SCIENTIFIC ABSTRACT KIRITSEV, A.D. - KOSTYUK, D.I.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000825310014-7
• Release Decision: RIFPUB
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 4, 2017
• Sequence Number: 14
• Publication Date: December 31, 1967
• Content Type: SCIENCEAB

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--~CESSIO~

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AUTEOR~ Sokolov~ L. ~,{ Eiritsevr A. D.~ igdryuahohen~o, P. P'{ Eost~uohenko, N. T.

'TITLE~ Effect of for�in~ reduction ratio on mechanical ~ro~orties/of forgings
from a 2Ob. t-�ct of steel 45

0ITED 30IIRCE~ Sb. Nnuokuo tr. Zhdanovsk. m~tallur~, in-t,.~ep 8, 1962, 140-145

TOPIC TAG3~ forgin$ method, anisotropy forgin&, forging reduction ratio, steel 46

TRAN$IATI0~ The total forgin� reduction ratio is determined ss the ~roduot of
particular �orgin~ reduction ratio during/draw-out without takin~ into account
~he �or�in~ reduo~ion ra~io a. u~eet~!nt-'~ Inves%i~a~ions were carried ou~ on
for�in�s of ~0t in�eta �rc~ steel i5~ t0~ upsettin~ an~ elon�a~ion wl~h ukova
of 1.5 to 7.~AnisOtropy of meohanioal propertie~, that ,us. treater in train
direction, wis observed in retied motal~ sigma sub b siena sub s depend little
on �orging reduotion ratio and on ~he direotion o~ grain in ~he forging~ psi,
delta and ak change more markedly when forging reduction ratio increases. Forging
reduction ratio of 2.5 to $.0 should be oonsidered optimum in �orgingwithout

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L 19189-63
ACCESSION ~R, AR~004202

upsettizg~ in order to obtain leetroplo propertieel in' the case when there
upsetting optimum forging reduction ratio ia 3 to 4. Four figures, $ references,
I, ~ndlLua.

DATE AC~I 21Jun63

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HI]DA, ~oPo; K0~Tk'UCHENKO~ To~o
Studying the pathogenicity of yeastlike fungi of the genus Candida
isolated from pathological material. 7isnyk KyivoUno
biol. noo2~88-90 '62o

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PALETSKAYA, L.N.; LOBOVA, Ye.V.; LAVROV, A.P.; RABOC}~V, I.S.; BABAYEV, A.G.;
TRAFEZNtKOV, F.F.~KOS.TYUCHF3~K%V'P'; NOSOV, A.K.
Grigorl! l?Ich Dolenko, 1886-196A; an obituary. Pochvoveden!e
no.5~I19--120 My '65. (MIRA 18:5)

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KDSTIUCHEI~K~ V.V. (Leningr~d)

Acute erythremia. Kiln.med.33 no.7:6/~-69 J1 '55.(MDRA 8:12)

1. Iz kafedry g~spital'noy t erapii (nach-chlen-korreapondent
~.~N SSSR prof. N.S.Molcbanov) Voyenno-meditsinskoy ordena
Lenina akadenii imeni $.M.Kirova)
(POLVCYTHEMXA VF~RA
erythomic myelosia)

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~OSTYUK, A. ~ �
a rotating, ring un']er the e�~_c., of
Kostyzuk, A. G. - "On the elastic defor~_atlon of
~ntri~'uEal force~," (Gomout~tion of the ste~ tt=bine governor), T~dy Studench.
nauch.-~khn, o-va (Mosk. ener~et, in-t ~. Mo!oto~a), Is~u~ 3, 1949, P.
SO: U-A35), 14 August 53, (~topts 'Zh~na! 'nykh St~tgy, ~;o. 15, 1949.)

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(~ml~ ,l~*~t~l n.m~m"-~ �

CZA-RDP86-00513R000825310014-7

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"Some Problems of Creeping of Turbine ?:isks." S-ab 23 Yov 51, :.:oscow
Order of Lenin Power Eno~ineering Inst imeni V. !.!. 5fo]otov
Dissertations presented �or science and engineer'.nM de~rees in
l.~.oscc-w durin~ ]951.

fO: Sum. ~,~o. f,~O, 9 ~.lay 55

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1~05r~)I[, .ii,. O.
Elasticity and Plasticity, Plasticity, Creep, Strength (2265)
lnzhenern.vy Sbornik, Vol 15, 1953, pp 15-20

"Stresses in a Rotating. Disk During Creep"
Discusses creep of a rotating disk of varying thickness and presents the author's
solution by the method of successive approximations.
Referativa~Y Zhurnal--Mekhauika, No 2, Feb 54: $0: CW-30785, 28 July 1954~

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KOS~flJK, A, ~.

UBSR/~athemattcs -. Elasticity Theory

Sep/Oct 53 ~?

"Calculation of the Profile of a Revolving Disk For
Conditions of Creep,l'iA. G. Kostyuk, Moscow~-Mosc~
P~er Eng Inst

Priklad Matem i Mekhan, Vol 17, No 5, PP 615-618

Treats the problem of d~termining the profile of a
revolving disk under conditions of stationary creep
according to a given law of variation of stresses or'
strains along the radius. Assumes the temperature

~76T89

field to be polar-symmetrical and the law of creep
to be arbitrary. Presented 2~ Jun 53. Refers to a
related work of-:Yu. N. Rabotnov ("Disk of Uniform
Resistance," PMM,.Vol 12, No 4~ 1948).

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. ~O$'~Vtx, 'C~PHASE I BOOK EXPLOITATION 446
Sherstyuk, Aleksandr Nikolayevich
Ventllyatory 1 dymososy ~Yentilators and Exhaust Pans) Moscow, Oose-
nergolzdat, 1957. 183 p. 7,000 copies Printed.
Ed.: Nevel,son, M.I.; Tech. Ed.: Medvedev, L.�a.
PURPOSE: This .is a textbook on blowi
engineering lnstlt,,* ....... ng engines for students of power
gaged in doo~--~-~'~ ~nu ~ may al~o be useful to engineers en-
~m-A,~ aha operating sues equipment.
COVERAGE: This hoOk deals With design and operation of exhausters and
f~ns. Special emphasis is placed on forced draft fans used in
heat power plants. The book contains contributions of the Heat
Engineering Department of the Moscow Power Engineering Znstitute.
The author begins with the basic concepts of hydraulics and
proceeds to the use of models for fan design and selection.
Operation and testing of fans are also discussed. One chapter is
devoted to modern types of fans and exhausters manufactured in

Ventilators and Exhaust Fans 446

~..-~..-.'~ e of Power ~nglneerlng.
There are ~ references, of which 59 are Sbviet, 3 German, and
2 English.

TABLE 0~
CONTENTS:

.Fo~ewor~

.Introduction

1. Classification of blowin~ engines
2. Blowing engine applications
3. Brief historical survey

Oh. 1. Pundamentals of Hydraulics

1. Ber~oulli's equation. Total static and dynamic
pre s sure s '

2. Resistance of duct systems
Card 2/S

3

6

6

8

9

11

13

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Ventilators and Exhaust Fans

Ch. III. Exhausters and the Fans Used in Mills

1. Uses of exhausters and fans for mills and their
characteristic working conditions

2. Wear in exhauster wheel-blades and discs
Basic measures for preventing wear

4. Effect of ashes on exhauster performance

5. Fans used in mills

6. Design characteristics of exhausters and fans
used in mills

Ch. ZV. Axial-flow Fans

1. Working principle of axial-flow fans

2. Princtpsul schematic diagrams for ax~al-�1ow fan
design

48

5O

55

57

Ventilators and Exhaust Fans 446

3. AP~~:q~R ~e~n~. t$~ 19~/~ile CIA-RDP86-00513R0008::~310014-7"
4. Forces acting on grid profiles 63
5. Grid efficiency 67
6. Experimental data for flat-g~id design 68
7. &xlal-flow fan wheel 71
8. Axial-flow fan guiding and straightening elements.
Collectors and diffusers 77
R. Blade element efficiency, hydraulic efficiency and
overall efficiency of axial-flow fans 80

10. Designing axial-flow fans 82
card 5/8

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Ch. V. Fan Characteristics. Model Testing

446

1. Dimensional characteristics of fans 88

2. Calculating fan characteristics for various speeds and
specific gravities of gas based on experimentally
established characteristic8 for given speed and s~eoiflc
gravity S~)

3. Calculation of characteristics for geometrically similar
fans on the basis of model-test results 91

4. Dimensionless characteristics of fans 93
5. Testing with fan model 95
Ch. VI. Combined Performance o� Fans and Duct-Mork
1. Performance of a duct system with a single fan 103
2. ~an stability. Pulsation 106
Card 6/8

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VentiLators and E~haust Fan~ 446
3. Combined performance of sewral fans

4. Fan control

Cb. VII. Types of Fans and Exhausters

!.

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Types of centrifugal fans based on All-Union State
S~ndard 5976-55

2. Cent. rifugal fans and exhausters

'Selecting exhausters and fans by catalog

4. Remodeling centrifugal fans

5. Axlal-flow fans

Ch. VIII. Testing and Operating Fans and Exhausters

1. Testing exhauste~s and fans

C ~.'~l 7/~

.1 '], 0

143

142

15o

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$~biOYLO~I~H, Oeorgiy ~emenovich; TROYANO~$Z-IY, ]~oris Hikhsylovich; EOSTNJE,
A.G., r~.; ~Y~, L.Ys., tekhn,red.

[Steam t~bines; a col~ction of problems] Parole t~bl~;
ebornik za~ch, lzd. 2-~, d~. i peter. Hos~, Gos. ener~.
izd-vo, 1957. 2~ p. (~ 11:2)
(Steaa turbines--Problems, exercises, etc.)

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~u~OR: Kos ..... G., ~(~.Io sc ow)
TITI~: ' ~ff~beac[/ Tempera~re Field Duc. ~o Heat Shock in Cmmec~ion
wibh bhe Determination of The~,mai S~resses in Tt~bine Parts
-~ERIODI,;.~: Izvestiya Akademii nauk SS;SR O~deleniye bel.lhnicheskikh
nau:~. Energeuika i av~omatika; 175): iii' 3. Dp 85--89 (USSR)
~,STl~Ci~: I~ is assumed: (1) tha~ the ~-~,...,
of ~he bod~ rises rapidly bo a cert,,in ~,'a!~ and ~hen remains
steady; (2) that the quantity a.~/L~ is small, where v is
ti:ne,, a is the diffusivity and L ~s a ch~acteristic dim-
cnslon of th.e body; (5) tr~a~ the Bio~ cri'berJon ~/k is
laz'rje: ;'zhere m is the coefficient, c.f h~:.at oxcitauje and
2:~ th~:~ t:hr~rmal conducbi'ziuy; (~) '['ha? the hee. g flow is normal
co e;z~ ~s,~face og 'the body~ The ;' ~'~ ......
~ a~_.z ..... al equation corres-
ponding to these conditions is seb up, allcwinS for the
vat,Are of ~he s~face of the bod.7~ and solved approximaUeiy~
A formula is ehen derived fo~' bhe te.~.~.era�~,e in the region
of an edge formed by two s~faces of a co.r. pone~t meeting at
a right ~gle~ . The me,hod e~abJ, es the ~er~Ioerat~a field in
a se~!ess forged gas turbine rouor :o be '[~alcu!abed ~d the
temperam~re distribution ~u a drmu type of rocor is shovm
graphically (Fig ~) after 16 mtn tae time corresponding eo
C~d 1/2

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Linst;eady Te~,~lperature Field Due ~ Heat; oaoc~ .~n Cunnection ~,,~
Determination of Thermal Stresses ~ Turbine
the m~ma bempera~ure difference between the periphery
and the centre. The resulbs ~e com~ared with those of a
similar investigation by Molch~ov (~ef 2). The solution
is also applied bo the determination of the bempera~ure dis-
tribubion ~ a disc. There are ) figures and 2 Soviet ref-
erences.
ASSOCIA~ION: Moskovskiy energeticheskiy institut (Moscow Power
Institute )
S~MI~TED: J~ua~y 28, 1959.

Cmrd 2/2

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SOV/96-59-10-4/22
AUTHORS: Kostyuk~ A.G. (Cand. Tech. Scl.) and
~0kolov, V.$. (Engineer)
TITLE: Electrical Modelling of Temperature Distribution in
Turbine Rotors
PERIODICAL~ Teploenergetika, 19~9, Nr 10, pp 22-27 (USSR)
ABSTRACT: The axially-symmetrical temperature field of a turbine
rotor may be modelled for calculation by an integrator
type EGDA: it is sufficient to simulate a wedge-shaped
longitudinal sector of the rotor. For use with
integrator type EGDA-6/53 the model may be made of
several layers of electrically conducting paper, pasted
together as indicated in Fig 1. The method of selecting
the radius of each layer of paper is described with
reference to Fig la and a simple formula is given� In
order to check that a suitable number of oieces of paper
have been used and to determine the accuracy of the
method, the results of temperature field modelling are
compared with a standard based on accurate calculations
of steady-state thermal conductivity for severa~ simple
Card solids of rotation. For example, an accurate so~.ution of
]/~ the equations of thermal conductivity for a solid cylinder
with the boundary conditions indicated in Fig 2 may be

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~/e~'~t~leal Modelling of Temperature Distribution in Turbin~ Motors
represented by a series of the form shown in Eq (1)~
Results obtained from the model are compared wi~h
theoretical values derived from Eq (1) ~ Figs 3 an~ ~.~
Fig 3 shows the temperature distrib~tion a~ross a dis~
at the centre of the oylinder~ and Fig ~ the tempera~ur~

_a~is 9f_the ~lin,~ez.~ ,~ompa~ed
t a ue~ ~ound i'or a I'our~.layer mode!~
A method of modelling the roots of turbine blading is then
~:onsideredo ~en the blades are fixed into an a~ular
slot it is easy to model the temperature field by
selecting a strip of appropriate width and leogSD, t,:,
zepresent the resistance of the working part of the
blading and to represent the rotor and f~in~ zone by
means of a multi-layer wedge~ as shown in FiE lo %~en
the ends of the blades are fitted -' ~
~n,.o slots in the d.[s,~:
the rotor is not axially s~etrical in the flying z,,~e
and~ therefore, the tempera~re field of the Ci~in~ ;~aae
and of 'the actual rotor must be considered ~eps.~ate]-~.,,
Car~ 2/g ~ approximate method of modelling in this ~:ase J~
described on the assump'~ion that the t~mper~ture fi.~]~d ;,n
~he blade f~ing zone is approx~te.ly ur:lfozm, It: ~.~:
well established that the main heat flow tn the ~'~ot

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SOV/96-~9-10-h/22
Electrical Modelling of Temperature Distribution in Turbine Motors
fixing zone is directed from the periphery towards the
centre� It is accordingly possible to determine the
parameters of the equivalent plane model of a blade root
fixing for which the law of change of temperature in a
radial direction is close to the real one� Since the main
heat flow in the root fixing is radial, it is necessary
that the radial thermal conductivity of the fixing
details should be the same for the actual part and for its
plane model~ This condition is given by Eq (2), which may
be used to calculate the sections of the plane model at
the most important sections shown in Fig ~ Fig 5~ also
gives in dotted lines the outline o� the plane model and
in chain-dotted lines the outline of the actual fixing�
The requirement that the quantity of heat passin� ~.hrough
the corresponding boundary surfaces of the actual root
fixing and the plane model should be the same is represen.-
ted by Eq (3) which is used to define the heat.~transfer
coefficient at the model surfaces� The conditions at the
Card boundary surface between the root and the rotor are no*.
3/5 given� To establish them and to completely determine the
temperature field both in the root and in the rotor, it

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SOV/96..~9-!o-4/22
Electrical Modelling of Temperature Distribution in Turbine Motors
is first necessary to determine the equivalent parameters
of the root fixing which governs heat flow from the bi.nde
root to the rotor. These equivalent parameters are the
nominal heat-transfer coefficient and the nominal
temperature of the medium that govern the heat flcw fzom
the blade root to the rotor through the section
c~onsidered. The method of determining these equivalent
parameters is then described. The heat flow to the rotor
t. hrough the surface considered is given by Eq (~.),
which Eq (6) is easily derived, and this is used to
:~alculate the equivalent parameters~ From these para-
meters it is possible to determine the boundary
',~:onditions on the electr'-al model of the rotor near ~.he
blade root fixings and so - ,~etermine the temperature
field of the whole rotor. � ~ mulae used in t;he proced,3re
are derived. Heat exchange through gaps left between thc
blade root and the rotor is then considered�
Formulae (ll) are given for heat removed by the air
Card the blade roots and hence the heat flow formulae (13) to
~/~ (1~) are derived� The application of the resu!t~_ to
modelling is briefly explained.

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SOV/96-59-10-4/22
Electrical Modelling of Temperature Distribution in Turbine Motors
Models comprising three or four layers give sufficiently
accurate results with electrical integrator type
Card EGDA-6/~3. The method is applicable to all types of
5/5 rotor.
There are 6 figures and 3 Soviet references�
ASSOCIATION: Moskovskiy energeticheskiy institut
(Moscow Power Institute)

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~AMOILOI~ICIt, ~eorgiy Semenovich; KOSTlq]X, A.D. red.; BORIJ~07,
tekhn.redo '

[Present-day steam turbines] Sovremennye parovye turbl~y.
Moskva, Gos.energ. izd-vo, 1960. 127 p. (Biblioteka teplotekhntka,

(Steam turbines)

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A~.14007g~7 ' ' '
~OOK EXPLOiTATiON .........
Koscyu~, Ashol~d Glebovich (Candidate of' Technical Sciences, Docent)

Vibrations in turbomachines (Kolebaniya v'curbomashinakh) Moscow~
~[EI, 1961. 213 p. illus., biblio. Errata slip inserted
700 copies printed. Spon~orin$1 Agency: Hinisterstvo Vy*s~hego
i Srednego Spetslal'nogo Obrazovaniya RSFSR. Hoskovskiy ordena
Lenina energeticheskiy insgituC.

TOPIC TAGS: turbine, compressor, turbine vibraclon, compressor
vibration, rocor vibration, place vibration

PURPOSE AND COVERAGE: This is a ~ex~book used in the course on
tu.rbomachinery ac the H.o~kovskiy cnergeticheskiy
Power Engineering Institute). Special attention is given
vibr~tion calculation for rotor blades, rotors, and disks amd the
application of the basic theory of ~urbi~e vibration.

IASLE OF CONTENTS [Abrid�ed]:

}ncroducCion -- 3

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KHCHEYAN, Eh. Ye.; PAVLICHEV, A.F.;_KOSTYU~K~A.O'
Production of phthallc acids from the mixture of xylenes. ~him.pro~.
no.5~327-335 My t61. (~L~ 14:6)
(Phthalic acid) (Xylene)

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~KOSTYUK,~ ~ A.G.~ ~kand.tekhn.nauk; SHUVALOV, G.I.

Use of gas-turbine systems in large power plants.
8 no.5:3-6 ~ '61.
~ (Gas turbines)

Teploenergetika
(m:RA

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s/ ~ ~o/~ ? /oo~/o ~ ~ /o~ ~/o ~ ~
BT ~o/~:47

Ushakov, V D,~ ~ezh~rova, L. P., Oalata, L. A ~
Khusnutdinova, Z. $.,, ~edvedev, S. S, , Abkln, A ~
Khomlkovski30 P~ ~!,

TITLE

Polymerzzation of styrene and butadzene witi~ st~'rene In
emulszons under the action of initiating redox syssems~
I. E�fec% of the nature of peroxide compounds on ~he rate
of polymerization

PER IODIC.iL

Vys�k�m�leku!3arnMye soyedineniva, v. 5 no,. 1~
1716_.~722 ~ , , ,?

TEXT: Aim. of ~he present ~ork was the determination of the most active
,-nit'.a*:n,, redox ',vstemg for the polymerization o� butmt]ene wi+h stvren~
~n emulslon=~, and e~pecia[ly of the effect of the nature of peroxides on
~.he r~te o:' :miymerzzat~on. Nekal with 20 ~ of Na2SO4 and NaC[ and
m,~rso]ale ('~!wtur~ of Na salts of su]~'onic acids of :he ali:)hat~c series:
~, u Na) '~th / 5 ~, of NaC~ served as emu!slfler:~. Peroxides were used
' )5")) "

APPROVED FOR RELEASE: 06/14/2000 CTA-RDP86-00513R000825310014-7"

"APPROVED FOR RELEASE: 06/:1.4/2000 C1'A-RDP86-005:I. 3R0008253:I. 00:I.4-7

2~ fa
$/~ ~o/
Po!ymer~za~on of' styrene and .. BIlO/Bld7
ox~da:~ts (Table) Potassium ferrocyanide and ferrous pyrophosphate
comr~l~x (~V) served a:~ reducing agents The rate of Dolymeri~*,.~
}o~ez'm~ne..i either d~latometr~cally or from th~-yield

Fe'z':x:d~-~ :~f, so!ved :n ~ (~0 f~ ~toiutioaj, Etd ~he ca!cuia~ed al~ouat et

a~ ~ certa~t~ :emperatare by m~ans of medical ayr=-~Ze~, Subata..c.:~

:f~; ~.,).'. pc. tass:um f~rrocyanide The temperature ~a5

and 0 ; ~( ~'" ;~e~ht cf :sopr-,pyl b~nzer, e n;,'dr: peroxide
u~.',: iu c~:ncentra,i,jns s'quimolecular to hydr