SCIENTIFIC ABSTRACT BORISAVLJEVIC, R. - BORISENKO, A. I.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000206320008-0
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 9, 2000
• Sequence Number: 8
• Publication Date: December 31, 1967
• Content Type: SCIENCEAB

BORISAVLTEVIC, Ru2m; FML, Franjaj KOSANOVIC, Duro
Application of the Bak*r-Philippoff equation in-determining
internal viscosity of pol-ymethylmethaerylate and the dimethylit-
aconate-styrol copolymer. Glas Hem dr Z7 no.7/89355-366 f62
1. Galenika Development Laboratory for Scientific Research in
the Organic and Pharmaceutical Chemistry, Belgrade-Zemm/

BORISAVLJMC, Ruza; MAMUZIC, Rast)-oj.; MIHAILOVIC, Mihailo Lj.
.. ...... ..... -.- - -
N-benzoyphthalimide,. Pt-4- Glas Hem dr 27 no.7/8089-395,162.
1. Faculty of Science, Institute of Chemistry, Beograd.

BoRisAVLJ.EVIC, Ruza,- BGSNJAK, Jovan; MAMUZIC, Rastko I.; 14IHALLOVIC,
'dIvUlo LJO
N-banzoylpthalimide. Ft. 2. Glas Hem dr 27 no*5/6.-299-)Il 162.
1. Institute of Chemistry,, Faculty of Sciencesj, Beograd.

ACC NR'- AP60321309 SOURCE CODE: YU/0001/66/000/009/1621/1624
AUTHOR: Boris;~y1jeyic,_Ruzq (Graduate chemist; Advisor; Beograd-Zemun);
Kosanovic, Dur (Graduate chemist; Advisor; Beograd-Zemun)
P
ORG: (Borisavljevicl Research Laboratory "Galenika" (Razvojne laboratorije
Galenika"); [Ko'sanovic] Pharmaceutical and Chemical Industry "Galenika"
(Farm aceutsko-hemijske industrije "Galenika")
TITLE: Development of methacrylate and acrylate production
SOURCE: Tehnika, no. 9, 1966, 1621-1624
TOPIC TAGS: methacrylate, acrylate, methacrylate production, acrylate
production
ABSTRACT: Development of methacrylate and acrylate production and the raw
material for such production are reviewed. A description of industrial processes
currently in use is given. Certain production methods are discussed 'for possible
future application. The acetone cyanohydrin and isobutylene (Escambia) prosesses
are the two-methods involved in the production of methyl methacrylate. For the
production of acrylate, five methods are presently in use: the ethylene cyanohydrin,
LCard I / 2 UDC: 678,744=8Q1

propiolactone, carbonyl (Reppels), acrylonitrile, and propylene processes.
[Based on authors' abstract] [KS]
SUB CODE: 07, 11 /SUBM DATE: none/ORIGREF: 001/SOVREP: 001/
OTH REF: 013t
2/2
~Card

ACC iNZ-. AP6032807 SOURCE CODE: IrTj/oool/661000/009/1600/1604
AUTHOR: Borisavlievic. R. (Graduate chemist; Advisor); Despic, A. (Doctor;
Graduate engineer; Associate professor); Kosanovic, D. (Graduate engineer;
Advisor)
ORG: [Borisavljcvic] Research Laboratory "Galenika", Belgrade-Zemun (Razvojne
laboratorije "Galenika"); [Despic] Division of Chemical Technology, Belgrade
University (Tehnoloskogr fakulteta Univerzteta u Beogradu); [Kosanovic] Pharma-
ceutical and chemical Industry "Galenika", Belgrade-Zemun (Farmaceutsko-
hemijske industrije "Galenika")
TITLE: Contribution to the study of methacrylacetone polymerization
SOURCE: Tehnika, no. 9, 1966, 1600-1604
TOPIC TAGS: polymerization, polymerization catalyst, methacrylacetone,
methylmethacrylate, intrinsic viscosity
ABSTRACT: Radical type bulk polymerization of methacrylacetone was studied in
the 0-10016 conversion range at various temperatures (50, 60, 70 and 80C) and
with different amounts of -azo-iso-butyronitrile as polymerization catalyst
C,rd l/ 2 UDC:'678. 744=861

.Rk1UU3ZB07
(0. 3%, 0. 516 and 17o). The results are compared with those obtained for methyl-
1 methacrylate polymerization. It was found that there is considerable similarity
!between the two'processes with the rate of the former being considerably lower and
1the gel effect somewhat less pronounced. The change in molecular weight during
Polymerization was also investigated. The relation between the intrinsic viscosity
and the molecular weight 'I 0.= KMI was a:ssumed and the constants were found
experimentally to be K = 6. 8 x10-5 and a = 0. 8. 'Molecular weight distribution
ifunction was* obtained by fractionation of a sample of the polymer resulting from
lpolymerization at 500 with 0. 5% of the catalyst. Orict. art. has: 3 figures. [Authors'
,abstract)
!SUE CODE: 07/SU13M DATE: none/ORIG REF: 003/SOV REF: 003/OTH REF: 016/
2/2

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The rowtim ad H"
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--=4 ~ou t6 " &in in the ivactim of lignin with hezu-
i methyleimetrantine. This reaction can be used as an
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Jan Micks

.. I I .. 1, "' , .I *t ~ :,," . I . . I . I '. , I - . . .
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~i. .I: ~ 1. .

Met Method for Determining the Total Sulfur Content of Sulfite Liquor@." p. 98.2ram,
Vol. 9. no. 4, Apr. 1954.
SO: Ust Jkrope Accessions List, Vol- 3, No- 9, September 1954, Lib. of Congress

Borig.ek, R.
Absorption tower helps in the regeneration of sulfur dioxide.
p1 195. PAPIR A CFLULOSA. (Ministerstvo lesu a drevarskeho-
prumyslu) Praha. Vol. 9, no. 9, Sept. 1954-
SCIURCE:, EFAL - LC Vol. 5 No. 10 Oct. 1956

"Su4nestel Methol for (~xick Determination of 502 in Gases." p. 108, Praha, Vol. 9, no. 5,
May 1954.
SO: Iket laropean Accessions List, Vol- 3, No. 9, September 1954, Lib. of Congress

-Bori - k, R. - -
Improvement of the regenration of sulfur dioxide. p. 257, PAPIR A
CEUJLOSA. (Ministerstvo lesu a drevarskeho pruWslu) Praha. Vol. 10.,
no. 12, Dec. 1955-
Source: EFAL w Vol. 5, No. 10 Oct. 1956

T
the affia of _"UU6Uk Con
.UgaL ,V'-
rbc,oloi,ical ~rqpertleg of the Itnt li4t colloidal and
asp5ndmm.
lsiava' Ulech.).
Sammwrl)__'~' th"ry
f org. dig.
'P_O~!'ngtAg_'ht'.g)c'nItO-. bef""'tc &111F~iDn is devrIc'Ped and thL,
~gnhl compin froin wmae iiulfi Ite liquor
zz studkd. '1~10 5trbffimtlckn Of COIIGkL-J amd r1imlogim) I
MPU-ti~-s of -miner-at c2ay of SirmsLian inner Alptu pan with
acid is dftA'ffbtd find compared to tle
t3r,j,S. Jan
A

13ORISEK,R., drAnz.; MIVARIK, F., inz.
Mechanism of sulfite delignification at high temperatures.
Sbor eel pap no.U47-67- ~62.

r%vruf .1 -rT I% If 411Y ,
USSR/Medicine Pharmacophysiology FD-864
Card 1/1 Pub-30 - 15/18
Author : Borisenka, R. V.
Title : The results of investigations oo the toxicity of manganese compounds and
alloys containing manganese
Periodical Farm. i toks. 17, 54-50, Jul/Aug 54
Abstract Experiments on frogs showed that manganese has a definite effect on
the nervous system and possesses various degrees of toxicity depend-
ing upon the compound in which it is introduced into an organism.
Soluble manganese compounds like manganese chloride were found to be
the most toxic. The toxicity of manganese in alloys was found to de-
pend upon and vary with the other elements in the alloys. Ferromanganese
proved to be more toxic than silicomanganese. Manganese dioxide and a
physiological solution containing manganese were also tested. The re-
sults of the experiments are presented on three graphs and two charts.
Nine Soviet references are cited.
Institution Chair of Labor Hygiene (Hea 'd - Prof. Z. I. Izrael'son) of the I Moscow
Order of Lenin Medical Institute
Submitted

- 1---, ~_ I "I
BORISMO, A.; SHIPOV, Yu. T
j
Condition of the Japanese laboring class. Sots. trad no.2:40-47
_v 158. (MIRA 11:1)
(Japan--Labor and laboring classes)

BORISENK09 A.
Give daily attention to educational work among employees. Sov.
profsoiuzy 17 no. 2:"-/+5 Ja 161. (MIRA 14:2)
1. Predsedatelf Rostovskogo obkoma profsoyuza rabotnikov
gosuchre-zhdeniy.
(Rostov Province-Labor and laboring classes-Education)

BORISENKO, A.; SHASTITKO, V.
Economic efficiency of foreign trade in socialist countries.
Vnesh..torg. 42 no.5:24-31 162. (MM 15:4)
(Communist countries-Commerce)

BORISMO, A.A., in2hener.
Level Indicator. ]Cnergetik 3 no-5:11 0 '53. (MLRA 6:10)
(Water meters)

BOPISENKO, A.A.$ Meter.
Welding nickel-chromium
wire. Bnargetik 2 no.1:20 Ja 154.
(MIaA 7:1)
(Slec,tric wire)

BORISENNO., A.A.-
Gas escape in davelopmnt workings. Zap. LGI 46 no.1:3-5 '62.
(MIRA 16:6)
(Mine gases)

--BQUSE-IIK-O,-,.~.o:-.-(Stavropol 1)
Establishing a regional study museum in the Krasnogorskaya
Secondary School. Stavropol Territory. Geog. v shkole
23 no. 6:65-66 N-D 160. (MRA 13:11)
(Krasnogorekays (Stavropol Territory)-Geographical museums)

BORISENKOP A.A.p kand.tokhn.nauk
Efficiency of degasifying aeams by development mining. Ugol' 39
no.2:55-57 F 164. (MITRA 17:3)
1. Shakhta No.18 kombinata Vorkutugoll.

30RISINKO, A.I.
Vortex layer method for solTing problems on flow past bodies.
Sbornstrudelabeprobebystr.sash. 3:89-111 153. (MA 9: 9)
(72uld dynamles)

BORISEIIKO, A.I.; GOROEURKIII, A.?., kandidat tekhnicheskikh nauk.
~, o:n-the investigation of ventilation and coolinr of enclosed
electric machines. Sbor.trad.lab.probl.bystr.mash. no.4:141-
150 '53. (MLRA 7:12)
(Blectric machinery--Ventilation)

BORISNIMO, A.I., k-ndidat tekhnicheskikh, nauk.
Theory of hydrodynamic lattices of circular cylinders. Sbor.
trud.lab.probl.bystr.mash. no.4:39-67 154. (KOA 7:12)
(EIydrodynamics)

-Kiv-
- -- I ---,

BORISRNKO, A.I.
;,:_''. ... ~ 4
Using the vortax layer method for solving problems @a a streamlines.
around solid, bodies. Sbor. trud. lab. probl.bystr. mash. zo-5:195-
197 155, (MLR& 9:2)
(Stretesokii, L.N.) (Tortox-motion) (Fluid dynamics)

BORISE11NO, h. I.
,Velocity and Temperature Field in a Fluid Layer Between Two
Plates with a Relative, Mutually Parallel Motion," by A. 1.
Borisenko, Khar1kov Aviation Institute, PrZkladna Mekhanika,
Vol 2, No 14, 1956, pp 425-437
The author presents an accurate solution of the problem on the dis-
tribution of temperature and velocity in a layer of liquid (and gas)
between two flat plates, one of vbIch is In parallel motion vith the
other stationary plate. The problem is solved by an analysis of the dif-
fusion of energy for any type of relationship change between the coef-
ficients or viscosity and beat conauctivity and temperature.
Sum 1239

SOV/124-58-5-5349
Translation frorn: Referativnyy zhurnal, Mekhanika, 1958, Nr 5, p 55 (USSR.)
AUTHOR: Borisenko, A.I.
TITLE: The Flow Past a Hydrodynamic Cascade of Elliptical Cylinders
(Obtekaniye gidrodinamicheskoy reshetki elliptic he s kikh tsilin-
drov)
PERIODICAL: Sb. tr. Labor. gidravl. mashin, AN UkrSSR, 1956, Nr 6,
pp 59-73
ABSTRACT: An integral equation is written and solved %vith respect to
the distribution of vortices along the contours of ellipses in a
cascade of elliptical cylinders exposed to a plane stationary
potential flow of an incompressible fluid. The solution to the
equation is obtained by the method of expansion into a series, a
method previously used by the author for the particular case of
a cascade of circular cylinders [ Sb. tr. Labor. problem by-
strokhodnykh mashin i mekhanizmov (Symposium on "Labora-
tory Problems of High-speed Machinery and Mechanisms), AN
UkYSSR, 1953, Nr 4, pp 39-67; also, RZhMekh, 1954, Nr 2,
abstract 2095] . The other method of solving the problem in
Card 1/2 question is well known [ Voytashevskiy, D.A., Raschety i

SOV/124-58-5-5349
I The Flow Past a Hydrodynamic Cascade of Elliptical Cylinders
issledovaniya gidrodinamicheskikh reshetok (Analysis and Investigations of
Hydrodynamic Cascades), Gos. '6.-tekhn. izd-vo mashinostroit. lit-ry, Mos-
cow, 1953; also, RZhMekh, 1953, Nr 2, abstract 6511.
G.Yu. Stepanov
1. Fluid fiow--~Iatbematical analysis 2. llydrodynamic research--USSR
Card 2/2

B sggg-A ilp kandidat takhnichookikh nauk; Y=OVSKIY, Ye.I., inzhanar.
Thermal resistance of the air gap in electric machines. Vast. elektro-
prom. 28 n9.3:53-56 Mr 157. (KLU 10:4)
1. Xharikovskiy aviatsieuW instituA i Kharikovskiy elektromekhaniche-
skly saved,
(Electric machines)
it

A
AUTHOR: Borisenko, A.I., Candidate of Technical Sciences and
~~ovskiy, E.I., Engineer. lio-6-V24
TITLE: Heat transfer in asymmetrically-heated ducts in elec-
trical machines. (Teplootdacha, v asimmetrichno nagreva-
yemykh kanalakh elektricheskikh mashin.)
PERIODICAL: "Vestnik Elelctro-promyshlennostill (Journal of the Elec-
trical I ustry)1,9,%&J;25,No.6, pp.21-26 (U.S.S.R.)
ABSTRACT: The cooling of some parts of electrical machines may
be considered as heat transfer from a uniformly heated
wall to a flow of air or other gas along the wall. The
conditions are always those of turbulent flow. If both
the walls of the plane duct give out an equal quantity
of heat the temperature distribution is symmetrical
relative to the axis of the duct and heat transfer can
be calculated by existing formulae. If the walls of the
duct contain heat sources of different intensity or if
one wall contains no heat sources the temperature dis-
tribution will not be symmetrical and the duct may be
Card 3:/5 described as asymmetrically-heated. Such cases are
often met in practice.
The article then considers steady turbulent flow of
01

Heat transfer in asymmetrically-heated ducts iii elec-
trical machines. (Cont.) ilo-6-V24
an incompiessible gas between two stationary parallel
walls. The pressure gradient along the duct, the inten-
sity of the heat source (and therefore the temperature
gradient) will be considered constant. In accordance
with modern views on the flow of liquid and heat trans-
fer in it, account must simultaneously be taken of the
action of two physical processes; olderlessmixing by
the exchange of small volumes of liquid which depends
on the conditions of flow and molecular mixing.
Since the mechanisms of internal friction and heat
conduction are the same, expressions may be written for
the tangential stress and heat flux density for laminar
flow. Similar equations are then written for turbulent
flow and for the total frictional stress and beat flux
density nomal to the direction of movement. An expre-
ssion is then given for the quantity of beat transmitted
in the direction of mo-,,-ement for unit time per unit
sectional area and then an expression is written, the
first term of which corresponds to the increase in in-
ternal energy of an element of gas flowing along the
Card 2/5 duct, and the second characterises the quantity of heat
reaching the element of gas from neiGhbouring layers
by turbulent and molecular conductivity. The equation

Heat transfer in asymmetricall7-heated ducts in elec-
trical machines. (Cont.) lio-6-7/24
will cover the case when the lower walls of the duct is
heat-insulated and contains no source of heat and the
other is heated. Otber cases can be obtained by summ-
ating individual solutions. The appropriate equations
are then derived and are finally expressed in terms of
dimensionless magnitudes.
The distribution of the heat transfer coefficient
across the canal is usually determined semi-empirically.
For a long time it was supposed that turbulent thermal
conductivity and viscosity passed through a minimum on
the axis of the duct. However, calculations of temper-
ature distribution based on this assumption lead to an
obviously false conclusion. Recent careful experimeits
have shown that the minimum of turbulent properties on
the axis of the duct is very smooth and differs very
little from the maximum value. Therefore, proceeding
from the approximate concept of turbulent viscosity in
Card 3/5 the foiz of a parabola with its maximum on the axis of
the duct the assumption may be used to obtain a resu--'Lu
in a form convenient for use which is, moreover, more

Heat transfer in asymmetrically-heated ducts in elec-
trical machines. (Cont.) 110-6-7/24
accurate than the assumption made in some works, of a
linear relationship between the turbulent viscosity and
the distance to the wall. A relationship is then given
in terms of semi-empirical theory of turbulence. After
further development the author arrives at a logarithmic
law of velocity distribution which differs from the
usually accepted law in that it is valid right up to the
wall and that the velocity does not have a discontinuity
on the axis of the duet. A formula is then given for
the law of velocity distribution and results calculated
by this fo-mula are compdred in Table 1 with published
results which are known to be in good agreement with
careful experiments. Good agreement is shown between
the two. Figare 3 shows a comparison between the temp-
erature distribution in an asymmetrically-heated. duct
determined by calculation and from experiment. It is
shown that the temperatLu-e distribution formula g�en is
in good agreement with the e:)Terimental results. The
greatest divergence occurs at the middle of the duct.
Card 4/5 For practical applications it is necessary to deter-
mine the temDerature difference between the cold aid hot
walls and a ~nethod of doing this is given. Fig. 5 is

Heat transfer in asymmetrically-heated ducts in
electrical machines. (Cont.) lio-6-7/24
a graph that can be used in place of a formula to cal-
culate the asymmetrical heating of ducts occurring in
electrical machines. Unfortunately data is not avail-
able to permit verification of the formula and graph
for high Reynolds numbers. In conclusion a practical
example is worked out. It is the determination of the
heating of the surface of the stator steel of an encl-
osea synchronous machine type MA36-? 2/4 above the
surrounding air.
~Iaxtl 5/5 There are 5 figures, and 3 references, 2 of which a-re
Slavic.
ABSOCIATION: Kharkov Aviation Institute (Kharkovskiy Aviatsionayy
Institut) and
KhEmz.
SUBMITTED; December 30, 1956.
AVAILABLE:

BORISENKO, A. I.
A paradox in hydrodynamics. Sbor. trud. lab. gidr. mash. no.7:
113-128 '58. (Airfoils) (MIU 12:9)

SOV/144-58-9-15/18
AUTHORS: . Borisenko A I Candidate of Technical Sciences,
Doc9nt,and Y tovskiy, Ye. I., Engineer
TITLE: On the Question of Cooling Electrical Machines
(K voprosu okhlazhdeniya elektricheskikh mashin)
PERIODICAL: Izvestiya Vysshikh Uchebnykh Zavedeniy,Elektromekhanika,
19583 Nr 9, pp 112-115 (USSR)
ABSTRACT: The need for some form of cooling, natural or forced, of
electrical machines is first discussed in general
terms in relation to its influence on performance and
design. Natural cooling is defined as purely convective
air-cooling which may be assisted by good geometric
design but does not employ supplementary blowers. In
forced cooling blowers or pumps are used to circulate
the coolant', which may be either gas or liquid. The
point is made that sharp temperature gradients, and
frequent and large temperature fluctuations in time,
rather than high temperatures themselves, often present
the more difficult problems of machine operation,
maintenancel wear and tear etc. Thus, a machine which
generates a high running temperature may not necessarily
Card 1/4 require cooling, if it is run continuously at this

SOV/144-58-9-15/18
On the Question of Cooling Electrical Machines
temperature without frequent starting and stopping, and
provided temperature gradients and fluctuations are
minimized by good design. Alternatively, if a certain
amount of cooling is still necessary this may often be
achieved by natural convection alone, especially if the
heat transfer surface can be maximized, e.g. by cooling
fins. Close attention should also be given to the
material of such heat transfer surfaces, if a choice
exists, since materials having equivalent mechanical
and/or electrical properties can differ quite markedly
in their thermal conductivity and emissivity. If the
above requirements are not met and forced cooling is
necessary, the rival claims of gas and liquid coolant
may be considered. The latter presents problems of
containment and, usually, of corrosion also; however
it is generally a more effective coolant because
specific-heat, mass-flow products can be achieved. That
would be impossible using gas coolants without the
installation of excessively expensive blower power.
Card 2/4 If a small amount of forced cooling is required as an
assist to natural convection, then a gas coolant is the

SOV/144-58-9-15/18
On the question of Cooling Electrical Machines
obvious choice; otherwise the choice between gas and
liquid will be determined by the peculiarities of
construction, performance and maintenance of the
particular machine under consideration. The paper includes
a r4sume of the salient characteristics of some typical
gas-cooled and liquid-cooled machines, namely, air-cooled
asynchronous motors, types IvIA36-52/4, MA36-52/8 and
MA36-62/8 and submerged (deep well and oil drilling)
motors PED-55 and MAPZ-273-54/2. The mass-flow
characteristics for the air-cooled types exhibit a power
law increase in cooling with flow velocity which, within
limits. more than offsets the cost of achieving the
extra ilow. In the case of liquid cooling of the stator
surface of an enclosed asynchronous motor, the
temperature drop between the surface of tl~e stator and
the liquid is only 5 to 10% of the over-heating of the
winding; the largest component of the temperature
difference is the temperature gradient in the active steel.
In this case efforts should be made to reduce the tempera-
ture gradient in the steel, for instance,by using Armco
U
Card V4 ste3-1 which has a higher thermal conductivity. If the

SOV/144-58-9-15/18
On the Question of Cooling Electrical Machines
liquid cooling is applied on the stator surface as well as
on the internal surfaces of the rotor (for instance, motors
of electric oil drills),, the heat fluxes are parallel and
thereby the heat flux -through the stator is reduced. In
such machines the greatest temperature difference is that
along the thickness of the insulation, which may amount to
70% of the total over-heating of the winding. In the
latter case measures for reducing the thermal resistance
of the steel of the stator ard the rotor or of the boundar.
layer of the cooling liquid will have little effect and
efforts should be mainly concentrated on reducing the
thickness and increasing the thermal conductivity (for
instance by impregnation with quartz-sand varnish) of the
windings.
There are 4 figures, 1 table and 2 references, 1 of which
is Soviet, 1 German.
ASSOCIATIOM Kafedra elektrotelchniki Kharlkovskiy aviatsiomir.,,-
institut (Chair of Electrical Engineering, Khar-kov
Aviation Institute) and Khar~kovskiy elektromekhanicheskiy
zavod (Kharlkov Blectro-Mechanical Works)
SUBMITTED: August 12, 1958
Card 4/4

0- 58- -2/25
AUTHORS,.L_Bo Candidate of Technical S-.:Lences and
Yantovskiy, Ye.I., Engineer
TITLE- The Thermal Design of Enclosed Induction Motors Typcs
DIA-36 and PED (Teplovoy raschet zakr,ytykh asin!:hror2-,ykh
elektrodvigateley tipov IAA-36 i PED)
PERIODICAL: Vestnik Blektropromyshlennosti, 1958, Vol 29, Nr 55
pp 25 - 28 (USSR).
ABSTRACT: Heat-transfer in an electrical machine ta'L:I-es place by
conductive and convective heat exchange to the cooling medium
inside and outside the machine. The temperature drop in the
gap between the rotor and the stator is determined from
relationships derived from the theory of heat-trans-fer in a
small gap between smooth concentric cylinders. The temperature
drop in the insulation is calculated by the usual methods, as
in a plane wall. The temperature drop along the teeth is
determined as for a heat-conducting rod with uriformly-
distributed internal heat sources. The temperature drop
radially outwards throurg the stator is also determined as foi-
,h
a plane wall with uniformly distributed heat sources.
A diagram of the enclosed self-ventilated motors, types 1AA-36
and PED, that are considered in the article are illustratetd
Ccrd 1/4

C,
The Thermal Design of Enclosed Induction Motors Types I'-,A-
diagrammatically in Figure 1, which shows their distinctive
feature to be direct cooling of the stator core by the
medium, which can move at a high speed. An important but
insufficiently studied magnitude is the velocity of ccoii_nl~'r
aii~ ween the core and the frame. This should be ca1r_U'.-tCJ
and/=h'ines of the type considered an approximate semi-
empirical formula gives satisfactory results. In calculatiz~r
the heating of the ventilating air the axial compoLient of the
air velocity should be included in calculations. Tile assu-m-ptions
that are made ir. the calcul-tion. are stated. The total heatinU
of the part of the stator vvindinS which is in the slots JLs
determined as -the sum of the temperature drops in the insulat-lon,
in the teethl in the outward path throu.,h 3tator and in the
g
cooling medium; the temperature rise of the coolin~~ r~-diurm
vast be added and is taken as half the total temPei-ature rise
of the cooling medium. To calculate the temperatures- rise of
the rotor windinCs, the temperature drop in the ;Tap, ia half,
r;,
the radial height of the rotor teeth and in the thickness
the ZDtor slot insulation must be added to the temp,~rature r.4~;e
for the stator. In loaded machines, calculation reveals a !a:,,-.;-,-e
Ccrd'2/4 temperature drop along the radial height of the stator teeth,

110-58-5-8/25
The-Thermal Design of Enclosed Induction Motors Types MA-36 and PED
which indicates that the stator conductors at the bottom of the
slots are less heated than those near the air gaps. The
design procedure and necessary auxiliary information are then
given.
The initial data for the thermal calculations are then stated,
including the dimensions, as indicated in Figure 1, the
heating losses and the velocity; also the physical properties
of the materials and cooling media, taken from published data.
The sequence of calculation is then described - in partic-
ular, husselt's criterion may be determined either graphically,
using Figure 2, or analytically. Then the special features
of the design of liquid-filled machines (submersible types)
and of machines with an internal fan are con6idered.
Test and design data for a number of machines are tabulated.
The winding temperature was determined by resistance, with
extrapolation to the instant of switching off. Usually the
e-wnprimental temperature rise is greater than the calculated
I - -- . -
value. This is probably because the stray losses generally
exceed 0.5% of the output. The procedure described in the
article is used at the Khar'kov Blectro-Mechanical Works
Card3/4 for designing enclosed and submersible induction motors.

110-58-5-8/25
Th& Thermal Design of Enclosed Induction Motors Types MA-36 and FED
. There are 3 figures- 1 table and 9 references, 6 of which
are Soviet and 3 English.
ASSOCIATIONS: Kharlkovskiy aviatsionnyy institut (KhaAov kvriation
Institute) and KhEMZ
Card 4/4

TARAPOV, Ivan Yevgenlyevich; BT-A ,
Ya.P., prof., otvorede; GRENUp V,L,, prof.. otv.red.:
TMUOYAKOVA, A.N., redo; TROPIMMO, A.S., takhn.red.
(Vector analysis and the beginnings of the calculus of tensors]
Vektornyi analiz i nachala tenzornogo ischislaniia. tharlkovp
Izd-vo Khar1kovskogo gos.univ.. 1959. 237 P. (MIRA 13:8)
(Calculus of tensors) (Vector analysis)

27564
S/170/61/004/010/019/019
B108/B102
AUTHORSe Borisenko, A. I., Ziminj E. P., Yakovlev, A. I.

TITLEa Flow of a liquid and heat exchange,in the gap between ty, 0
'
rotating coaxial cylinders
with initially axial motion of the'
liquid
PERIODICAL: Inzhenerno-fizicheskiy zhurnal, v. 41 no. 10, 1961, 129-133',~:
TEM Thermal calculations for certain kinds of electromotors requIre
knowledge of the velocity and temperature fields between stator and rotor.i .,
Therefore, the authors studied the laminar flow of a liquid between two

coaxial cylinders axis-z with the radii r, and r 2 (r
',r,). Density
2
specific heat c , viscositY4~~
~, and heat conductivity t" of the liquid ar
P
assumed to be constant. Steady flow and heat transfer are described by:
the equations ?(W-,)w Vp +( 0-W (1), ?c W7T ('T +~-D (2), divW 0
P
(3), where /-,D is the function,of viscous dissipation. The conditions
d/d~~ .. 0 and W 0 are postulated. Consequently, W
W (r). Under;
.
r z
Card 1/4

27564
3/170/61/004/010/019/019
Flow of a liquid and. heat exchange in the ... B108/B102
these conditions one may:write p (r) + ..Z,, where
dz cons t, EJOI
Ip V
that and Aj(r). Eqs. assume the.form
~X Mr
W2
r
i+
(9)
r
_00)
W,
-I=1 0'.
r2
The primes.indicate differentiation with respect to -.The 'solutions
2
to these equ'dtions are W 0 1n rl r. + C a + 0 /r (13),
z 2 4
r2 + C- I ;r C 2/2r2 The
and ~(r) r(r) C where I ~(i 2C n
5.' 2 3 4 4
-C. maybe deter -from boundary conditions., 'Assuming that
constants mined
Card 2/4

27564
3/170/61/004/010/0-19/019
Flow of a liquid and heat exchange in the ... BlOB/BI02
z - 0 and p . p, at the inlet and z - L, P - P2 at the outlet of the flow
channel, one obtains )/L. The calculations show -that the
7r- _(P1 - P2
velocity distribution is independent of the temperature distribution. The
energy balance equati~iqJ2) ~L~~tkmes_theform_____
T + &T) +
PC, W"ET + .(15)
az r Or
L+ I
dW WIL), + dW-z
+ r
dr
For this equation, a a tion of the form T Az + 6(r) (1.6) may be found.
Elementary calculations show that
R 1 (11 pA Q pA CIC4
0 +1 (C. C", - r2
64 V~ - 4 2). (17)
C, (In r)2 +PA CX, r' ( in r+ D, In r + D,..
2X 4). r
Card 3/4

S11 27564
76/61/004/010/0-19/019
Flow of a liquid and heat exchange in the... B108/B102 L-4
The constants D 1 and D2 can be determined from boundary conditions. For
numerical calculations, either the teiaperature gradient on the cylinders
or the specific fluxes q, and q 2 on the walls of the cylinders may be
given. The following relation is found for At
2(qrj+qeO1(rj+r,)+S(~D)dr
a T,n (19),
A az
PC, JWdr
where TM is the mean temperature of the liquid. There are 3 Soviet
references.
SUBMITTEDt February 20, 1961
Card.4/4

PHASE I BOOK EIPLOITATION SOV/6017
Borise lym2y~gh
Gazovaya dinamika dvigateley (Engine Gas Dynamics), Moscow, Obo'rongiz, 1962.
793 p. Errata slip inserted. 9000 copies printed.
Reviewer: G. Yu. Stepanov, Doctor of Physics and Mathematics; Ed.; 1. Yo. Tarapov,
Candidate of Physics and Mathematics; Ed. of Publishing House.- F. G. Tubyanskaya;
Tech. Ed..- V. P. Rozhin;, Managing Ed.: S. D. Krasillnikovs Engineer.
PURPOSE: This textbook is intended for students in aviation schools of higher
education, in aviation divisions of other schools of higher educations and in
power-engineering divisions of machine-building institutes, and also for readers
from turbine design offices and laboratories.
COVERAGE.- Fundamentals of gas dynamics for aircraft engines., mainly gas-turbine..
are presented. One-dimensional and linearized plane flows, inletas and nozzles
are discussed in detail. Included are the theory of blade profile and of the
grid profiles, cavitation and pulverization of liquids, and the mechanics of
Card 1/0

Engine Gas Dynamics SOV/6017
highly rarefied gases. Elements of magnstogasdynamics and the derivation and
analysis of the equations of continuous media are also considered. The au-
thor thanks I. Ye. Tarapov, Docent; G. T. Pozhidayevs Engineer; 1. L. Povkh,
Professor; B. S. Vinogradovp Docent; G. S. Stepanovf Doctor of Physics and Math-
em atios; K. N. Davydovs, Docenty Engineer; N. 1. Akhiyezer.. Corresponding
Member, Academy of Sciences UkrSSR; 1. M. Kirkho, Corresponding Member, Academy
of Sciences, Latvian SSR; A. D. Myshkis, Professor; A. 1. Bunimovich, Candi-
date of Physics and Mathematics; A. V. Vatazhin, Engineer; V. N. Yershov,
Docant;_Yu. V. Stepanov, Docent; and E. P. Zimin, B. N. Meltnikov, and I. P.
Miroshnik,studmts. References accompany each chapter.
TABLE OF CONTEF- [Abridged]:
Introduction 5
1. Subject of pps dynamics 5
2. Physical propertied of liquids and gases I
Ch. I. Kinematics of Liquids and Gases
1. Velocity and acceleration of a particle 21
2. Decompdi&ition 6f total motion into sisple Lelements] 27
Card 2,1#2- t

BORISEITKO., A.1, -9 kand.tekhn.nauk; Yako,vlev..-A,I,., inzho
------------ -
Indeperdently operating nride~~" fandforcooling dc. machinery with
medium power ratings. Vest. elektroprom. 33 no.8:23-26 A 362.
~OA 15r,7)
(E"-.ectric machinety---Cooling)

BORISFMO Aleksandr Lvanovich,,-Iand.tekhn.naukt dotsent; YAKOVUV,
ksandr Ivanovich
Hydraulic resistance of medium-sized electrical machines. Izv.vys.
ucheb.zav.; elektromekh. 5 no.10:1137-1144 162. (MM 15:11
1. Zaveduywhchiy kafedroy gazotermdJ-namiki i reaktivnykh
dvigateley KharIkovskogo aviatsionnogo instituta. (for Borisenko).
2. Vedushchiy insbener laboratorii promyshlemoy aerodinamiki
Khartkovskogo aviatoionnogo instituta (for Yakovlev).
(Electric maohinory-Cooling)

6 C/AFMDd/0D. Pd-4
MM ~3_ b) AEDC/AFFT
jL2 -6
ACCMION NRt AP3003320
060 134
THORs Borisenko, A.~ D. NharkoV)
AU
A
~TITM Plane flow of an ideal- I.-Igompreisibie fluid of thin profil Ie around Ia Jar
ge.
Aend
~SDURCEs Ukrainskly matematicheskiy zhurnalp Va 159 no,, 21 3963,p 319-1 4
3
TOPIC TAGS s. vortex layeri, incompressible fluid, thin profile., large bend
!ABSTRACTt It is known'that the problem of plane flow of an ideal incompressible,-.
!fluid of thin profile around a small bend, as well as a lattice of such.profiles.,
me own
can be solved by the method of vortex layers, This thod considers the unkn
:flow to be the result of a.system of'vortices distributed along the chords of the i
rofile
where the density of vortices is detemined from the boundary condition on:,
p
the Profile., This leads to an Integral equation ~orthis density,, In the case of
bends.. treated by the authors.. the method of vortex layers can also be used
if the vortex is situated on the-centhr line of the profile. Themethod of vortex
twers leads to -the necessity of effectively solving a singular integral equation
for a single profile and one for a lattice of.profileso A single parabolic profile:~
As discussed in detail* In this case the equation assumes another form., and its _77
so
lution is found in the form of a series with undetermined coefficients which are
tard

L 3406-63
ACCESSIM, NRI- AP3003320
'db an Inf inite systela of linear equations whose coeff
y means of icients are
-,expressed by double Fourier coefficients$ :A rapidly 'converging iterational method
11v indicated for finding.the latter; the system of equations is also solved by
s of rapidly converging iterations* The method may be extended to polynomial.7
mean
.,profiles higher than second power and ona lattice.of profiles without essential
!changes* The work does not,contain full formal proofs* Orig* art* hast 28
formulasp 1 diagramp and I tabl6v
!AMCIATION.- none
J
SLYMTTED.- 28jan6i DATE ACQt 24JuI63 ENCL- 00
NO REF SOV: 006
:SUB CODE: PH.OMM OTHER: 001

q TCJ AFFTC
:L BDb/EIP( -OW /ASDI JD/JG
-1291&-63 - : I
ACOMMON MI j&3060
SIODS016310361OD41681810824
AUTHMs Borisenko. -A. I.; Artamlyev, V.: II 1ntohova, N. 'I.
o
i.TITLEs Diffuaioh mobility of, lion a pr tective coafind%r n1obium ahd
molybdenum ap'l
SOURCEi Z OY no A 1963, 818--8U
hurnal prikladn khbdit vo 36s, P
iTCPIC TAOSs. niobium,-nibbium diffusion coating, zaDlybdenum,, molybdenum
I diffusion coating glass coating, iron diffusion,-. thermal expansior,, coefficient
1 ABSMCT: The diffusion of Fe In two-phase systems of Nb-glass and; Mo-glave ha I
been studied by the mathod-of tagged atoms (Fe59) in an attempt to clarify the
effect of Fe on the protective ability of glass coatings. In the preliminary
experiments the parameters of Fe diffusion in individual components were determine&-
Films of Fe*59 ~were deposited on specimens of 366 glass .(58% SiO2, 20% Ba203', 5.0%
'.each A1203 and CoO,, 6% T102P and 3,0% each &02.and B90) and sintered 99.7%-piTe MO,
99.8%- e.%.uhich were.then held at 1000-2200C (Nb and Yo) or 700-900C.
(glass) for 10 00 hr in argon at 150-180 nm 11g.' It was found that the temper-
ature dependenlof the coefficient of Fe diffusion in Nb and Mo is exponential i
!and is expressed by the equations D. 1.6.x 30-3 exp 54,000/RT] for Mo and
Card 1/0-

L 12916
-.'ACCF
MIONI. NRV AP3660i
ID 3.0 x 1073:sn 151tooo/RT) for,. Nb,:, where 344,ODD and 51000 are the valuea of
the activation energy in cal/g-atome. Thelov values of the activation energy appear
to be a result of diffusion proceeding predominantly alongdtho grain boundaries,
lvhich4e usual in sintered Nb. and Md. ~ The diffusion-of Fellin the 366 glass-in the
:700-906C range Vas found to be-negligible. In the second series of experiments-,.,
'the 3 1
66-glass coat ng with unifornly distributed F659 was fused on Nb and.M6
.-specimoub at 1380-WOO In an argon atmosphere., and the coated specimens were
annealed for 45 br at 22ODC in argon at, IW m Hg.. In both cases, the Fe atom
were found to vwe toward -the glass-metal interface* Stresses resulting from a
X
~differsnce in the~coefficiente of thermal expansion '(NbP 84 x j0-7; Mo, 5? 10
i366 glasss, 30 x 10 7 in the 23-~6= a) intensify the Fe migration. In the
rang
'cave
of Vb almost all the Fe is concentrated Inthe glass layer adjacent to the i
Nb with very little - Fe migration into the surface layer of Nb, owing to mi crocracks
by thermal stresses., No microcracks are formed in coating on Mo, which
:facilitates formation of a continuous glass-metal interface through which Fe atoma
readily'diffuse Into Mo. Orig..arrt. has: .2 tables# 4 figures, and 10 formiUs.',
'ASSOCIATION: none.
Cord
2/k

06k,kolf); Immus, A.D. '(narfkcv)
Plane flow of anideal incomp3*osiWA liquid past thin profiles
with large flexures. Ukr. mat. ihur. 15 no*23119-134 163.

A Pi(~ E'Vi'AfeOW
L- 60899,;-65 S - . ' ~ k '416
A
)/Ewp( )/q1Pfb)A_VA(0-':' IJP(C) JD, i 'I/
Z
yLTEMA
Pi9747-- 0-
__-BOOK Mcrub i . --
iT,4TIOlf Z
UR
iy Ididoicividh- (D6ctor:.of -Technic_al-&)__`_:_7
Usov iLeonid Ilik6l~ye2~i1ch-; 11oIr
01
-S
clence
n6 us'e of . -Aa-sma for ootaining.'ref'ractory'coatins
rimeneniye plazmy dlya
oiuche'~:-Lyavys6kot e -Vok Owl-Izd-vo "Nauka", 1965. 84 p.
p mperaturnykh r;YtiY) MsC
itle.:~.-Akademiya.' nauk SS
i1-1Usw-,~:-bibliov-(At- head-of-A, SRY 400Q-copies..prin.ted
TOPIC TAGS:. plasma, -plasma.-ase, _:refract~rj 0 c 0 ru m e
-c ating, . orr sion, st - ctural at rial
corrosion, 6ELS COrroslon, corrosdon,prevention.-
L
SE Mr~ COVMGE,: This s entifi works, technologists and
-book I intended for sci c
designers engaged in resbarch on means.-for-prote-cting structural m6tbrials a-
gainst bigb-temperature gas corrosion.,q The book reviews present engineering
possibilities of obtaining an ionized tas jet. It describes methods of obtaining
plasma and present vari us designs of elements of a unit serving for deposition
ective coa letb.rs of depositing certain refractory compounds with
of prot tLgs c F;-"
the aid of a plasma jet Data on the physical properties of coatings
-intended for the protection of naterials against hiEb-temperature gasi
corrosion are presented.
Card, 114

L 401399- 5-
fA9.747

IntroduCti ...
on 3
I., Phy fS
si al a~damenta.ls for'. obtaihing plasma
-ar
Device for obtaining a plasta C 10
I.: Stabilization of the: arc -10'

stics.-of:plasina 13
2- Factors~ aff6eting power: ch6racteri
3. Plasma-forming 'gases 17
4. Selection of _material -for -electrodes and-deteriainatio'n of their size 20
~sn
pp-d
7-
7~
6f h66ft
C
6

of a-- t P~ i~,-
pn3.t- -]p~~a-~arc os ng-_-,-,4~
C
or.
7

Mat
TIT.~ erials 35
_QXI-4 _39
2
3, 4T,~,
48-
sw

:7

L 60899,--65'
-019747
No REF SOV: 019
"B CODE mm SUBIRTTED.1 -16jan65

_15747! EY?'A/E (O/Ell,? (,b)/ETI-
rk -66 K
SOMCE GODT-1 MVWW/65/0W/G00/0147/0155
AGG 9: 05027950
MUM Silolayevat L4. 6;Bode (DDetor of technical iseiences)
1, CRGs none
TITLEt Pliable giMs enamei coatings for chromel and alumal 1dr-9-9-
SOIRGEs 132%dnar Ro---* gtakin n -Up-)-M-_LAnin 194t arps 4"
-p9.kry.,Uya,_ (Aqpkk,!7Te#stant coa~t~iah.,,i~~-iim-inara. Leningradj, lzd--vo Waukaj, 1965
2,47-155
TOPIC TAGS: Vcoating, glass product, thermocouple,
ABSTRACTs Chromel-alumal thermocouples 0.5-0.1 mm in diameter are often set Into
metallic blocks heated to 7OD-8000. Attempts to insulate them by glass enamel
coatings applied fromaqueous suspension failed because of the brittleness of the
thick layer-obtainedo A method was*proposed for theapplUation of a 2-3A
pliable layer from a semicolloidal solutioup while'retaining the electriwa
en-at hlgb tamperatureme The S102 hydrolynate and the highly dispersed
solutionawere prepared by thelsolution. ceramic method (S. V. Bradstreet, solution
V3

L 15747-66
ACC Nits AT5027950
ceramic for ename3ingp Geraido Age 66t 6# 1955, 24). The calculation of the re-
quired concentrations of salts in solutions was made according to the formu3aa on
hydrolyslej, (during-coatin f selected compounds, e.g... jZ~R,,O)Oi H4SiQ
9)+
9H20 W8 -the 11
SiQ2, or 20rW03- 'Qr2C~ + 3W204 + 1.502 + ISH D' Th-z quality 3
aolution mixturep and hence the quality of the coatings., Qended on the sequence
of mixing. The solutions of various salts should be mixed by adding--%-hem into the
SI.? en UN p NaNO3., Ga N
roljysafe in the fonowi cei ~ (1) H BC~P~ P92'
12 zn(NO 'I'l ;:ju 4)
Sr X(~ (2 N b N(
3)29 Al 3; 3 1
GO f the wrre should b-0
NI(NC5)2p G* ~10 Die Gurfacti;0Zr(" Uleansed of oil
and grease. An immersion o the wire for 5-6 minutes into a heated (70-90G)
mixture of NaGO3 25-30 g1l and reagent OP-10 3-6 g1I with subsequent washing in hot,
water and acetois was aufficiento The coating could be made either by Immersion
into a solution or by-drawing through a plastic sponge wetted by the solutione
1, in
After coating wireelvere dried for several minutes at 60-70C and rapidly, baked
i an elee-tri-e-Nir dace at the melting temperature of the coating (850-950G)o The
coatings obtained sometimes had n-11 defects easily removable by repeated coating*:....
~g (1) 25.0% SiC i
The three coatings entainin % 13.0% GaOj, 12.0% B2C~q 5.0% ZnOs
3.0% M90j, 4.0% Mnc~# 2.0% NIO; (2)-33.0% SiOs 0.45% 120P 0.5% LIL Ot 5.8% CaO
6.5% B2C~q 43.0% PbOP 10-0% B&O# 1-0% 000, and U) 42-0% SiC~s, id-O% k0j, 5-6%B2ID3,_
2/3

ACC NRt
AUTHOR$
IT~Pr- 71197 -~rj !---T
W6- 5 oob - f84/ i
AT6027145 SOURCE CODE: 00016-10 00 0 o 89
Nikolayevap L. B.0. Borisenko, A. L
01 Iri t none
TITIZI Thin-layer glass-enamel coatings for cbromel and alumal wire'
SO`URCEs AN SSSR. Otdolaniye obshchey i tekhnichoskoy khimii. Issledovaniya V oblasti
khLiLli silikatov i okislov (Studios in the field of chemistry of silicates and ox1d[,4.j1
Xoscowq Izd-vo NaWca, 19651 184-189
TOPIC TAGSZ protective coating, thermocouple, glass property
ADSTRACTI: Me article describes compositions of glass enamels and methods of their I
deposition from sendcolloidal solutions on chromol and aliunol wires to be ir,3d as
flexible, insulatod them, ocouples. Stable solutions wore proparod which contained ca-~
tions of the hoajy metals barium and lead in addition to r,111c acid vol. Solutions
containing zirconiwn should be used within 24 hours of thoir preparation. A now moth-;
0d of depositing the coatings was worked out which makes prior heating .-If tho S-00cimen:
to be coated unnecessary, The methocV-conrists in immerf3ingr tfie 14tro in the Sol-ativil
or passing it through a J~~~Liq)~~ponge wetted with the solution. Composit ions of!
soluble glass enamels are proposed which under tho samo f1ring conditiona aro fusud
onto chromel, a
luitkol and their alloy, so that they can be deposited on fillished thor-
112

ACC NR; AIT6I02-7-IIV51----
mocouplea. Continuous, flexible coatings having an adequate 1)9.;Lt-xUIQIR=&-mLt 6oo-
7501C were obtained. Orig. art. has$ 2 figures and 2 tables.
SUB CODE : II/ SUBM DATI';: 18J'ul(14/ ORIG REFS 0051 OnI REFS 003
2/2 egx-,-

B&BUSHKIN, V.N.; BORISENK09 A.I.
Unit for studying diffusion in solids. Prib. i tekh.eksp. 10
no.5t158-160 S-0 165. (MIRA 1911)
1. Institut, khimii silikatov AN SSSR, Leningrad. Submitted
July 25, 1964.

USOV, Leonid Nikolayevicb; BORISENKOy Anatoliy Isidorovich,
doktor tekhn. nauY"'---':'--' ~'"" - -: ~ - -` ' 1. -
(Use of a plasma in producing heat-resistant coatings]
Primononia plawq dlia. poluohenita vyaokotomporatux,nykh
pokrytii. Mosha., Nauka, 1965. 84 p. (KRA 18:3)

- - -v