcvtrd emitain, Cr : 00 ant) C 7-W'r. It - Pf"00- It"All A "-"%I 'I' ' 0 1-r-Cr S5411). Fe-NIn 37-40 And d%-111, .311-1 bo"c"ms, 00 r 1' tic t1l"'I im. 1, -1 mg, timn lnltl)lc 10q in watcr -00 00 1 lira lical virwl"411t. ate at -Ittlite r ' ' 00 j t- ," Of thr cifft'l-If 3"d -Al- i" " rolling wrighinK3445 I " J 1 I, ' I -ite clectmd" with the mittlix vitial 11, L =00 : wt. of the rUctrodc. The-,c dirlit-Irs at,- ')-,I zo 0 00 he Cr --J %In v)'-v;r(xjm. B. Z. Kai,; 1; It --09 00 _i zoo ~00 00 1:~ ZOO Ono :00 00f coo 04 00 00 0 0 00 IRS 00 ' i0e -13 It 'j AA I 'W 0 0 0 *1* 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 6 a a a 6 46 a 00 0 0 0;9 0 0 0 0 0 0 0 0 0 0 0 0 if 11 W q m 17 A, A., C - a L-I-, -(L -k-j I -J.. AL- )i F A X- I-LIVI-I P110CMIS ..a PAM111,11 A. UIWW d Limere wift Dun and A. A. Davvdo%-. tV=ftik Mma 00A 1960.,mol W-47. in RIIIIIIIIIN'Lu). Bona cylis an have bsm lined with a i Used in ::.,,r C r7T--20/, of boron to improve the wear remistence. anigkg WISQ, of boron) was produced by m ishunk 0 LI U and Use borom-Cm;Q hom, by melUng in an electric furr q, 0: 0 untity of the alloy was plawd in the liner. which was i 003 welded ormareired on. The alloy was then maltal in th 1200' C., after which the coatins was fanned by roIAL cm for 4-4 min. The immide of Ow liner Shmn V had , hardness cbftocktill C. 67-70'...A liner got lm#Ad lanes, then nine plain steel Moore. Ai 1.11111AYLINI CLAIMOCATIO11 A I III I t A IIIJILL104GICAL S.J083 LP Ov age a 0 0 a 0 00 a 0 0 1) 00'a Ly U 41 111 It 12 9 M 1 W L v 11, 41P Q 4) k--4 ..k - t- a -IL : .00 soda ftd hmL -60 )"-3vhWu-WtL -00 or linsm of mud .00 at irm omt&UiWg Ferro-bummon (oon. go* itherivilo remetion- ca. The requialte mcel by md platime Cte iner by, heating to =00 X the liner at 800 und to mi". The iated am described zoo nee c4r7.v7r. Ia 1W Q 9 v "I is 14 1 13 a I V - 1: u is IV Ail; 440 0411 0 0 oil A- 4 go 0 0 0 0 00 0000 F, 7 a 0 0 4) a 0 9 9 0 0 w a 111 31 U 11 M M it I~ alloy for Cssfing 10016 Imm-base thmuu--bt-u- 111POL'Ifill AII(I 1). 0. SilAviu. U.S.S.R. 65,933. 14-b- Will. The alloy volit.011% C 1.5 ;1 "), Ct S' 15. .111.1 'I'I III addit. 2 '.V;' III Ni c-an III, addvd III Ow Alm-ILA MITALLO&KAL LIT111,11TIONIF CtOSWIC01.10 sdmnv~ "It 0.9 1 U' If 'I of a 0 0 0 0 0 0 0 0 0 4 -00 roe :200 0* .'oo 00 9 0 0 _Fw 0 4 a I v IN a I 4 0 0 0 49 0 is 0 0 0 0 0 0 0-6 0 a a USSR/ketals - Electron microscopy Noy 50 "Investigation of Metal Powders With the Aid of Electron Microscope," 1. S. Brokhin, L. M. Bursuk, All-Union Sci Res Inst Hard Alloys "Zavod Lab" No 11, PP 1331-1335 Describes procedure, giving results for examn of various metal powders under electron microscope at 6,000-10,000 X magnification. Studied powders of wolfram and its carbide, nickel, and cobalt. Repro- ductions of several electron photomicrographs. i8m77 AUTHORS: Brokhinp 1.3.9 Funksp V*F- 131-12-7/9 TITLE: Obtaining and Investigating' Certain Properties of Ceramics From Silicon Nitride (Poluoheniye i issledovaniye nekotor7kh evoystv keramiki iz nitrida krorniya) PERIODICAL: OgneuPorY, 1957, Nr 12, pp. 562-566 (USSR) ABSTRACT: According to published data the silicon-nitrogen system has three phases: SL3 N4P S'2N and SIN, where the phase S3N4with 39-.5% nitrogen is chemizi; the most stable aM the most important in practice. Further, the properties of Si N are described in detail as also the method by which it is obtained from silicon powder, the chemical composition of which is shown in table 1. Figure 1 shows the saturation ourves of silicon by nitrogen at various tempera- tures. Figure 2 shows the nitrogen content in silicon in dependence of the duration of nitration at 16000. Table 2 shows the influence exercised by an addition of silicon upon the sintering of the sili- con nitride ' hot pressings at 14000 and 800 ka/cm;e).-In table 3 the properties of test samples of silicon nitride are describea (Nitration temperature 15000). Also bending strength and the re- Card 1/2 sistance against oxidation were tested in dependence on temperature. 131-12-7/9 The Discovery and Investigation of Certain Properties of Ceramics From Silicon Nitride (See tables 4 and 5, as well as fig. 4). There are 5 figures, 5 tables, and 8 references, 2 of which are Slavic. ASSOCIATION: All-UnionScientifto Research Institute of Hard Alloys (VsesoYuznYY nauchno-is sled ovatell skiy institut tveAykh splavow) AVAILABLE- Library of Congress Card 2/2 nR A I -R, M I-V 1W L. X=. vo 31 ~M j ry - 15 .7 `17 a~i ,c Win rg f, ~, .. F :j I. 7... ... I . I I I A I "I - L. 'i I :! WPM T- !77 'a7 77, As, 6r fr s gam;- 3'n'- 7A0 ;~~- RN , 2, a-alwq iV AUTHORS: Brokhin, 1. S., Funke, V. F. 78-3-4-2/38 TITLE: Investigation of the Solubility and Phase Composition in the System Silicon-Carbon (Isaledovaniye rastvorimosti i fazovogo sostava v sisteme kremniy-uglerod) PERIODICAL: Zhurnal Neorganicheskoy Xhimii, 1958, Vol* 39 Nr 4v PP, 647- -853 (USSR) ABSTRACT; The solubility of carbon in silicon, the phase composition and the structure of silicon-carbon alloys as well as the problem of the dissociation of silicon carbide in vacuum at higher temperatures were investigated. The investigation of the phase diagram in the system Si-C was carried out in three parts: l.-Determination of the solubility of carbon in silicon; 2.-Determination of the phase composition in the range Si-SiC; 3.-Explanation of the formation of the SiC phase. For the investigation of the phase composition and the structure of the alloys metallographic and x-ray structural analyses as well as the determination of microhardness were carried out. The metallographic investigations showed that the alloys Card 1/2 consist of one phase up to 0,7% C. Investigation of the Solubility and Phase Composition in the 78-3-4-2/38 System Silicon-Carbon The alloys containing more than 0,8% C consist of two phases: solid solution C in Si (light field) and silicon carbide (dark field). In the thermal treatment of silicon carbide in vacuum at 2000- -21000C a complete dissociation of silicon carbide occurs with Si evaporating and C forming a graphite residue. The graphite lines were proved by the x-ray structure analyses. No solubility of Si was found in silicon carbide. There are 14 figures, 3 tables, and 5 references, 2 of which are Soviet. ASSOCIATION: Vsesoyuznvy nauchno-issledovs+ellskiy institut tverdykh splavov, Moskva (Moscow, All-union Scientific Institute for Hard Alloys) Card 2/2 AUTHORS: Smiryagin, A. p., Potemkin, A. Ya., 78-3-4-3/38 Martynyuk, R. P. TITLE: Investigation of the Phase Diagram Nickel-Molybdenum-Chromium (Issledovaniye diagrammy sostoyaniya nikel!-molibden-khrom) FERIODICALz Zhurnal Neorganicheskoy Khimii, 1958, Vol. 3, Nr 4, pp. 853-859 (USSR) ABSTRACT: The nickel corner iri the phase diagram of the system Ni-Mo-Cr (UP to 40% molybdenum and up to 40% chromium) was investigated using the thermal and microscopic analysis. Eight polythermal sections of the nickel corner in the phase diagram nickel-molybdenilm-chromium were constructed. The phase composition and the hardness of the alloys were investigated at temperatures of 12700, 12000, 9500, 8000 and 7000C. The saturation limit of the ternary solid solution o-' the basis of nickel was determined at temperatures of 700 0, 8000, 9500 and 10000C. It was shown that with a drop of temperature the solubility of molybdenum and chromium in nickel decreases markedly. Also the sectional diagrams with a constant content of Card 1/2 4%, 8,5%, 3,5% and 20% of chromium were constructed. AUTHORS:-Ilr-~~7. ~., Zolotarev, I.S. and Baranov, A.I. Z~TLE: Some Pi-o-,)erties of Molybdenum Disiliuide (Ne'---Gtoryye svovstva distilitsida mollbdena) V PERIODICAL; Ts,,otnyye 11etally, 1958, Nr 9, pp 61-67 (USSR) ABSTRACT: Molybklontuii disilicide has good resist tance to s-aling at te,niperatures up to 17000C combined with other useful propcrties (e.g. metallic alecbrical conductivity) and the study of this compound has been )roceeding in recent years (Refs 3-7). The authors describe their investiga- tion of the high-teweratura mochanical )roporties of tho c:om~)ound and of a preparation with an excess of silicon. The disilicide was prepared by sinterinq at 1100-12000C fron ITYdrogen reduced molybdenun, (0.0051.' Fe7 0.0021% Ni, 0-03/c~ 0, rest Mo) and grade Kr-O silicon (99A' Si) furtner C. 'jurified by acid treatment and the blanks obtained (Table 2) were -round and made into 6 x 6 x 60 mm pieces 0 (Table 3) by sintering under pressure at I' 0--15500C. '50 Frai,,i these the test picoos wore pra,-)ared. Tile chemical nat'.ure of s7)ecimiens obtained -vias confirmed by X-ray and 1/2 uhem.-Ica-1 analysis and by determinations of micro-hardness )P' -ties of Idolybdenum Disilicide and resistance to scali&,-. The hai-dness has been determined up to 1 000 0 (FiLure 2) an' the Liicro- hardness and scaling resistance (1 200 0C). Tests on specimens vith 3, 5 and 10'~'~ excesc Si shov:ed that 51/0' excess Si is beneficial. Long-term bendin:7- tuests were carried out in a special installation (Fiz,,ure 3) to determine the plastic deformation of 1.1oSJ_2 and MoSi 2 x 2 x 5116 S-i at 1 200 OC with relatively small (up to 20 kg/mr, stresses. Tensile strengths in bending i-re also determined at 20, 1 000, 1 100 and 1 200' 6C. There are 4 figures, 4 tables and 8 refcrenccs, 1 of which is Soviet, 3 German, 3 English and 1 Czech. ASSOCIATION: VNIITS Card 2/2 -1. Molybdenum silicides--Properties 2. Molybdenum silicides --Temperature factors 3. Molybdenum silicides--Mechanical proper- ties 4. Molybdenum silicides--.Test results SOV/136-59-3-14/21 SUTHORS: Brokhin,_I-S-, 011khov, I.I. TITLE: The Scale-stability of Cermet Alloys Based on Titanium Carbide (Okalinostoykost' metallokeramicheskikh splavov na osnove karbida titana) PERIODICAL: Tsvetnyye Metally, 1959, Nr 3, pp 61 - 66 (USSR) ABSTRACT: The initial materials were titanium dioxide, niob-ium pentoxide, powdered niobium (containing 1-3% tantalum.), tungsten carbide, lamp-black and powdered cobalt reduced from its oxalate. Alloys were prepared by mixing for 24 hours and then heating in a hydrogen atmosphere in an electric furnace. X-ray analysis of the specimens prepared from individual carbides of titanium and nilob.ium. qhov,,,ed the Iines correspond'ng to the two carbides (TiC - 4.32 BbC - 4.46 1), whereas the alloy c,:intaining 87% TiC and 130,16 NbC shQwed only one phase with lattics parameter 4.37 � 0.03 A' (TiC-NbC solid solution). The microhardness of niobium carbide and of the complex titanium-niobium carbide was shown to be 1 822 and 2 -"72 k6/mm~. All the samples of titanium-tungsten carbide were single-phased with a crystal lattice of TiC. The Cardl/4 powdered carbides were mixed with cobalt by wet grinding SOV136-59-3-14/21 The Scale-Btability of Cermet AlloyB BaBed on Titanium Carbide for five days, pressed wit a stress of 1 000 kg/cm 2 and sintered at 1 450 - 1 560 0 in hydrogen. Figures I and 2 show typical microstructures of TiC-NbC-Co ando TiC-WC-Co. The alloys were tested at 900-1 200 C for 100 hours, the gain in weight and the thickness of oxide layer being noted. Diagram 3 shows that with increase of NbC in TiC-NbC-Co alloys there is a sharp decrease in weight gain from 5-1 &12 per hour. With further increase in NbC the weight gain is practically constant. Figure 4 shows the weight gain of alloys containing 25016 Co and 3-15PIo NbC. The scale- stability is a maximim with 15016 ITDC at all temperatures. Further increase of NbC to 25~o' has no further effect. Varying the cobalt content showed that the weight gain was a minimum at 25% Co. S-Decimens prepared from simple carbides gave similar results -',-a those prepared from complex carbides but in all cases the formsr had a greater weig4t gain than the latter. At 1 000 0 the surface has/grey coloBr due to breaking up of the ecale and at 1 100 - 1 200 C there is a thicker layer on the Ca.rd2/4 surface. The TiC-WC--Cc. alloys were prepared from the SOV/136-;9-3-14Z2! The Scale-stability of Cermet Alloys Based on Titanium Cp-6bide complex carbides. Figure 5 shows the weight gain of alloys Sontaining 15 and 3001o WC both with 18 wt.% cobalt. At 900 C, the weight gain is practically the same for both alloys but at higher temperatures the 30% WC allOY has a lower weight gain. The effect of Co content is shown in Figure 6 (the ratio TiC:WC is 65:35). With increase from 10 to 20016 Co there is an increase in oxidation resistance whah is more marked at higher temperatures. With alloys with TiC:WC ratio of 85:15 the effect of Co increa8e is less marked. At temperatures higher than. 1 100 C all the alloys oxidise rapidly. In 'both TiC-ITbC and TiC-WC alloys oxidation spreads in the first instance along the cementing phase. The TLC-NbC-WC-Co alloy containing 10-15% NbC has better scale stability thaa TiC-WC-Co alloys but not as good as TiC-RbC-CS alloys. The TiC-15NbC-25Co alloy is suitable up to 1 100 C and the TiC-30WC-15-2OCo up to 900 C. Card3/4 SOV/136-59-3-14/21 The Scale-stability of Cermet Alloys Based on Titanium Carbide There are 7 figures, 1 table and 13 references, 8 of which are English and 5 German. ASSOCIATION: VNIITS Card 4/4 1~5.2210, 15.2220, 18.8200 AUTHORSz Brolthi _,I.A,,-~ 01~khfiv-. I.I. ztj,,-i 1 1T.,T-v- A d. TITLE-. ~jecjlanical I-Iropert-Les ot Ccv,iw~~ Hard Alloys at Elevai,~.-d PERIODICAL: Tsvetnyye metall-,. 195,) ABSTRACT7 One of the ne-w application ill the manitiac-(kirt, dies and other woar-resist.,W- material based oii ~-;ititerit-J -i1!! Moscow Hard Metals Combiiie 1:!I,iZ This product, structure (avera_c (spec if ic gravi t y 9 grade a-allimina w-L th a sma I L by sintering at apj~roximatclv j-', j~; ]-I Ik I Li~ ~-l I-rri C sintering amounts to 18 to -:W~,, l -, Obji--~'L Q C I 111,~ investigat�oji described -iii e I w a - -, 0 measure hardness, trailsvej~.~, .-21 Y t i 'UT 6 compreassive sti-ength of T5,N i i-- , It- t ;-i i nothf.,r v~t!ar- resistant materiaLs both .-i Hardness measurewcllt!~ werc Card 1/7 diamond iudentej J - 65696 SOV/136-59-10-13/i8 Mechanical Properties of Ceramic Tool Materials and Hard Alloys at Elevated Temperatures pieces 15 nim diameter and 5 mm high. The specimens were held at the test temperature for 20 min before applying the load of 30 see duration; not less than six measurements were taken at each temperature, each new test temperature being attained by cooling. After cooling to room temperature, the specimens were photographed (x 420), the diagonals of the indentation were measured and the VPN values were found from the tables. The results are reproduced in the form of an Hv(kg/mm2) versus WC) curve in Fig la (curve 3) where, for comparison, the results obtained by other workers are also shown: curve 10 based on the measurements of Betaneli (Ref 5), who used a 250 kg load, and curve 2, based on data due to Kazakov (Ref 6), who used a 1 kg load. It will be seen that hardness of TsMA-332 decreases monotonically and linearly with rising temperature from about 1800 VPN at room temperature to about 600 at 10000C and to 350 at 1100%, Fig la shows photographs of the diamond pyramid indentations made on TsM-332 specimens Card 2/7 under the following conditions of loading and temperature: 65696 SOV/136-59-10-13/18 Mechanical Properties of Ceramic Tool Materials and Hard Alloys at Elevated Temperatures 1 to 5 kg, 200C (H. equal 1800 k-/mm2); 2 to 1 kgj (H equal 960 kg/mm2) - 700*C v . 3 to 1 kg, 1000*C (Hv equal 540 kg/mm2). Hair cracks (originating at the corners of the indentations), visible clearly oil these photographs, occurred even when the hardness measurement was taken at the highest test temperature! ' they were even more pronounced when a Rockwell machine (scale A, load 60 kg) was used (see Fig 3). No cracks were observed on specimens used for microhardness measurements (load 100 g) at room temperatures which gave values of Hv equal 1900 to 2000 kg/nut12. In the next stage of the investigation, hardness of tile folloi,7ing hard alloys was measured: (a) standard titanium-tungsten alloys T5K10, T14K8, T15K6, T30K4 and T5K6; (b) new types of tungsten- cobalt alloys (VK6VT VK8V-. VK15V) characterized by high strength and coarsely-crystalline structure (average grain size of tile WC Olase -- 3 to 5 VO made by the method developed by VNIITS and based on tungsten obtained by .reduction at 1200OC; (c) alloy vK6m, characterized by Card 3/7 improved trear resistance and finely crystalline structure 110 65696 SOV/136-59-10-13/18 Mechanical Properties of Ceramic Tool Materials and Hard Alloys at Elevated Temperatures (average WC grain size of approximately 1 ji) and made by a process involving intensified wet grinding of the powder mixture. The results of these measurements (load 1 kg, loading time - 30 sec) are reproduced in Table 1 (for the titanium-tungsten alloys) and Table 2 (for the tungsten-cobalt alloys) in which the test temperature (OC) is given in the first columns. Curves plotted in Fig lb show the temperature dependence of Hv for the following alloys: 1 - T30K4; 2 - T15K6; 3 - T14K8; 4 - T5K10. The same relationship for the tungsten-cobalt alloys is illustrated by curves plotted in Fig 1B: 1 - VK6M; 2 - VK6V; 3 - VK8v; 4 - VK15V; 5 - (for comparison) TsM-332. Photographs of diamond pyramid indentations obtained on T5K10 specimens at (1) - 20, (2) - 600 and (3) - 10000C (corresponding to Hv values of 1650, 850 and 260 respectively) are reproduced in Fig 2b; finally, similar photographs for VK8V specimens at 200, 600 and 1000*C (the corresponding Hv values being 1500, 650 and 200) are shown in Fig 2B (1, 2 and 3 Card 4/7 respectively). In the next series of experiments, the 65696 SOV/136-59-10-13/18 Mechanical Properties of Ceramic Tool Materials and Hard Alloys at Elevated Temperatures transverse rupture stress, cIA3Z. , of the investigated materials was determined at temperatures up to 12000C, a universal testing machine P5, equipped with a silit heating device, was used for this purpose. The test pieces, measuring 5 x 5 x 40 aim, resting on prismatic supports made of heat-resisting material, were maintained at the test temperature for 5 to 7 min before the load was applied at a strain rate of 11 nun/min. The results for the TsM-332 specimens are given in Table 3 under the following headings: test temperature, *C; kg/mm2. a IA31, I number of tested specimens; scatter of results, Yo. The data given in Table 3 are also reproduced graphically in rig 4. The temperature dependence Of OiOr of VK and TK alloys, is illustrated in Fig 5a and 5b respectively. Flat, radiused test pieces were used for the determination of the UTS of the investigated materials. (Tested TsM-332 specimens are shown in Fig Q A standard tensile testing machine,or a specially adapted creep testing apparatus, was employed for this purpose, a gradual application of Card 5/7 the "dead weight" load being attained by the use of copper 65696 SOV/136-59-10-13/18 Mechanical Properties of Ceramic Tool Materials and Hard Alloys at Elevated Temperatures granules; particular care was taken to ensure axial loading of the brittle specimens and the results of any test, in which fracture of the test piece occurred at a distance of more than 5 mm from its centre, were ignored. UTS of TsM-332 determined in this manner was 15 to 16 kg/mm2. In the final series of experiments, the compressive strength of TBM-332 was determined on cylindrical specimens (10 mm diameter and 15 mm thick), tested on a 30 t hydraulic machine equipped with hard alloy supports. 90 Specimens, taken from two batches of TsM-332, were tested; the scatter of the results amounted to 20%. The average values of the compressive strengths equal to 80 to go kg/mm2, were much lower than those obtained by other workers. In the conclusions, it is claimed that the results of the present investigation are more accurate,than those quoted in the literature. Attention is drawn to the fact that hardness of the VIK6M alloy decreases with rising temperature at a rate much slower than that of other investigated materials (Hv of Card 6/7 this alloy being 1400 kg/mm2 at 6000C and that both 65696 SOV/136-59-10-13/18 Mechanical Properties of Ceramic Tool Materials and Hard Alloys at Elevated Temperatures hardness and UTS of at 12000C are higher the ceramic inaterial based on A1203 than those of other waterials. 3 tables and 10 references, 8 of There are 6 figures, which are Soviet and ASSOCIATION:VNIITS 2 German. Card 7/7 S/736/601000/002/002/007 AUTHORS: Brokhin.I.S.. Zolotarev,I.S.. Baranov.A.I. TIT LE: The making and investigation of the properties of Mo disilicide. SOURCE: Vsesoyuznyy nauchno-issledovatel'skiy institut tverdykh splavov. Sbornik trudov. no. 2. Moscow, 1960. Tverdyye splavy. pp. 24-36. TEXT: Mo disilicide has recently gained in interest because of its exceptionally high scale- resistance up to 1700oC, especially in the making of heating elements for resistance-type electric furnaces. Three Mo-Si compounds are known to exist: M03Si, M03S'z, and MoSi?. R. Kieffer Is and E. Cerwenka's phase diagram (Zs. f. Metallkunde, v. 43'. no. 4. 1952) is used. Si solubility in Mo at 12000 is 0. 15% and at 14000 0.8% Si. The types of crystalline lattice, densitiess m. p. 'at and micro- hardnesses (100-g load) of the three compounds are tabulated'MoSi2 is a metallic conductor of electricity (21 [Lohm/cm) and is the most highly Cale-resistant Mo-Si compound, owing to the formation on it of a dense and strong vitreous SiO2film, 0. 03 to 0. 1 mm thick. Oxidation at 1350-14000C is most effective. Above 17000 the SiOz film melts, coagulates in droplets, and loses its protective properties. The oxidation mechanism of Mo disilicide changes abruptly at 450-600" at which point a rapid intercrystalline corrosional disintegration takes place. Whereas in- candescence at 1200- 15000 over thousands of hours does not produce either an increase or a loss in weight, 30-50 hours oxidation at 5000 will redu.ce the disilicide Card 1/3 The-making and investigation of the properties ... S/736/60/000/002/002/.007 to powder (except under a shielding atmosphere). Mo disilicide is termed brittle 2 and of medium hardness. Compressive strength at -room temperature is 70 kg/mn-i bending strength at 12000 is 37 kg/mm2; 100-hour strength at I 1000C is 6. 3 kg/mm Z (all three values0from Western sources). It is high-temperature plastic; creep strength at 1000 is termed unsatisfactory. If Mo disilicide is to be employed, e.g., irl will enhance its ,gas-turbine parts, cementing substances must be found that toughness and strength. Unfortunately, attempts to produce sintered combinations of MoSi2 with various metals have not been successful. The MoSiZ for the subject experiments (work done in 1952-3) was made of powdered Mo (grains up to 311) with 0.00576 Fe. 0.00216 Ni, 0.03% 0 . and of thoroughly ground Si (2 ~L) with 0.087o Al, 0.037o Ga, 0.015% Mg, 0.015% ie. The two powders, taken in stoichiometric ratio (63.147o Mo, 36.8676 Si),were thoroughly mixed in alcohol for 48 hours. Cylindrical specimens 50x25 mm were sintered from this mixture at 1100-12000 (3- 1 min hold- ing). The special graphite pressing dies were compressed at 150 kg/cm - The Mosiz formation is fast and complete; the fracture of the specimen is steel-gray in color with a metallic gloss. The specimen surface forms a thin carbide crust in contact with the graphite. The results of three chemical analyses are tabulated. The MoSi2 was once more nd to a fine powder (grain size 2 ~L) and subjected to 00 a second s"intering at 1500!lr5o5u int3 6xbx6o-mm rectangular rods. The unit weight increased to 6.11-6.13 g/cm owing to reduced porosity. X-ray analysis reveals only a single pha6e with tetragonal lattice; parameters: a = 3.2 9 and c = 7. 86 Card Z/3 Mosi 1"I V va t if, !;l. 1"tat ~vc-~",~, it ~'. . 'J ~. I p _7 "' % ~ p ~. ~~ 3 Sbc, y 1;) v ~ Y" TEX:i.'-. i a !aljuratovy 1 0% ~ 1) , . " T, ~,j in - f;,lrength tc ~4.s -n a large nitmlo~! of specilylenb tilf: sov:- Y!"U, 9 oxide ceraraic lJased cjn sintered 1~0 "ll-lineraloceraillic whic h w e r e r a t 6 e v c- (1 pr. d a t t hos c ov. In s t i tu t ~- !) f C h e i nic a 1 Thvc)'~- gii i D. 1. h-,.-_;w proJuced _;T,.dk:-,-;aL!v by "iv_ Allo,r Pavlushl~i_-i, N.M. i Ilna:,;~-,!,~-, 3 1%4~-t a;; u 0 fiat p c J.,'! i U60 I n s,z I "I I r, r1t: s in t t. T t c 1-1 t o. 5:,lOv.-n. The 3 .9 T)r e r4,- r f f. 1-j C a n d'b e n 6; n C; a r d I / 4 . -- 11 r) C, S SC)nl;- te it 1 r -un s d I T!'~! aoil a sj)~! -':ij t e W, ern, indentc3-s a 11 A -1 1111 ri i: i i T e ti tit)ad 103d(, Oil I 'N iiz,'hed Sr)CC',Mt'; TI ind wure tested at ezich temperaturc up Lo I I (101~' with indt-I-)tations per specirntt:.,~ Temperatu:-!,~ soaking: 20 min; indenLatioll 7-1-fj(~ Ujj(; e- r load: 30 sec. Tests werf~ performed during temperature reducL~wl. Afte- coo,.n~; ~~ V1 In e and the ludentation diagona.~-' to ruc;in -12~0% e ad wLi-e ri;easured. fo~.- til,- 11Y A nearly 4,traight line (if Vickers harci- n e s s v 9 . t -_,xi in e ri to r e-~ i, in v f'r- o n 1 14 13 0 0 kg / n i rn ~ a t0 C)C t o H = 3 6 0 k a V rnipzred to referenced Ldata by Betancli a' W, "I'las Ali'T(l .:'il' Sov I r, e. K rtzveal thin branching 'is!~ures at the c, t)f tile il6~_Catijlg brittlenesr, 11-1) to the highest h-st tuiliperaikires, Rok", n Iens ret3aited. s_n ever- niore pro- 'Vell te'~ts (scale A, ad 0 1 g) ( ~he sarne specin notinced radial ~_racl,s, Microhardneso .ests of the TsM-332 ceram;'c oil the RMT-3 (PMT-3) instruinent jj, -ooin teinpwrauir,',~ an(~ with a 100-g load yielded a hardness of 1900-2000 ~- cr/rrirr.'~' i.e., loo-no " " n_~ higher than the HV, and xthout evi- dence of corn~'~. -.-.-iicrofissures iv. the indentations. High- te ni tt-sts vere perforri(_~d an 5x5x40-in-ii rl-pecirriens or, tive unive--sal P-5 (Fk- rn-tchini- with a simpli-, --esting spLn of _~10 rnirt. As in all tests of hrit!ie riLit"erld". trie data Card _- 14 Sol) scatter iF randont-t-- or di.Mr:~~ -.-1jojj, the ti at aare an.:il~zed by tl~v statistIcs. The beading strenFth wa.9 determined from the batches of 9-pe.---imeng. Resultr- are tzkilated and graphically Portrayf".i; n.- straight- I'Mr, vitr-iation goes fron-l 3--, k hnm at ZOIC to 28.7 kgi`inn-~" al, 8 ' U, O'D C followc-d by a curve through ?3.6 kgin .1 at 10000 and B.5 kghiim ZLt !21DOO, V.-I a scatter of from ---'0 to 900', r~sitng to 17. 3/o at 17-001- B. P. prih-ylov repor-L, P - - -th Prihvlc)-, 'hard alloys 8 kg/M17I, 0 0 c3,A a-isor- s data on BY, (VK) anj i7i-:11 LverdyMi splavov - The mechanical .141-a Dzerzhinskogo,.. Pr I' C1 It., 70,1, f5 - lz d: .D o n_nzhenera (~J~jj, 1955) il,,-trd 1-I'loys are Mronger at roorn temperature, the r-erarnic lwl~ strt-ligth n;orc sloxiv vvith rising temperature$ especially beyoncl 700-8000; so that beyon-d l2c)ooc. th~e strength of TsM-332 exceeds that of the pla-qt;- defor~--,,able hArd allov-s. '.Vension tests of plane, svi-nmetricaNy (concavely cL1r,,;'11;n--af,1,,,) tipe,-,-fj c-nr, ,,ncountered difficulties attributabie to ir-ezu~a- -lerl Iry somewhat uncertain; P-3 C In geoinel. to lz~-16 --nin dia- ard c-lindr~'-al nip-,!ci-nens w"h haiA-al~~)y suppo- nzL..,- 1, cornpenetrat-Lc~n and f7- (-Ai,~,nal L:Cittt.~r: 20%. Mean comprcss;,.,~~ st.,eng - gtl Gpr-1: 3/4 /"0 "000 1002 / 0 p ~-'~Pe rties 8 0 1repc'rLetl in the litc~r--, 1, z, r d r ,fl oii the are coxnparrd with Oi Btand;--' -.W al I E, T 5K L '-J, T II 4K8 ; T 1 5K 6 ~ T 3 'he Y, ew 'N Iloy's Br~,6; and BK 1 5B (V 1; 1 W" %k ith la i ge-gr4in ini ro- ?truciur': FlZ-,2 3-5 ji), and the NKOM) extrafine-gf-'I'.!~ alloy (WC-ph.~~i !L) pi-cpared hN wct grinding. Data on a~'. of the test., a-t, tabuLttr-d an(: ~,raphed. The HV of all alloys decreases to 250-101') kg/-Yim2 at 1000"C. TJG an,~ alloys have substantially paT-allel curves; HV in- crtase:-, wi~!i ;ncreat,itw' Ti~~ -,.nd Go. in the WCo alloys a similar effect of Co is uer'.Ie~ll for nn!-~ alloy, BK15 (VK15). The fine-grain alloy BKbM (VY-fjhl~), has nnort: uh--How in HV up to 600 0 thau the analogous coarse- gra-n alloy BK6B ;'j" at higher temperatures the decrease is so steep that the HV at I, alloys. Dian-;ond-pyrarni~ indentations ii. the TK (TK) and BK(""I,'J alloy.~ -e tif Jissurat;on :!;j the their rnicrc;- brittleness .`~; -iign~fican'lv 'Ll". it that of TBM-33Z. Ln suniniary: At the highest terii.-F-xatu~-(ta t~-.tzf.-d tl-~e St-rvngth and hardncs~ -~f sirtered Al-oxide cerarnics was found to L%,-- grca't~ r tha n -~I' sintered n,.-~tallic. ci al loys. This advantage, C 'Ii it 7 1 h-owever, --,t 'h,-- c,-' an increascd micru- - -e~ ess. There are 15; Russian-langung--- Soviet, I Russian-lanouLgt- T; u r e S zill -iarslat:loi, the Gi-~-iijan L );I, -,)n hard alloys by R. Kil-If'rel' and P. Schwarzkopf, arid 3 A.S'SOG)A'J'Tf--~,-~J: Nione given. Card 4/4 S/736/60/000/0021006/007. AUTHORS: k4in ~Z,, Ollkhov. I.I., Ashmarin,G.M., Barano~#A.L, 15latov, A - B Ri pkin, V. P. TITLE: The high-temperature of sintered titanium -carbide hard alloys. SOURCE: Vaesoyuznyy nauchno-issledovatellskiy inatitut t 'verdykh splavov. Sbornik trudov. no. 2. Moscow, 1960. Tverdyye splavy. pp. 135-147. TEXT: , Following a review of recent Western progress in the manufacture of heterogeneous carbide alloys ain.tered with Cot Ni. Ni-Cr, and other cementing binders, and more especially the.Austrlan WZ and the U.S. "Kanthanium" alloy (cf. Harwood, //no initialal, Maiterials and Methods., v. 36, no. Z, 195Z), with refer- ence to the manufacture of gas-tu.rbirAe blades,'the brittleness and thermal-shock sensitivity of such alloys is criticized. The authors experi .mented with sintered. TiG-NbC and TiC-WC alloys cemented with re. Co powder from 1950 through 195i. PU Short-term and' 100-hour strength tests were'made'at *room temperature and'tempe-. ratures up to lZ000C. For details on the source mateiialp, cf. the'paper by I. S, Brokhin and I.I.Ollkhov on P-.148 of this compendium -(Abstract S/736/60/000/002/ 007/007); the compound carbides were obtained by the calcining of a mixture of finely-ground powders of the simple carbides at ZOOO-22000. Test ipecimens com-. prise (a) TiC-NbC-Co with 3 to 30% NbG and 10 to 40% Co, and (b) TiG-Wc-co' w 'ith 15 to 35% WC and 10 to 25% Co. -Ben' ling- st reingth test specimens were, Card 1/3 The high-temperature strength...*.. S/736/60/000/OOZ/006/007. 0 prismatic', 5x5x40 and 6x6x50 mm. Tests up to 1000 C were made on a special Silit-re~istor heated accessory (cross-section shown) installed on the P-5 (R-5) universal testing inachine. The -specimen was supported as a simple beam on hard- alloy or sintered aluminu m*-oxide supports with a 30-mm span and was subjected to a ball-centered load advancing at a rate of 11 mm/min. A PtRh-Pt contact thermo- couple meas"ured the.ternper;itura; mean results were --taken from no less than 15 spe6im'pns. The tensile- strength test'specimens had the shape proposed by Prof. ..S. V. SUrensen (Ruvaian trans lite rAtion' "Sorenv;sn"); they were UO mm long. 7 mm 6.2 mm thick, 21.2 mm wide at the ends. and had a ZOO inward straight taper for Z from the ends and a R= 194..S.-mm circular fairing between the tapers to arrive at a 2 neck section at the cente r. Precise dimensions were obtained by 40 to 45 mm e boion-carbide rubbing of the sintered specimens. Only the central 20 mm of each specimen- were brought to the test temperature (15-20 min heating, 20-min holdiner), ..while. the asbestos-padded hinge-dlamped ends remained outside the furnace. During the IZOOO tests, the upper end did not exceed 800-900'. the lower end 700-8000. Tests in which rupture occurred 6utside of + 5 mm from the midpoint of the speci-- men were not included in the evaluatio- - A structural cross-section and a general- view photograph of t~e testing machine, the TM-1350 (PI-1350) tubular Ptheater (manufactured by the "Platinopribor" factory), and its installation on the JICT- 5000 (DST-5000) creep tester are showrv. Roorn-temperature tension-data sc atter was IZ:-*15%, as against 10-lZI74 at high temperature. The bending-data scatte-r-was--- -Card 2/3 'The high-temperat.ure strength. . S/736160/000/0&/006/007 10-12%,and 7-10%, respectively. TiC-NbC-CoIalloys: 10- 157o NIbC increases the scale resistance of TiC alloys by some 150-Z oC -.but engenders some loss in strength. In TiC-NbC-Co alloys a Co content from 10- 407o was tested (with 10- 1570 NbC); Maxi- 3purn s.trength in beading occurred at 25-30% Co. Tests with a 25loCo content and 3 to 3016 NbC contents showed a nearly constant bending strength (-90kg/mrn,2) up to 12-13%NbC. followed by a significant drop-off at NbC contents up to 20%. The bend- S strength of an alloy with 150j'o NbC and 2516 Co (optimal scale resistance) increased i ng steadily' from 80 jo 90 kg /rnmz from 20 to 7000 (aitributed to. plasticity), then drop- ped to 65 kg/mm at 10000. The tensile stren th of the same alloy decreases in a straight line from 34 kg/mM2 at 9500 to 13 kg'7gm? at IZOOO. 100-hour tests indi- .cate that*the alloy retains high-teinperature strength only up to 10000. TiC-WC-Co anoys: The'scale resistance -of the W-cointaining alloys is lower than tha-F_oflt'~e _Nb- 7o-ntaining alloys. Variatidns in WC content from 15 to 307o and in Go from 10 to 23% do not affect the strength of the TiC-based alloyd appreciably. The ai~-vs.-T curves of the 107oCo and the 25/oCo alloys cross over at 8000and-80 kg/mmZ, and at higher T up to 10000 the 10% Go alloy is Istron'ger than the 25% Go alloy. The tensile strength of the 3AWC, 157*Co. 559'oTiC alloy descends linearly from 40 kg/r.ImZ at 9500 to 12 kg /mm2. at 12000. 1 1 00-hr. te n*s-;Ie tests indicate a high-T st ength limit of only 90100. SummaEr. TiC-WC-Co'alloys are stronger (E=38-40 - 105 kg/mm2) but less high-T resistant (Tmax-/100 hr= 9000C) than TiC -NbC-Co (E= 3 0.5- 31.5 - 103 kg /mmZ; Tmae 10000)-. There are 13 figures and 7 refs. (3 gnglish- language. and 4 German) Card 3/3 ASSOCIATION: None i given. AUTHORS: TITLE: 3 6 7 5 15 S/08 62/000/001/032/067 B 151 YB1 01 Brokhin, I. S., Ollkhov, I. I. Scale stability of metalceramio:solid alloys based on titanium carbide PERIODICAL: Referativnyy zhurnal. Khimiya, no. 1, 1962, 3o6, abstract 11182 (Sb. tr. Vaes. n.-i. in4t tverdykh splavov, no. 2, 1960,148-157) TEXT: A study of the scale-stability of 3 seriesc.,df experimental metal ceramic solid alloys based on TiC at temperatures up to 12001C has shown that in the TiC-NbC~-Co series the optimum effect is given by an alloy containing 15% NbC and 25% Co, the rest of the alloy being TiC. Its scale-stability is considered to be satisfactory at temperatures up to 11000C. Among the TiC-WC-Co alloys the beat is one containing 30.,4 WC; 15 - 20~6 Co, the rest being TiC,.. The scale-stability of this alloy is considered to be satisfactory up to 9000C. [Abstracter's note: Complete translation-i X Card 1/1 b~362 1100A 19, 61 oo S/136/60/000/04/017/025 E091/E235 AUTHORS: 32okhin, I. S., Ollk-hoov, I. I., Ashma in, G.-M., Baran atov. A. B., and Repkin, V. P, TITLE: Heat Resjstanc,~~of Titanium Carbide:_j~ase Cermets~p PERIODICAL: Tsvetnyye metally, 1960, Nr 4, pp 67-?0 (USSR) ABSTRACT: In this paper, the results of an investigation of the refractoriness of Ti-Nby'~and Ti-WAbase alloys produced by p2wder metallurgy,gle-thods (carbide solid solutions) with Co as binder are reported, The influence of the NbC,, WC and the binding metal on the mechanical properties of TIC alloys has been studied at room temperature and at elevated temperatures in short-term and long-term tests. The experimental alloys were made by methods generally used for the manufacture of titanium carbides. The complex carbides TiC-WC, TiC-NbC and pure powdered cobalt were used as the starting materials. The complex carbides were prepared by water quenching a mixture of fine powders of the respective simple carbides from 2000 to 22000C. In the TiC-Nb-Co alloys, the NbC content was varied from 0 to 25% and the Co content from 5 to 40% (remainder TiC), and in the TiC-WC-Co alloys, Card 1/5 the WC content was varied from 15 to 35~6 and the Co 69382 S/136/60/000/04/017/025 E091/E235 Heat Resistance of Titanium Carbide-Base Cermets content from 10 to 25%. The elastic limit in bending was determined for prismatic specimens, 5 x 5 x 40 and 6 x 6 x 50 mm. Bend testing at high temperatures was carried out in a specially constructed device with a silicon carbide heater which was attached to an R-5 universal testing machine. The specimen was placed on supports made of a heat resisting carbide and fractured with a concentrated load; the distance between the supports was 30 mm. and the speed of loading was 11 mm/minute. The temperature was measured by a Pt/Pt-Rh thermocouple, the junction of which was in direct contact with the specimen. For the determination of the UTS in tension and the long term refractoriness, flat radiused specimens, as proposed by S. V. Serensen, were used. The main feature of the high--E-emperature testing of these specimens (Fig 1) is the fact that up to a given maximum temperatiire only the central "working" portion of the specimen is heated; the ends of the specimen which are fixed in grips are outside the hot Card 2/5 zone of the furnace. The temperature of the "cold" ends 69382 S/136/60/000/04/017/025 E,091/E235 Heat Resistance of Titanium Carbide-Base Cermets of the specimen does not exceed 800 to 9000C in the case of the upper, and 700 to 8000C in the case of the lower ends. The electric furnaces with a single piece tubular platinum heaterl type P-I-1350, enable lengthy tests to be carried out at temperatures of up to 13500C. The furnace is attached to the creep testing maching DST-5000, which has been specially reconstructed for testing cermet specimens and has been re-equipped with electrical Sear registration and regulation apparatus (potentiometers). Damping asbestos packing was inserted under the supporting surfaces of the side faces of the specimen adjoining the grips. The temperature was measured with the Pt/Pt-Rh thermocouple passing through an orifice in the solid platinum heater; the junction was placed within 0.5 to 1 mm of the central portion of the specimen. Short term tests to fracture at high temperatures were carried out with the same machines and attachments as the long term (100 hours) tests. Fio- 2 shows the UTS in bending of TiC-IIqbC-Co (10 to 15% NbC) alloys in relation to cobalt content (1 - at 200C; 2 - at 16000C). Fig 3 s"hows the Card 3/5 UTS in bending of TiC-NbC-Co (2501o Co) alloys in relation S/136/60/000/04/017/025 E091/E235 Heat Resistance of Titanium Carbide-Base Cermets to NbC content. Fig 4 shows the chanGe in UTS on straining a TiC-NbC-Co alloy in relation to temperature.FiG 5 shows the UTS in bending of TiC-WC-Co alloys containing 300/66 VIC at 10 and 23yo Co, in relation to temperature (I - 10% Co; 2 - 23% Co). Fig 6 shows the change in UTS in tension of a TiC-WC-Co alloy of the basic composition (65 : 35) + 1,CP/0' c0, in relation to temperature; Fit, 7 shows the limiting long-term (100 hours) refractoriness of a TiC-'WC-Co alloy of the original composition (1 - 950OC; 2 - 11000C). For the investigated cermets, the relationship Ob/ abending := 1 - 2 (approximately 5C%) is characteristic. The spec fic gravity of the TiC-NbC-Co alloys is 5.9 to 6.2 g/cm~ and that of the TiC-WC-Co alloys u is 6.5 to 7 g/cm3. For the determination of the modulus of elasticity of the experimental alloys, the angle of bend under various loads was measured directly and from that, the value of E was calculated by a well knoun formula. The specimens were plates 0.3 to 0.5 mm thick, made by compressing and sintering plates of 1 mm thickness and subsequently grinding with boron carbide. The tests Card 4/5 were carried out at room temperature in a device made 69382 S/136/60/000/04/017/025 E091/E235 Heat Resistance of Titanium Carbide-Base Cermets by B. I. Pribilov. The specimens were placed on refractory supports and loaded gradually with loads of 50 to 1000 g. The degree of bending was measured with a micrometer. For TiC-Nb~_Co alloys, E was found to be 30 500 Go 31 500 kg4mm , and for TiC-WC-Co alloys, 38 000 to 40 000 kg/mm'. There are 7 figures and 3 referencas, 2 of which are Soviet and 1 German. ASSOCIATION: VNI',-*TS Card 5/5 i 1 7 5 ITRCE: Porosh.!:ovava metallurgiya. no. 7, 1965., 34-40 -TOPIC TAGS: titanium nitride cerroet, molybdenum enTitaini riz c- c r T-n c t for Ow i~rcn, lor "11(, ~~f Uk ACCESSION Nil: AI'501,1,271 cont. Ang Ow minimuni az 'T! la"L' C "'d 2/22 - "A~ZI.L.~-~-.~~-1-,--i~~~.~~-,~ INIA-~d~~-ffl..;~-W~. 1 627107-65 J.- F'-atov, A. B. TITIZ A'203-MO and Zr02-1'10 cermets and their structure i4 ljq SOURCE: Foroshkovaya metallurgiya, no. 7, i965, 7h-79 ~-j vq ~ - ,TOPIC TAGS: cermet, molybdenum base cermet, disriersion strengthen-4. alloy, molyb.- denum, al-, 1 Dy, aiurLnu-m oxide containing alicy, -7 ,13 S T RJ. -e:-me'-S c-=~-~sed oC molybdeni=-and 5-70.r, -~11LI~--1:.-L;:. an b e T r od uc e d t- e r v h,~ t o omp a c t -in g a I -. 7 0 0 rl C ccld commas-' '-rq~ under !-';-~-121, dan/cm' p-ressure, fcllow~---! fii-s-~ al, a- 1700-C. The ,I S t ff 7* z on 1: 1-- ;--rain s i z e f comDoren'tc; in 1, e S 'r- in e r -i s ei me n s ~hal Wp 1 ~he -2, -~,nt en r . Jrip- ai-~. ?ias: i-, ,Card L- 62707m~6615 ;-ACCESSION AT5018276'- ASSOCIA77LON: Vse-~oyuzny-y nauchjo-issledovatel'skiy institut tverdy~r.'n, S-plavov, Moscow (All-Union Scientific Research Institute of Hard Allovs) S, U--- Na- D : 15,- un '_" 14 nO REF SOV: 002 L-N CL : DO =R : 006 F : 4C,64 :-Card DGGADKINI B.A.; ZACHESOVA, G.N.; ABRAMOVA, Ye.N.;_BROKHIN, Yu.N. Aqueous dispersions of polyethylene. Koll. zhur. 25 no.4: 427-430 J14g 163. (MIRA 17:2) BROEHOVETSUI,-B - Watching over the work of machine industry workers* Okhr. truda i sots.stral-1. 5 no.1:11-34 Ja 162, (MIRA 15:2) 1. Zaveduyushchiy otdelom okhrany truda Volgogradskogo obkoma profsoyuza rabochikh mashinostroyeniyae (Volgograd--44achinery industry--Hygienic aspects) RRAWRI i W66 Conservative surgery of the stomach in peptic ulcer. Trudy LSGKI 20:152-163 '54. (KIRA 10:0 1. lafedre operatlynoy khirurgit i topografichaskoy anatomii Loningraclakogo sonitarno-gLgiyenichaskogo seditsinskogo instituta, zav. kafedroy - zael. deyatell nauki. prof. A.Yu.3ozon-Yarioshavich t khirurgichaskoys otdoleniye bollnitsy zavoda Im. Frunze. glevnyy vrech - V.V.Ashkov. (PAPTIC UICIR. surgery, conservative) BROXHOVICII, A.I. Technic of stump management following gastric sesection in peptic ulcor. Trudy IPSMI 39:303-311 158. (MIU 12:8) l..Kafedra operativnoy khirurgii i topograficheekov anatomli Leningradskogo sanitarno-gigiyenicheakoy meditainsko o inatituta OaV.kafedroy - z.d.n., profA.Yu.Sozon--yaroshevich Mceaeedl). (G&STRWTOKY, stump management in peptic ulcer (Rue)) BROKHOVICH, A.I., dotnent Secretory activity of the stomach in parathyroid insufficiency. Trudy ISGMI 59:222-234 160. (1-11M 14:9) 1. Kafedra operativnoy kbirurgii i topograficheskoy anatomii Leningradskogo sanitarno-gigiyonichaskogo meditsinskogc inatituta (zav. . lt.jj~I~', J64W ~ kafedroy - Prof. K.A.Grigorovich). ". - ~FARATHYROID GIAMS--DISEASES) (STOMACH-SECRETIONS) BROMOVICH, A.I., dotsent d state-of'the peripherd'I Changes in the venous pressure an vessels of the ,,.I-i.n in experimental plastic. 'r~eplacement of magistral af~~ies in extremities. Trudy ISGMI 74:301-309 162. (141RA 17: 10)