SCIENTIFIC ABSTRACT YERSHOV, V.N. - YERSHOV, V.V.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001962910010-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: March 15, 2001
• Sequence Number: 10
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

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Influence of the Radial Gap on ... E194/Ei84
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Influ~nce of the Radial Gap on ... E194/EI84
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SUBMITTED: June 1, 1960
Card 7/7

a
AUTHORS: Yer_a_h2y,,__L&.,
Stepanov,
Pavlenko,
TITLE- Extending
compresso~r
34657
S/096/62/000/002/001/008
E194/E435
Candidate of Technical Scionces,
Yu,V., Candidate of Technical Sciences,
G.V,, Engineer, Brekhov, A,F,,, Engineer
the region of stable operation of an axial
stage
PERIODICAL4 Teploenergetika, no.2, 1962, 41-44
TEXT. A typical form of instability in axial compressors
operating at low speeds is the formation of rotating zones of
breakaway of fluid from the blades. These zones of' breakaway
usually begin only at the blade roots or tips but increase as the
amount of throttling is increased and, at very low rates offlow,
may cover the entire blade length. In multi-stage axial
compressors running below the rated speed, critical angles of
incidence occur mainly on the first stages or on stages immediately
beyond air bleeding points. Total breakaway may occur on a few
stages but may sometimes occur on all. with great loss of efficiency~
The trouble can be overcome by increasing the flow through the early
stages but this is wasteful. Attention to blade design cannot
Card 1/3

s/oq6/62/ooo/oo2/ooi/oo8
Extending the region of stable E194/E435
give much improvement. TheorotIcal Invf�,qUgaLIont.* )r ti)o ;itowwy
of an axially symmetrical flow indicate that when stability is lost,
flow may take one of two forms," with the forniauon of rotating
zones of breakaway; or with an axially symmetrical annular zone
of breakaway, or annular swirl, associated with the occurrence of
a counter flow. The relative stabilities of these two kinds of'
flow vary according to circumstances but, by promoting annular
swirl, it is in principle possible to prevent completely the
formation of rotating zones of breakaway. Tests were made with
compressor stages in which various measures had been taken to
promote annular swirl, namely3 cutting annular slots in the casing
just ahead of and just beyond the tips of the blade;s~ installing
an annular step or ridge in the casing just in frorit of the ring of
blades, also, blowing air into an annular slat located just ahead
of the blades, All of these measures were found to extend the
zone of stable operation; however, the most convenient and
structurally simple is that of blowing air through an annular slot,
With this stage, tested when air was blown in at a head two or
three times greater than that of the stage, the boundary of stable
Card 2/3

S/096/62/000/002/001/008
Extending the region of stable E194/E435
operation was displaced by 25 to 30% in the direction of lower
outputs and the maximum energy of pulsation in the zone of
breakaway was reduced by 40%. The amount of air blown in was about
2.5% of the minimum flow necessary to ensure stable operation.
Additional tests have shown that the effect of blowing in air in
this way differs for the different stagts. There are 6 figures and
3 Sovlet-bloc references.
ASSOCIATION: Kharlkovskiy aviatsionnyy institut
(Kharlkov Aviation Institute)
Card'3/3

8/124/62/000/010/009/015
D234/1130B
AUTHOR:
TITLE: Problem of minimum dissipation of mechanical energy in
a stream of viscous liquid
'PERIODICAL: 'Referativnyy zhurnal, Mekhanika-, no. 10, 1962, 82, ab-
stract 1OB508 (Tr. Kharlkovsk. aviats. in-ta*, 1960,
no. 20, 13-18)
T,M: Helmholtz' theorem on minimum dissipation in a non-inertial
laminar flow is extended to a turbulent flow, assuming a linear
relation between the tensor of turbulent ptresseb and that of de-
formation rates of averaded flow. The proof is given formally for
the usual equations of laminar 'flow in which the viscosity codffi-
cient is variable. It is pointed out that, apart from non-inertial
flows, purely solenoidal and potential streams also obey the prin-
ciple of minimum dissipation. Z Abstracter's no;te: complete trans-
lation.`7
Chrd 1/1

11T IN N! ti ffilf I 1 6, H-M -,M_6d__t
MMHGV.9 V. N. :Lnzh.
Accurac7. in the rolling of I-beams and charmels on existing
rolling udlla. Stall 21 nc).3.24ft-11.105 D 161. (MIRA W12)
1. Kuznetf3kiy meto-Uurgicheakiy koutbinat.
Rolling(MetalWDrk))
tams and girders)

YMIIGVP V.N.
ViAiition in wall thickmas of double-T boam and ebannels during
rolling, Izv.vys.ucheb.zav,; chem.met. 5 no#4:54-60 162.
(MM 15 :5)
1. Kuznetskiy metal-lurgicheskiy kambinat.
(Rolling (Metalwork)) (Thickness meazurement)

TERSHOV, V.N., kand.tekhn.nauk; URSHOVA, N.M., k anti, toklin. nauk
- I ~ - -1 J
Electric thermo-moisture moter. B!La.tekh.-ekon.in'-Porm.Gos.
nauch.-issl.inst.naucti.i tekh.inform. 16 no.8:39-40 163.
(MIRA 16210)

~Jjj ~Jljjtjj I
7~- jj~_,
L 01,807-66 -,,nT1r-w (I)AVP(P)IT-2 TUN
OW ($610910C13100
ACCESSION UR: AP5020633 71 /0075
AUTHOR: Beldn, N* Vs; Yershov, Vo 11 o.
............
TITLE t Plotting the lef t brartch of a pressure-he(id cur,,,e of ntl a~c i a
compressor rotor
SOURCE.$ IVUZ. Avistsionnayn takhnika, -no, 3 , t !iA 5 1, - 7 5
TOPIC TAGS, axial compressor, compressor stage o, qnTjLt:(1q,;or dos ign
compressor rotor, compressorstall
ABSTR&M The Instability of an axi a~l compresst: in 10te form of a
rotating stall is daterrmined by the atage c1jaracj:erJ.r,.tfcs, particular-
ly the dependence of the preti,oure hend an the fivoil r4itill. The rotItilip,
stall usually occurs at a flow rate beLow that wlrich corrosponds t:0
the maximal pressure head, I.e., under the condition.,j described 1)j
the left branch of the compressor charec"-erist9c curive, which is of
interest In calculating variable operating conditiorit; of multi-stage
compreasors, The authors present a method for obtaloing the left
'branch of the curve for a coinpressat rotor with d. relzitively large
Card 1/2
11111111101111-111 WIIPRIi~
0111 "l, Maj. "wo M11 .. No MM F 11 M, Mi

L 01P.07-66
C"
AAC ESSION HR-. APS020638
;hub diametar, The method is based an mez~suring.th'e prosoure-head
ivariation under rotating stall, conditt6na, ~-'t car, alfj~j be app)Aad
Ito compressor stages With smaller, hubl' -dLameters wAder .,conditions of
total stall. Orig. art. has: 7 fig=es and 6formulas. [AC)
i ASSOCIATON: none
iSUBMITTED: l4Uec64 ENCLt' 00 SUA CODE: PRO HF,
!NO REP SOVt 005 OTHERt 000 ATD PRESS I
/2

-V 10266-66 MIT(I
ACC NRE AP600s,01-
AUTHOR: Yershor, T. N.
!UR('W MIX::
ORG: none
TITLE: Vortex theory of rotating stall
SOURCE: IVUZ. Aviatsionnaya tekhnika, no. 1965, 118--12N
TOPIC TAGS. vortex theor7, rotating stall, difrusoir, blada I'Mscadj_' AJ-41-
ABSTRACT: Experiments Ghaw that during transition to large:anglea; of attacX In an
annular vaned diffusor, stall zones may be formed which moTe'vith,a certain angular
velocity relative to the diffusor. There are tTxo types; of poasib1l.- r-talls in a single
rane cascade: a veak stall, characterized by,~the formation of stfiU Zanes whose
number increases as the flow rate decreases, and a strong stall, characterized by a
wide zone with an intense counter-flov inside the zone. Mtt;pite the great iLttention
devoted to this problem. by investigators, a detalled soluticia reflecting such r-sDectl3
as zone displacement velocity, flow parameterziaside the ixiae, and the number of
zones is lacking. Therefore, in this article,, aa attempt Ili made to analytically
determine the forin and displacement veLocity 6f the! stall z0aes L111 a 13i2ZIe- rofile
ascad--. The obtained results are shown, in, ftr,. 1, vhere G is the flo-'r rate;
fl, zone displacement velocity; a, mechanical !!nerg3t of the Tlow; and Ca is the axial
component of the flow velocity within the stall rorte. In awn-ular cascmdes with a
card

ACC NRx AP60031336-
Fig. I.; Cascade flov,, chameteristics.
Z_ A
VI
small relative hub diameteri the- for=t icn of a noxTov zGne of stlwg stall is fo=d
to be umlikely. The narrov zone of a-weak nt~.11 carreiponda; to &'mitLximta preaoure
head regime. Same recormu-tadat ions for selecting stable oporating' regimen are gi,-12tn.
Orig. art. has: 6 figures and 10 formulcLs. (AS]
20/ 'S(BH DATE: ManO/ CRIG FIEIP:* 002/ OTR 9ZF: 0,04/ ATD PPESS:
2/2
L 10268-66

L 161-Lg-66 z,,Ln M/31 w,
-ulta =2- 1111 617 01.1111 3' 004,
Acc In. P.F6w-,*+l22 so D/C, 00 .4
ATYMORI; Yershov, V.
(Kharikovigl0y, xvial~s I wjl;~.kr itt if t. k Lut
0AII Pvtekov Aviation Institute
TITLE: Conditions of m=iwiur, mecbanical eiwrjty~ flor "'Int; 441 (ill, IIItnri cl,
floir patterns in axial turbomachlnel,7
tekdmk" vo,.,duelmogo
SOURCE:
flota, no. 1, 1965, 57-44
.TOPIC TAGS. turbomachinery, flow field, floir isepaxatioli.0 aximl flov tu:Tbine,
vwiational method
ABSTIRAW. A qualitative discussion on. the use of 'the. Nii~-riatlonal principle, of
.maximwa mechanical energy- flow in turbomschinery aalctilia~iow; is presented. The
aAthor claims that most of the solutions of Vior, fields do not
copaider the uniqueneao of the solution. ~ Thua there iv to filinzantee tl-~t the cal-
culated fields will not be differoat for difforent aawliziDtionz or for
different met!-Lods of nuzz-arical integration at the gavei*ning alluntions. 7he vaxia-
~tional relation in the fo= of the pwinqiple of mx~rjm madbiatiml eno-",4zr f1ow at
Card
Im, I M M131111111 " wtma Oil w7mw

L 16119-66
~~ACGIM:- 'AP6004122
,the critical section can be used-for that ptwpoae (Yo H. Yerfhhov. Variatsionrqy
~printaip makjaimur= potoka mele-hanieneekay emergii. Izveatiya vyssh.Xi uahebnyIr2I
e a ;ha L
t zavedeniy. Aviatsionnaya, tekhnilaL, No. 10 1959)- Tile Princild e r -11-11-ire i the
'function
Ir J'WCA'
ibe at P- maximum for a givea flow
(normal nomenalature). The variational prin6iple also be usei to deternine the
flow field in areas of flow separ&tibn I as demnstrated by !Ie wAbor
(Neustoychivout' potoka v kompreeEorakh. Iziestiya vysslaikh ucbqTvivkh zave-deriy.
:Aviatsionnaya tcklLnikat No. 11 1560), A briekf discuavion'ar t1he casz ahown in Fig.
~1 is presented.
Fig. 1. Flow I'n
Card 2/3

L 16110,66
ACC N-R, tP6004122
.The variational criterion can also be applied, h-A linding: th'Irl if."Pt
compressor stage characteristics. A uliort diso=sion of t7o m(;I";)wd iu-
and rerailta aro compared with acne experimental data,, TLW~v-arii).-Uonril criterion i0
claimed as a powerful tool which rdmild flznf~ wider applivMvLon4, ID r I,-. art. hus:
figures and 4. formAas.
SM COD'z"-. 113/ SUBU DATE: none/ ORIG RF.F..:
Ca, d

L 07585-67 EWT(1)/gWP(m) RM
,FACC NR3 AF 030 25 SOURCE CODE: M1/0420/6610001GO06/0014/0017
Polyakoy
AUTHOR: .j
AL_X0
ORG: None
TITLE: Effect which nonuniformity in the oncoming flow has on looser. in cascades
with blades which have a low aspect ratio
SOURCE: Samoletostroyeniye i tekhnika vozdushnogo flota, no. 6, 19056, 14-17
TOPIC TAGS: turbine cascade; compressor blade,.secondary flov, nonuniform flow
kBSTRACT: Experimental data are given on.comprescorcancadeft with various degrees Of
nonuniformity in the oncoming flow. Three cascades were tested in all: two modifica-
tions (A=0.5 and A=l) with a chord b=50 mm and one modification (X=0.5) with a chord
of 100 mm. The leading edges of the blades were rounded and ~he trailing edges were
beveled. The curvature of the profile iwas 450 and all cascades were made with the
blades set-at an angle of 521301 and a relative spacing blt=2. Plat cut-off plates
were used for changing the aspect ratio and for eliminating the boundary layer or, the
walls of the casing. Nonuniformity in the field at the input rc6ulted in thin
strands close to the leading edges of the cut-off plates in a direction nornal to the
velocity of the oncoming flow. Variation in the number of strands and the distance
between them was determined by the shape of the velocity profile. The results show
Card

L 07585-67
AP603o425
an increase in losses with nonuniformity in the oncoming flow. The region of propa-
gation of secondary flows is practically independent of the degree of nonunifo-xmity
in the oncoming flow although the intensity of secondary flows increases with non-
uniformity resulting in higher losses. The experimental data indicatte that ordinary
theoretical methods should not be used for determining the characteristics of blades
with a low aspect ratio. Orig. art. has: 5 figures.
SUB CODE: 13/ SUBM DATE: None

ago
t"'tj 7
41 .4'
d
F.
1

L 08269-67
ACC NR: AP6029789 (A) SOURCE CODE: UR/0119/66/000/0011/0010100a
AUTHOR: Yershov. V. N . (Candidate of technical sciences, Docent); 3 1?
Yershova, N. M. (Candidate of technical sciences, Docent)
ORG: none
TITLE; Hygrometers for disperse materials based on the Peltier effect
SOURCE: Priborostroyeniye, no. 8, 1966, 10-11
TOPIC TAGS: hygrometer, moisture measurement ti'li"
ABSTRACT: Conventional instruments for measuring moisture content in
capillary-porous materials are often inapplicible because of the effect of the
electrolyte involved on their readings. Hence, anew hygrometer in proposed
which consists of a number (ZO-100 or more) of thermocouples connected in
series through which a direct current is passed; the time rate of rise (or fal.1) of
Card 1/2 UDC: 621.317.39:533-27D
d

L o8969-67
ACC NR: AP6029789 0
thermo-emi is measured. As the thermocouples are brought in contact with the
test material, the thermo-emf rise (or fall) rate will represent moisture content
in the material'if the thermocouples were previously calibrated with the same
material. The thermocouples are connected to a d-c source for 5-10 sec b.~ a
relay and then are switched over to an emf-rneatiuring instrument, the emf 2ise
(or fall) curve is assumed to be linear. Two gets of thermocouplels connected in a,
differential circuit permit determining both the value and direction of deviation of
the moisture content from a set value. Orig. art. has: 3 figures.
;SUB CODE; 13, 09 SUBM DATE: none ORIG REF: QQ3
2/Z n,
cnrd

7
SOURCECOYi.- UW l4jfi~61666?00610iV~di26
70
FACC
AUTHOR: Anyutin, A..N, (Engineer); Griga, A. D. (Engineer); Kovalevokly, V, V.
(Engineer); Yershov, V. N. (Docent)
ORG: Kharkov Aviation Institute (Khartkovskiy avistsionnyy Inatitut)
TITLE: The effect of a decrease in axial velocity in a iowpressor stage an its
efficiency
SOURCE: IVUZ. Energetika. no. 8, 1966't 117-120,
TOPIC TAGS: axial compressor, compressor efficiency, compreasor stage, compressor
stage model, axial 'compressor., J&o -4,e;-AJ
ABSTRACT: Due to the lack of dati on the subject, an experimental investigation was
made of the effect of a reduction of the axial velocity in.the flow passage of an
axial-flow compressor on its efficiency. The basic tests were performed on a K-50-1
stage model at the TaKTI. The axIal-flow velocity was changed by varying the shape
of the flow-passage cross section so that Its Natios of inlet-to-outlet cross-section-
areas were F /F1 0.92, In 1.00i and 1.10. The angles of the rotor-blade setting
(at the middie of their heights) were 27*401. 32'409, and 37'401; this permitted the
testing of niae versions of the model stage. The angle ,a of the inlet and intermediat,
suide vanes were 15*300 and 32*301 and were not changed during the investigation,
The circumferential velocIty of the blade tips was u 200 m1swe at a Reynolds number
wd 1/3 VM 542a-M

A
r
-C M A?6031065
1614
:44
A
'1

X1
illj Is,, IM dependence of the efficiency.
am. K*'- Ya for U 270 afese
Re 3.7 x 105. For most of the stage-versioup the.tests were repeated at.
u -'270 m/sec. The teMMratures were measured at the Anlet and outlet of the stage
and the static pressures, at the hub-and the casing'. The velocity distribuiion in the
radial direction of the flow passage In front of and behind the rotor va'6 also deter-
mined. For the each version of the-stage the.characteristics were plotted aod the
regime of tie maximm of f iciencip n was determined. For this regim the dif fusivity
factor-# - Nm X--W2)/Wl was detendned.; here, 1110,V2) &to the relative velocities at
the InUt loutlet) Of. the rotor cascadee Axi approxim.telorixula for determining the
efficiency of 4-stage of an axIsl-fli&v,tow~rea~or with a rough approximation of the
air compressibIlity to proposedt. is I + KO Wtorv, In the eff Iclency
Cc~-d

ACCZNRo 'AP6031065
of the stage.when A# and K Is a paramitet'dependinit on the.blade geometry.
and fl:(r4. characteristics,'. Re test results (with added characteristics of six othcr
compreai~r-stageij.ars'plotted in a diagram in which the colid curve corresponds to'
the equiatiou (1-1)/I-no) a I + 1.45K+ 2.16 0 (9=N& 1). Tdo equadon Is remainded fox
extimating the affect of a decrease in tha-Mdal flov velocity an the efficiency Of.
OrIg, am hass '3 f1gures.and Lformula. (WA-761
SUB CON313,201, SMIN DATX# 2Uul65/ 0110' Ws, 003/
3/3

ACC NRt - AP6031065
AMOR: Anyutin, A. N. (Engineer); (Znginecr); Novalevskly, V. V.
(Engineer);1ershay
(Docent)
ORG: Kharkov Aviation Institute (Khar'kovskiy avintsionnyy institut)
TITLE: The effect of a decrease in axial velocity in a compressor stage on its
efficiency
SOURCE: IVUZ. Energetika, no. 8, 1966P 117-120
TOPIC TAGS: axial compressor, compre sor efficiency, compressor litage, compressor
stage model, axial.*,flow compressor, AO L-.1AJ
ABSTRACT: Due to the lack of dati on the subject, an experimental investigation was
mada of the effect of a reduction of the axial velocity in the flow passage of an I
axial-flow compressor on its efficiency. The basic tests were performed on a K-50-1
stage model at the TsKTI. The axial-flow velocity was changed by varying the shape
of the flow-passage cross section so that its ratios,of inlet-to-ouclet cross-section,
areas were F./F, 0.92, in 1.00; and 1.10. The angles of the rotor-blade,getting
(at the middle of their heights) were 27*40', 32'401, and 37*40'; this permitted the
testing of nine versions of the model stage. The angles of the inlat and intermediate
guide vanes were 15'30' and S2*30' and were not chwaged during the investigation.
The circumferential velocity of the blade tips was u - 200 m/sec at a Reynolds number'
1! Cord 1/3 UDC: 542.78

ACC NRt AP6031065
Fig. 1. The dependence of the efficiency
on K. 96 for u 270 m1sec
0
KI
2 -4I a 4,1 43
""Re 3.7x 105. For most of the stage-versions the tests were repeated at
u 270 Wp~.,c. The temperatures were measured w: the inlet and outlet of the stage
and the static pressures, at Lite Itub dtid tha cani,ng, 7%* valnci;y distribucion in th
radial direction of the flow passage in front of and behind the rotor wits uIriv detor -
mined. For the each version of the stage the characteriaticB were plotted and the
regime of the maximum efficiency n was determined. For this regime the diffusivity
factor 0 (Wmax-W2)/Wj was determined; here, WIND are the relative velocities at
the inlet outlet) of the rotor cascade. An approximate formula for determining the
efficiency of a stage of an axial-flow compressor with a rough approximation of the
air compressibility is proposed: (1-n) / (1-no) - 1 + K, irbere- 7) * is the ef f iciency
0
Co.-d 2 / 3

V
X

ACC--NR. AP6031065
of the stage when 60 Ol- 02 - 0 and K is a parameter depending on the blaaa geomacr;/
and flow characterist7cs. The test results (with added characteristics olf six other
compressor stages) are plotted in a diagram in which the solid curve corresponds to
the equation (1-n)/J-no) = 1 + 1.45K+ 2.16 K2 (swrig.1). Ildbequationis recommaidedfor~.
estimating the effect of a decrease in the axial flow velocity on the afficiency of
an axial compressor. Grig. art. has-, 3 figures and 1 formula. [WA-76)
SUB CODE;1.320/ SUM DATE., 23jul65/ ORIG REP: 003/

T 'Inat;r-AA r1'jT(A1/9WTt1 DAVI 11fil
ACC NRo AP6013391 SOURCE CODE! uR/0096/661000/005/0089/0090
AUTHORt Yershoy, V. N. (Candidate of technical sciences);Pavlenko, G. V. (Candidate
of tech iile'nies); Nikolayenko. Yu. G.(Engineer)
ORG: Khar'kov Aviation Institute-(K6r'kovskiy aviatsionnyy institut)
TITLE: Determining the discharge coefficient when calculating anti-surge bleed ports
in axial compressors
SOURCE: Teploenergetika, no. 5, 1966, 89-90
TOPIC TAGS., compressor, compressor surge, compressor operation stability
ABSTRACT: Air bleeding from a compressor stage into the atmosphere is considered to
be one of the simplest and most effective methods of expanding the range of stable
operation of a multistage axial compressor. The discharge coefficient V of a bleed
port is usually determined'from detailed experimental data for the general discharge
of a fluid through an opening, without taking into account the special flow
characteristics in a compressor stage before the bleed port4 To investigate the
accuracy of this method, experiments were conducted to determine the bleed port
discharge coefficient under various bleed condWons. Testm were conducted with a
ten-stage axial compressor In the range of bleed flow Re numbers of 0.3-105- 1.2-105
and M numbers of 0.1- 0.4 with various locations for the bleed ports. The obtained
results are shown in Fig. 1. Based on the experimental data, it Lm concluded that

L30955-66-
ACC N16 AP6013391
Fig. 1. Relationship between discharge
coekficient; p and XjXF ibr vezious
locations Whe bhed pDzta. (TO = Wit
w3attye dr bleed-, AG -was f kv rate through
bleed port; AF - ratio of the bleed port
-area and the area of the ring corres-
ponding to the blade height) Fifth stage
411F (1-4) bleed port locations:
J
JL
1 - Above guide vanes; 2 above rotor;
3 - aboveguide vanes and rotor; 4 - axial
clearance before rotor; 5 - eighth-stage.
the discharge coefficient Is dependent on the location of the bleed ports, and is
highest for the bleed ports above the rotor blades and in the axial clearances before
the rotor. The obtained values of P shown In Fig. 1 can be used directly in
calculating anti-surge bleed ports in axial compressors. However, for ports having
shapes and Re and M numbers different from.those'investigated,.p should be corrected
using the following expressioni
pt . p#kl k2sk3
where, P' Is the corrected value; p, vaiua-from Fig.(I; and kj, k2 and k3, the
correction factors. The results also showed that air.bleedinj from a compressor has
a strong effect an the flow-characteriatice.in the stages adjacent to the bleeding
stagei. Orij. Art has: 2 figures. [AS)
SUB COD9: I/ SUBH DATE: none/ OIUG.UF:. 001j,~ ATD 0IMSi'l 11-21011
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t,trd for thrit reaction mpacities wkh Tilt app. Pit
v,ijryjijg ojiL tho expd, %%ozk cciatsiAd clikily of 2 Silit
Il 11 fill, rwit 10 W111411 will llvf~~ ior P104(161l~j thA

The temp, M tl:t v,il .11 O-C nit f~!-r tbn~ C ifti; vloal4ired
by of d - 0. 1
The: tokt~-) Iyurc pt 1-pil. In tht ro0owinp rity: From it no) 11rid
Coke Was Obtallltd bY "dillititkIl Ill it At IRW ill 3
Stre-1 M of N uniij cosa tion of the Sepa, of VIIIII Hills, I bell
~lhe coke ivp..,i ground to pairtlck5 of 70-80 P. Tfin ficssider-
Vbmined v.-as presird into the boat and apin plaml In ;I
~
II it te-1 tilt-
curumt of N at DW' und -ched crj*t. wt. For
'elipt, the C bv~.Ittd over a pCritA of 1.5-3 Jim. to the
de-hed lenirl. ;r1 A currelit 0 N, Itt which1crilp. the et
, tilwit

N W
f Z-4s rrpl;
o
l,:tA by a Strefull of Col. Cmlillg (if

lle C
also procietcled In a etarcu! of IN for 1,5-2 hr-j.. after irbich
the reaction tubc was dismaotled, atid the C wits w6rhed..
Zrt the expts- the follot%ing vr"e trie"tired., (1) tht- dis-
charge of gas trp :o and after the rev:tlon; (2) t,!mp. of the
ha:% and thi: sur(jicp_ of the C, iiind (J) the afrit. of C reacted.
Fxpts. vvere made In a temp. -rane of W-1000". Con-
Sumption of CO, tMohnivi to 1,2 cc./see. The a6is --c-
tion of file reaction fw-.urui ww-i"0:15 sq. cru. The method
zl~rd t ted th c d e: tn. of t lie kin c tic ch a raderis ties of t h c
be-
react + C02 - 2 CO tor diffefent coals sit tMid
lo%vM'. The niethod can be r(comnitlided far deln-oi the
reaction capncity of cokes from natural coa!s. Th-, expd.

data
UP- Well 11113111.1tCd, and M dia&rR*nl of the exptl. 11111). is
D17016"(1VI. "Mndys S. Mv;.-y
Ah'
11 114A , IN11014 111111011 IIA , 11 i l1 idlill

'
H
I Q
n-RSMOV~ V. I
USSR/Physics Moisture of dispersives FD-572
Card 1/1 Pub. 153-12/28
Author Yershov, V. N., AND Yershova, Ne M.
Title Ai- acprew method for determining the moisture of capi llaxj -porous
dispersive materials.
Periodical Zhur. tekh. fiz. 24, 854-858, May 1.954
Abstract Find a new criterion for the moisture content of capillary-porous
dispersive materialG, that permits one to reduce this quantity to an
electrical parameter. Describe a 'practical device for such a study.
Refer to relatedwOrks of A. F. Chadhovskiy (zjff.F, q, No 11, 1938;
Sbornik Trudov AFI, No 5, 1952, and No 6, 1953).
Institution
Submitted june 16, 1953

YERSHOV, V.H.; YERSHOV, II.M.
Thermal method for determining the nointure of fine-grained
capillary and porous substances, Zhw.*.tekh.fis.26 no.6:1306-
1308 is 156. (Hoieturs-Reasurement) (MM 9:9)

1 7 ;1'; J ; 1- J Jill', F-l III II . 11.11 :41 11. ;114,1, 11 WD, I .~j I I- ~ I ., 1.
-1-'-L- L-A ft-L~ IF: ~::I A Hit 1;: A It 11 1 i nL~L2
PHTF Hil I
1.97T fl

I
-- ~. d -It --- I - AL~' :A .1-H 3
IL;4L li Ll ~ , 1;
.i
ii; 1 1 j 11i q ; I
,H V! 1 1: Wil h 11
I ,

-A il .. LA LJ, 1.

'.", "I . I., . . .~ I
ll~' - '--' . - I - -1 - - - I ~. TI- , _ 1 1. -, " 'I'-r !-;H:'..-. " - t"', 11 1, ,1'
-- 2 - I .- ~ ~ -." ~ 1 " . II! !! 1 ' "' ~!l I! I - -Ilffi
11-9, - - !: : , I - I :;L . ; 1 1 . -! I~ 11. , ~ 1- HII ~ k ~ 11, .1 '1 :1 LI it . SJUfN
I I I
I i

---~ ~-V-N~-
Device for rapicl determization of moisture contsat in disperaed
and fibraas materials. Blul-tekh--ekoninforn6 no.8:33--~34 160.
(HM 13:9)
(Moist-are-Neasurement)

YERSHOV V.P.
9 -
I Thermoelectric moisture Ln(Ucator. Zav,.Iab. 27 no.2.,222-213
161. (1,111RA 14:3)
1.. Taningradskiy politekhnicheskiy institut imeni M, I, Mlinina.
(Hoisture)

YEMHOV2 V.N., kand.takhn.nauk
ntactless radiation mointure gauge for a=U-mades moisture
v0
control of the paper aheet. Bum.prom. 37 no.lOt29-30
o 162. (MIRA 15:11)
1. Leningradskiy politeklinichookiy institut int. M.I. Kalinina.
. (Moisture-Measurement)
(Woodpalp industry"Zquipwnt and snpplias)

UMHOV, V.H., kand.tekhn.nauk
-------------
Contactless radiation moisture gauge for oontlamme moisture
control of the paper sheet. Bum.prom., 37 no,,20.-29-30
0 162. (MLU 15:11)
1. Leningradskiy politekhnicheskiy institut im. H.I. Kalinina.
. (Moisture--Measurement) -
(Woodpulp industry-Equipment and supplies)

KOBYZEV, V.K.;,YERSH(YV. V.Nj;:MNETSOV, A.F,; ~WURIK$ P.M.;
RYAZANOV, D.G.;-FMKES, N.Ya.
Ifastering the rolling of two-layer sheets with ar busic
layer of low-alloy steel, Stall 24 no.l*.50-52 Ja 164.
"'fmA 17-.2)
.1. Kuznaii3kit~t*'tA3.14r~giches~~'Xi3mbirtat.
TI,

YERSHOT, V.P.
1Q~~4~ ng flanked gear wheals an HAAG gear-grindimg meMnes.
Stan.i instr. 29 no.1:7-9 Ja 158. (MIRA 11:1)
(Gear cuttinO

11 "
SOV/121-58-8-2/29
AUTHOR:
TITLE: Production Procedures Capable of Increasing the
s (Teklmologiches-
Productivity of Gear Grinding Machine.
kiye vozmozhnosti uvelicheniya proizvoditellnosti
zuboshlifovallnykh stankov)
PERIODICAL: Stanki. i Instrument, 195A.'Nr 8, pp 7-9 (USSR)
ABSTRACT; Discussing the possibilities for increasing the output of
Maag and simllar gear grindersq the view is taken that
neither the advance per cycle nor the number of passes
nor the basic grinding scheme (whether single or two-
sided)-can be changed without reducing the quality. The
only factor affecting the output which can be varied is
the number of wheel carriage strokes per minute. It is
shown that this cycle speed can be increased without
increaaing the Inertia forces by varying the setting
angle Qf-the grinding wheels. Increasing the setting
angle from its customary value of 150 reduces the length
of the stroke corresponding to the upper part of the
Card 1/3 tooth and increases the length corresponding to the lower
part of the tooth. The larger of the two values

01-
O,,
VP %
0
Kt 4LI'
0
4
Cli -k
4b 0
4 .10
Ki Ki
oil 10
Kl
A
o%p e- 00
Cie? IP IOP 40
f'0
ID.
K,
eK40
KP KO -$i d
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K~ Kp 0�.2,$p
to
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0,
L

L-1 BOV/121-58-8-2/29
Production Procedures Capable of Increasing the Proftotivity of
Gear Grinding Machines
determines the actual stroke required. In one method of
grinding the two whdals grind two flanks of the same gap
between the teeth; in another method, two tlanks of
neighbouring gaps. In the first methdd, thf se.-tting
angle corresponding to a minimum stroke JLs 2r-.' in the
second method 300 By usingthe optimum angle,
instead-of 156, ma;hining times can Do -rffduced by a
factor which increases with the YnAmber of teeth, At
30 teeth, thq"factor is about 1.1 for both grinding
methods. At 80 teeth, the factor increases to 1.45 for
the first method, and to 1.65 for the second method.
The change of setting angle requireE a small modification
of the grinding machine, Practical results have con-
firmed the analysis of the present paper. The
C~ard 2/'j-

BOV121-58-8-2/29
Production Procedures Capable of Increasing the Productivity of
Gear Grinding Machines
accuracy of the gears does not stiffer and no surfaco
burns or grinding cracks have been obiterved. However,
the machines must be in excellent condition.
There are 5 figures and 1 table
Card 3/3

YERSHOT, V.P.
Technological processes of preparla; gear wbools for lapping. Stan. i
I
instr. 30 no.2:15-18 F. 159. (HIRA 12:3)
(Gear outtine)

YERSIIOVl V.P ; MARTYNOVA# A.P. (Moakva)
Work schedule in modern forging and Otamping production (practice
in the Likhachev Factory). Gig. truda i prof, zab, /+ no. 7:23-29
n l6o. (HM 13:8)
1, Institut gigiyeny truda i profzabolovaniy AMN SSSR.
(FORGING-HYGIENIC ASPECTS)

3/121/60/0c)0/010/006/015
A004/AOOi
AUTHOR: Yershov. V. P
TITLE: Increasing the Efficiency of Heavily Loaded Hlgh-Sptped Geared
Transmissions
\1
PERIODICAL: Stanki i Instrument, 1960, No. 10, pp. 21- 22
TEXTs The author suggests to Improve the efficiency of heavily loadod gears
by lapping. He points out that the toeth of these gears diAring operation often
break off, which he ascribes partly to power ami speed factors and partly to th4t
grinding process itself. One of the main defects in this respect is the origirra-
tion on the surface of the ground tooth of a more or less dtep defective boundary
layer. It contains metal zones subjected to tempering, which ax-- originating ow-
Ing to transformations under'tbe effect of high. temper&turas in the grinding zone.
At normal grinding conditions the tempering depth generally does not exceed 30p,
while the damaging effects of Umpering show ordy up to lot". The presence of such
sections on the tooth profile surface causes the formation of fatigue mic2!,ocracks
which, in the course,of time, under the effects of high hydrodynamic pressures
quickly spread out into the depth. Teeth Impacts connecti~d with errors of the
Card 1/3

S/121/60/000/0,140/006/01551
A004/AOOl
Increasing the Efficiency of Heavily Loaded High-Speed Geared Transmissions
principal pitches of conjugate elements do not only cause thenoise of geared
transmissions but lead also to the destruction of the working surface of the teetb,
The most efficient way of eliminating these above-mentioned defects is, according
to the author, lapping of the teeth profile. In order to warrant the elimination .
of the harmful defective zone, a layer of not less than 15/4, has to be removed.
However, it is not expedient to leave so big an allowance fo), since flie
efficiency of the process and the precision of the toothing elemVits depend on*the
itude of allowance; this refers in the first place to the tooth profile --*ror
f, the play of the indexing circumference e 0 and deviation of the tooth direc.-
r
tion 6B . Therefore, the right lapping allowance is of utmost importanice, and
0
should be in the range of 15 - 30/A, Also the %ifferance, in pitch" and th'-,
principal pitch can be corrected by lapping. The table presents some data bn the
accuracy and surface finish of ground gears before and aftor the lapping process.
Lapping was effected with a paste of 100 grain nize ... the wuthor recommends an
abrasive grain of 100 - 150 grain size - made of white ele::trocorundum, while the
lap was made of gray pearlitic cast 11ron of HB 180 - 210, With -,mall allowances
a paste of 220 - 240 grain size is recommended, The author reco=ends to carry
out the lapping operation of ground gears on machine tools operating according to
2/3

S/321/60/000/010/006/015
A004/AOOI
Increasing the Efficiency of Heavily Loaded High-Speed Geared Transmissions
the principle of internal gearing, because of their more balancod specific
pressures.

Toothing Tooth Machining Finish
Hsk in Microinches Maximum Difference in Adjacent
Principal Pitahas in
Characteristics After After After After
Grinding LApping Grin(Ung E"aPI)Ily:
z 130,
m 7 mm, 42 - 53 28 - 35 32 - 45 11 -
200
z 39,
m 6 mm, 41 - 46 26 - 32 23 - 31 10 - 12
200
There is one table and 2 Soviet references.
Card 3/3

IMEOVt V.P
Dynamic factors occurring In lapping gear wbeelo, Stan,i instr. 32
no,3M-16 Mr 161. (Gear cutting) (MIRA 3.40)

Problems of Induatrial hygione In tho production of nl,l,,jyod ptnelfi
in electrometallurgical plants. Gig. tinida i prof. zab. no.2t3-10
162* (MMA 15:2)
1. Institut gigiyany truda i proftabolevanly ANN SSSR.
(ELEcTRcmETALLuRr.Y-HYG1HNIC ASFMTS)
, - -- ~77
-7117
7

... 34-
YERSHOV, 7.1'.; ':`ELGR0Yj--, V.A.
C(.~;f:parative evaluation oil ths aerosol of efiror-fur. oxide
condensation and its mixture with chromium anhydride.
Toks. nov. prom, kbim. veshch. no.7:162-180 '65. OCR,,. is:?)
1. 1z gigiyenicheskogo otdela (zav.- prof. L.K. Kho'-:yanova)
i patologoanatoriehnskoy laboratorli (zav.-- pr(ff. 11,F. Dvdzhkcrr)
T giyeny ~NN
.1 no ~u ta t~.,,
SSSP (direktor - prrZ. A.A. Lntavet).
HN

YM ovo V.S.
Yorabovs V.S. aW X.T. Skl7abln
*Helminthima of Ewsesp* Moscow-LonimaMp Sellkhomgis,, 1933.
SO: K.I. S&yabin, Moscm, 194.9 (bk). p 20%

0 V'~V~h
VOW, V.S., Prof., Chief, Adin. of Vot. and Zootec~riical
1-11inistry of Pligher Education, USSR
I'Veterimr, colleges in the new academic year."
SO: Vet. 24 (8~ 1947, 4
0 0 0 0

YERSHOVO V. S.
Antipin, D. N. and Yershov, V, S. "Academician Konstantin Ivaw7icb Skryabin", (The
helminthologist,, on the 40th anniversary of his scientific activity) Sbornik rabot
po gellmintologii (Vs soyuz. in-t gallmintologii im. akad. SkryabinZ Moscow,
1948p p. 5-13, with Xtrait.
SO: U-3042, 11 March 53s, (LetopisInykh Statey.. No. 10,, 1949).

YERatov, V. S. Pr4 PA311h':'?T~3

YMSIIOV, V. S.
- -E, - -1
I L arls Za z-
25897. YMSHOVY 7. S. TsMI razvi' i;ra Delafc=
1:1.
v organizme loshadi. Avtoreferat. Voterinarlya. 1949, ITr,. 8, 26-2~'.
So. Letopis' Zhurnallnykh Statey, Vol. 34, Moskvas 1949

qlusvov, Lv.s
in "A Brief Course of Parasitology of Dc'mc-Si"I.C the
authors altucrto the data of4srshov (o"n naE;e 327 :.n =scticn ~;r, thi
development of Delafondia in the organism of the horse).
CO: Veterinariya; Vol. 27; No. 11j61-63; Movembe.- 1950 uncl dc! g
.1
Trans. 26h by L. Lulich
0 0 a G 0 a 0 410 0 0 0 0 0 0 G G 0 0 0

Yjs?mov~ V. S.
Liver Flulp
Use of carbon texacl3loride in cases of facsioliasin in sheepo Veterinariia 29, No. 2,
1952o
iNll-Unl'9r% (V%tf- 14CliktAOAOIOjj "- K-1- Skrl*'b"Vl
tf -XI58, I* " 4
9. Monthl List of Russian Accessions, Library of Congress, 1953, Uncl.

pIAKHOTh,yA, R. A., KRIM. cv, YERSHOV V -. S., and GOREERTS, A. D.
Novyy metod diagnostiki askaridoza svinoy, "Works on He3minthology" on
the 75th Birthday of K. It. Skrcyabin I%dat. Akad. Nauk, SSSR, kj'oskva, 1953,
page 240
All-Union Inst. Halminthology in Acad. K. 1. Skryabin and Chatir of Parasitology
Belays Tzerkov, Agticultural Institute

YERSHOV, V. S.
Osnovy veterinarii CPrinciples of veterinary science_7. Moskva, Sellkhozpiz,
1953. 448 P.
SO: Montbly List of Russian Accessions, Vol. 6 No. 2-2 March 1954.
~ .: !f-~ -
II

Ull
MIRSHOT, T.S., prof., daktor Yet, nauke
Clinical a"cts and diagnosis of Alfortia infections in horses.
Trudy VIGIff 5r109-123 153* (MIRA, ll.-l)
(Ifamtoda) (Parasites-Horoom)

ANTIPIN, D.N., dolctor vaterinarafth naukg profooeor; YuS,4Qj,._Tj,,, doktor
veterinarnykh nauk. professor; 201MAR117. N.A.,-6'kior Yoterlaarnykh
nauk, professor; SALTAYZV, V.A., doktor vaterinarWkh nauk, professor;
SOIGVAY, A.S., redaktor; VISKOTIA, Ye.l.. takhaichookiy redaktor
(Parasitology aad festatious of farn aaimals] Paratitologiia i
InvactomVe ~olezni sellskokhoslaistveaufth shivotTWkh. Pod red.
V.S.Irshova. Koskva,,Gos. ltd-vo selkhoz. lit-ry, 1956. 478 P.
(Parasites--Domestic auimals) (MLU q: 11)

W1 I ~
TUSHOV, V.3olprofe
Professional veterinary training in the Chinese Peoplels
Republic.(jeterinarila, 35 nool2t7l-73 D 158. (YrOA 11:12)
hina-Teteripp.ry medlcins;~Study and teaching)
-: j:, 1,11;- F7777

TME10T, V-S-9 , 0,tv. redo
halminthology,
=11, no, ne
80th birthd*71
vjk-AdGmtWz
1959. 1
Aksdemiyg
1. Veesoyus
V.J~Leuinao
cademiclOrl
On tho occasion Of A Igii; k 80-latilu
RabotY TO 9611m'ntolCj'.khoz.5s5a,
I(Oulma, Izd-,Yo M-VO so 0(in 13%6)
.8jovkOkhOsyayfitvGWlkh nouk im6ni
(galminthologY)

otvsrede; WDINAp M.P., redo; PMOV, A.H., red.;
PODNTOWMATAs V.P.. red,l OMMOVICH, TeJoet rods,;
KARTASE13VA, V*Xes redo; AXMOVIO N.M.* khudosh.-teklin.rod.
[Works on halminthology; 9n Academinlan X,1,61criabin's 80th
birthday] Raboty po gelliontologlia, k 80-latiiu akeidemike
X.1.31criabina. Koskya. Izd-vo X-va sell.khos.SSR. No.j.
1959. 217 P. (KIRA 13:4)
1. Vaesoyuznaya skademiya sel'skokhozyaystTOnnfth naulc imeni
V.I.Lenina.
(Worms. Intestinal and peraisitic)

r.0
-'?~qf tl~jv-'Ina.
Prcotentlicm
36 no..,
4 t I j iTI.
-parasitic)
(Pbpn .othivz~ -10) (Sorr-CO lilt a Gtj-n,,;tA anQ

YERSHOVY V.S. (Prof]
"Problem of Imnunization of Agricultural Animls Against
Helminthiasis."
report presented at the 16th Intl Veterinary Congress, Madrid, !959.
(Veterinarila 37(2).75-76, Feb ig6o)

TEMOT, V.So. prof., dolctor vater.nauk; ZMMIMI, A.A., prof., doktor
.veter.nauk: YRSOBRAMMUSKIT, N.M., doteent, kand,veter,nauk;
TMITSff, S.G., prof., doktor vater.wak; IMN, B.Zo, doteent;
NOSKOV. N.M., doteent, k:and.vet9r.nadk:; TIMITABOYA, HVI*#
red,; BALLCD, AJ., takhn.red.
(Principles of veterinary medicine) Oenovy veterinaril. Izd.2.,
ispr. I dop. Moskva, Gos.izd-vo sellkhox.lit-ry, 1960. 437 P.
(KIRA 13:10)
1. Direktor T esoyuznogo inatituta &I'miAtologli im. K.I.Skrya-
bina (for Ter:hov), 2. raveduyushchLy kafedroy f Iziologii Lenin-
gradskogo voterinarnogo institute (for Zhuravell), )o HookoveVnyo
vaterinarnaya akademiya (for Proobrazhenskiy). 4. ZnvodI=ehchiy
kafedroy operativnoy khirurgii Hookovokoy vaterinarnoy akademii
(for Tel'teov). 5. Zov6duyushchly kafedroy opizootologii Oren-
burgskogo sellskokhosyaystvanncgo Inatituta (for Hoshov).,"
(Yeterinory medicine)

YBRSHDY, V.S.
Tx=nization of larm animals againsit helminthisses, Tmdy
Inst.sool.AIW Kazakb.S= 12t96-103 160& (MM 13-17)
(Vorus,j Intestinal and IxLrasitic)
(IMU., *)
(Vaterium-k parasitolo&)
,.~i_ ; .

YMS11OVp V. S. Dr. , Director#
wfthinococcus and coonuroels*
To be submitted for the 29th Session of Tnternationsl Office of Spizooticep Pari3,,
Frave,, 15-20 Msy 1961.
W-Union Scientific Reserch Institute of Helminthology Imai L 1. Ma7bin,, and GAWMU
(fau), Dr., Now Zealand.

, , , t I, ,. .. I
KOVAIMIROO Ya~R~; YEP3110VO M"
Session devoted to the 60th anniverijai-y of t1m Bulgarian Central
Veterinary'Institute for Infectious and Parasitic Diseases.
Veterinariia 39 no~1:88 Ja 362. (MIRA 15:2)
(Bulgaria-.Veterinary reseaxah)

YERSHOV, V. S., KOVALENKO., YA. R.)
"Session,, dedicated to the 60th anniversaryof the Bulgarian Central 7et-
erinary Institute of Infectious and Parasitic Diseases."'
Veterinariya, Vol 39, no 1. 1962 Jan. pp 66

YERSHDVS V. S-
wAllargy in ascaridosis in hogs."
report to be 3ubmitted at ths 17th World Veterinary Congmaup
HanoTars Idest Garmiqp 14-21 Aug 63a

SHIKHOBALOVA~ P.P.., otv. red.- YERSHOV V.S., red.; PARAWNOV.,
A.A., red.; FODq!;;L qt. ; RYZHIKOV, K.N.,
red.; IVASHKIN, V.M., red.izd-va; T11G:G11JLAOVA, S,G..q
tekhn. red.
(Helmintha in man, animals and plants and their control;
on the 85th birtbday of Academician Konstantin Ivano-vich
Skriabin] Gellminty chelovekap zhivotrVkh I rastanii i.
bor'ba a nimi; k 85-letiiu akaderika Konstantiva, Ivanovich
Skr;iabina. Moskva, Izd-vo AN SM, 1963. 523 p.
(KULA 16:12)
1. Vsesoyuznoye obahchestvo gellmintologov. 2. Vaesoyuznyy
institut gellmintologii im. akad. K.I.Skryabina (for Yershov).
3. Institut meditsinskoy parazitoloigii i tropicheskoy me-
ditsirfy im. Ye.I.Martsinovskogo (for Pod"yapollskaya).
4. Gellmintologicheakaya laboratoriya All SSSR (for Parpmanovo
Ryzh'k'ov)' (Worms, Intestinal and parasitic)

ror. I., kan-I . V,~ Lf, r. Till., i-,,
kand vl~~vr. nauk
Ar.p--,-'car,-4(-,n of piperazine salts in veterinm,y
VIGIS 10:198-206 163.

-YERSHOV, V.-S. -
[Helminthiasis of swine] G0117jintoV BvInot. ~Joskvag lzd-vc,
Sellkhoz. lit-ryj, zhumalov i plakatovp 1963. 233 pq
(Milill 28:9)
i~l-

YERSHOV,, prof.
Immunity of farm animals in helminthiasis. Veto-rinariia no.12:17-20
D 163. (MIRA 17:2)
1. Vsesovuznyy institut gellmintologii imeni, akademika K.I.Skryabina.

YERSHOV, V.S., prof.
Pat to use the achievements of halmintholog-leal science.
Veterinariia 1+0 no.4:1-5 Ap 163. (MIRA 17:1)
1. Direktor Yeesoyuznogo institute. gellmintologil imeni
akademika K.I. Skryabina.
I I - !T4I

L I 'f
Ylasliuvp V.S., prof., red.; YAI,,JIYKIf, A.M.., red.
1 - 17 ~
(Manual of veterinar-i helitintho2o[g] Spravo2~xlk po -,e-
terinarnoi gellmintologli. llonkva., lzd-vo "Koloa," 196-1.
367 p. (mRfi 17:8)

ILOTAREV, N.A.; S.-MAYM, V.A.;
prof.; ZO
ANTIPIN, D.N.; JEJ 0
DREVI.YANSKAYA, N. red,
[Parasitology and irrvasive diseases of agricultural animals]
Parazitologiia I invazionnye bolezni sell skokhoziaistvennykh
zhIvoUykb# (1.1y) D.N.Antipin i dr. Monkvnp Tzd-vo IlKolos"
1964. 494 p. (min vwl)

YERSIROV, V. 15.
"Immunogenesis in ascaridosis' trichinellosis and 14--tastror-5-jylilcsis of
pig. It
report submitted for lst Intl Con~Z Parasitology, Rome, 21-26 Sep 1964.
Inst of Helminthology, B. Cheremushkiy 90, Moscow B-259-

1=z
iLyp-tonb ana sani -
tatiwi, Teachin~-
Medicine Social Hyglene
-!%-Real Problems of Sanitation V S.
ef Section on Sanite.--~au, afro
1th USXR, 5 PP
CO
Diueu2eaa Third Plenum of the Sovie-ts for S=i-
an EC111dati on, M1 n.1 striae of- lLaalth USSR
,=d:RWSR, bola at the and of 1948. Ccmmento.
ebaracto-z and value of ropor-ta submitted.'by
dateg. Speachea revealed the great or-~,
9tamt1axJ- work in-sanitation eftcati=..
.-UM/149dicine Hygiene and Xl=~Apr 49
Sanitation, Teaching (Contd)
-uses importance of urginG rill pbyeicians
and medical uorkers to particirate in plannea
iwanitation oducation In accordance vith Decree
go log.
14
118/49T56

YERSHOV. V.
25949. Yershov, V. C. Dolg chesti kazhdoro rieditol.nskcfo relvtnlka. Netalflece
organizatsil san. prosveshcheniya v SSSR). Folldsher I mkueb~t&caj 20,49, Yo 7, a. 3*0-43
SO: Knizbneye Letopis', Vol. 1, 1955

BOGOLEPOVA, Lyudmila Sargeyevna-, YLTMOV, V.S., red.
I --------
(Health education in the u.S.s.R.] Sanitarnoo -pros-veshchenle
v SSSR. Izd.2. Moskva, TSentr.nauchno-isel.in-t sanitarmogo
proeveahcheniya, 1958o 58 p. (MIRA 12:4)
(HS"H EDUCATICK)
7

SENBLEV, A.B.; YKMOV, V.S.; MAYSTRAM, X.V., red,; SENCHILO, K.K.
tekhn. re'a-.-
(Safeguarding the health of the Soviet population] Okhrana
zdorovlia naselenlir v SM. Koskva, Kedgiz, 1959. 36 1).
(HIU 13:3)
(PUBLIC MULTH)
V
Hill1liflil HM If 11111MI lilli1i'll ill 11111" Ill H1:111iIiI

VMHOV
Develop hygienic practiaps in our work and lifa. Zdaravle 8 no.5:
1-2 My 162. 1 (MIRA 15:5)
(IMUTH EDUGATION)

,MMHCV,, V.S., prof.j NAUMYCHETA, M.I., kand. vet. nauk; POLLIrAYEVA,0.0.,
m~dhiy naucbnyy sotrudnik
Manifootation of a-Uergy in exparimontal mLltiple infection of
piglato with accarlagin, Trudy VICIS 11854-58 161,. (HIIIA 1802)

IZIU, L.Ye.; BOROZDOV, I.A.; MOILO, V.Ye.; TMOMON, F.V. Prinimali
uchastiye: BELTAUT, P.R.; BV.?I'MOY, 11J.; BUBYRI, T.A.; VARSEUIVSKIT,
I.N.; D=O, ~-GIN, Ye.V.; DUKAWY, H.F.;
IVANOV. P.S.; KOUREVA, V.F.; HOUT11, K.I.; MOGILKO, A.P.; PAUGHEI[KO,
A.I.; PCKALYUKOV, S.H.; PRIKHODIKO, H.D.; RIJBIN, I.A.; SIDORENKO,
P.A.; TYUTYUNIK, Ya.I.; HEMINITSKIY, L.Ya.; BONNO, V.I.; KRIVTSOV,
A.T.; LOKSHIN, V.D.; SOPIMER&O, H.P. RABINKOVA, L.K., red.izd-va;
BCLDYHXVA, Z.A., takhn.red.
(Types of mine cross section] Tipovye eechenli-tt-gornykh vyrabotok.
Moskva, Gon.nauchno-tekhn.izd-vo lit-ry po gornomu delu. Vol.4.
(Cross section of mines supported by a aectiowil reinforced-concrete
lining of URP-11 panels for l-, 2- and 3-ton nilroad cars] Secheniia
vyrabotok, zakreplennykh abornoi shelezobetonnoi krepliu iz plit
URP-11, dlia 1-. 2- 1 3-tonnykh vagonetok. 196o. 278 P.
040A 13:12)
1. KhBrtkov. Gosuderstvannyy proyektnyy institut Yuzhgiproshakht.
(Mine timbering)

YERSHOV, V.S., st. prepod.; KOPIYEV, S.I., otv. as vypusk
(Design of a polyspast] Raochat polispasta; uchebnoe
posobie k raschetno-graficheakoi rabote po kurau
"Detali mashin." Gor1kii, Gor1kovskii inzhonerno-stroit.
in-t im.V.P.Chkalova, 1962. 26 p. (MIRA 16:8)
(Pulleys)
...~ ~ i ~ -,

BADILO, Me.; BOROZDOV, I.A.; TMWHOV, V.S*; HOG-TJXO# A.P.; NIZOLATHY,
G.P.; DUGIN, Te.T., otv.red.; WMALOT, N.Y., rod.; RIBUI, V.A.,
red.; VARMIAVMT, I.N.. red.; TMTMIIK, Ta.l., red,,; ROBIN, M.I.,
red.; PAUCHKNKO, A.I., red.; BRUAM, F.R., red.; WINKOVA, L.K.,
red.izd-va; DOLDYRIVA, Z.A.0 takhn.red,
EStandard cross sections of mine workings] Tipovye sechaniia gor-
nykh vyrabotok. Moskva, Gos.nauchno-tekhn.izd-vo lit-17 po gorno-
mu del-a. Vol.2. [Gross section of workings lined with concrete
and artificial stone, for 1-ton caroj Secbeniia vyrabotok, zakrep-
lennykh betonom i iskusstvannym kamnsm, dlia 1-tonnykh vagonetok.
1960. 459 p. (MIRA 13:11)
1. Moscow. Gosudarstvennyy proyaktuy7 inatitut Tuzhgiproshakht.
(Mining engineering)

RAYKOVO I.Ya,,, kand. tekbn. nauk; TMHOV, V,,T.
Film formation in carburptor engineo* Arta prom* 30 "OnUt
6-10 if 164 (MIRA l8t2)
1. Moskovskiy avtomekhanichaskiy Institute
;~:J: ~~
I 1 11 M

-----------
L
0
41,
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-.04 64
q, --V. - L, ~--
49
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vi-

18816
Cylindrital bending of three-ply 9/147/61/000/003/003/017
c081/3135
equations are quoted and reduced to a sixth order differential
equation which in solved for the deflection in terms of mixed
polynomial and hyperbolic functions. Similar formulae are also
derived for the axial displacement and stress, The boundary
conditions appropriate to freely supported, clamped, hinged
supported and free edges are statedt and an extensive table of
formulae in derived for stresses and deflections in plates
subJected to distributed or concentrated loading and to various
combInatlons of clamped and supported edge conditions (20 cases),
assuming vanishingly small flexural rigidities of the outer layers.
Thanks are expressed to Doctor of Physical and Mathematical
Sclences Professor Kh.M. 14ushtari for directing the investigation.
A.L. Rabinovich and L.E. Bryukker are mentioned for their
contribution In the field.
There are 23 figures, 3 tables and 4 Soviet references.
SUBMITTED: December 10, ig6o
Card 2/2
Mil"11117111111111 1111, M'1111~ U1111111,11 1111

S/147/62/000/001/014/015
0 E200/E435
AUTHOR: Yershov, V.V. (Kazan')
TITLE: Stability of asymmetrical sandwich plates
PERIODICAL: Izvestiya vysshikh uchebrtykh zavederiiy.
Aviatslonnaya tekhnika, no.1, 1962, 120-124
TEXT: Using an equation derived from the equations of
Professor Kh. M. Mushtari, in his previous paper (Ref-3: ibid,
no-3, 1961), the author obtains an equation for longitudinal
axial force N acting per unit width of the upper and lowgr
layers of rectangular sandwich plate supported along two opposite
edges
N
(2.19)
Crit to 12
0
where 2h - thickness-of th-e core 2h1 of upper layer,
210 of lower layer; z' = h + h1f Z11 h - h"t
2E1h1
Bf V. -Vt - rigidity of upper Idyer,
12 21
Card 1/2

Stability of asymmetrical
S/147/62/000/001/014/015
E20040135
Bit - rigidity of lower layer, BOB"/(B'.+ Bit),
G3 - transverse shear modulus of core,
Lo - L/k, L- length between supports and X - support function.
Both edges simply supported or one edge clamped the otlier restrained
against rotation only 4 = 1. Both edges clamped X = 2.
One edge clamped the othur simply rjupporLod X u- 0-7,
One edge clamped the other free X = 0.5. If BI = Bit and
2h' = 2h"9 Eq.(2.19) reduces to Lliat given by
A.P.Prusakov for symmetrical plates. There are 5 figures.
SUBMITTED; April 13, 1961
Card 2/2
;14T

FOPOVAP G.B.; YERSHOV) T.V.; KIJ7,NETSOV,V.A.
Experimental study of melting and cr-Istallization proceanas in
pentlandite. Dokl. AN SSSR 156 no. 3:575-578 164. (HIPA 17:5)
1. Predstavleno akademikom V.I.Smirnovym.
94h;

................ . ........ .. ...
7- 7-
0001
AU.ILFDR: Kostrov, A. V. (Candidate aftechnical aciences); r AjYsk--Lj:j' TemLej~.
V. V.
6RG: Koscov Automechanical Institute (Mosko"ki~~ wirtomekhwii0makir ilastitut)
TITLE.~'Transfer of heat~to the lubricating oil n eng
SOURCE: Avtamabillnaya promyshlenno6t', no.A, 1966j,,1-3:
TOPIC TAGS: heat tranrfer, vehicle emg1ae, lubricat"g oil, ve4d.cle ellgine cooling
syEtem
ABSTRACT: The authors considdr transfer of heat t.o the lubricating oil in automotive
engines under various operating'conditions I since the lubricaticia systmit haz become an
-Important- factor In lengthening the service lifex~r engineis in 111ev ar the recent ten-
dency toward increased engine paver by raising the efficiency oT the ccmbustion cycle
and Increasing the rpm. Heat is transferred to the oU friom. caiiLponerAa, heated Lry fric-
tion and gases end from gases which leak into the crankcase tbrtush InTerfectionu in
the piston rings.. The third factor (lealtage of hot gases into the crnmkcase) van not
taken into consideration in analyzing the components of heat tninsfer Eis it vass Llssuaed
that the same quantity of heat is dissipated into,the ambient atmosplinre from the lover
walls of the crankcase during stand testing. Heat transfer to Via cranitcaae oil in the
IMA-408 and ZIL-130 engines was experimentally studied in the Autcmoljile and Tractor
Engirte Laboratory of the Moscov Automechanical Institute. The tim em(liner. were stand
tested for kpproximately the same number of hours corresponding to am automobile trip
7~- d: - -536.t-24-.621.431-73