SCIENTIFIC ABSTRACT P.N. CHERNOBROV - V.P. CHERNOBROVKIN

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000308520010-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 12, 2000
• Sequence Number: 10
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

CHERNOBIMV, P.N., dotsent
~ -
. Longevity and average life expectancy of the population of
.Douth Kazakhstan Province. Zdrav. Kaial-ch. 21 no.8.-3-6 161.
WIRA 14:9)
1. 1z kafedry organizatsii zdravookhraneniya i istorii meditsiny
(zav. - dotsent R.I.Samarin) Kamkhakogo meditainskogo instituta.
(SOUTH UZLMTAN FROVINCF~-LOMEVITY)

CHEM-10BROV F,N.
Sources of Kazakh popular medicine. Zdrav. Kazakh. 23 no*2:
77-80163. (ITIRA 16:10)
1. Iz kafedry organizataii zdravookhraneni-ya I istorii medi-
tsiny (zav. - prof. R.I.Samarin) Kazakhskogo neditsinskogo
instituta.
(KAZAKIISTM-MEDICILT, POPULAR)

CTIEPNOMOV S. IT.
."Determination of Nickel Admixtures in Cobalt by
!Spectral Analysis," S. M. Chernobrov, D. M.
Shvarts, Inst of Nickel, Cobalt and Tin Ind
",ZaVod Labn No 12, PP 1505, 1506
Used anal of sdstances in powder state to det
small amts.of Ni In Co. Method excludes localiza-
tion of Ni, vhichLUSually happens when ordinary
metal specimens are used, and facilitates prepn
.of otds. Single detn-, including preliminary
.chem treatment, takes 2-3 hrs. Av relative error

JPUS 1-.974-K
090: 17,63-9

A= vi;,ma op THs App~icztovr or xorr-
Kr=RULS
?early* L Praktika PrIzenaniYa 9. V. Ch:rutow
Xawobmwwkh Naterialov, Moscow,
1955, 1-264.

2AM or CoNrEfts
Foreword . . . . . . . . . . . . . . . . . . . . . . . .
Yo. A.. Partunanova. V. 1. Ph"100-Obecical
"
~
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lon-excharxcerv . . . . . . . . . . 3
teristice of
C
ALeksandrovs. L. S., Gapon, T. a.. Chmutov. K. V.
Investigation of th7e Physico-chemIcal Properties
of Ion-emahange Realus for their Rating . . . . ' * ' 16
fj
k
To. B.. Loney. I P. Cation Exchange --1
. . . . . . . . : . . . . . . . . . . . . 31 k
Loser. 1. P., line A. a., Trostyanakaya, Te. B.
Cone-irning T protlez of the structure of
balfophanol-foroaldehydo Ion Zxchango
Sorbents . 0
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Davydov, A. T.
Wt
- lbwbance by Domestic Ion Mxchangers . . . 40
*
'- A. Coacerning the Problem of t6
'y=
;;
ive fttractlon of Ions out of Eolutions . . . . 59
Prokhorov, P. 0. Anion Exchnnger Aging and the
Problem of Water I)eivnization. . . . . . . . . . . . .
v, 0. If., Vol f, 1. V. Results of the
o
W
atigation .. Ion ExchwW Ldxorbente of H=lc
Cr
Oubstanc*v .
"=k1y. T. V:
~.craphie ?'Atbod in the Study of 3orption
PhOnomerld, . . . . . . . . . . . . . . . . . . . . . . 120
A. A., Veni ley. A. A.. Okbrimenko, 0. 1.
of Quantitative Determination of the
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ti
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on
en
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bu
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roup an
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roup
Xechaves" by Titrajion . . . . . . . . . . . . . . . 245
Ze_Ldea. V. Y&., GqXvlik, Te. M.
-,;D*Rcktl Ion Exchante by Cation SxchAneers . . . . . .150
$0

USSR/Inorganic Chemistry Complex Compounds CO
Abs Jour : Referat Zhur - Rhimiya, No 2, 1957, 4o94
Puthor : Kolonina, N. P.
Title : On pH Value During Formation of Cobalt Hydroxides aL.d
Carbonates
Orig Pub : Zh. prikl. khimii, 1956, 29, No 5, 7011-70a
Abstract : By potentiometric titration using a glass electrode,a
determination was made at 60P of the p1l values during
the formation of cobaltous hydrates and Co carbonates.
It is shown that the pH of the beginning of formation
of precipitates on t1trntioxi of CoC12 with a solution
of NaOH decreases from 5.6 to 3-8; oil titration of
COC12 with a solution of 11-a CO3 It decreases from 5.45
to 3r9; on titration of C with a solution of
'0�04
Na2co3 it decreases from 5.5 to 4.4 with all increase in
the concentration of C02+ ill the initial solution from
5 to 100 g/liter. Composition of basic salts formed on
Card 1/2 - 11 -

USSR/Inorganic Chemistry - Complex Compota-ids C.
Abs Jour Referat Zhur - IGiimiya., No 2., 1957) 4094
addition of NaOH to COCI corresponds to the general
forn.ula CoCl2.nCO(OH)2' A20; from the equation of ac-
tivity product a linear correlation between pH and 1g c
has been determined, c being the concentration of C02+
in moles per 1 kg water. Experiments confirm this cor-
relation. In the system COC12-Na2CO is forried a Vreci-
pitate having the composition COC12-AICOC03 n,Co(OH)2'
x H 0. The pH value at which the precipitate separates,
ils in this instance practically the same as in the case
of the system CoC12-NaOH. A linear correlation between
pH and 1g c has also been determined in the case of the
system COS04-Na2CO I but the inclination of the
straight line in r9ation to the 1g c axis is less in
this instance than in the case of the chloride.
Card 2/2 - 12 -

SOV/137-58-9-18784
Translaiion from: Referativnyy zhurnal, Metallurgiya, 1958, Nr 9, p 89 (USSR)
AUTHORS: CZernobr ,�,~~j,,Porelik, Ye.M.
TITLE: Use of Ion Exchangers to Extract Nickel and Cobalt from Am-
monia Solutions (Primeneniye ionitov dlya izvlecheniya nikelya
i kobal'ta iz a,mmiachnykh rastvorov)
PERIODICAL: V sb.: Materialy Soveshchaniya po primencniyu obmena v
tsvetn. metallurgii. Moscow, 1957, pp 64-72
ABSTRACT: A description is presented of methods of extracting nonfer-
rous metals from NH3 solutions of low metal content. Sulfo-
carbon, (I), an ion exchanger made by sulfuric-acid treatment
of a natural carbon, was used. The rate of flow of the solution
was 1 m/hr in all experiments. In some experiments, deter-
mination of the dynamic exchange capacity (DEC) of I for Ni
was quantitatively determined. Experiments in Me simultan-
eous absorption of Ni and Co from ammonia solutions and in
extraction of the absorbed metals from the I were run in a
column 35 mrn in diameter, the thickness of the layer being
900 mrn and the quantity of I being 400 g. The initial solution
Card 1/Z contained 1 g Ni, 0.2 g Co, 50 g NH3 and 100 g (NH4)2CO3 /liter.

SOV/ 137-58-9-18784
Use of Ion Pxchanger5 to Extract Nickel and Cobalt (cont.)
The experiments showed that I possesses the capacity to absorb Ni and Go
from ammonia solutions. The DEC of I for Ni was found to be 0.5 and for
1~
1-o 12 mg equiv/g. The absorbed Ni is virtually completely extracted
from the I by the HZ ion; extraction of the Go is somewhat more difficult.
Joint absorption of the Ni and Go from ammonia solutions shows the Ni to be
the first to appear in the filter. The DEC of I in terms of the combined total
of Ni and Co ions is 1.9-2.0jo. When Ni and Co are displaced by 150
HZS04/liter, up to 9076 of the original Ni and tip to 8616 of the original Go
are extracted in the final fraction. The volume of the concentrated fraction
upon extraction is appx. one-tenth of the volume of the initial solution.
0. B.
1. Ammonia--Processing 2. Nickel--Separation 3. Copper_-Separaticn
4. Ammonia--Test results
Card 2/2

(~ t_ C ~- ~, ')
6-
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44
-
,
/
AUTHORs Chernobrov, S*M.j Candidate of Technical Sciences 28-4-16/35
------------
TITLEs ------------
Cobalt (Koballt)
PERIODICALs Standartizatsiyal 1957P # 49 PP 57-58 (USSR)
ABSTRAM The new standard for cobalt, rOCT 123-57, which will
replace roCT 123-49 on 1 October 1957, contains a new grade,
"K011, of high purity in addition to three other grades IM",
11K2'1 and "K311. The formerly used method of production by
thermal, recovery from cobalt oxide, gave a 99,25% pure cobalt,
which ib insufficiently pure. The author's institution -
Gipronikell - together with the combine Yuzhuralnikell,
started experiments in the obtaining of pure cobalt by elec-
trolysis in 1949. In 1950 the production of cobalt by use of
insoluble anodes was organized. The obtainp.'-.W metal was purer
than that obtained with the heat method, but still not suf-
ficiently pure. Gipronikell continued the work in 1956-1957
and obtained a dense metal which meets the conditions of the
new standard. The permissible contents of all impurities
(hydrogen, sulfur, manganese, nickel, copper, etc.) are indi-
cated. As the obtaining of a cobalt with a nickel content
not over 0.005% required a second electrolytic precipitation,
Card 112 this grade was omitted in the new standard as impractical.

Cobalt 28-4-16/35
The nickel content in the grade "K011 will have to be stipu-
lated in each order for the metal. It is,stated that for
some time past the fire-cobalt of grade "U"(produced by the
old method) approached the "K011 grade of the old standard
or the "K11' of the new in purity. Most metallic cobalt
produced by plants is of the old grade 11011.,
ASSOCIATIONi Gipronikell
AVAILABLEs Library of Congress
Card 2/2

P 1:-~ X A)O ~ A 0 V'f 5~ p,
WrHOR; GhernobrQvj 5. BI- 32-9-7/43
TITLE: Application of the Ion Exchange in the Analytical Chemistry of
Metals (Primeneniye ionnogo obmena v analiticheskoy khimii met-
allov)
FERIODICALi Zavodskaya Laboratoriyat 19571 Vol. 23, Nr 91 pp. lo52-1055 (USSR)
ABSTRACT: Here a survey on the most important papers on determination of
the metals according to the method of ion exchange chromatography
and on the theory of the process, which were published in the se-
cond half of 1953, is given. This survey is briefly summarized
in three chapterst 1) Theory of the ion exchange. Ion exchange
materials. 2) Methods of the! cation exchange. 3) Methods of the
anion exchange.
There are 61 references, 33 of which are Slavic.
AVAILABLE: Library of Congress.
Card 1/1

BRIA)ZERSKIY, N.A.; ORHOW, B.F.. prof., doktor, reti3entent; FILIN,
prof.doktor, retsenzent; MYFETS, Y.L., lond.tekhn.nauk, retsenzent;
GHHRNOP40Y,_S.X., red.; KAKAYLTA, O.H., red.izd-va; ATTOPOVIGH. H.K.,
+'~~nerede
[Carbonyls of metals] Karbonily metallov. Moskva, Cros.naucbno-
tekbn.izd-vo lit-ry po chernoi i tsvetnoi metallurgii, 1958.
372 P. (MIRA 11:7)
(Carbougs) (Organometallic compounds)

(A) 66557
SOV/81-59-15-52784
Translation from: Referativnyy zhurnal. Khimiya, 1959, Nr 15, p 69 (USSR)
AUTHORS: Chernobrov, S.M., Kolonina, N.P.
TITLE: On the Cathode Polarization in Electrolytic Deposition of Cobalt
PERIODICAL: Tr. Proyektn. i n.-i. in-ta "Gipronikell", 1958, Nr 1, PP 150-159
ABSTRACT: The cathode polarization (CP) in electric deposition of Co, depending on
the temperature (4o, 60 and 8oOc), the nature of the anions and H3BO3
additions, has been studied. CP decreases with an increase in the tempera-
ture and increases on adding H 3B0 and on substituting chloride solutions
by sulfate solutions. The dependLee ( f, lg i) is linear, in the case
of a chloride solution the transfer coefficient a = 0.7 - 0.8. Addi-
tions of H3DO increase the CP; in the presence of Cl--ions; CP is less
than in the Resence of SO 2--ions. The opinion has been expressed that
the deposition rate of Cc h determined by the stage of the discharge,
that H BO increases the activation energy of the discharge process and
that tge ~1--ions are specifically adsorbed on the cathode.
Z. Soloviyeva,;
Card 1/1

SMEWIS, Kh.L.; TATTS, A.Yu., OULTANITSKIT, B.S.; PAZMIIN, T.A., prof,,
doktor takhn.nauk, retsenzent; KHEYPITS, Th.H., kand.khim.nauk,
retsenzent; VMUGIN, V.N., kand.takhn.nauk, reteenzent; FImm,
A.Ta., kand.tokhn.nauk; retssnzent;.TSWTIM,.Ta.A., kand.takht.
nauk. retsenzent; MUCOT, G.S., inzh.. retsonzent; KRIVORUCHEMO,
V.Y., inzh,, retsenzent;.CHHUOBROV,,S.M., red.; ARKHANGELISLATA,
H.S.. red.izd-va; ILEYMUN. M.R., takhn.red.
(Kagnesium metallurgy] Metallurgiia magniia. Izd.2., parer. i
dop. Moskva, Gon.nauchno-tekhn.izd-vo lit-ry po chernoi i tovetnoi
metallurgii, 1960. 479 p. (KIRA 13:5)
(Kagneoium--Metallurgy)

CHERNOEROV, S.M... otv. red.; LASKORIN B N.p red.; KLYACHKO, V.A.,
LAN;Z
-TOd-.,-MA?EROVA, Ya.A., red.;
A.Z.f red.; VITTIKH,
M.V.p red.; SHOSTAK, F.T., red.; SAVENKO, O.D.,, red.;
ZYKOVA, V.V., red.; GIAZYRINA, D.M., red.; ALFERGVA, P.F.,
tekhn. red.
(Theory and practice of ion exchange] Teoriia i praktika ion-
nogo obmena; trudy. Alma-Ata, Izd-vo AN Kaz.SSR 1963 186 p.
~MIRA i7:3)
1. Kazakhstanskaye respublikanskoye nauclmo-tekbnichoskoye so-
veshchaniye po ionnomu obmenu. 1962. (MIRA

CHICRNOBROV. S.M.
Development of the methods of ion exchange in the analytical chemistry
of metals (survey). Zav.lab. 29 no.11:1281-1288 t63.
(MIRA 16:12)

BOGDANOV, O.S., doktor tekhn. nauk, prof., otv. red.; BRAND, V.Yu.,
kand. tekhn. nauk, red.; DERKACH, V.G., doktor tekhn. nauk,
red.; ZAKHVATKIN, V.K., red.; OLEVSKIY, V.A.,, kand. tekhn.
nauk, red.; LOKONOV, M.F., kand. tekhn. nauk, red.; PODNEK,
A.K., kand. tekhn. naukj red.; TUSEYEV, A.A., red.;
FINKELISHTEYN, G.A., kand. tekhn. nauk, red.; F%IIN,,Ya.I.,
kand. tekhn. nauk,
kand. tekhn. nauk, red.; LHER011
red.; KUTUZOVA, L.M., red.
[Transactions of the Fourth Scientific Technological Session
of the Scientific Research Institute for Mechanical Concentra-
tion of Minerals) Trudy IV nauchno-tekhnicheskoi sessii insti-
tuta MEKHANOBR. Leningrad, 1961. 665 p. (MIRA 17:5)
1. Leningrad. Nauabno-issledovatellskiy i proyektnyy institut
mekhanicheskoy obrabotki poleznykh iskopayemykh.

CHERNOBROV No ptlchnik~.
On the path tawsa~d -tba g6ala-i4t Afin6Vitors. Sov. profaoiuzy 2Q
n6oitl6-17 Jt: 164. (KIRA l7i2)
1, Sovkhoz "Tlxdryaz6vokiy" Nikolayevskov oblasti; chlen Nikolayevskogo
oblastnogo sellskogo soveta professionaLlInykh soyuzov.

CHEMOTAOVAI-T-K*--
.....
Prevention of birth inJury in tranaverve and oUique poaition
of the f etus,. Vop. okhr.- materin. dets. 8 no.1:59-63 163
(MRA 17 t2)
1. Iz kliniki alcusherstva i ginekologii ( zav. - prof. G.H.
Smirnov) Ryazanskogo meditsinskogo inatituta.,

CHERNOBROW V~K,
Infl.uence, of prolonger; prcv-,nanf~y -;ri the cc,-,irc-e and outccme of
labor. Naurlh.trutr R-*az.med.1rst. 18 no.2-1237-243 16~.
Ili atonorpliologi ml chwigps in the in prc,~onged orrpiancy.
Ibid. -2/-~. A 'I
1. Kafedra akusherstva i frlnekolui,ii prof. G.114.Sn.-imov)
z-
T~razanskoryo meditsinskogo instituta.

C;
CATEGORY Parri Animals.
General Problems.
ABS. JOUR. I RZhBiol., No. 3.4 1959, Noi 3.1971
-)7 Ch;:,rnobrovenko, P. S.
Tho Methods of Strc,-n.-
L- _,thening Lho Feed B
in Kolkhozes of tho Vovo1iezhs?.qya Oblast'*
OR 1,73.. PUBt Zap. Voronozhs1c. q.-kh. in-ta, 19,58, 27. No 3,
25j.-26---
tract.
No abs
Card- 1/1

CHMMOBROVINA, S. M.; ZHIGALITSEVAp M. I.
Preliminary'resulto of using electric equipment in orchards
in Moldavia. Izv. AN Mold. SSR no.9:68-75 (162.
MIRA 16%1)
(Moldavia-Fruit-Diseases and posts)
(Moldavia-Insect traps)

CJqERNOBYO -B
Sow data on electric equipment used in the field of plmt
protection against flying egricultural pests. ~ I;V. AN Mold.
SSR no.9838," '62. (MIRA 16: 1)
(insect traps)

C V k~ I
Subject USSR/Aeronautics AID P - 3472
Card 1/1 Pub. 135 - 7/20
Author : Chernobrovkin, A., Col.
Title : Winter sports for pilots
Periodical Vest. voz. flota, 12, 32-35, D 1955
Abstract The author lists various winter sports and games
considered advisable for the general training of
pilots.
Institution None
Submitted No date

MX; NK% AP7001081 SOURCE CODE: UR/0439/661045/003/0375/0%-#32
AUTHOR~ ~35
Chernobrovina, S. M.-
ORG: Kishinev State University (Kishinevskiy gosudarstvennyy universitet);
Institute of AppTied Physics-,AN Moldavian SSR, Kishinev (Institut prikladnoy fiziki
emii nauk Moldavskoy
TITLE: Application of ultraviolet-ray sources to insect pest control6
SOURCE: Zoologicheskiy zhurnal, v. 45, no. 3, 1966, 375-382
TOPIC TAGS: insect, insect reproduction, disease vector, insecticide, pest,
ultraviolet light
ABSTRACT: The following genera of the insects were tested with respect to their
response to visible light including the ultraviolet light region: Homoptera,
Cicadina, Psylloidea, Aphidoidea, Coccoidea, Coleoptera, Cerambycidae,
Scarabaeidae, Curculionidae, Ipidae, Diptera, Lepidoptera, Tortricidae, Cossidae,
Gracilariidae, Glyphipterygidae, Plutellidae, Hyponomeutidae, LyC;-._-ttidae,
Cemiostomidae, Coleophoriidae, Gelechfidae, Pieridae, Lasiocampidae, Orgyidae,
Noctuidae, Arctiidae, Aegerfidae, and Hymenoptera. The actual field testing
'Card 1/2 UDC: 595.7:579.6

ACC NR: AP7001081
indicates that it is mainly the young unfertilized or nulliparous females that are
attracted to light. By the selective application of various light sources it is
possible to attract predominantly harmful or innocuous insects. The former may
subsequently be exterminated by insecticides~It is concluded that light sources of
various types could be used for selective attraction of different insect species, thus
making it possible to estimate the insect population and reproduction of a given
genus and to carry out a series of studies related to the disease-vector problem.
Ox~ig. art. has: 2 figures and 7 tables. [WA-501
SUB CODE: 06/SUBM DA,rE: none/ORIG REF: 009/OT.H REF: 005/
212

A. F.
Dissertation: "Investigation of the Turbocyclorie Vlet'hod of Cleaning a DuA-Laden Flow. ~l
Cand Tech Sci, Plloscow~.6rder of Labor Red Banner/HiFher Technical ichool i:-~cri P-awman,
31 Mkv 54. Vechernyaya Moskwd, Moscow, 21 MaY 54.
SO: SLE 2e4, 26 Nyov 1954

CvieRr4o6PWKIN, A-P.
USSR/Engineering - Gas Turbines FD-i454
Card 1/1 Pub. 41-8/17
Author Chernobro-,rkin, A. P., Moscow
Title Investigation of a new system for purification of a dust-laden
stream
Periodical : Izv. AN SSSR. Otd. tekh. nauk 7, 77-86, Jul 54
Abstract : Describes new 'centrifugal-type experimental plant for purification of
dust-laden air stream to be used in conjunction with gas turbine oper-
ating on solid fuel. Gives results of experiments conducted on above-
mentioned plant for determination of following: degree of purifica-
tion of gas at various peripheral speeds of turbocyclone, effect of
various concentrations of dust on degree of purification at a given
peripheral speed, fractional degree of purification, and hydraulic loss
of turbocyclone. Diagrams; graphs; tables. Three references.
Institution :
Submitted : July 16, 1954

UVAROV, V-V., prof., doktor tekhn.nauk; IM)NDTkNSKIY, L.S., konstruktor;
014IROV, V.S., insh.; CHMWOBROVKI&_.At9,,# kand.tekhn.nauk, dote.;
V-Pf 0 1nzh.
SMRGOVSKIY, R.I., :inzh !, ~U F
The 6.000 hp. gas turbine locomotive constructed by the Kolomns.
Plant. Izv.vys.ucheb.zav.; mashinoetr. no.6:io4-lo8 '58.
(MIRA 12:8)
1. Hoskovskoye vyaeheye takhnichaskoye uchiliahche im. Baumana
i Kolomenakiy t lovozoBtroitellnvy zavod im. Kuybyeheva.
lGas turbine locomotives)

SOV96-59-10-2/212
AUTHORS: Uvarov, V.V. (Dr.Tech.Sci ), Qhernobrovkin, A.P. (Cand.
Tech.Sci.). Beknev, V.S. ~Cand.T_e_cHT.5-6-17r-,
Manushin, t.A. (Engineer) and Pankov, O.M. (Engineer)
TITLE: The Development of High Output Gas-turbine Sets
PERIODICAL: Teploonergetika, 1959, Nr 10, pp 8-17 (USSR)
ABSTRACT: The availability of gas and oil for power station fuel
makes the use of gas turbines economically attractive,
yet they are still looked upon as essentially small- or
medium-output machines. Although the Khar1kov Turbine
Works has designed a gas turbine of 50 MW and the
Leningrad Metal Works one of 100 MW, the possibility of
designing gas turbines of 300 MW and more has not been
fully studied. Theoretical investigations at the Moscow
Technical High School have shown that it is quite
possible to develop gas turbines with outputs up to
300 MW or more at gas temperatures of 700-750 0C. Output
can be raised by a combination of the following factors;
increasing the axial velocity at the outlet from the last
stages of the turbines and using special diffusers;
Card 1/7 replacing the regenerator by additional coolers and
intermediate combustion chambers, with simultaneous

SOV/96-59-10-2/22
The Development of High Output Gas-turbine Sets
increase in pressure to 60-80 atms; and driving the
generator from the high- o:~ medium-pressu.-e shaft of the
gas turbine. These factors are then considered
separately in more detail. Axial outlet velocities are
made low to avoid high outlet losses whi,::h may, however,
be reduced by the use of a diffuser. Diffusers present
certain problems. The Moscow Tech-nic-al High School has
investigated a diffuser that is represented diagrammati-
cally in Fig 1. On leaving the blading of the last
stages, gas passes through rows of fixed blades in wh4j-(,,h
it is retarded and turned through an angle. Fig 1 shows
three rows of blades but it may be necessary tc, use four
to turn the flow through 90 degrees. The overall
efficiency of such diffusers should be 75-86%, but this
requires experimental proof. In an exp6rimental .-ig the
width of the gas flow was 80 mm, at a mean diameter of
240 mm. The Ts-diagram for the diffuser is inoluded in
Fig I and efficiency formulae are given. The outlet
Card 2/7 velocity from the Leningrad Metal Works 100-MW gas turbine
is about 130 m/sec; in the absence of a diffuser the
associated loss is about 2 kcal/kg and with a diffuser it
is about 0.6 kcal/kg. If the speed is ID.Creased to

sov/96-59-10-2/22
The Development of High Output Gas-turbine Sets
260 m/sec the output is almost doubled and becomes 195 MW;
the outlet loss with a diffuser is 2.4 kcal/kg, or without
one 8 kcal/kg, which increases the fuel consumption by 9%.
The effect-of cutting out the regenerator and increasing
the pressure is then considered and the design of Brown
Boveri turbines at Livorno, Betznau and in Peru are
discussed. The general conclusion is that gas turbines
with regeneration have considerable aerodynamic loss and
it is interesting to note that recent Brown Boveri
turbines are made without a regenerator. Efficiency
calculations were made on four cycles% cyclesl and II
have regeneration; cycles III and IV do not, but have an
increased number of coolers and intermediate combustion
chambers. The optimum value of pressure increase was
chosen for each cycle. Ts-diagrams for the various
cycles are shown in Fig 2 and the main operating and
performance data are given in Table 1. Examination of
the data shows that all the cycles have about the same
efficiency, but with no regeneration the number of turbine
Card 3/7 stages Increasest for example, from seven stages in
cycle I to ten stages in cycle IV. The number of

SOV/96-59-10-2/22
The Development of High Output Gas-turbine Sets
compressor stages will also be increased in a similar WaYo
Much greater outputs can be obtained from the cycles
without regenerators. A Jiagram of the turbine and
compressor layout for operation on cycle III is given in
Fig 3, in which turbine Nr )+ may have either single or
double flow. The turbine outlet temperature is 82 OK
which is the same as for cycle 1 but the pressure is
2.66 atm, whilst for cycle I it is 1.04 atm. The output
that can be obtained from ~,ycle III is a little over
three and a half times that obtainable f-rom cycle 1.
whilst with cycle 11 the possible output is appreoiably
lower than for cycle I. The effect of driving the
generator from the high- or medii)n-piessure turbine shaft
is then considered. A somewhat similar arrangement to
that shown in Fig 3 was used by Brown Boveri at Bet
and Peru, but the circuit of Fig 3 offers certain
advantages. The governor may oontrol the fuel consumption
in the three combustion chambers and can ensure the best
load distribution between the various turbines. A number
Card 4/7 of output and efficiency calculations are then made.
Eq (4) gives the output per up-it area of flow and Eq (5)
the efficiency. Stresses due to centriPagaa force are

sov/96-59-10-2/22
The Development of High Output Gas-turbine Sets
proportional to the area of flow and the permissible
stress depends on the temperature and the steel. For
the purposes of the calculation steel IKhl3 was assumed,
and calculated values of temperature and efficiency are
given in Table 2. Calculated values of output per unit
area of flow are given in Table 3 in MW/m2. Table 3
shows the extent to which the maximum output is reduced
by the use of regeneration; thus with cycle IV the
output is over three and a half times that of cycle I
for the same efficiency of 37.4%. In the Leningrad
Metal Works 100-MW gas turbine the output area from the
last stage is about 2.7 m2, which with cycle I would give
an output of 117.6 MW and with cycle IV 415 MW9 if double
exhaust were used. Other cycles of somewhat higher
efficiency but somewhat lower output are possible. The
compressor and turbine efficiency data were assessed on
the basis of the comparatively small Brown Bovari
L
turbines; higher efficiency and Reynolds numbers would
be obtained for large turbines of 200=400 Y1W. as indicated
in Tables 5 and 6. For a large turbine an overall
Card 5/7 efficiency of about 40% would be expected, Figs 47 5 and
6 show the Ts-diagrams for cycle I, cycle IV and the

SOV/96-59-10-2/22
The Development of High Output Gas-turbine Sets
.cycle of the Leningrad Metal Works 100-MW turbine
respectively.. Calculated -;-alues of efficiency for all
three cycles are given in Table !+ in whiz~h the turbine
output is given in megawatts per square metro of exhaust
area. It follows from the data givtin dn Tables 3 and 1+
that if the generator turbine has a single exhaust,
Outputs UP to 300 MW can ba obtained with an outlet
velocity loss of 1+% and an outlet area of 2.5-2.7 M2. It
would be relatively simple -to construct a turbine of
200 MW with a single flow. or 400 MW with double flow,
and an efficiency of about 40%. Allowing somewhat highei
losses it should be possible to build a 600 MW gas
turbine with double flow and an efficiency of about 39%.
Questions of cooler surface area and quantity of cooling
water are then considered and it is shown t"hat the 300 MW
gas turbine would only require about one seventh the
cooling water of a 300 MW steam turbine. The results of
a number of strength calcu.1ations are then given,
particularly for the blading, and recozded in Tables
Card and 6. It is concluded that it would 'be quite pra,~ti(~able
6/7 to-build-gas turbines of 1+00 MW or even SOO MW. The
weight of a 300 MW turbine using cyole IV and the circuit

SOV/96-59-10-2/22
The Development of High Output Gas-turbine Sets
of Fig 3 would be about 1200 tons, excluding the weight,
of the pipework. A weight of 5-6 kg/kW (excluding the
alternator) is to be expected. The calculation of
permissible bending stress on the blades is of great
interest as it largely governs the amount of metal re-
quired in the turbine. The article does not consider
the cycle with high-pressure regeneration. This cycle
is somewhat more efficient than those considered, but
gives rather lower output than cycle IV. Moreover, the
design of a high-pressure regenerator presents a number
of problemsy but before a final choice of cycle is made
it will be necessary to consider the cycle with high-
pressure regeneration.
Card 7/7 There are 6 figures, 6 tables and 4 references, of which
2 are Soviet and 2 German.
ASSOCIATION: Moskovskoye vyssheye tekhnicheskoye uchilishche
(Moscow School of Higher Techniml Eduzation)

CHI RMOPERITEM, A. P. / Al 4 -/~
Gazovyye turbiny fb. F C Rc-jfNil
_7V.V. Ivarov rL Mloskva, Mashgiz, 1960.
.L. --.r
140 L'1_7 p. illus., dia&s graphs, tables. (Sovetskoye
~6shinostro)7eniye v 10059-1965 g;~
Bibliographyt p. 140- Z-141-7

6/14~/60/000/002/004/020
D221/D302
AUTHOR: Chernobrovkin, A.P., Candidate of Technical Sciences
TITLE: On selecting a locomotive gas turbine installation
PERIODICAL: Izvestiya vysehikh uchebnykh zavedeniy. Mashino-
stroyeniyep no. 2, 1960, 40 - 51
TEXT: The coefficient of efficiency of single-shaft gas turbines
made abroad is 16-18 %, compared to 26-28 % of steam locomotives.
This is, howevert compensated by a greater power per weight of the
formerg as well as by cheaper fuel used in gas turbines.The single-
shaft installation with electrical transmission has 19-20 % effi-
ciency at maximum output# and this drops when the load is reduced.
The 3500 HP'gas turbine at the Kolomna Steam Locomotive Factory
weighs 9 tons compared to 30 tons of the electrical transmission.
The Department of Oteam and Gas Turbines at MVTU im. Bauman consi-
dered various schemes of economical gas turbine sets for the Kolom-
na Plant. The arrangement with a regenerator was not successful.
The introduction of intermediate cooling and after-burning resulted
Card 1/3

5/145/60/000//002/004/020
On selecting a locomotive gas D221/D302
in a marked improvement unsavings and calculations revealed that
the efficiency may reach 28-29 %.The arrangement consists of a two-
shaft set with after-burning between the high and medium pressure
turbines that are mounted on the same shaft as the high pressure
compressor. The cooler can be cut off during winter. The author
considers the variation of fuel consumption at different loads of
gas turbines with intermediate cooling and after-burning. Higher
efficiency with relatively little design complication can be en- -
sured when higher gas temperature is used. This also results in mi-
nimum dimensions for the equipment. The d-esigned variant envisages
a power of 7000 HP with a gas temperature of 11000C, and cooling
both stator and rotor blades of the first stages. Two-cascade air
compression is chosen to ensure a ratio of pressure increase of
Ir -18o The design provides cooling by air drawn from the last stage
k
of the compressor. The internal cavities of blades and the radia-
tors that are welded to blade roots are filled with the liquid
heat carrier. The unit has a coefficient of efficiency of 30 %.
The inclusion of a cooler between the cascade of the compressor can
bring further improvement. Overall dimensions of this set are equal
Card 2/3

S/145/60/000/002/004/020
On selecting a locomotive gas ... D221/D302
to the size of a gas turbine made by the Kolomna Factory that is
half its power, and where the gas temperature is 7300C. The author
includes a tabulated comparison of projectap all of which have a
electrical transmission. The latter can be discarded because mecha-
nical tranSMiBBion has a greater efficiency. Its use inetead of an
electrical tranamission,will enhance the efficiency coefficient of
sets and also reduce their weight. There are 8 figures, 1 table
and 3 Soviet-bloc references.
ASSOCIATION: MVTU im. Baumana (MVTU im. Bauman)
SUBMITTED: December 15, 1959
1. Moskovskoye vyssheye tekhnicheskoye uchilishche imeni Baumana.
(Gas turbine locomotives--Design and Construction)
Card 3/3

'~_~_OBROVKINq A.P.p kand.tekhn.nauk..4otsent
Locomotive gas-turbine units. Izv.vys.ucheb.zav.; mas4hostr. no.3:135-
146 160. (MIn 14:3)
M6skovskoys tekhnicheskoye uchilisbche imenj N.E. Balmamp.
TZhe-ve Gas turbine)
Locomotives,

UVAROV, Vladimir Vasillyevicb; BEEND, Viktor Sorgeyevich; GKYA7,NOV,
Nikolay Dmitriyevicb; 111KHALITSEV, Vsevolod Yev,genlyevich;
I,TUSATOV, Aleksandr Konstantinovich; PCHELK31', Yuriv. Nikhqlovich;
CUMOBROVK324 Alek Petrovich- YUNOSHEV, Viktor Dmitriyevich -
BART j e. .. kand, te naukq reteenzent; GALATIOVA, N.S.s inzh.,
red. izd-va; UVAROVA, A.F.., tekhn. red.
(Gas-turbine units for locomotives; design and cz-aculation]Loko-
zotivrWe gazoturbinnyo ustanovki; raschet i proaktirovanie. (By]
V.V.Uvarov i dr. Moakva, 14ashgiz 1962 547 p. (KHA 15;9)
(Gas-turbine locomotivesj . -

UVAROV, V.V., doktor takhn.saukpprof.; CHERNOEBOVKIN. A.P., dotsent, kand.tekbn.nauk;
MAIIUSHIN~ E*.A., inzh, mmmmmmmmm~ ---
Higb-power gas-turbine unit with a high pressure of the actuating fluid.
lzv.vyx.ucheb.zav.;mmahinoBtr.no.1:130-139 163. (mRA 160)
1. Hookovskoye vvasheys tokhnicheskoye uchilishche imeni Baumana.
(Gas turbines)

7
~-ACC -N& AP65155-25 SOURCE CODE z UW/6596T657655766576567/0016
AUTHOR: Uvarov, V. V. (1?octoi~of technical sciencest Professor); Beknev, V. So (Can-
didate of technical sciences); Kilthalltsev, V, Yea (Candidate of technical sciences);
(CmxUdate of technical sciences); Lapin, Yu. Do (Engineer)
:Cherepnin, L. So (Engineer) 'VD
Z3
~~.ORGt MM in* Bauman
-TrIVIEt High-efficiency 200 magawatt.gas-turbine installation
SOURCE: TeploenergetiJmo no- 5, 1965. 7-16
TOPIC TAGS: gas turbine, electric power plant
ABSTRACT: The advantages of building a high pressure non-regenerativo 200 megawatt-
'gas-turbine installation with an approximate weight factor of 3.5 kgjk-%r are describedi
This factor Is 2.5 tims.smaller' than in steam gas installations and seven tives
smaller than in,steam power Installations. Calculations indicate that a gas-turbine
installation requires about 50% lower capital investment as compared to a steam power
installationj lowers the- volwe and-aost of the main strxicture three times and the
we
~cost per )dlowatt-hour not less than 15%. The possibility of building po rful gas-
turbine, installations with gwter"rature.of 750-BOOOC is indicated* Adoption of
still higher temperature up to 3200 C. vill increase the efficiency. to 53-55% and
double the powere Orig'* art. has: 10 figures and 5 tables$ fad-J
SUB.CODE: 10 SUM, DATE t none ORIG REF: 006 OT11 FX- F; 001
Card 1/1 uws 621.438.001.5

CH2Pl,,lOBROVYU-,,, A. I.
CHERNOBROVKIN, A. 1. 0. Inzh. i IVANOVA, A. V. 0. Ml. Nauchn. Sotr., ILIFA) N. P.
Kand. Tekhn. lqauk
Akademiya Kommunallnogo Khozyayatva isi. K. D. Pamfilova
Meropriyatiya po borlbe s korroziyey stalln.,*h Krovell Page 70
SO: Collection.9 of Anngtotigns ot �cientific Research Work on CojWtructio, cgnplet2d
in 1250,
llosccd, 1951

AUTHORs Chernobrovkin, B.S., Engineer, 28-6-7/40
TITLE: Plotting of Nomograms for the Determination of Allowances and
Tolerances by the Principle of Equal Allowance Lines (Postroye-
niye nomogramm dlya opredeleniya, pripuskov i dopuskov po printsi-
pu liniy ravnogo pripuska)
PERIODICAL: Standartizatsiya$ 1957, # 6, pp 25 - 28 (USSR)
ABSTRACTt In " FOOT 7062,54 "-standard for allowances and tolerances
of steel forgings produced"by free forging in presses the re-
commendations are subdivided in forging-size groups within
which the allowance remains equal. In this way, one and the
same allowance is recommended for the largest and the smal-
lest forging of a group. The difference in length and diameter
of the largest forging in a group and the smallest in the
next group is only 1 mm, while the allowance increases by
8 mm. The author suggests nomograms, plotted by himself, for
allowances and tolerances. These would eliminate the un-
necessary machining caused by the state regulations.
There are 2 graphs and 2 sketches.
ASSOCIATION: Uralmashzavod
AVAILABLE: Library of Congress
Card 1/1 1. Industry-USSR 2. Forging-Standards

UiIKOV, Grigoriy Georgiyevich; KOLTUN, Sergey Ivanovich, inzh.;
NPROV, Vaoiliy Prokhoroviali, inzh.;. Poris
Sergeyelvich, inch.; POLYAKOV, V.P., inzh., retnenzent;;_kAZJW0Y*
Box*# inzh., retsenzent; KONIKOV, A.S., dotsent, red.; DUGINA,
4,Ao, tekhn.red.
(Forging operational Kuznechnoo proizvodstvo* Izd,3., ippr. i
dop. Moskva, Gos.nauohno-tekhnJzd-vo mashinostroit~lit-iy, 1959.
447,P. -(KIRA 12:8)
1. Uralmeahzavod 4for Koltun, Chernobrovkin). 2. Sverdlovskiy
zavod transportnogd mashinootroyaniya (for Raumov).
(Forging)

LEBEDEV., Aleksandr Aleksandrovich, doktor tekhn. nauk,, prof.;
CHER110BROMKIN, Lev Semenovich; THACHMO.. Ya.Ye.., retsenzent;
~TY
retsenzent; XMYFETS,
N.A., doktor tekhn. nauk., retsenzent; GORTSUYEVA, N.A., red.
izd-va; ROZHIN, V.P., tekhn. red.
[Dynamics of the flight of pilotless aircraft]Dinarnika poleta
bespilotrWkh letatellpykh apparatov. Pod red. A.A.Lebedeva.
Moskvap Oboron~lz, 1962* 51+8 P- (MRA 15:12)
(Aerodynamics) (Guided missiles)

8/0147/64/000/001/0037/0046
ACCESSION NR: AP4033038
AUTHOR: Chernobrovidn, L. 8.
.................. .
TITLE: Determination of the relative fuel mans and dumat capacity of an aircraft when
its law of motion is prescribed
SOURCE: MUZ. Avintsionneya tekhnika, no. 1, 1964, 37-46
TOPIC TAGS: aircraft, fuel, fuel mass, thrust, thrust capacity, aircraft design, mach
number drag, angle of attack, rocket engine, altitude, alight altitude, jet engine, trajec-
tory, aircraft trajectory, aircraft gravity, Idnematics
ABSTRACT- The author notes that, in the design of aircraft, it frequently becomes
necessary to determine the relaUve mass of the fuel Pf = mf and the thrust
Mr
F(t) = 21"hich ensure flight according to a prescribed law. Some techniques for
Mrg
accomplishing this are discussed and It Is pointed out thtt, in general, In order to deter-
mine the relative mass of the fuel and the fluvat It is Asceseary to integrate a system of
Card 1/6

ACCESSION NR: AP403303.8
motion equations for the aircraft, Involving the use of extremely time-consuming nu-
merical methods. On the other hand, an analytical solution of this problem is possible
only if certain assumptions are made, the fundamental assumption consisting of the fact
that the angle of attack is considered to be prescribed, as a result of which the drag (head
resistance) factor ex is a function only of the M number, In the present article the author
has posed the problem of finding approximate algebraic expressions for pf and ~W free of, A:
any constraints on the fOrm of the trajectory of the aircraft (previously this had been
accomplished by other Investigators, for roctilinear flight), In addition to the assumption
made above, two additional assumptions were made. 1. The angle of attnck 0( and the
setting angle of the engine relative Ito the axis of the hull Wenct are small, so that
) v:e-I 2 The specific thrust of th constant and is equal to the
cOs V"Ve e engine Is
mean valt eng in the prescribed range of speeds, flight altitudes, and engine operating
conditions (this assumption is almost always acceptable in liquid- and solid-fuel rocket
engines, since In these engines Pengr_ changes within narrow limits; for jet engines the
assumption P const. is accepUible only in the event that the range of speeds of the
n .. t
aircraft is note llige). The second section of the paper deals with the derivation of the
calculation formulas For the relative fuel mass the author obtains the following formula::2
V!
+ (SIR 0, + 4 ali 104
9 6
Vt- V
P + _I- -CP_+_(2$1n.40'3+B1F101)t
Card 2/5 6

ACCBSSION NR-. Amnon
and for the thrust of the ship at the beginning, middlo, and and of the flight time:
+ sill Do' + (2)
9
+ sin (0.6 + A"O.S) I&, + qOAQO'Sj (3)
75, (kL~+ 510 0) (1 -~ PT ) + ql71'.
9 - - (4)
The valued 0. 5, found in these formulas, Is determined by the expression:
75dt - 0,5 + 0.6.
PYA I-,
4 P,, p,
Three special cases are -considered an the basis of the formulas derived: c_
1) if the traje
tory is rectilinear and accifleration Is constant (that is, .0 = coast and V Y1 - VO = coast);
2) if the flight occurs at constant altitude and constant speed (0 - 0, V = const), as charac-
teristical in the case of aircraft; 3) if energy losses for overcoming We forces of gravity,
Card 3

ACCESSION NR: AP4033038
and drag equal zero. The above-described method for computing pf gives good results if the
functions V(t), Q(t), c< (t) are smooth. However, occasionally the kinematic characteristics
at several points of the trajectory may undergo sharp changes. The author points out that, 'In
these cases, in order to increase the accuracy of the computation, the trajectory must be
broken down into sections. Several examples of this kind of operation are considered in the
paper. An evaluation of the accuracy of the formulae derived was made on the basis of nu-
merical computations, for which trajectories with a rather wide range of characteristics were
selected. These data are given in Table I of the Enclosure. The results show that, for all
their simplicity, the approximate formulae have an extremely small error. Thus, they may
be recommended for practical use, in which case it will almost always be possible to limit
the computations to the first approximation, having recourse to the second approximation
only in those individual cases In which increased accuracy Is a requisite. Orig. art. has:
35 formulas 5 figures and 2 tables.
ASSOCIATION: none
SUBMUTED: 03Sep63 DATE ACQ: 11May64 ENCL; 01
SUB CODE: AC NO REP SOV: 003 OTHE R: 000
Card 4/5

ACCMION NR: AP4033038 ENCLOSURE: 01
Table 1. Trajectory Characteristics
No. of Speed V m Angle of Inclination 9 Height H KM
example of the trajectory
Ho
H0, 5
Hi
1 t2 15" 2 7.5 17.5
2 v = 600 +
3 450' 2 16.9 44.4
3
40 150 2 8.2 17.5

4 V = 600 +
3 t 0
45
2
19
44.4
6 1
2 150 2 8.6 17.5
6 V=1200-7(60-t) 45* 2 20 44.4
7 0-90-2.4910-3S 2 16 25
20
8 V-400+ 3 t 0 - 2.49 - 10-3 S 2 6.75, 25
9 V - 600 + 480 t 0 16 16 16'
-Ti-
(at 0