SCIENTIFIC ABSTRACT MOROZOVSKAYA, M. I. - MOROZOVSKIY, V. T.

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SCIENTIFIC ABSTRACT
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-'@A P7 Yicw, _Z KOROZOVSKATA, N.I.; TISHCHENKO, O.D.; IEMCHJ&NKO, I.A.; GOR&LYSHCVA. I.I.; In""T M.K.: YXVLAKHOVA, V.P.; AGAFONOV, I.N.; BESPAMILNAYA. P.S.; CFWJWNKO. Tu.P. Anti.malarial measures in the construction zone of the Kakhovka Hydroelectric Power Station. Ned.paraz.i parat.bol. no.1:61-66 Ja-Kr 154. NLRA 7:3) 1. Iz Ukrainskogo nauchno-Iseledovatel'skogo instituta malyarii i meditsinskoy parazitologil im. professors, V.Ya.Rubashkina (direk- tor instituta I.V.Damchanko) i Khersonskoy oblastnoy protivo- mal,Fartynoy stantaii (saveduyushchiy stantsiyey I.A.Agafonov). (Kakhovka region--Kalarial fever) (Malarial fever--Kakhovka region) 0 fr KCROZOVS]CAYA, X. 1. Kalarls control in the Ulemine. Ked, paras. I pares. bol. no,2.* 164-167 Ap-je 154. (MM 7:8) 1. Is Ukralnskogo nauchno-Issladavatel'skaCto Instituta mlyarli I md1tvinalboy paraxitologii Imani prof, I.Ta.RubaaWdua. (dir. InetItuta I.A.Dowhanko) (MAYARIA. prevention and control, *Rmssla) NOROZOVSKAYA H.I.; D304CHERKO. I.A. TISHCIMIKD, O.D.; GORMTSHWA, I.I.: T.F.: RAMCHKIY, S.S.; GALIPKRIM, L.Tu; BELTY, Ta.M.; LAZEBNTY, N.V.; DKRMHKO, V.I.; SMVINIM. G.A.; SMCMX, M.K.; DITACHMM, V.I.; AGAMHDV, N.I..- BISFA14IL'BATA, P.S.. CHKREMO. Tu.L. Preventive antimalarts. measures for lunberjacks saployed In clearing the bed of the future Kakhovka Reservoir. Ked.paraz. I paraz.bol.24 no.3:207-208 J1-S '55. (KLRA 8#12) 1. Iz Ukrainskogn nauchno-isoledovatellskagn inatituta nalyaril I maditsinskay parasitologit Ineni prof. V. Ya. Rubashkina (dir. Inatituta I.S.Denchanko) I Zaporozhokoy, Dnepropetrovskoy i Khersonskoy oblastafth protivomalyarlynykh stantaly. (KALARIA. prevention and control, in Russia, in forest workers) WROZOTS"TA, U.T., assistant, kand.tekhn.natLk Conditions for the autonomy of two-stage automt1c control s7stems. Trudy MIIT no-117:66-7) 160. (MIRA 13:10) (Automatic control) 41798-65 E1Yr(j)/EEC(m)/EEC(k)-2,/EWA (h) Pb_4/Pq_4/Pg-4/Pob/Pi-4/P1-4 CWICH VRt AR40391" LR/0274/64/000/003/A076/A.076 DURCS t Raf ab, PwdioteY=Wm i elaktrosvy" I Abe - 3448 U=t Morozov-jkay V. ITLE Choosig--op parameters for resonance frequene meters 7/3 ITED SOURCEt Tr. Moak. in-ta inzh. zh.-d. trpma., vyp. 171, 1963, 68-78 OPIC -TAGS.--- -frovenCy meter., radio, frequency -motor - RANSUTION -.--Frequency -is-6ften zeastwed- by two- res6iiant_circuita slightly off the ominall freqnzMay and by a differential rectifier whose output voltage is used to ndicate the frequency deviation or to control the frequency by means of ouitable inal devices. The op:timal detuning of such resonant circuits and their Q-factors re considered. The relations are found between the circuit detuning, Its sensitiv-j ty, and the working,bandwidth. The recommendations on choosing the circuit detun- ng-, their Q-taotors, and frequency-deviation bandwidth can be used in designing eas.uring devices which operate jointly with mapetio or electronic amplifiers and !so in designing frequency motors based on the ratio maters. Bibliography: 5 titles@ UB 0012"s W EXCL: 00 0 I-Ioo" 114 AUTHOR: Nlorozovskaya,Ye.N., @@nd Parfcs@@a, r,.I. 'TTLE: 7he Influcnee of thr r,)uling ?.atE -r t@iE Pr,ict,ire -@f SmE 1'_e', -metal 7'1 iE 3Kh2V8 "Illy anly L sk @ rr@s ,,eniyL n;.I strukt,.@ru n@., iav.Ern@:.-c ti;a AC.2v", Ph?IO[ICAL: Avtomatic,eskaya svarka, Vol 14'_ , Nr C' ":j-49 (USSR.) APSTFACT: The article describes research into thr str-_@rt,@rE: of Metal 371L.V8 smelteG --it variouz tcm@cr;.t1,-L5 n v;iric-us cond'itions. It i.'@so studies t@,.e i ro,.-,,rts of tl,(- isin- tcgri@tlor. of' AustLnite ;-It cooling r@.tcss f .,-I CI@O p(-_x s(-cond. At cooling rates of more than 1@0 sF(-)nc ~ Martcnsitc, tr-nsformation of Auster,.'tt_ takcs .arc- %@ ~ temierature .1' 4.300; (it coulinr ral'cs of 1@ -.10 a sccon6 ( tsintej-,ration t;ikes Iacc Lt :.@cut 4, th the, formation of' ncL61e troostitc ar@! t 1.F_ o f I suri lu@@ c,,rbiac..s; at coolin[ r.-.tc-:: "S, t. n G' . 10 the uisintegration of' AustL-nite t..kc-s @Iace 'Erniera- Card 1/3 tures bctween 870-6_`00 and i.,er.Litf- is for7Ec. . -hE mini- SOV/11 Th e Influence of the Co,,@Iinj- i,.ate on the -Strurt-,:-c- TY Pe 3Kh2v8 inum statIc temi,erature for Austu-nite is 71'@00. Y ; E r ments in smelting using v@-,riL@us thermai r( @.cs- critec, the tasir -yrle 1-einF instan*Lnc. -, , -I. the minimum statle temleraturc fo,- Austcn;te. C E ocology for the i's looke(, at, I D i iv, c : ty the structure ul' the smeited metal. It is lourd fha+ a reduction in the cooling slet-c :euut:s i-,@,@ntitv @,f Martensite, anc in the final anaiysizi t@-.L v, h c, I c s +c t - UrE COnSiStS 01' SUI-titO-periitL. t@icn acal with viith the mechanism of' the formation of the struct- ure, and also vith surplus jhLscs. A dei OSit Of 57C1"Ed metal cooled at 100 a second contained: Pe7C, Vv',@C, Fe,*7C, Fe-,W, The chemicai com@osition c@ dc-:0sit was: Fe, ;. i J- - I % cr, 1. 1" W the whc' t@ of t- E mE t;.' t e np 1OU5. The concu.-3ions re that -Y,;VB irEn @,rcl*e- s a number uf vaiu,.Ibie @uallities aeterm-'ret. @y thc micro- st.-ucture of* the smeltEc. metal. This str@..--urE `L ceter- Card 1/3 mined by the initial temperature of t.-,e has.!c mtt;il. SOVLL@-11 4 -4/14 The Influcnee of the Coolinp Patr on t@-.c Struc,@urc --f Mcfal TYPe 3Kh2V8 Secondly, at less than 00"@ a structure of Martensite is d formed with reduced har-ness and w"th insuffi,,Ien@ dura- bility. The best technological @ro@ertiEs arc -ossessed by metal smelted with preliminary hcatinF ct' the bLsic metal to 300-6000; it has a structure of nee(,,iE-f'crm troostitE and martensite which ens-crE ztLbi1-'1-.- and strength. In the smeited stat( oi 3Kh2V8 t hc 3'ur@ lus phases which strengthen thc matrix ui th(- m(.tal conslSt of alloyed ccmentitt, very stable doubl@ r;,rb,'(:e wolfrim (Fe W)6 C, alloyed chrome and vanad4um anc -,@IframidE Fe-z&. Thcre are 1 gra@.h, N illustrations, I tatl( and retcrences, 8 of' which are Soviet Lnd I German. ASSOCIATION: Ordena trudovogo krasnogo znameni in-titut elEktrosvarki imeni Ye.O.PatonaAN USSR (Oraer of t@,e Red @ianner- of Labor Institute of Liectric Wclding imeni Y(-.O.Paton of the AS UkrSSh) SITBMITTEL: August OL7, 1J58 Car6 3/3 o Z_ PHASE I BOOK EXPLOITATION SOV/5975 Internatiom-il institute of Weldinv )U] krngresB Mezhdunnrodnor,10 infititutn svirld, 21 iYully.-I - 5 Iyulyn !"'.!I V g. Opatii (Twelfth Annual Assernbly of the International Institut., of Weldinv, Opatija, June 29 - July 5, 1959) Moscow. Mashgiz, 1961. 359 p. 3000 copies printed. Sponsoring Agency- NatsionalInyy komitel SSSR po svarke. Ed. (Title page): G. A. Maslov, Docent; Tranfilated from English, Fr@n,h, and Serbo-Croatian by N. S. Aborenkova. K. N. Belyayev, L. P. Bugtchovn, L. A. Borisova, K. V. Zvegintseva, V. S. Minavichev, anti M. M. Shelechnik, Managing Ed. for Literature on the Ilot-Working of Metals: S. Ya. Golovin, Engineer. PURPOSE: This collection of articles to intended for welding specialists and the techmical personnel of various production and repair i3hops. Card I/# Twelfth Annu-i I As!,ernbly (Cont. ) "'Ov COVENIAGE- The collection contains abrid,!,-d -it the T welfth Annual Anaembly (if the Jn1t--rn.-Iti0tI:Il '+,'Ir@ Reports deal with problenis of welding arc] r,@Iated ww.l in r,,i-ir work, repair techniquen, and the probler,is irizurig in -orin-li(m with tiv- natut-7 of the haEm- and filler materials. I-.'xampletj of r(,pairini: varioos p.-irts are given, and the organization of repair operationS in worksholm ilrd under field conditions is discussed. Economic aspects of w,@Iding and , -lated processes as used in repair work tire annlyzed. No personalities are infln- tioned. There are no referenc-ra. TABLE OF CONTENTS jOnly Soviet and Soviet-bloc rpl)ortB ari- given hrre) Foreword 5 PART 1. THE s,rUDY OF REPAIR-WORK Tl-"CIIP.IQI:F-.S (PROCESSES, METHODS, PRLPAjtA'rjON. HKATIN(;, AND OTHER TYPES OF PROCESSING 0DNTR0l,) Alyuntsner, L. (Czechoelovakia). Welding of Broken Crank,3h;,fts t; Caro 219 Twelfth Annual Assembly (Cont. ) SOV/5075 Tesar, A., and Yu, 1-,ornbar(ilrJ(Czechoi3lo-,ralJa), Isothermal and Ultracold Welding of Hardenable Steels 42 Paton, B. Ye., G. Z. Voloahkevich,_D,_A._Did_ko, Yu. A. Sterenbogen, A. M. Maknra, P. 1. Sevbo, and D. 0. ltozenberg (USSR). Electroslag Welding in Repairing Heavy Machines and Mechanisms 411 Frumin, 1. 1., A. Ye. Asnis, L. M. Gutman, G. V. Ksendzyk, V. A. i-ipchenko, Ye. 1. Leynichuk, Ye. N. MorozovskAya, 1. K. Pokhodnya, V. P. Subbotovokiy, Automatic Weav-Resistant Submerged-Arc Surfacing G 0 Snegon, K. (Poland). RestoFation of Rolling-blill Rolls, Crane Rollers. Forging Dies, and Shears by Are Welding 72 Card 3/ 9 S/I 25/61/C,00/0(,3/',-0r,/rj P< A161/A133 AUTHOR: Morozovskaya, Ye.N. TITIEs Automatic build-up welding with austenitic high-manganese G13 stee, PERIODICALi Avtomaticheskaya avarka, no. 3, 1961, 32 - 41 TEM The subject r13 (013) steel to the Soviet equIvalent of a U.S. stard- ard steel grade of extraordinary wear resistance (Table 1): AWS - ASTM % C Mn N1 Cr Mo 31 P EFeMn-A ... 0.5-0.9 11.0-16.0 2.75-5.0 !@'0-50 - 0.3 - 1.3 0-0@ EFeMn-B ... 0.5-0.9 11.0-16.0 - 'P-0-50 o.6-i.4 0.3-1.3 G - 07 (Ref. Is American Society for Testing Materials, American Welding Society, Tenta- tive Specification for Surfacing Welding Rods and Electrodes, A-399-56T, 1956) It has been only little used in the USSR, mainly for the filling of surfaTe de- fects on castings and other repairs, since it is difficult to weld, develops hard and brittle segregated layers that cause crumbling and breaking off of the c"@ated layer. Reference is made to two Fr4@nch works treating the properties of G13 and giving technological recommendations (Ref. 2: G. Collette, C. Cr-assard, A. Kohn, Card 1/3 S, i2'1' Y, @ r Automatic build-up welding wl'-t austenitic AIWA113 I. Plateau, 0. Pomeyet, M. Weiz, Gontribution i letude des tra;-.6fcrmat.'c@ns deb austenites A 12% Kn. Revue de Metallurgie, no. 6. 1957; Ref. 3: F. Danhier, La soudabilit6 des aciers austenitiques au manganese. Arcos, no. 126, July, 1912) The article gives information cn ways of cbtaining good G13 steel coatings: 1) Multi-electrode welding with an "A-513" or "A-348" welder fitted with a spectai three-electrode attachment. 2) Building up with oast G13 steel electrod- band and a welder with adjustable electrode feed because of varying G13 bait cr,:6s ser- tion area, and water cooling. 3) Using an additional electrode that is ionn-?,%P! to the work so that the are is burning between the main electrode and the work (the method Is descrited In Ref. 5: Ya. Luka8hek and K. Lebl', Sposob avtomatl- cheskoy naplavki vysokoleg1rovannykh staley I splavov pod flyusom. Avtcmatl@hes- kaya svarka, no. 12, 19!q ). 4).PuUd-up,-e1dJngvft electrode inclined 450 fcrwar(@ Detailed information on all these methods can be obtained from the Electric Weld- Ing Institute im. Ye. 0. Paton. A special dephosphorizing fused flux AW-16 (AN- -16) developed for welding 013 steel Is recommended (20 - 25% MnO, 30 - 35% Cao, 20 - 25% A1203, 15 - 20% CaF21 up to 7.0% S'02' f;;' 0.02% P) and chemical compcsl- tion for cast or powder electrode band (1-0 4-1.2% C, 15 4-18% mn, up to O.C)6c% P and up to 0.2% Si). Twelve photographs Illustrate the all8tenite in G13 coatings obtained in different heat-treatment processes. Conclusionst 1) The major cause Card 2/3 3/1 25/61/000/CGVX@/'@l Automatic build-up welding with austenitic.... A1(')1/A133 of cracks in 013 type steel in building up and welding Is the formation Df Inter- crystalline layers containing P and 31. Steel with 0.8 - 1.1% C, 13 - 16% Mn, 0.030% P and 0.5% St is not prone to cracking. 2) Automatic build-up we.(ting by the submerged-are process Is possib2e when deposited 013 metal is slight.'y di.it- ed with the base metal. 3) A new powder electrode band, TMI--13A (PPG-13A) and a cast electrode band have been developed for build-up welding. 4) A r-w a-!6 welding flux has been developed for the automatic buIld-up vieldingof 131--- The flux dephosphorizes the coating in the process. 5) Multilayer coatIng dep- sited automatically by the submerged-arc process has a purely auctenitic j-:- ture. 6) An inter-layer of met&l with gradually decreasing and Kn-c')ntents f-'-Ms in automatic coating of 013 steel on low-carbon or low-alloy steel. The rjeptr of this layer &ad its properties depend on the build-up welding method. No br4**1e inter-layer forms In build-up welding using additional electrode. There '3r@ 1: figures, 5 tables and 5 referencest 2 Soviet-bloc and 3 non-Soviet-blop_ The reference to the English-language putlication reads as followss Amric&r SC-le-y for testing materials, American Welding Society, Tentative Specifi-@atlon Surfacing Welding Rods and Electrodes, A-399-56T, 1956. Card 3/3 S/125/62/000/009/002/008 A006/A101 AMOR Morozovskaya. Ye, N, TITLE- AH -16 (AN-16) flux for hardfacing hIgh-manganese r 13 (r,13) steel FERIODICAL: Avtomaticheskaya svarka, no. 9, 1962. 22 26 TEXT: Existing fluxes do not meet the requirements to the hardfacing of 013 grade steel. Therefore a special flux was developed, which transfers phos- phorus and silicon from the metal Into the slag and binds the hydrogen and oxygen in the are atmosphere Into non-soluble metal compounds. When thin material was developed the following factors were taken Into account: the flux shojild contain active oxygen In the form of Mn 2 03; It should have high basicity and low ductility, It should contain Al 203' The new AN-16 flux contains (in %)- 0 1.3 - 1.6, Al 2 03 20_ 25, CaO 30 - 35, CaF 20 - 25, MnO 15 - 20, SiO 7. 0; FeO .@_> 1. 0, S __- 0 - 15, 2 2 P -,0.03, C -,.-0.03. Hardfacing 013 steel with this new material produces weld de- posits without pores, cracks and slag Inclusions. A method was also developed of preparing AN-16 flux with a low phosphorus content by using Al-Fe addition alloy Card 1/2 S1 125/62/00VG09/'@C 21&-, 8 A H-16 (AN-16) flux for hardfacing high-manganese ... A006/A 10 1 wlth(15% Fe) as a deoxidizer. The possibility is shown of obtaining atelted flux containing Mn 203 by roasting in air atmosphere at 650 - 700 0C for 2 112 - @ hours. The use of AN-16 flux with Mn 203 does not cause the oxidation of liquid metal In the welding pool of grade G13 steel. It was found that the metal built-up with AN-16 flux contained 0.015 - 0.020% 14nO which corresponds to least oxidat!nn of the metal. The oxygen In high-manganese steel is mainly present in the form. of manganous oxide, singled out along the grain boundaries. There are 4 tables. ASSOCIATION: Ordena Trudovogo Krasnogo Znameni Institut elektrosvarki Imeni Ye. 0. Paton AN USSR ("Order of the Red Banner of Labor" Instituteof Electric Welding imeni Ye. 0. Paton, AS UkrSSR) SUBMITTED: December 8, 1961 Card 2/2 MOROZOVSKAYA,, Ye.N. 14schanired hard facing of rallroad frogs. Avtom. svar. 17 no.3:92 Mr 164. (MIRA 17: 11) :c.,,, Ir S t, i tU t rt,:; L F)7 EWT(m)~EVIA(d)/~COP(v"/T/EWP(t)/-IIP(k)/E-?iP(z)/~--flP(b)/L--4A(c) Pf @A Ar1r-.CCTMfi VT?- AVrM14711 62: ,Dh2 !AUTHOR: 14crozovsk a, ye. X. iTITLE: Vibular electrode wire. Class 21, No. 171055 7 ---@7-- 'SOURCE: Byulleten' izobreteniy i tovamykh znakov. no. lo, 1965, 51 Topic T.AM: @@Velding,*hlgh manganese steel, steel welding, welding electrode, elec-;' trode wire, tubular wire ABSTRACT, Tbis Autbor'Certificate introduces a tubular electrode wire for semi- automatic welding of high-manganese ateel. To fncilitate open-arc welding. the contains ferToalloys, iron and slag oowder co@-e of the wire Ts 0 TiO2-41gG-11aF system in the folloving amounts- 10.0% rutile, 8.0% magnesite, 7.0% cryolite, 44.0% manganese, 12.0% nickel, 15.0% iron povder, 1.5% ferrosilicon, and .2.5% graphite. [NDI iASSOCIATIM, none uBmimm @@6NovQ- ENCL: 00 SUB CODE: IF., M14 110 REF SOV. 000 OTHER: 000 ATD FRESS:*4038 F-wP(k)/&M(m)/rAwA(ci)/EwP(*)/E~&(v~)/EWP(i-@ JD/W ACC NR, - URIG1251661000/004/002 AP6015037 Al SOURCE CODE: AMORt. Natozave a, -Yee X. ORG., ',vue iie WeLdirsk: Institute Lae 'tee 0. Paton -AN OSSR (UwtLtut elektroavarki. i4xnz: The etruetti and provedigs of hi @-Wlanexe mt&l devosited with a j,powder-core eloictrode' SOURCE: Avtomatichaskaya avarka, no. 4. 1966, 22-25 TOPIC TAGS are de6osition, steel, high manganese steel, steel deposit ion steel structure, steel propgrty/G13 steel "Miat High vachanical properties were obtained In G13 high-manganese austaultic s e I (0.7%C, 14-56% Ka. 3.88% MI) weld deposits. The metal was deposited with an open-are PP-GIX14-0 tubular glectrade with a rutile-coutaining core. The electrode caning was made ft.. steel - Ah a ratio of electrode-tube volume to powder @and cote volu@of W-38%, the deposited metal had a tensile strength of 58.9-63.6 kg:/m a yfeld shwgih of 38A-1A2kg/=7, an elongation of Z0.4-25.6Z, and z an Impact toughness of 22-25 krulcm, . The deposit had a fine-grained disoriented structure. Chemical analysis showed that t is partially reduced during welifn and Is.transferred from slag to tat In unt of 0.03--0.06%0 which ly h;d a beneficial effect on mechanical properites of the deposit. A f*tft CeNd UDC,.- 621.191.92.046 ACC Ngs AP6015037 improveimmut. in'the, mechanical properties was obtained by* depositing metil, by two @'arcs In secies# where the second arc.deposited the metal onto the first layer when the latter hid. -,t te*eratilre of about 850CI the tensile -strength was 6901-16.9 kgjms%.,th*: yield strength 44A kg/mK?-,o the elongation 35-SX9 and the :..I!IP&Ct.tO~oness,24Z*'-~drig. art. has: 2-figures, and 3 tables. (INS] M COU91-J10'131 AMM DAM 10act65/ @@-'ORXG' REF: @007/ CFM RZF: 002/ ATO PRESS @2 65@ MARGOLIN, S.S.; KORCZOVSKIT, B. 1. laying veneer on boards by the hot method. Der.1 losokhim.prom. 2 no.12:26 D '51. (HUA 6 - 11 ) 1. Rechitskiy mebel'nyy kombinat. (Veneers and veneering) HOROZOVSKIY.B.I. @-i@ a"design of a veneer repair mill. Der.prom.4 no.6:31 Je'55. (KLaA 8:10) 1. Rechitskiy mebelInyy kombinat (Woodworking nachinery) B. 3.) @JIA MOROWISMY 13. T. =4 Llectrification of Airrraft -tatr_- of the Defeni3e I14dustry, 1@05(.. A trunclation of tne PrfA'ace iind tlic Tnble of Coll Wnta filso for- warded. @@10: 11239f'(,' MOROZOVSKIY, K. Kh., Cand Vet Sol -- "Certain awtu=_idevel- opmente of compensation-adaptation processes In animals after splenectomy under fft conditions of suprapleural novocalne blockade and wIthout It." Omsk, 1961. (MIn of* Agr R3FSR. Omsk Vet Inst) (KL, B-61, 256) - 401 - MO-IL07- J T7) 1: Y I i I - 9 . Fown, ' inr iop,,@r fur form mLx,ureq. 1,). .@ro :, zv. ':o. 2, 1-1 J. 9. Monthly List of.Russian Accessions, Library of Congress, ' 11-1 @-' -1953. Unclassified. KORMTUIT, K.S. Conveyer for returning a=ses natal to the mixing yard. Idt. prolev. no.4:29 Ap 055. (KLRA 8:6) (YoundrIes) (Conveying machiaory) AUTHOR: Morozovskiy, 1.'.S. SV-128-'59-10-10/19 TITLE: A Swivel Blic?et @!r)lnt for Charging rf C,,j;-jla F,;rra@es (11ovorctny, bad yevoy pod-y6nnik dlya zaprizk'1 vagranoi,.j PERIODIChL: Liteynoye prcizvodstvo, 1958, Nr 10, pp 2d - 73 ABSTRACT: The charging bkip uied for blest furnaces advergely affect- ed the prcce,3o of smelt in cupolas, especiall:,- those with a large diamf..ter of the charging shaft. This can be changed by the use of bucket hoists. A swivel type is preferable to a stationary type, which would be idle for periois of ti.me, w@-@ile the former is able to serve several cupolas. One such sswivel type b@icket hoist (fig 1_ operating highly satisfactorily in the new foundry of the Kharlkovs- kiy traktornyy zavod 'Khar'kov Tractor Plant) since 1956, is deicribed 't has a useful load-lifting Capacity of 2 tons with a lift@ng height of 13 m. A full operation cycle takes 2 minutes 7, .s operated by an a.c. electrcmotor of yps ,"T-51/8 -n@zh a performance of 1'7,'; kwt and '79 rev Im-*n. t I The o-mr-a2l wpip'ht of the @icist is ?r,; tons, 7-ere is I diagram. 1. Fu:-naces--Equipment 2 Furnaces--Performance 3. hoists Card 1/1 --Applications AUTHORS: Lipovetakly, Morozovskiy, M.S. SOV/128-58-11-20/24 TITLF: A Vertical Shaft for the Cooling of Ingots (vertikal'naya shakhta dlyn okhlazhdeniya otlivok) PFRIODICALt Liteynoye proizvodotvo, 1958, Nr 11, p 30 (USSR ABSTRACT: To improve the anfety conditions for founders, the designing section of Giprotraktorsel'khozmash at Khar1kov developed a special shaft for the cooling of ingots. The new Instal- lation is of an improved design; the waste gas and heat are completely eliminAted and the ingots are automatically charged and removed. The described shaft is now being In- stalled at the Rostsel'ma3h. There is 1 diagram and 1 table. 1. Foundries---Safety meaoures 2. Foundries--Equipment 3. Metals..-Cooltng 4. Gases--Disposal Card 1/1 LIPOVLVSKIY, G.Z.; IMOZOVSKIY. M-S. Buokethoists for the charging )f cupola@. ZAt. Proizv- rw.gt2l-25 s 60. (MIRA 130) (Youndries-3quipment ani sipplies) (Cupola furnaces) MOROZOVSKIY N.,, kand.tekhn.nauk Submarine planer. Tekh.mol. 29 no.5s24-25 '61. (MIRA 14, 51) (Submarine boats) MOROZOVSHY, N., kand tpkhn,naLik Submarine tracts. Znan sila 36 no 12: 5- 1) ' Cl ( y @ ?,.-. - @ " ) (Ocean currents) (Fetrulpum--Transportat4@-)n) ACC NRI AP6011842 60 SOURCE CODE: UR/0029/65/000/011/0018/0021 AUTHOR: Iforozovskiy, N. (Candidate of technical sciences) - ------------ ORG: Ilona TITLE: A wind through mountains SOURCE: Tekhnika molodezhi, not 11, 1965, 18-21 TOPIC TA08: wind 3yelone + ABSTRACT: The origin and foimation or a cyclonio type storm-in the Teemeaskaya Bay of the Black Sea., near NoVorosslysK, are described, and the deflection of the North-East wind (called "bora") by means of moun- tain tunnels is suggested. The storms usually occur in the fall and winter periods bringing heavy damage to the Novorossiysk harbor. The wind velocity exceeds 40 m/seo and sometimes reaches 60 m/sec at tem- peratures falling to -20 0 In the winteri causing Weighty accumulations of snow and ioes The "bora" storm is a result of a formation of a high-pressure antioyolone behind the northern Varada mouhtain. ridge (400 to 650 m, high) and a low-pressure cyclone above the Black Sea. Th ridge has a pass (Markhotakiy pareval) located 430 m-above the Tsemesukaya Bay. Due to the differences in pressures and temperatures$ L 39794-66 ACC Hit, AP6011842 an intensive air flow is formed in the pasoland the bay and the city are hit by a violent storm. In order to deflect the air flow from the pasag the author proposed to dig three Inclined tunnels under the pass with one common outlet located at 150 m above the sea levele It was mentioned that a similar project had been proposed before the revolution by a group of British specialists). In the author's opinion, the aoou- mulat6d--air masswill be sucked into tunnals and funneled to the outlet where e'turbine-gonerator unit can be insealled for power production.,' The ariangement of tunnels and the power plant was illustrated. A chart @.howing the occurrence of "bora" storms between 1901 and 1954 was also e-41 nresenteds A SUBM DA TN: SbB COM 04 None ORIG ralf: 000 OTH REF: 000 MORG.1,011`@ " , '. .@, . 9 @ont.r. idmi ril zs-paaa .-1 ' i F I on rour-qp . Mor . 3br.r . 4" n,, @ . ',- -)3 Je 164. 'MI@A :@17) SULBZHI 11 SK A! A, y N lK '):a Y-@vliuj y Conc i L@Fj marl, t JiLe ilc t I for yoi@r.-, pefj mor i:, a, r anspe, Y PHASE I BOOK EXPLOITATION POL/3440 Kulebak1n, Viktor 3ergeyevlch, V. Morozovskly, and 1. Sindeyev Lotnicze elektroenergetyczne urzidzenia pokladowe (Electrical Equipment for Aircraft) Warszawa, Wyd-wo Min-wa obrony narodowej, 1958. 546 p. Errata slip Inserted. 600 copies printed. Eds.: Maria Kowalska, Master in Engineering, and Jerzy Domd'naki, Engineer; Tech. Ed.: Helena Malczewska; Leslaw B4tdkowski, Master in Engineering; Jdzef Krug, Master in Engineering, and Janusz Dombrowl--kl, Engineer; Revieweri Jdzef Sienkiewicz, Master in Engineering. PURPOSE: This book is a textbook for students and aircraft engineers and technicianB. COVERAGE: The book describes the design and operating principles of basic modern electrical power equipment of aircraft. It discusses theoretical principles of various operating processes Card l/ 14 Electrical Equipment (Cont.) POL/344o of individual unitn and of the system as a whole. The book also describes the construction of electric power systems and lists technical requirements of the most widely used kinds of equipment. There are 43 references: 36 3ovlet and 7 English. TABLE OF CONTENTS., From the Editors of the Polish Translation Authors' Preface Introduction 9 10 11 1. Use and Importance of aircraft electrical equipment 11 2. Brief review of the development of aircraft electrical equipment 13 3. Classification of aircraft electrical equipment 16 4. Operating conditions of aircraft electrical equipment 17 5. Basic technical requirements of aircraft electrical equipment 22 Card 2/ 14 Electrical Equipment ((:,-)r)- , ) POL/344o Ch. I. Chemical Sourc-@; of Power 25 1. Use of chemlc-al power &ources in aviation 25 2. Operating principle of an acid storage cell 27 3. Construction of air.-raft storage cells 28 4. Electrolyte u&ed in acid storage cells 32 5. Characteristics of a@ld storage cells 37 6. Installing Etorage rells In atrcraft. Connecting airfield power sources to the aircraft elertr1ral clr.ul@ 43 7. Charging a_iid divicharging, slorage cells 51 8. Servlolng a1r:raft Qtorage ceI13 55 9. Alkaline storage rells 59 "N Ch. Il. D-C Generator:-u 6@ 1. ReqtLirements and -hara,terlsti:-s of d-, aircraft generatorz-@ 62 2. Brushes and brush-holder arrangement In aircraft generators 66 3. D-c aircraft generator drives 72 Card 3/14 Electrical Equipment (Gont.) POL/3440 Ch. III. Basic Electric and Magnetir Characteristics of D-C Generators 79 3.1. Magnetic r!haratertstirs 79 2. External rhararterlatirQ 83 3. Conditions for sell'-excitation of generators 86 4. Reststance-speed characteristics 89 5. Static equilltbrIum of excitation, and static equill.brium (riteria of a shunt-wound generator 94 Ch. IV. Voltage Regulation In D-C Air,.-raft Generators 97 4.1. Basic methods of' voltage regulatlon In d-c generators 97 2. Excitation-current regulation 99 3. Methods of 7onnecting excitation regulators 100 Ch. V. Voltage Regulation by Means of Regulators With a Smooth Change In Res.1stance 104 5.1. General propertt-Ps of carbon contact resistors 104 2. Operating principie and design of carbon-plle voltage regulators 106 3. Adjusting a carbon--pile voltage regulator ill 4. Dynamics of voltage regulation by a carbon- pile regulator 115 Card 4/14 Electrical Equipment (Cont.) POL/344o 5. Evaluating the regulating stability and precision of the regulator 126 6, Means of increasing the stability of carbon-pile voltage regulators 128 7. Installation and operation of a carbon-pile voltage regulator 134 Ch. VI. Voltage Regulation by Means of Vibrating Regulators 135 6.1. aeneral theory of statics of voltage regulation by means of vibrating contacts 135 2. Amplitude of voltage ripple at a constant frequency of contact vibration 143 3. Operating principle of a vibrating voltage regulator 145 4. Construction of a vibrating voltage regulator 1 5. Amplitude of voltage ripple and the frequency of oscillation of a vibrating voltage regulator 148 6. Methods of increasing the frequency of contact vibration 150 Card 5/14 Electrical Equipment (Cont.) POL/344o Ch. VII. Parallel Operation of Aircraft generators and Parallel Operation of a Generator With a Storage Battery 153 7.1. Essential conditions for parallel operation of generators 153 2. Method of switching on voltage regulators with parallel operation of generators 154 3, Significance of the equalizing winding 157 4. Parallel operation of two generators equipped with voltage regulators 159 5. Parallel operation of several generators equipped with voltage regulators 168 6. Parallel operation of a generator and a storage battery 173 7. Effect of the degree of loading of the storage battery 177 Ch. VIII. Protection of D-C Aircraft Generators 181 8.1. Protecting generators against reverse currents 181 Card 6/14 Electrical Equipment (Cont.) POL/3440 2, Protecting generators against overload 189 3. Short-circuit in teminals of d-c aircraft generators 196 4. Protecting d-c generators against short circuits 203 Ch. IX. Generating Alternating Current in Aircraft 2o6 9.1. Parameters of a-c aircraft generatoits 2o6 2. Basic electrical characteristics of a-c aircraft generators 20T 3. Excitation of a-c generators 214 4. Methods of driving a-c aircraft'generators 220 Ch. X. Regulating the Voltage of A-C Aircraft Generators 10.1. Special features of voltage regulation of a-a aircraft generators 238 2. Connecting the windings of a single-phase voltage regulator through a three-phase rectifying system 24o 3. Connecting the windings of a single-phase regulator through a voltage filter of a positive phase sequence 243 Card T/ 14 Electrical Equipment (Cont.) POL/344o 4. 3tabilizing the passive load ratio in the parallel operation of generators acting on bus bars 248 5. Automatic voltage regulation of synchronous aircraft generators 252 6. Voltage regulation of synchronous generators with permanent-magnet excitation 257 Ch. XI. Parallel Operation of A-C Aircraft Generators 263 11.1. Condit@ons of parallel operation of a-c generators 263 2. Parallel operation of two generators rotating at the same speedone of which has infinite capacity 264 3. Parallel operation of synchronous generators with constant excitation and variable power (load transfer) 273 4. Parallel operation of two generators of equal capacity 275 5. Automatic division of power between synchronous aircraft generators operating in parallel 2 Card 8/ 14 Electrical Equipment (Cont.) FOL/344o 6. Connecting synchronous aircraft generators for parallel operation 281 Ch,. XII. Short-Circuits and Protection of Synchronous Aircraft Generators , 286 12.1. Short-circuits on the terminals of a synchronous generator 286 2. Overcurrent relay protection of synchronous generators 292 3. Longitudinal protection of synchronous generators by means of directional current-differential relays 295 4. Methods for automatic de-energizing of generators 298 Ch. XIII. Current and Voltage Converters 301 13-1. Converting low d-c voltage to higher d-c voltage 302 2. Converters for changing d-c to a-c 306 3. Methods of stabilizing a-c frequency In converters 308 4. Static a-c to d-c converters 316 5. Rectifier circuits for a-c rectification 323 Card 9/ 14 Electrical Equipment (Cont..) POL/344o Ch. XIV. Diagrams of Electric Loads and Selection of Blectric Power Sources for Aircrfft 327 14.1. Loads diagrams of aircraft electric power sources 32T 2. Choice of main sources of electric energy 327 3. Choice of reserve sources of electrical energy 333 4. Fault load diagrams; load diagrams of synchronous generators and of distribution installations 339 Ch. XV. Basic Information on Systems for Transmitting and Distributing Electrical Energy 344 15-1. Function of transmitting and distributing systems 344 2. Requirements of transmitting and distributing systems 345 3. Types of aircraft electrical systems 345 4. Systems for the transmission of d-c energy 352 5. Systems for the transmission of a-c energy 356 Ch. XVI. Components of Transmission and Distribution Systems 360 16.1. Conductors in aircraft 360 2. Mounting and installing equipment 364 3. Connecting and protecting equipment 371 Card lo/ 14 Electrical Equipment (Cont.) POL/344o 4. Types of aircraft electrical networks 380 Ch. XVII. Calculation of Aircraft Electrical Networks 386 17-1. Special features of the calculation of aircraft electrical networks 386 2, Calculation of conductors for heating in aircraft electrical networks 327 3, Determination of conductor cross-section according to permissible heat loads 392 4. Oeneral problems of calculating electrical conductors for voltage drop 394 5. Basic parameters for the calculation of circuits 398 6. Calculation of d-c radial electrical networks accoiding to voltage drop 403 7. Moot'favorable operating curpent densities and voltage drops 414 8. Calculation of aircraft d-c closed-loop electrical networks according to voltage drop 417 9. Special features of calculating aircraft a-c electrical networks 427 Card li/ 14 Electrical Equipment (Cont.) POL/3440 dh. XVIII. Faulty operating Conditions In Aircraft Networks and Calculation of Short-Circuit Currents 433 1. Faulty operating conditions in distributing and transmitting systems on aircraft 433 2. Resistance of electrical equipment components under short circuit cohditions and voltage-current characteristics 434 3. Volt4ge-current characteristics of d-c power jou@rd es 436 4. Voltage-current characteristics of d-c power receivers 442 5. Calculation of short-circuit currents on the basis of voltage-current characteristics 447 6. Grapho-analytical calculation of short-circuit currents 456 7. Calculation of short-circuit currents in Iairoraft a-c networks 459 Ch. XIX. Protectift of Aircraft Electrical Networks 464 1. Basic requirements for the protection of aircraft electrical networks 464 Card 12/ 14 Electrical Equipment'(Cont.) POL/3440 2. Oeneral information on the protection equipment for the aircraft distribution network 468 3. Time-current characteristics of safety fuses 471 4, Time-current ch4racteristics of aircraft automatic switches 475 5. Protecting the distribution network by means of fuses and automatic switches 48o 6. Protecting the electric-power supply by means of fuses and automatic switches 485 7. Differential protection of the aircraft electric- power supply 488 8. Automatic switching on of aircraft reserve supply 488 19,9, Special features of the protection of aircraft a-c power supply 495 Cho XX. Basic Problems in the Theory of Switching of Aircraft Electric Networks 499 20.1. Switching conditions and the action of interrupting the electric circuit 499 Card 13/14 I Zlectrical Equipment (Cont.) POL/344o 2. Voltage-current characteristic of a d-c are 502 3. Conditions of steady burning and interruption of an a-c are 50 4. Special features of burning and interrupting an a-c are 5o6 5. Methods of interrupting an electric arc 512 Ch. XXI. Operation of Electrical Transmitting and Distributing Systems for Aircraft 515 21.1. Insulation requirements of a1kcraft electrical transmitting and distributing systems 515 2. Checking the insulation of aircraft electrical tran8mitting and distributing systems 517 3. Detection of short circuits in aircraft electrical networks 521 4, Locating points of interruption in aircraft eleotrical networks 522 5. Safety measures on aircraft 524 List of graphical symbols 532 Bibliography 545 Available: Library of Congress Card 14/14 JP/Mq 1. 1. -1 ZISGIHXAN, Ya.P.; KOROZOVSXIY. V.A. Investigating the nonuniformity of work junctions on metal surfaces. Prib.1 takh.ekap.no-3:65-6c Y-D '56. (NLRA 10:2) 1. Institut fiziki AN USSR. (Ilectr6n emission) (Oscillators, Blectron-tube) SOV/100-3-8-6/18 AUTHORS: ZiiiSerrnan, YF-.P. and L,nr-i7nynkiX.-Y-,,A- TITLE: liavesti-ation of the Process of the Penetration Df 0 Ba-riur, -'.--hrou,-_h the Porous Plue of an L-cathode kIsuledovaniye protsessa prokhozhdeniya bari:ia skv-1z' poristoGo metalloplenochnoCo termokatoda) e,u ku IER!--@:ACAL: Radiotelchnika i Elektronika, 1958, VD1 3, Dr 8, pp 1017 - 1023 (USSR) ABSTRACT: Persurerients were carried o,it by ireans of a E-cc-481 tft,@ (Fir@_-ure 1) -,,.,hicl-. vas in the form of a di--,de; t@A5 c:;n- in A and t-.e ar.@A,: 2, ed t@e investigated cathode Tne an@)de was in the form of a movable t,jni-sten -,late v.hich could be periodicplly cleaned inside t1-.e tube by raisin,.- its temp,-rr@ture u-n to 2 000 OC 'jy @iears of the electron bombErdraent, provided from a t!1nC.:ster 'N'le c-tl.odc fixed on movable sup 'orts arid c-i-'J @e set in two diffei@nt fixed positions. IL, in-s of tl.e--,e positions (Fi6ure la3, the piuC of the cathode was in front of the anode; the electron emisLion and tI,e v@lDc-:*y of the evaporation of' barium were measured in tl-.iE; In the second -)osition (Figure 16), the apert--ir@ -f t!-1e Uardl/4 cathode chamber .lias in front of ne anode an-'A ti-e am,-,@nt SGV/109-3-8-6/18 Investigation of the Process of' the Penetration of bar-Luz tLrouFh the Porous Plug of an L-cathode of barium issuing from the aperture was measured. The barium evaporation velocity from the plue and from the cathode chamber were determined by measurinC the variation in the work function of the anode which was subjectea to a bombardment by barium (issuing from the aperture in the cahmber the plug). This method of measurement was des- cribed in detail in an earlier work by the authors (Ref 2). The experimental tube of Figure 1 was also used to mea--ure the electron emission of the c9thode by usinr_ e",onential voltage pulses at the anode. The pulses hqd a time constant of about 100 @,sec and a repetition frecuency of 1-2 pps. Three types of c@,thode were used; ti-e chemical composition of these, their2emission density and the eva- poration velocity @in @LClcm h) are shown in the table :)n p lU20. The dependence of the barium vapour pres5ure oD the temDerature for the ccthode of the fi-st type is illustr,-,ted in ribure 2; Curve 1 shovis the pres-ure tLe cathode chamber, while Curve 2 Jves the nres._;,-_ire 3bove tLe cathode pluG. Similar curves for the cath3de of the C.rd2/4 third type k see the table) axe shown in FiE:urt. 3. SOV/109-3-8-6/18 lnvef,tit.otiori )1' the Proceuu of the Penetration of Barium through the Porous Plub of an I_cathode and Pr ins @de The quantities P. /in these f iL-ure S represent the pres-zures tLe c4amber and ,fabove the cathode plug. The ratio of py/pjr as a function of temperature, for the cathode of the third t-ipe, iii plotted in zigure, 4. From the above investigaLi,)n, it, is concluded that the migration of barium through the plug can be explained by two processes. At lovi pres-ures, the mech-anism of barium transfer can be explaineJ ty the miE@ration of bErium alonE the walls of the pores 3f the tungsten plug. On the other hand, at hjCzh tariuia-vapour piessures (inside the cathode chamber), the tr-nsfer is caused by the Knadsen-type leakage of the subbta--ce tIro ii-h t,'--e I .3res. The authors riake aknoviledgement to Correspondin t Llerber @)I' -the Ac.Se.Ukrainian SSR IT.D. !j'orgulis for his interest in this work and for valuable advice. Card3/4 SOV/109-3-8-6/18 Investigation of the Process of the Penetration of Barium tLxou,--@. the Porous Plug of an L-cath-ode There are 4 figures, 1 table and 10 references, 6 of which are Soviet and 4 English. AS-@@CCIATION: Institut fiziki All USSR, Kiyev (Institute of Physics of the Ac.Sc. Ultrainian SSR, Kiyev) SUBbLITTED: January 29, 1958 1. Barium--Properties 2. Cathodes (Electron Vjhe)--Performance Card 4/4 3. Barlum--Vaporization 4. Thermionic emission 84089 tqt 31 -,W AUTHORS: ,113?1 13-1 3 7, S/18 "-'-,'3C 2/7 - -,,'C 32,:'_-@36 TITLEt Zingerman, Ya- P_ Ishchuk, V. A , Yorozovskiy, V. A. V_ The Electronic and Adsorption Properties of Film0of Barium Atoms on Tungs4 - -i'j PERIODICAL- Fizika tverdogo tela, 1960, Vol, 2, No. 9, pp, 22706-2286 TEM In an earlier paper (Ref. 1), the authors described a new method of studying the kinetics of adsorption processes. In the pre-,ent work, this method was used for the adsorption of barium on tungsten surfaces. The experimental tube and the measuring methods are described ir Ref 1 A tar'-,et made from a polished, 0.5 mm thick sheet of high-purity tungoten, whose surface was purified by electron bombardment at T >26C)OOK, wes used. The target surface in this case had a microcrystalline structure (Size of the microcrystale 50 - 100p ). In individual cases, 20P thick tungsten sheet3 were used, and the microcrVtals attained a size of 0.2 - 0.7 mm after the electron tombardment. "bATO" ("BATI") getter pills with 99@- of Ba were use as a barium source. The investigations were carried out at (I - 2).10 @ torr. The change in the work function of tte tungsten during Card 1/4 8hOP9 The Electronic and Adsorption Properties of 9/181/60/002/009/0321,'036 Films of Barium Atcms on Tungsten B004/BO56 covering with barium atoms was measured by means of an electron beam. The dependence of Ly on the surface concentration n of Ba was determined by two methodat a) By measuring the desorption heat Q as a function of n; b) by measuringdq as a function of the adsorption time t in a constant atom stream NI' Tho experimental data are given in Fig. 1: Ion current recorded by an 31TIT-09 (EPP-09) potentiomoter as a function of t and of the temperature of the W target (300 - 1650001 Fig@ 2: surface concentra- tion n of the bariun atoms as a function of time and temperature; Fie, 3s desorption heat Q and modification of the work function A Vas a function of n; Fig. 43b 1 as a function of t and temperature; Fig. 5:6F as a function of t and tomperature in a W target purified by heating; Fig. 6: dto. in a target purified by electron bombardment; Fig. 7: @j as a function of the coating degree 1,9. The dependence of L@ on temperature and on the manner of treating the target (occurrence of a minimum for,6? (n) at low temperatures), which was found in this paper, is explained by the change in the Impurity content of the adsorbed barium film. The impurities are probably atoms of tk.e residual gan whose stream is of the same order of magnitude also at 1",-9 torr as the stream of barium atoms. This could be Card 2/4 84089 The Electronic and Adsorption Properties of S/181Z60/002/OC,9/032/036 Films of Barium Atoms on Tungsten B004/BO56 experimentally provan by the adsorption of Ba on a W target c@vored with an adsorbed renidu&L gas film (Fie- 8). Electron bombardment leads to a lower durability of the residual gas on the target (Fig, 9) The change in 64 is related to the dipole effect p of the adsorbed atom The following 3/2 relation is obtained from equation6@- 4Tpn (2): n . (po/@Ck) ( 1 /p) - 1 /W (4), whereas, is the lattice constant, This interrelation was confirmed by experimental verification (Fig 10). The authors drew the following conclusions: The ad.-jorption of the barium atoms on the tungsten surface is not activated The condensation coefficient equals unity, and with a covering degree of from 114@@01 to V'@ I - 5 it does not depend on the latter nor on temperature. In the adsorption of barium atoms on N bombarded with electrons, the valuE ofdymonotonically approaches a limit which is near the work function fcr compact Ba, This limit is attained in the case of monatomic covering r Ce(5 - 6)-1014 atom/cm 2, The authors thank I. M., Dykman, Candidate of Physical and Mathematical Sciences, for his assistance and discussions. There are 10 figures and 11 references: 6 Soviet, 2 US, 3 British, and 1 German. Card 3/4 The Electronic and Adsorption Properties of S /16 1/614@)(080!2/009/0 ' 210 36 Films of Barium Atoms on Tungsten Bb04/BO56 ASSOCIATIOM Institut fiziki All USSR, Kiyev (Institute of Physics of the AS UkrSSR, Kiyev) SUBMITTEDt February 22, 1960 Card 4/4 89281 3/18 61 /00 04 2 Bc c, @ Y3- C7 AUTHORS; Zingerman, Yi. P. a@d Morczovskiy. V. A. TITLE: An ionization metY.od cf investigating thf, KintiZ@ of ads:)rp- tion vrooes.:@es on th- surface of 5olli- PERIODICAL: Fi--iica tvPrd,:gr) +-,I,t, v, :, ric. 1, 19@,), TEXT: As the conventionaI mothodo -- f i@.ves ti he qJ3o rpt ion and J-- 3orption rave aeveral ir-iwua-,k.,, 'he aulhor:, ha,;e a new experi- mental method whi@,h I's ba5ed upon me@isurlnt@ tht- :n4priiily of atom bpamF b.-i means of their ionizati on ijy ijlect rc-n 4 mp--i.-@ The funlamentals of 'fii-; method, th- method lt.,e'f, ;tr,d tne .-.ns arc! dP6,r4t,?J in . he prejent papPr. The ionizAti-)r, motnof -1" 11,7`@,@L@--qt-inS *,'@f- -r* 'L -, p- tion pr-r-ssee , suggested by Zingprm,iri, is de:3cribed cn th- uasiq @f Fig. Fig. la 6..,Y..ematically 3hows tha main e-leuis,n's If 1,1v? tute -1-@ed f@r tho experiments; 1) is the 9oijr--,e of 01-., -itorr, or m-)1eculn biam, 2) is th,@ diaphragm through which the latter paj6ej, I., a ro,oriing --ind mea-,irin6 device, 4) is an Ionization ch-ambor, ind '@) th'? t,trg-t-ad.,iorb-rit. Thp not -)rly 'he direct beam may bt- quickly .3hu' of Vy A, .11 ilj-ins ' Card 1/6 89281 S I 181/6 1/00 5/_@" @/014/042 An ionization method of... B006/BOc@6 atom 'beam, but also the reflected and desorbed atoms (coming frcm the target surface) fly through the ohamber. Therefore, the ion current in the collector circuit is due to ionizations by both direct and reversed atoms- These two intensity components for the atom f'luxes N 1 ani N2 are given by I,_1@11, and Y&Y2; 0(1 is relatnd, to the ion charge, the impact icnization cross t)ention of the atom, the intensity ;ind gecmL-try r f the br-mbirding electron beam, the flux intensity distribu-Icn in the iGniza*ion chamber and the temperature of the nources of N,, 'Ind N., It i-D ther-efcrv F051@ible, by measuring 1, and 12 and their dependence cn tim@, and temFerature of the adsorbents, to obtain the entire complex (--f Pxp-rimenta. data necessary for investigating the kinetics of z@or@ti)n prrocesz3es . TIL41 eXF @ r " M,,O a realization of this idea met w4. th a nijmti_@,r @,f di f f icul ti e5 wl@ich are described in detail. Provided certain conditions are satisfied, they way be avoided. In compliance with these conditions, Ei tube was conqtru-,ted, which in shown in Fig. 2 The target In a hot tantal um cyl inder ( I ) whJ ch may be placed above the auxiliary tungsten electrode M, above the ioniza- tion chamber (II), or above the electron gun (VI). The ionization chamber Card @/6 89251 S/1 8 1 /6 1 /Oc3/- 1 /C 14 /042 An ionization method of ... B006/KaJ6 is a three-electrode system (cathode, anode, collector ,'. The entire system is surrounded by a cylindrical shield (electron re lector). The ionization chamber has an operating volume of only 0.5-0.6 cmi. By means of a Ba beam the tube operat.d under the following conditions: V an = 200 v, Vcalh@_ 90 v 10 2 Ie - 4- 5 ma. The Ba ion flux was 10 atoms/cm .sec, which c,:rresponds to an ion current of@1_110_ 1@ a. IV denotes the molecule gun (the electron gun, VI, serves for measuring the work fun,ti-n by thp cuntact-potenlial metho@), and III is the ahutter for shutling cff 'he atcm beam. Studios rf the AI(t) and n(t) curves by rneans of this tUbo qre finally Jiacuss-d . F, t:. shows AI as a function of the duration of adsorptln -f Be atnm:, cri W; the dependence of the surface concentratica of the Be itoms cn ',h(' tion time was determined frcm these curves; Fic. 5 show- the n(t) -,drves thus obtained. As the adsorption of' Be on W does not esaenfially iffl>ct the work function of W, the determination of the ad8crpti,@n properti@,q of the system W-Be is practically imposjIble by the use of -:@nventiorial methods (electrDn emission, contact-potential difforence); by m,!,,ins r)f the method described here, however, thii-, 11a aell po;',,,jib1P. Tije FAit!or_ ttlarv Professor 11. D. Morgulls, Corre3ponding Monber AS UkrSSR, for fiir@-iSoiori.9- Card 3/6 89281 S /16 1/6 1 Pr) I /C 14, 0412 An ionization method of ... B006/BO56 Ya. M. Kucherov is mentioned. There are 5 figures and 6 referenc'?O: 3 Soviet-bloc and 2 non-Soviet-bloc. ASSOCIATIONs Institut fiziki AN USSR, g. Kiyev (Institute of Phy.-,icii, AS UkrSSR, Kiyev) SUBMITTED- February 22, 1960 (initiall May 3, 1960 (after revision@ Card 4/6 An.lonization method of... B006d its) ri 4 rib-[ ale r H./Z nir tO r Card 5/6 )14,'342 vi 2@039 AUTHORS: Zingerman, Ya. D;hchuk, 7. A. , 7. TITLE. Adsorption of atomn of the a,'Ltluli@,,-,,(Lvtt, ;.,rou polycrystalline tuni,,.,iten r, 3, no. z'j, 19ul, 1 "",-lo" PZRIUDICAL: Fizika tverdo o tela, v. TEXT: With roburd to the adscir-,tion @f fl,:r.!@-tw litprature it; still, v..,r.y incompleto -nd %:, j.Ub2ir,j:(-i 1!.t -1 ' vj r. Therf-f or,@, ','I,? autiior-, , lanned an o7h:iuo'.j lnvc@-,@ ; @:-l @n nf t 11 k- rrm i o n -; c-in(] propertle,.; oft ic fi eartlu, on tur The ayotem W - Ila already )revious articQ (:-t. 1: FTT, 11, 11, Z776, 1 1960) ,thoi.1 un@-@i Y;az; one newly devoloped by _-,ed "ionization method for the invejti. tl@)n -,f rL! -)f 301i@ bo,lipsll and in, , it) -tef. 1 )6 J) .T h @? retmIt.9 -)f invevtigations rolative t@,, thr- recidual ;,'kalinp carth nri tun,-,vton ArO in 1.1,o pl- ionizati"I" vlafl UZ.14,H to @ltudy tho 'L,lool-pti"n of Card I/la 22035' ,loorption c f rv tor-,@@ ,ind Ca ttio sim,;Irr c .t k,t i@ @-Ised n file Mell' ftLjjtt! it, I n d u r rL a oba ri c a(J. t C! I n 4 - r m e t r in 1.1ef 4 Yu Velu);,, V. @,Ivril'lluk, Sr, Ca, and -ro @t frqm @rO, ,,i- , by ther aii reduction '.@LT't Be v;:.@s. ch,,-.ie,,.Il, ure Be met,-1 ',.y t@ v-, i ., r tur. -t. ar iite oi' t,iELh purity , , ,r@ r. v C,; clectron 1, '-1mbardment at T > 0017 It had n j-.olrcrystalline 7trw,,,zz,- in the final 3tate With :1 0 -'i70 Of @11'0-1-" 1) n t t.,".e invtt!Tt it,-;L t ions arc il III Lratr 1, "Or-9 C', tyj)ical oneo being repro,',-c-d hev 4c:-tl da-,@i ur( PC* - t -.' @le. c:xample , F.,' @ . 5 and t V, -,rk of t liv ,- ur- fac v con cent ra L i j n n o f t 1.o r,)-b (A P. t, @ @Ir t I ,r:r 3/2 .1-41-1 -@- t i0m) /I lip0Yl/ 1 + 9@ n t Ke v - .@O. o 'fc) -..!i d n in tno mriximum 1, V P 3 0 aml n a (9u/2)-' are correctly I-C,)J. @Ck I '@Y t: of r ,lard 2 1 U 22039 3/181/61/003/0 04 /D'D5'/'3C Adsorption of atoms ... B102/B214 Po denotes the dipole moment for n = 0 and u the polarizability of the adsorbed atoms. The experimental results lead to the following conclusions: 1) The condensation coefficient of Bat Mg, and Be on W in a large range of T and n equals one. If the flux of the atoms being adsorbed is constant, the rate of adsorption is constant, which indicates the mobility of the adsorbed atoms in the surface layer. 2) On adsorption of Be on W the adsorbed atom shows no marked dipole moment. The work function of a thin atomic layer of Be on W equals 4.53 ev. 3) The adsorp- tion of Bat Sr, Cat and Mg on polycrystalline W which has been heated to remove gas impurities and subjected to electron bombardment, shows a monotonic decrease of atf of W during the formation of a monatomic coating. Adsorption of the same atoms on a cold (Tt;e 3000K) W surface leads to the usual maximum of the Ltf(n) curve, which is a consequence of interaction of the adsorbed atoms with the residual gas on the W surface. 4) The change of A,p on adaorption of Ba, Sr, Cat and Mg on W can be described theoretically if the dipole moment of the adsorbed atom at n = 0, its polarizability, and the surface concentration n11 of the adsorbed atoms in a monatomic layer are taken into consideration. 5) Desorption of Card 3/10 Adsorption of atoms 22039 0"/181/61/003/064/005/030 B102/B214 alkaline earth from W is characterized by a linear decrease of the desorption heat q with increasing n. This must be explained as due to the adsorption inhomogeneity of 71, and not to a change in the inter- action energy of the adsorbed atoms. The electrostatic binding between alkaline earth and W appears to be unimportant for adsorption. The authors thank Yu. G. Ptunhinskiy, Candidate of Physical and Mathematical Sciences, and Engineer B. A. Chuykov for the mass-spectror-etric analysis. There are 7 figures, I table, and 11 references: 7 Soviet-bloc and 4 non- Soviet-bloc. ASSOCIATION: Institut fiziki An USSR Kiyev (Inotitute of Phy,,iico AS UkrSSR, Kiyev) SUBMITTED: May 24, 1960 Card 4/10 S/', @Y62/004/007/01 5/057 B102 B104 AUTHORS: Zingerman, Ya. P., and Morozovskiy, V. A. Interaction of molecular oxygen with the surface of tungsten 177iIODICAL: Fizika tverdogo tela, v. 4, no !)62, 7, la33-1840 '171.17: Vite adsorption of molecular oxygen on solid tungsten vas inve3ti.aated by a version of the ionization method used for investigating the kinetics of adsorption which the authors published in FTT, v.3, 125, 1961. Data relating to the kinetics of adsorption are derived from measurements of the time dependence of the ion current I - 1 1+10 +19+1 3' '@he components of I are the currents of molecules atriking the target, the currents of molecules elastically reflected from the target, the currents of molecules thermally desorbed by the target, and the currents of the residual gas molecules in the ionization chamber. Using the relations between ourrent and flux: 1 1 . a1NJ, io . a ovo , is a a 9V9 and @@I - 1 1 + i0 + 1 9 as well as the quantities illustrated in Fig. it is possible to describe the surface concentration of adsorbed molecules by Card 1/4 ---2 3/181/62/0()4/007/015/037 Interaction of molecular oxygen ... B102/B104 a ) di @0- - - (6). VO - V A (t) (NI ILO 0 0 Since 0 00 + 'Vg a) I it follows that if. 7- ie -'j'. di, (9). n (t) = i [ a, 0 If a a,,, then n(t) . I 0 a Ico - @@I)dt - S/a 9 and the reflection coefficient is given by k(t@ - 10 (t)/(i 000 + i g 00 if Ili is known, it is possible to calculate a 9 - (1 000 + i goo)INI . The validity of these relations is based on the experimental arrangement fulfilling certain conditions. This was carefully checked, the necessary linearity of I, (P ) and IOD (N being verif i ed . PI denotes the oxygen pressure in Card 2/10 S/181/62/004/007/015/037 Ynteraction of molecular oxygen B102/B104 the source chamber. The apparatus proved suitable for work with molecular beams in a very high vacuum (UP to 3-5-10- 10 mm Hg) and also for investiga- tions on N21 00, etc. There are 6 figures. ASSOCIATION: Inatitut fiziki AN USSR Kiyev (Institute of ?hyeias AS UkrSSR Kiyev) S U B *,.' 1T T E DFebruary 10, 1962 Card 5/0 DIMUN, I.M.; ZINGUMAN, YA.P.; ISHCHUK, V.A.; MORMZOVSKIY V A IfonequLlibrium electron emission from a p - n-junction in silicon. Fiz. tver. tels, 4 no.8:2015-2025 Ag 162. (KMA 15:11) 1. Institut fiziki AN UkrSSR, Kiyev. - (Electrons-Fmission) (Junction transistors) z 044,@@ IA., a A*@ AL A. fqm At- IL IL IRV 1. 10 It I C- Itr a C. to (c am rw "m comb-mal Nmtfft r Us 9.%Metrzo rosionlact"a *"[At, 4c ftemwim me slocku" G=wmzft*liiiiio in. A. ftrm ("w), *mw, Ams. jrio- 1-mvittee on bteiin PrIze#i (of the Council of Hintaters USSH) In the fields of science and Inventions announce* that the rolltsriag scientific works, poptilar OCIP.0- tiiic bookep and textbooks have been submitted ror owpatItUm for Malin Prizes for tht varz! 1952 =d 1950-3. (S=tv'ZVa Nuiturs Moacm, go. 22-40, 20 Feb 3 Apr 1954) Tit= ule--d'al-cin, 7.3. V. 1'. V.D. Sinde-I'l-v) I.,,'* Title of WorIc &.=InAted by Ai i- Ai@-c al'@" Z 1530: V-3o6o4, 7 JUI.V 1954 KUTABAKIN, Tiktor Sergeyevich; NOROZOVSKLY, Vladisir Titchonovich; SMUNT, NP -0 1 Igor' Mtkhaylovich;IARIONUV, A.u.,-prOT-"G P-0-13ROUTTOF, A.M., 0 Imadidat takhnichaskikh nauk. redaktor; BOGM014)VA.M.F.. isda tell Sk17 redaktor; ZMATIN, I.M., tekhnicheskiy redaktor (Production, transformation and distribution of electric power in aircraft) Proizvodstvo, preobrazovanie I rasprodelente elektrizheskot energit as se-soletakh. Koskva, GosAnd-vo obor. promyshl.. 1956. 479 P- (141&4 9: 11) 1. Taveduyushchi7 kafedroy elektrooborudovantya samoletov 1 avtomobi- lay Moskovskogo anargeticheakogo inatituta imeni Holotovs, chlen- lcorrespondent Akadamti nauk SSSR (for larionov) (Slactricity in aeronautics) 1-1`2 OAC tj L) VU 2"V 9 9411 2 i;!*-@-715.j, Ejql 5 @jj A* 11-8 - ; is I I 1 2, :011-filpi PA. a . 0 2--1 - " l @ i '" ` K t 4 'ON CA F Ef .30V/24-59-2-12/30 AUTHORz_MQEaERXa@S@_T. (Moscow) TITLE: Tile Stability of'-identical Synchronous Generators Operated in Parallel (Ob ustoychivosti parallel'noy raboty od-not- ipn,ykh sinkbronnykh generatorov) PERIODICAL: Izvestiya Akademji nauk SSSR, Otdeleniye tekhniclaeskikh nauk, Energetika i avtomatika, 059, Nr 2, pp 77-86 (USSR) ABSTRACT: The paper by the same author in issue Nr 10, 1958, of this journal, is reproduced virtually without change. The load is assumed constant, and the problem is treated in terms of the relative motion of the rotors. The only changes are Fig 4 (which is new), the text and unnumbered equations between Eqs (25) and (@6), and the mathematical appendix in small type immediately above the references, which serves only to explain some of the quantities appear- ing in Eqs (19) to (24). The paper contains 6 figures and 4 Soviet references. SUBMITTED: December 18, 1958. Card 1/1 MOROZOVSKIr, V. T. . wChOic* Of OptimUM Co".nsstion Circuits for Autonomous Systmems Of Automatic Controi.ff paper presented at the First International Congress of th9 International Federation On Automatic Control (IFAC(p Koscow, 27 June - 7 July 1960. S/024/6o/ooo/oi/ol3/O28 AUTHOR: Morozavokiy. V,T (Moncow)9194/9355 TITLE: Tff-e-Kn-fluence of the Nature of the Load on the Stability of a Single Synchronous Alternator PERIODICAL: Izvestiya Akademii nauk SSSR, Otdeleniye tekhnicheskikh nauk, Energetika i avtomatika, 1960, Nr 1, pp 111-118 (USSR) ABSTRACT: In practice, a single alternator often works on a complex load. The alternator usually has a voltage regulator and is driven by a prime mover of commensurate output. The nature of the transient processes of speed stabilisation in a set of this kind depends very much on the change in amf and reactance of the generator on change of speed. The rogion of stable operation of such a set has also been found to cbpend on the nature of the load. The present article attempts to assess the influence of the nature of the load on the conditions of speed stability of such a set fitted with a governor on the prime mover and a voltage regulator on the alternator, with allowance for the amf and reactance of the alternator as a function of Cardl/5 speed. Because of the short duration of the electromagnetic S/024/6o/ooo/ol/013/028 elg4@115� The Influence of the Nature of the Load 0 tability of a Single Synchronous Alternator processes in the armature circuit, the aperiodic component of the stator current is neglected in this as in most other works. The differential equations of the generator may then be written for both instantaneous and r.m.s. values of current and voltage, so that the vector diagram of the machine may be used in formulating the differential equations, as has been done by other authors. With the usual types of prime mover the torque may be represented as a function of the speed, of a control parameter and of a parameter characterising the load on- the prime mover. All equ"tions are written in terms ofrelative increments, taking as a basis a given equilibrium condition. Eq (1) for the prime-mover torque is thus rewritten to the form of Eq (2); the equation for torque equilibrium on the prime mover shaft is expression (3). The load torque on the generator shaft is given by expression (4). Ignoring the ohmic resistance of the stator winding, the vector diagram and equivalent Card2/5 circuit of the generator are drawn in Figures I and 2, S/024/6o/ooo/oi/ol3/028 Elg44fll5atability of a Single The Influence of the Mature of the Load 0 Synchronous Alternator respectively. Expression (6) is written for the alternator field voltage and expression (7) for the alternator emf. The latter is solved and substituted into the expression for the field voltage to obtain expression (8). Finally, expressions (14) - (17) are derived and Figure 3 shows diagrammatically the way in which they are used to represent the set. It is assumed that voltage and speed control are affected only in proportion to the deviation from the normal values and that the governors are inertia links. The characteristic equation of such a system is then of the form of Eq (20). Several particular cases are next considered. If there are no speed controllers and voltage regulators the characteristic equation is of the second order, Eq (21). Here, the condition of stability is given by expression (22) and the corresponding stability curves may be derived from Figure 4. If the set only has a voltage regulator, the characteristic equation is of Card3/5 S/024/6o/ooo/oi/oi3/028 The Influence of the Nature of the LoKA94040M Stability of a Single Synchronous Alternator the form of expression (23) and the condition of stability is given by expression (24). Comparison of expressions (22) and (24) shows that the voltage regulator reduces the region of stability. Consideration is then given to the general case of a machine with a speed governor and a voltage regulator. Figure 5 shows a stability curve for the characteristic equation (20) for given values of the various time- constants of a 30 kVA alternator driven by a gas turbine. The curve shows that the inductive nature of the load extends the region of stable operation. The influence of the nature of the load and of the voltage regulator on the region of stable operation is illustrated by Figure 6. The oscillograms show the change of speed (Curve 1) and of voltage (Curve 2) and the coordinates of the speed control element (Curve 3) for a synchronous alternator driven by a gas turbine of commensurate output. The three-phase 400 c/s alternator operated on resistive Card4/5 and resistive-reactive load both with and without a voltage S/024/6o/ooo/ol/013/028 a o The Influen--e of the Nature of the LJA9443M Stability of a Single Synchronous Alternator regulator. The oscillograms of Figure 6a and b correspond to no-load, Figure 6a being taken with a voltage-regulator and 6b without. It will be seen that in the latter case the process of speed stabilisation is more stable. The next two oscillograms correspond to half and full resistive load. The bottom oscillogram relates to an application _. of reactive load to the alternator carrying half resistive load when provided with a voltage regulator. It will be seen that connection of reactive load promotes stabilisation of the system. This confirms the theoretical conclusions, namely, that the voltage controller impairs stability, that increasing the resistive lead restricts the region of stability and increase of reactive load extends it. There are 6 figures and 4 Soviet references. SUBMITTED: September 1, 1959 Card 5/5 24408 3ZILA@ S/024/61/000/002/oo6/oA 3 Eo6l/E135 AUTIJOR: Morozovskiy, V.T. (Moscow) TITLE: On the rational choice of a structure of compensating cross-links in multi-variable systems of automatic regulation PEPIUDICALl Izvestlya Akademii nauk SSSR, Otdeleniye tokhnicheakikh nauk, Energetika i avtomatika, 1961, No.2, pp.92-105 TEXTt Multi-variable coupled systems of automatic control are considered, in which the number of controlled variables is equal to the number of command inputs. In general there exist both direct and feedback cross-links between the controllers and the controlled plants. The cross-lInks between the controlled plants (or within a single controlled plant) are due to the properties of the plantj the controller cross-linka are compensating, that is they may be chosen to obtain the desired properties of the system. It is stated that multi-variable control systems are beat represented in inatrix form. It is shown that in the general case a system with multiple inputs and outputs can be represented in the form: Card 1/8 q) I 2408 S/024/61/000/002/Oo6/ol4 Eo6l/E135 On the rational choice of a structure of compensating cross-links in multi-variable systems of automatic regulation where h11 h12 h13 hIn H, (a) h2l. h22 h 23 h2n Ih nj hn2 hn3 . . . hnn] The h terms are functions of the Laplace variable a and are determined by the cross-links with the system. W, lAt q are column matrices, the elements of which are Laplace transforms of the outputs, command inputs and disturbances respectively. Such a system is then considered to be the controlled plant of the automatic control system shown in Fig.3, where R(a) is the controller. The controller can then be described like the controlled system byj ji - R(8) (h wheret Card 2/ 24408 S/024/61/000/002/006/ol4 Eo61/E135 On the rational choice of a structure of compensating cross-links in multi-variable systems of automatic regulation r11(s) r12(s) r13 (a) r21(s) r22(s) r23 (a) R(s) . . . . . . . . . . . . Lrnl(s) rn2 (a) rn3 (a) and 4, X and T are column matrices, k representing command inputs. The above control system can ... r1n(s) ... r2n(s) . . . . . . . ... rnn(s) the be represented by: @p = (I + H(s) R(s))- I (H(s) R(S) X + H(s)q) = Gq(s)q + G % (s)k (12) where G (a) is the closed loop transfer matrix with respect to the distarbances, and G%(9) the closed loop transfer matrix with respect to the command inputs. For the purposes of system synthesis it is advantageous to write down: Gh (a) = H(s) R(s) - H(s) R(s) G,(S) Card 3/8 U 2WO S/024/61/000/002/oo6/ol4 E061/E135 On the rational choice of a structure of compensating cross-links in multi-variable systems of automatic regulation Gq (a) = H(s) - H(s) R(s) G (a) (15) The matrix equations (14) and (15) are useful in the formulation of the transfer matrix of the system. They correspond to n2 algebraic equations connecting the elements of the left and right matrices. In these equations the transfer matrix of the controlled plant is fixed and so may be diagonal elements of the controller matrix. By solving the equations one can determine the elements of the controller matrix which will ensure the required properties of the system. A control system is then considered having two inputs and two outputs in which the variables are coupled by two feedback cross-links which are determined by the internal properties of the system. The conditions of autonomy of such a system are studied for various systems of compensations which are given in Table 1. W01(:), W02(s) represent the plant transfer functions ; Wpl(S)1 W P2() the controller transfer functional L12(s) and L21(s) the coupling transfer functions; and K12(s) and K21(s) the compensation transfer functions. The values of the compensating Card 4/8 h 24408 S/024/61/000/002/oo6/oi4 Eo6l/E135 On the rational choice of a structure of compensating cross-links in multi-variable systems of automatic regulation transfer functions which are required to ensure autonomy are tabulated. The conclusions drawn from the examination of the results of this tabulation are that the conditions of autonomy with respect to command input and disturbances are not in general identical, and that the beat conditions of autonomy are achieved where compensating links can be connected between the same points as the internal coupling 1-Inks. It is pointed out that not all the forms of compensation are equally achievable in practice and that each system must be considered separately. Further, it is stated that partial autonomy with respect to steady state conditions may be achieved by the use of links with simple gain only. A simple system with two inputs and two outputs is considered, in which; W = W = --i-, W @ W 10 L = L = 0.5 01 02 @ a P1 p2 I + 0.058' 12 21 in which the compensating links are K12 - K21 = K. The effects of a step increase of the command input in one channel on the output in the other is examined, and the results of an analogue simulation Card 5/8 2W108 S/024/6l/Ooo/oo2/oo6/ol4 Eo6l/E.135 On the rational choice of a structure of compensating cross-links in multi-variable systems of automatit regulation of the problem are quoted. It is concluded that for the particular system, the compensation scheme I of Table I is the best. Acknowledgments are expressed to G.V. Privalov for his assistance. There are 5 figures, 2 tables and 8 referencess 7 Soviet and I English. The English language reference reads as follows: Ref.1i M. Colomb, E. Usdin. A theory of multidimensional servosystem. J. Franklin Inst., V)52, V.253, Ne.l. SUBMITTED: January 28, 1961 Card 6/8 6 --S/0000 M A&M /64/060/000/028310300 T* OZ"ak -aut tic _cvntt!ol- -systems @: .-autonomous _-=dtidbiensional am kfiell 7@ @l @VAIAMMUAnthosti -Lipen-vrimenenip!-v-@-_ e t elkisk1kh 2d, Kiev, 1962; Teoriya Invariantitosti v statemakh laniya.--(Theory~bf-invarianca,-;-in:automatic contr ew) 4@rtowtuh4fiki0io- UPT4V ol syst -tru Y@`sdft -it aulci 964i 1 00" --digltal, ccm--i@-- bj4iriarae eory, TOPI t46r_@@ uationi-contra"yetem-stabil AM Aph tialwinliona"-, utowat-i"ontrol-@: e @-eolmne dit4imimt, (on-.',of-th&--trans- 74t-W -taissi rice's --and @--W6 - multidizensional-ACSO-Tie -author -then in- Oasrotms of t qc a-*.-- --f-t W-. th@ --autonomy-o 6618- -,of autonomous- aad--.-_-_l-_` -he- 4 --- awd-by- lour -diffiftear _lw_ f t ACRA". jgtgfi@_V*Aints of-thi-blo A- 7 NO REP BOTIo. 006 OTHER; 002 Card 2/1 20749 a 00 3 113 2-) AUT11uR; 'ilorv z ov.-,K;. 140!@c W, y TITLE A tneory of on-,ype rollpled uutc)m,ji,, -)wr(@, symmetric -.r,ip.1ngs 7 PERIODICAL AvtomatiKa : ct,@?m-kranika, V 22, TEXT. T:-,(, author of' t!.,- progent pap,,!, stwi,,-i ,n,@ of ing oyatem@i t,at lire@ (iquiwtlont tc ;jy i rr. @, x, r,, OqUal Ch-afln(116 Of thP U11tOM1.01 @:5nirol, -,(-%nocied t,,v rq.,a@ ziiL3,emaK% -,i', c mat ing3. A, Krascvskly dvurri,.Vanal ny, '6 regulirovan-.ya a ant isimmetrir:@nym.* j,.ryazya.,n- antisymmetric coupling3 in autrmati@. ccntro.1"; AVt,',Mr*tiia , eiemoei.rinikrt, 18, no 2. 1957@ Jr,* ,rc, ri -, - ---i I t; @, ;I- r r:. @@ : f s y m m,-- * r *. c a 1 r - r., d a P ' 1y mm F, ', r i r a coupiinga in guch 3ySt1-1m3 dnd dove- ---pe,J a lecrinique @.f examinir,g -n.-ype tw,:-shannell systpms witt, rantisymm-it ricui ;(-up@ingi; L)y M@--!r,, "' -M, --X transfer functions. In tne present paper, '.tla tect@niqu,@ is f,ir*Lr.-:- developed and extended to a 3pe,@ial Kind Of one-type Systems. Theae systems are (list ingui-3r.w] ty 3o-:.;.!1ed synchrcr-z,,ni-! lind it-rteng C a r d 11/.14, 2074@ A theory ---f - r@ t y e - u p cross c@-,uiA inFs. rz-r-d Fl-,, 1 shows the s@@home of, ri --;ne-3-p.-@ mul t 1-crannel sy 9 em. r I'T'i, two kinds of mut cn of t I.E, input ir d cj'j,ut rt, lnrat'c-o t d @ o - i , o.-I'j I r- h'. ar unita are introduced. 1' Averagod m,- I L,,ri value of the coordinates at input ;.r,,] outpu, of iri;@ Aeri* i -;,a i Uri i n denotes the number of @hannols. ri - frie riumtor -@f dri- a The coordinate mear, value for i id@r.*ical units ii t:-,q ia I , n -, (.1 ! x d@nc,@,@,,, me;,,r n L Xik K@ I i - t h g-ro u j., of unit i. x trio Va'Up of' t @.o I o k-th channel. 2 ) Relative mc-tion@l Co r r-c-, pond ing % t,, I i f input ari - it put coordi nate- s o 11 t n(- ident ical uni 1.3 TV'eequa t !on Xik.- @ xil - x ik (2) hc1da f or 'Le k-.i,, channe'.. 6Ln.- Iri r-:a'.1'y parameters can never be identical, the autt.or ai,icu'3se,; err, a 9 to whether an idealization Is pormiqiciible It Is shown t!.- linear multi-channe-1 sys',ems di-c-ia@iefl h@re, ar@L- "coarse" ir *:@e j-r-3@, of A. A. Andronov not explirej -re; und a :31iO't f'r m Card 2/4-1,-- t4 20749 ej f f C Z) f t c i -:l y v e '-'zLl c-?] tUnit of a anc-t cn@inn el- s t r: - C:.039 COUI)Iinco for I':, ric-a- n r C- ,-, c - 0 0 0 In %L output + i f r i t CrOsr, c t i 01-1- f-O,' t "ic re a t iv t i r'-. r S f er fu7lcti@)n of direct cr=,z@,p nce n :,-,@c c,? c;. c or. t i c Ll c 7 2 C1,0SO -0;,,: C, z 'Cn 31 of onc-type couj-'cd ... diucufmoud: 1 ) 'I I 10 i - t 11 i 6 ". n t i r "L I -.I n 'l t @'@ L r '1 .3 c c t e 6 t 7, 2 r c' au to croim back couplinf,,:, --,)r ti-.e functio,i, 'h(., equation xlk .rik* wj, n,,, 0 L,) rik mix XI) wix TV, XM "31 '"(1 Dx T-- is obtained for relative motiDn, and t:i(? equation Card 411V 20749 -@)ry of onc-tyj"e cou: I ed rL x(k 11-1 1 111 - 1; 1 Tlk k-1 k-1 'Tik wax k-1 i Ll f1f ux for avera6ed notion. 2 '@:-e 1-t @, llden, ica- un 41 tz@ are PC' cr." "o and crooo lback cou@)I-Jng-o. Ti-.e signalo of croso becv, ---re Sum%led up -.,fter the point from whi ch the cignals of diren cr- _r,2 taken, the oign-als of dircct crars P-re t'llc c'f cros@; E;r- cros,, couplings locato-11 wit-in cllc)'"s 1" 1-1 c 4 1- c @;urd 20749 theory of one-type coupled ... s/i 0 /022/ )C) 1 2 0 4- TViL3 - L@L,)(-TQ ntjx - Zil (IV, Ll)(X(k_xx - 2:(j xlk Owl - Zif B""t Tvi L, xi* ax -,r(jax TT WXL. __411. C ar d 6 n (n - 1) IV,L2 - L,L2 - (n - 2) nL,L,l 71 XtAf Bus k-1 (vVj - L, + nLj) Xlk zz k-l IV,+ + (n - (n