SCIENTIFIC ABSTRACT LIVSHITS, S. P. - LIVSHITS, V. S.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000930310012-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 20, 2000
• Sequence Number: 12
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

89232
s/o96/61/000/003/002/012
E194/E155
Interaction Between the Diffuser and the Spiral Chamber in a
Centrifugal Compressor Stage of the End Type
500 mm water under certain conditions, If the stage were operating
on condensed gas, so that the specific gravity is 35 times greater
than that of air, and if the peripheral velocity were 290 m/sec.
the maximum pressure difference would be 130 times greater than
before, namely, 6.5 kg/cm2. During each revolution each of the
ducts in the runner would pass through one zone at minimum and
one at maximum pressure which would give rise to pulsation in the
runner. Cases are known in which effects of this kind have
occurred and have led to runner failures. It is concluded that
in certain circumstances the use of guide vanes of the type
described can offer considerable advantages,
There are 6 figures and 4 Soviet references.
ASSOCIATION: Tsentrallnyy kotloturbirmyy institut
(Central Boiler and Turbine Institute)
Card 4/5

88232
S/o96/61/000/003/002/012
E194/E155
Interaction Between the Diffuser and the Spiral Chamber
Centrifugal Compressor Stage of the End Type
-7 -
. Fig.
2
Card .5/5
in a

3951
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23951 2/005
slo96/61/000/008/00
E194/EI55 fU5er of a
jdth and angle of installation of the bladed dif ere made
W I coingre,,or stage Testsw
er is bladed. widths.
centrifuga 9s marked when the diffus f various relative ika NO-101
width is 1 diffusers 01e in TeplOenerget were made
stages with bladed in an artic of tests
on f:Lve .,,r1bed fr-uP- easure
de TwoI and to m
The rig used Was present author- ical se ctions racter istics Of
.) by the low in tYP' cha
1955 (Ref-3 the direction of f Of general d for the
to Measure necessary fO construction commonly use
propertie 5 low , formula is (1)
stag8s. The follow 0 the diffuser: b.
the Of flow at inlet t= tg a2 1;
direction tg OL3 30f the
:)f the vector
between the direction `ngent to the runner
is the angle runner and the tu cannot be used in
where OLZ beyond the formula) cjablY
velocity show that this IC is appre., with
absolute The results when the width rat. 1. stag
periphery. bladed diffuser test resu Its show that than unity the
designing a roM unity- The /b2 is greater path; the flow
different if the ratio ':)3 over Its whole
., diffuse 5 uniform
bladeles comes les
flow structure be
Card 2/4

23951.
s/o96/61/000/008/002/005
El94/El55
Width and angle of installation of the bladed diffuser of a
centrifugal compressor stage
breaks away from the blade, and reverse currents occur which
reduce the head and efficiency under almost all conditions. When
the diffuser is bladed, the zone of markedly non-uniform flow
structure and reverse currents that results from increasing the
width ratio occurs only in the annular bladeless section beyond
the runner and in a small section of the inlet duct of the bladed
channels. At small flows and also under optimum conditions,
increasing the ratio b /b2 above unity reduces the efficiency and
stage head. on the oNer hand, at high rates of flow, increase of
this ratio may somewhat increase the head and stage efficiency.
It follows that when the stage is intended to operate over a
narrow range of output it is beat to have the ratio b3/b2 near to
unity, Howeverg if high rates of flow will frequently be
enczuntered in service, it is advisable to make this ratio some-
what greater than unity. As previously mentioned, the formula
generally used to determine the direction of flow at inlet to the
diffuser is not confirmed experimentally. Therefore, when b3/b2
Card 3/4

23951
s/o96/61/000/008/002/005
E194/E155
Width and angle of installation of the bladed diffuser of a
centrifugal compressor stage
is greater than unity, the angle of installation of the inlet
edges of the diffuser blades should be such that the angle a3
differs little from the angle Q2 of the flow at discharge
from the runner.
There are 7 figures and 3 Soviet references.
ASSOCIATION. Tsentrallnyy kotloturbinnyy institut
(Central Boiler and Turbine Institute)
Card 4/4

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. the the 5r
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342511
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OillonS*101113 -ilt 5 5
The Oj
tb
5 ve~~y dif ficult to
d JL n Lt a-Uticie
clomiftonlY Us )T-oblemS and this.
"(111"It-jon on tbese t- .n the
alculatio%,,,,,,,,t rried out 3
c , a 1. - t ud.y .c adiffusers of differ
x of an exp St aFe with
.gives some reallits tS were made Ona isturbing 8-xial ond
Tsy which tes To avoid d tlie flow bey
.T I in s using a single runner. s were used. Here livered to
ent width intel,mediate-type stage ines and is then de
o e.,
r,ym etry, ing guide V~ t tag
m - revers' the inlet to he -nIIt
the diffuser enters .mulates tion of the Main-Meas-
1 aperture which s1 th loca
a centra perimental Stage W' parameters are as
. 1. The runner 0,0(
of the ex ~15;
diagram oints is shown in Fig.-096; b2/D2 the ay-ial
urement P 0 535 ; bl/D2 0* is the width in
: Dl/D2 = b - n the
follows =480, Here, Igle betwee
300301 02 the diameter and 6 the at the
on, D - d the tarigerit five
directi to the mean line of the blade an Tests were in,"Kie on
tangent centre of the 1-unTleri
periphery at the
Gard 2/f

34254
,Prjf~ eati~., of the dimenzleln.-; of IA /t/
witti the rmi--i diame
1. t; r, e, d i f t'u ~; f! vs w,--,,.; 54/1)~,; 1.74. A ';'Utloy vto
1. influence, of the, brenrirn ratio b 3/ h~?
i s~' mude oC L
V
J*L(~w !tr) a bladeless di-ft'usfr.
nr.,; %vere in:~t-alled across the entire height of the appar.1toz;
commencing from the diameter near dischnrz~e from tile runri(,v wheve
D/D2 = 1.06 and thence up to D/D2 = 1.?3 near the peri-1hr;ry ,r
the diaphragm. The measurements were made -)t sixty paints
the width of tile apparatus Undev al. _- (.o,i i.itions. Te!,to T.-tt.3(jitz
are given and the following conclusions were drawn from t'n-?jn: 1;1j('
direction of flow remains approxim-tLely tho same acro.31.3 '010 width
of the apparatus only when the rat,io b3/b~2 z 1; as this r:ill'io in-
creases the flow becomes less uniform across the width. Whon
b3/b2 = 1.5 the curves of ce. = f(b)
maximum near tho middle, and the diffev(.nce
near the centre of the apporatus and
more. Forther -in(;rease in the ratio
i j
-rregularity of flow structure, bo;h
apparatus and across the radius, It
have s clearly expreil.:;eo
between thr~ anglo
:1
at the walls may be 50o !ril
b3/o,? caui;es
across, the width of oLe
is evident that exor-.,osion
Card

31054
The ratio of the dimensions of ...
E j. 94 ~-1'5 5
(1), which is ofte.a used for desi-., ~!j par-11--om;:3, is v--~ry
truth. A study was then made 0v t.ij~! irifL~j~,,aL;e of
width ol' the diffuser on Oic g:r~r:1-:iL ot,
it was found that, tinder all -at exL;T.-;
flow rate,~;, irtcv~,~ase in the vk-1,40'v" ij5/b2
develo-ped and LiLe adiabatic It mi-3h-' ?1:-VO W:011
exuec,te~l rhst Iricrease in t'ne widtri of the d.lffuser wo,,L:1
r1o.. t; S.-)
inc.rease the ootp it, but thi.-i i..- Tne optimum
bladeless diffaser is b / b p = i j. v t i I e !Ti o ~; k;
structu.re beyond the runner ond ;he nead. and
Th,ire are 5 figurt-~, and 5 Ooviet.;-bloc rere~-erices.

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5/09(3/ 05 5 C'
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ef~_ ol~ * 015N5 %,e t-.4 0
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etT
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r, Z% tl. 0"(v V6 lrotO' bl, ie de
d3'ACOC' ef o1v .,oe5 5) '-" e
e66
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stv, edes ,,0'tptevs. 01,1-1 09 t IS
ty%.e
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,,,,,,YC-e 5e1:
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GOS
s/oq6/62/oOO/003/003/oO8
E194/E455
The use of rotating ... The inlet edge of one
fferent discharge angle,* which were used to The
having di contained two small ducts Angles-
blade an the blade and flow Ekrying
diffuser ent betwei .1gle and vc
measure the al',gnm h with a fixed diffuser a'. th the flow- The
,tage was t0st" 1)ot ted to line up wl effici.ency.
"ith tile angle adj11S rVes Of hoad and tile f low
load and re plotted in the form of " align with ead curves
results a justing the blade angle 11 "S. the b
It is seen that ad ~,sor characteristic Iaway from
improves the compre ncy higher at discharges mprovement
greatlY ter and the efCici e characteristics- TheI
become flat . ;n point of th of delivery. An
the optimum de-911 oticcable at low ra,tes
is particularly n h the adjustable diffuser is
of control in whicusual methods of control
integrated method one of the flow to swirl, or
used in conjunction with causing the inlet performance of
ling the intake, improve the s of the
(thrott 9 the speed) can considerably inlet edge
alterin The forces that act on the cti,, during the signal
the compressor, of the change in flow dire be used as I
blade as a result e85or conditions can of the inlet
process of change Of compr draulic or electric control
to operate an automatic hy
Card 2/4

The use of rototing ...
blade angle of the diffuser.
5 Soviet-bloc references.
S/096/62/000/003/003/008
3194/E455
There are 8 figures and
ASSOCIATION: Tsentrallnyy kotloturbinnyy :Lnstitut-
(Central Boiler and Turbine Institute)
3
J,
Card 3/4

i,mcHITSs S.P.9 kand.tekhn.nauk rifugal compressing macbines.
fusers in cent (141RA 1~: 2)
Use of revolving dif 162,
Teploenergetika 9 no-3:25-29 14r
institut.
1. TSentral,nyy kotlOturbinnyy (compressors)

LlVSHITSP S*P- kand tekhn-nauk
"~" "-10
lation between the dimensions of
Re .
the centrifugal compressor stage
F 762. (compressors)
diffuser in
, wheel and
a working enie 8 no.2:4-8
Energomashin05tro OuRA 15:2)
-

U277
s/o96/63/000/bol/oWoo6
0 El94/El55
AUTHOR: Livshits, S.P., Candidate of Technical Sciences
TITLE: Calcuiat-i-on--o-r-We characteristics of a multi-stage
centrifugal compressor
PERIODICAL: Teploenergetika, no.1', 1963, 21-26
TEXT: At present, compressor characteristics can be.
calculated only under the design conditions, but knowledge of
performance under other conditions is often required at an early
stage of design. Such calculations may be based on test results
obtained with indivi Pal stages or models thereof. The two
peincipal problems here are to select the'best system of
coprdinates foe cons ~ruction of the characteristics of the model
stages and to ensure the bead agreement between the calculated and VK
experimental characteristics of the multi-stage compressor, with
determination of correction factors to allow for the mutual
influence of stages on one another. It in then recommended to
plot head and efficiency as functiodi of velocity ratio defined
as the ratio of the radial component of the.absolute discharge
velocity to the mean' peripheral speed.. Factors allowing for
Card 1/3

s/o96/63/000/001/003/oo6
Calculation of the characteristics ... E194/&155
between stages, must be determined experimentally.
Three separate stages were.tested on a rig and the results were
used to calculate the characteristics of a three-stage compressor
built up from these stages and also tested. Details are given of
the individual stage designs and test results and of the
calculation procedure. Calculations on the multi-stage compressor
Should use as argument the,inlet flow to the first stage, and
calcula'tions are made stage by stage for each point on the
characteristics. The procedure for making the calculations for
each stage in turn is explained and after determining discharge
conditions from the last stage calculations are made of the over-
all compression ratio and the adiabatic head of the compressor#
The calculations can be simplified somewhat 'if the compressor is
intended to operate on the same medium as that in which the model
stages were tested. Calculated and experimental characteristics
of the three-stage compressor were plotted and showed.good
agreement. For the particular type of stages tested, with blades
curving backwards (P2_= 20'- 50*) the op'erating characteristics
of the stages considered an. a group were practically the same-as
Card 2/3

S/096/63/000/001/003/006
Calculation of the characteristics ... E194/E155
their characteristics considered separately, at any rate under
regions of stable operation. However, in the three-stage
compressor# surging occurred at somewhat higher flow rates than
in the individual stages. It is concluded ihat accurate results
can be obtained by calculating the characteristics of multi-stage
compressors from dimensionless static characteristics of the
individual stages constructed in terms of head and efficiency an
functions'of velocity ratio.
There are 6 figures and 1 table.
ASSOCIATIONs Tsentralinyy kotloturbinnyy institut
(Central Boiler and Turbine Institute)
3/3

p kand. teuht. naull
GOFLIN, A.p., kand. tekhn. nauk; ~,tnkel,
by K.I. Strlgkhofich, f
n,i*,,ewed by flinp
g achinery'F,,jjjs.
ncompressin and V zav.; energ.6no-91119-
Kondriako'lv cheb. ()41RA 16:12)
IZV. VYSO U
S.p. Livahits-
121 s 163. titut ime.ni polzunovao
rbinnyy ins
TSentrallnyy kOtlOtu

L 22158-65 AZDC'(9)/AMY(f-)r4
ASD(p)-3/AFTCA/AFr-.rR/A,---iC(p)
ACCESSION M AP5002203 S/0096/65/000/001/0054/0058
AUMORI: Livsh-its..,-S.P-. (Candidate of technical sciences)
TITLE: Problem of designing reverse direction apparatus in a centrifugal compressor
/ Z' -
SOURCE: Teploenergetikai no. it 1965t 54-58
TOPIC TAGS: centr1rugal compressor, diffuser design, flow uniformity, flow
structure, Bernoulli equation, centrifugal p,.=p
ABSTRACT: To match the flow direction with the iraet region of a reverse direction
apparatus, the flow in the circular elbow (see FiG. 1. on the Enclosure) of a
centrifugal pump was studied theoretically and experimentally. In the meridion
plane of the elbow, the diaphrc4-,n and diffuser curves -were assumed concentric at 0.
Usin6 the momentum conservation equation for circ,.=Serential (c U) as well as
neridional (C ) velocity components, the expression a mr - constant 4s obtatned.
comuning thin with the mass conservation equation, the following expression is
obtained for taxi c c we + r sin 9) Q- )
M~ U 2rc..R. (R, In 't +At sin i"
From a set of ezperimental da+,a determined at TzK-11, it is found that the above
Card -1/3

L 22158-65
ACCESSION 1M.- AP5002203
formula agrees well with tl:e datas at the. midsection 0-0 (8 - 909). However, the
same data taken at the reverse apparatus inlet (section 5 in Fig- 1) show a
significant lose in the equilibrium structure of the flow. The curves agree in
general with the for=Lla. derived above at 9 - 1801 for relative di-rfuser width
b3/b2 ' 1 and '[A 5L - 42 (opti=um installment angle for the reveraing vanes).
Averaging Q 5 along the channel width and using the opti-nur o~ 5 curves from experi-
mental Alata, a new formula is arrived at for o( 5 given by
arctg 7 T T in better agreement with the experizeatal. reatats.
fj %I
2?cR, In Cu&
7T)
Orig. art. has: 21 formulas and T figures.
AS-SOCTATIOIT- Tsentrallny*y kot1,'.*Wrbinnr7 institut (Sqxk#al _Steam Tuxrbine-
_-Institute)
SUBMIT'I'ED: 00
SUB C03% PR, "M
Cord
NR REP SOV: 000
ENCL: 01
OTHER: 000

L 22158-65
ACCE-SSj()jj ZM.
A1,5002,203
4j
~4j

Fri

Fig.
ca, d 313
ENCLOSURES 01
C)

U-,,/00q6/65/000/005/oo4ajb654
ZWT(d) Ijp(a)
01-~44-65
A-P50 i774 (Candidate Of techn'cal Bc iences)
IL-jT*'q'q-I! _L116111-SL -S-P- -, -reasor wheels
-- --- ------ -"en ts for comp
Cin the Oj,,latIon coeff'
T11-
no. 1965, 46-54
So-,jRcE. Teploenergetika r e uation
bladet
T,D-eTr TAGSt jentr,fugal compressort for centrifugal
C
vs-
pheral we
Iry-,tial -Aracter are thO Per"
0 and
I where I U 2U Def ining
q j, 'he !a
of the wheel and
t I
th-
j, the t-ieal -'a"
'I.1co -----
for VL == .
+ ~ sin$,
7, (1 - r,jr.) t:-ob eLhnY7
-re j13 the Ejame aB used. ~rj- StrakhO (Tsen
'tation used he
n,
Card 112

laxssiON TIR, AP50li774 T, 194()')- Tile end coefficie-nt K is obtained az
e S g 0 rrlyy 831ashiny - GONT gin V. +1
0 cte
K tv. '
--kLrt. haB: 19 equationOt 8 figures, and 1 t4ble. teactor-Turbing
-F ktj.trblnVy
10, 1 T S EM tralrQrY
T
Laot tute)
E21 C-L 100,
71 K - 00
'31j, =1
rJoc 000
SOV
12

L 45972-66 S',r1T(qY
XC_CNf' AT6026h3h SOURCE CODE: uR/oooo/66/ooo/ooo/oo83/O09l
AUTHOR: Livshite, S. P.; 1~e
yinq9n 1~..
ORG: None
TITLE: Results from a study of centrifugal compressor stages
SOURCE: Leningrad. Nauchno-issledovatellskiy konstruktorakiy institut khimicheskc
r ntrobezhnyye kompreasornyye ~a~~iz~y trifugal compressorsT.
AAsb,J&nostroZ i a.
jj_y _
]Moscow, Izd-vo Mashinostroyeniye, 1966, 83-91
IN TAGS: centrifugal compressor, compressor stage, diffuser, Euler equation, com-
zsor rotor
ABSTRACT: The authors present some of the results from the studies carried out at
the Central Scientific Research Design and Planning Boiler and Turbine Institute im.
_&n_(i pre'ssor "stages., The'-'
I olzunffovanTW_oEF,_-r-6fj~En-f i&Z_fo_n_s
authors cons er the work done on the circulation factor, the optimum interrelation-
ships of the dimensions in the transient region between the wheel and the diffuser and
the use of rotatable diffusers in control systems. Expressidins are given for calcu- 1,
lating the circulation factor. The equation of Euler is used for calculating pressure,,
and other expressions are given for cu and the correction factor V. In the case of 4
several formulas are given which were proposed by various authors. The autbors pro-~~
Card

L 45972-66
1--ACC NRI---AT6026h34
pose their own formula for calculating the correction factor ti. Three methods are
described for controlling centrifugal compressors: throttling the flow at the intaka,
'I
twisting the flow at the wheel intake; varying rotor rpm. Of all of these methods, , .
Ee use of a rotatable diffuser is most economical and efficient for controlling cen"'
Itrifugal compreBSor operation. The rotatable diffuser uses rotatable intake elements--.4,
which automatically tidjdat tc~Ahe direc"VIM bf the wig.- art. "-.!L-
Ias; 5 figures, 9 formulas.
CODE: 13/ SUBM DATE: 08Jan66
Card

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.1. loaded into the kettk. then ppolusite was added in small I.wtimii. 71M heatinat -
was effected by a %mail burner. The tractim Imoiluct was steamed tit tiC thr milt
id figurne, Hill and HiOlf. the laref mitit. tigurnt and fill[ was wild, Wash"I with
a Ni4C(% %.1n fi-c the rcluo,lai -( 11#011 and ttvptcd with Williffitir to wt., Ilk aldchydir.
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J. (;fq~ Chem. 13, ir-'10.,lis(191.1.1. AltAlki.m..
ill :PI %V. fienirlIC WA`4 treatc.1 slimly "till I st. NAtill
its 24-1. WAI.-I at 15 20% All-I 1 -KN K. C.,;6 brifil-fl.
a AliCt 609 1 Ill - Ill.-$, WA. fill 61 ell 1-11 tl.- , yiq Will k"
-40. 6, Vol; .4w 4 till, all W wait$ 44, .4
44 ZwOAv), -ht. tit give K13"; ~l th.
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Ill Jul"". Will till.) she /a S411, m. L!, SOO
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Ul'Atcll -till 11.21 g. S chl,witle lit A cc. MAI Awt fill. -I
f-w I lit. tit yield almmt Im-, :::
1,11a,uNP, in. Tot rahwir,timiquimilm, M-5 g1 CO 0
lit 15 v, licturtir isa% irratrtl loith 0.0 K. N*Riill ill 11:1 4100
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in 6 cc. HI to with stisTins; reammal
Wes* yielaw OJ6 C. J- won k*sj=;:
comp. 87*. 3-Pipecolime (0.5 s.) In 20 cc. Hr.0 was
miffM with OM X. N&OR La 0.46 cc. 160. followed by
0.44 C. C$. In her. HIP with ctmAinti; after mitring I hr.,
r4stwo. iN mwo$ anti tj P140 save I 'g. X4 J
lolmsdAMMOOnsdis, 11M.Aml. Ifffan
fit tall 11(nin IN No aall awl In 44.11010): oil,
moin twnse"o and mtm. 'rht its smit I % ) in m re,
HtO stinet! 34 lurs, wilit 11.37 a, rVto In re. 14.0, pwe
.03.3% J-Pipwolixtdiwsw hemsolAdo, In. 107-P Oloot
CSP-Et*O). 4-Pipecoline (OAS g.) in 2 cc. Ftto ad-W to
0.17 g. Css In I cc. culd Ht'O gave 902.0r; 4ppatahor 4.
cu. 155-6' (from tOH); the
Na sak nuwle analogously to that of 2-pip"ine. tn. 2OD-
V Wain FtOll-EtO); Zo sail, to. 210~19.5* (from
bensent). Cd ask, mIntwitbous, high-umIlling solid, mJmmt
insol. In llw usual crii. molwow The No oall (0.5 g.) in
t6 cc. utfo trosted With cootins with 0.2 F. SVCh In a Cr.
I hr,, d Oomd
I .
a. UvAlts and 14. A. nakil (Inst. Vine
Chlm.-Teih., Mawow). J. Gen. CA*m. (U.S.S.R.) 17,
Russian); cf. C.A. 40, M721-2.
Mpecallne (0.6 11.) In 20 te. BW Uented with rouli
and dkyft with 0.26 g. N&GH In 0.4 cc. H#0, lol=
by 0.44 X. CS. In 6 cc. IftsO,
lkwadowsk, M. It?-19*; Utya*rldgr~Lyns&
In. 216". Zo saft. m. 193-4% sal. In beumno. The No
ash (0.4 s.) In 30 cc. RtvO was trewed with 0.16 a. SXh
of
am
miress(Ms, as. 1044,11" (from CSs. 67.7q); it an
(30-W%) of Sj" is used. the product is doushlike.
7-1~~L~CKAL LIMIT-
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LIrSHTTS, S. S.
USSR/Chemistry - Quinoline Derivati*es Jul 51
it
Research in the Field of Organic Polysulfide
Compounds. III," S. S. Livshits, N. A. Preobra-
zhenBkiy, Moscow Inst Fine Chem Tectinol imeni
M. V. Lomonosov
"Zhur Obshch 1(him!' Vol XXI, No 7, Pp 1303-1308
Worked out syntheses of various salts (including
Na, Zn,) and thiuramsulf idea of Y-etbyl- and
r-isopropylpiperidyl-dithiocarbamic acids,
7-lethyl- and jr-isopropylpiperidine, trans- and
cis-decahydroquinolyl-dithiocarbamic acids, and
trans- and cis-decahydroquinolines.
191T29

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LIVSHITS. S.Y.
Manufacturing and measuring prealsioa load screws used on lathes.
StanA insir. 27 no.l.o:IC-14 0 156. (MLU 9:12)
(Screw cutting) (Lathes)

LIVSHITS p S.V. --,
Mechanization of assembling OpOrationse 6 1tajj instro 32
no.9:16-20 S 161. (PMA 124:8) tions)
(1409cow-Agoembly-line methode-Teehnolog04.imnava

ACC NR, AP6035726 ~A) SOURCE CODE: UR/O413/66/ooo/o1q/oob6/oo86
iINVENTOR: Kasimov, R. G. ; Kirichenko, 1. D.; Livshits, S. Ya.; Yozheritskiy, A. M.;
Fomichev, A. V. ; Chirteov, V. 1. ; Yudin, S.
ORO: none
TITLE: b1ethod of extracting mercury from tailings. Class 40, No. 186706
SOURCE: Izobret~niya, promyshlennyye obraztsy, tovarnyye znaki, no. 19, 1966, 86
TOPIC TAGS: mercury, mining enLdneering, metal extracting, & C. I-M A AA-4.1
AB STRACT: To raise the yield and sanitary work conditions for mercury extraction
by nitric acid and electrolysis, the electrolysis is carried out in a solution con-
taining 230-260 gram/liter of mercury and 20-40 gram/liter of nitric acid and using
a nonsoluble anodq and a mercuric cathode; the anode and cathode current densities
are 300-450 and 45o-6oo amp/m2, respectively. (WA-961
SUB CODE: 08,11,16/SUBM DM: 30Dec64/
Card 1/1 tmc!_66q_7q1.3:54i,ns,2i

ACC NR, AP6035726 SOURCE CODE: uR/o4l3/66/ooo/o1q/oo86/0o86
INMITOR: Kasi.mov, R. G.; Kie,&,enko, 1. D.; Livshits, S. Ya.; Yezheritzkiy, .4. 1M.;
Fomichev. A. V. ; Chirtsov, V 1. ; ~Mn,
ORG: none
TITLE: Y--thod of extracting mercury from tailings. Class 40, No. 186706
SOURCE: Izobreteniya, pronVshlennyye aztsy, tovarnyye znaki, no. 19, 1966, 86
TOPIC TAW: mercury, mining engineering, metal extracting dt'4~"44
ABSTRACT: To raise the yield anc~,sanitary work conditions for mercury extraction
by nitric acid and electrolysis Athe electrolysis is carried out in a solution con-
taining 230--20"0 gr_a-m7_1iter of nercury and 20-40 gram/liter of nitric acid and using
a nonsoluble anodq and a mercuric cathode; the anode and cathode current densities
are 300-450 exid 450-6oo amp/m2, respectively. (WA-961
SUB CODE : 08,11, &/SUBM DATE; 30Dec64/
upce 669.72ij&54i.~i5_2i

LIVSHIT , Sh,".' inzhaner, redaktor; POKIN. I.V., inzhener, redaktor
""o-72-da-fe-Pstva; TIKHANOV, A.Ta., takhnichaskiy redaktor
LPlans for the modernization of knee and column milling machines,
sories DZYS models 680M, 61OG and series GZYS moldels 680M. 6100.
68ou, 6loB, 68oD, 68o, 610m. 610Y, 610, 610D] Tipovoi proakt
modernizataii konsollno-frezernvkh stankov vypusica DZFS modelet
680K, 610G i vypuska GZIFS modelai 680M. 610G, 680U. 610B. 680D,
680. 610N. 61OV, 610. 610D. Moskva. Gos. nauchno-takha. izd-vo
mushinostroit. lit-ry 1957. Ill P. (MIRA 10:6)
1. Dwitrovskiy xavod frezernykh stankov. 2. Otdel modernizatsil
I remonta stankov Nksperimentallnogo nauchno-isisladovatellskogo
instituta astalloreshushchikh stankoy (for Livehits)
(Milling machines)

. a,,,,.inzh., red.; YOKIN, I.V., red.izdatelletva; MODEL
_~~~JJOL 1, B.I.,
tekhn.red.
[Standard plan for the modernizAtion of model 255 and 2A56 radial
drilling machines] Tipovoi proekt modernizataii radiallno-averlillnvkh
stankov modelei 255 1 2A56. Moskva, Goo.nauchno-tokhn.izd-vo mashino-
stroit.lit-ry, 1957. 142 p. (MIRA 10:12)
1. Odeaskly zaTod radial0no-sverlillnykh stankov. 2. Otdel moderni-
2at9ii i remonta stankov,., SkaperimentallnV nauchno-issladovatellskbgo
inatitift notalloreshushchikh stankov (for Livshits).
(Drilling and boring machinery)

LIVSHITB Sh To., inzh., red.; IONOV, P.M., insh., red.izd-va;
iih- , A.Ta., tekhn.red.
[Model-plans for the moderni%ation of knee-type milling machines
6B82, 6MN, 682, 682G. 6B12, 6121 Tipovoi proekt modernizataii
konsolino-frozerhykh stankoy modelei 6B82, 6B82G. 682, 682G,
6B12, 612. Moskva, Gos.nauchno-tekhn.izd-vo mashinostroit.lit-ry,
1957. 287 P. (MIRA 11:1)
1. Ikeperimentallnyy nauchno-iseledovatellskiy institut
metalloreshushchikh stankov (INIMS) (for Livehits). 2. Gorlkovskii
zavod frezernykh stankov.
(Milling machines)

LIVSHITS9 Sh.la., iuzh., red.; DANILOT, L.R., red. Izd-va; IILIKIND, TO.,
tekhn. red.
(Standard plan for the modernizati on of model 532 and 5D32 gear-
cutting machiueol Tripovoi proakt modernizataii zubofrezeruykh
stankaw modeloi 532 1 9FJ2. Nookwa, Goo. nauchno-tekhn. izd-vo
mashinoistroit. Ut-ry, 1958. 291 p. (KIU 11:9)
l9YsgorIyevsL-jy%avod OKomoomolets.11 2, Otdml modernizataii i
remonta stankor skeperimentallnogo nauchno-looledovateliskogo
instituta, metallorezhushchikh stankov (for Zivabits).
(Gear-cutting machines)

LIVSHITS, Sh.Ta., inzh., red.; GOLUB07, B.M., red. izd-va; TIKMO7, A.Ta,,
iea.
[Stands d plan for the modernization of model 1720(45) and 1730(44).
semiautomatic multiple-spindle lathes] Tipovoi proakt moderni-
zateii mnogoreztsovykh tokarnykh poluartomatov modelei 1720(45) 1
1730(44). Moskva, Goo. nauchno-takhA. izd-vo mashinostroit. lit-ry,
1958. 369 P. (MIRA.11:9)
1. IrrasW Proletariy, Moscow. 2. Obdel modernizateii 1 remonta
stankov eksperimeutallnogo na=hno-iseledovatellakogo instituta
metallorezhushohikh otankov (for livehits).
, % (Isthe a)

VASILIYAV, Vladimir Sargeye'vich; kMO, Fetr Stanislavovich;
BOGUSLAVSKIY, B.L.. prof.,'retsenzent~j4US=S, M4ra., '
inzh., red.; IVANOVA, red.izd-va; SLIKIND, V.D.,
tekhn.red.
EXachines and instrumento for dynamic balancing) Stanki i
pribory dlia ainamicheskoi balansirovki. Mosk"va, Goo,
nauchno-tekhn.izd-vo mashinostroit.lit~-v. 1959. 166 P.
(MIRA 12:8)
(Balancing of machinery)

FOKIN, Bergey Fedorovich; LITSIUTS, Sh.Ta., lnzh., red.; SOKOLOTA, T.F.,
tekhn.red.
(Adjustment of the 1112-1136 and IA112-lAI36-type automatic
lathed Naladka odnoshpindellnykh tokornykh avionatov mod.
1112-1136 1 1AI12-lAl36. lzd.2., perer. Moskva, Gos.nauchno-
tekha.izd-vo mashinostroit.lit-ry, 1959. 280 P. (MIRA 13;2)
(Lathes)

SYSOYEVI Vl"diml-. lv."ncvlchi LIVSHITS', Sh.Ya., nauchnyy red.;
BOBROVA, T.L., red.-PERM"'T' M.N., tekhn. red.
I I
(Handbook for a young drilling machine operator]Spravochnik
molodop everlovshchika. ~Soskvq, Proftekhizdat, 1962. 270 p.
(miRA 1612)
(Drilling and boring)

~',TLAEED, G.I.; Tbl]F-TKCJV, V.D.; D..;.; ZOTOV, G.I., inzll.~
retsenzent; LIVSIIITSj Sh.Ya.) inzho) red.
[~%cliino-tool units] Agregatmic stanlki. ~Ioskvaj Izd-vo
tl WIRA 17:6)
Mashinostruenlo," 1964. 422 p.

rA cy
~iw tion c
r-j gjt~ r
47
prc;rl. s

(A) L 12140-66 Vr(m) RM
ACC NR: AP6000455 SOURCE CODE: UR/0064/65/000/009/0022/0023
AUTHOR: Sokolov, N. M.; Nakha etyan, L.A.; Fomichev. A. V.; Livshits S Ya-;
I .-P
Chirtsov, V. I.; Kasimov, R. G.; Lukina, M. Yu.; Zhavor~nkov,
ORG: None
TITLE: Experimental industrial preparation of pharmacopoeial cyclopropane
SOURCE: nimicheskaya promyshlennost', no. 9, 1965, 22-23
TOPIC TAGS: cyclopropane, organic synthetic process, cyclic group, pharmaceutical,'
propane A.0
ABSTRACT: Pharmacopoeial cyclopropan was synthesized via the following steps:
CH2=-CH-CH2Cl + HBr -0 BrCH2-CH2--CH2Cl (1)
BrCH2 - CH2-CH2Cl + Zn -+ CH2-CH2 + ZnClBr (2)
CH2
In the third step, propylene and other impurities are removed by distillation In
packed tower. The operation of the experimental industrial assembly used in this
process is descr%ed and its diagram Is given. The reactor for the synthesis of
cyclopropane is also illustrated. The propylene content of cyclopropans was
Card 1/2 UDC% 661.715.4:547.512

L 12140-66
;ACC NR: AP6000455
C
determined by gas-liquid chromatography with a thermal conductivity detector, and
the cyclopropane obtained was found to meet the specified requirements. The study
permitted the refinement of certain parameters of the process by which cyclo-
propane is produced at the various stages, and improved the flowsheet
iof the synthesis considerably. Orig. art. has: 3 figures.
iSUB CODE: 07 / SUBH DATE: 00 / ORIQ REFt 005

VIOR0131YEV7 A.I.; LIVSHITS, Sh.Ya.
Development of the prcduction of machine-tcol units and
automatic lines. Standartizatsiia 29 no.6:9-12 Je 165.
(MIRA 18:12)
1. Eksperimentallnyy nauchno-issledovatellskiy institut metallore-
zhushchikh stankov.

-- LIVSHITS, S.Ye.
Roundoff errors in the solution of economic problems using
electronic digital computers. Trudy LIM no.55:72-78 165.
(MRA 18:11)

-JtIV44~%. S.Ye., red.
-
(Container recovery of metal; story about progressive
practices) Konteinernyi s"em metalla; raoskaz o peredovom
opyte, Magadans Magadanakoe knizhnoe izd-vot 1963. 14 P.
(MIRA 170)

LIVSHITS, S.Ye.; BREKHOV, A.M.; SMIR'NOVA, T.I.
Problems of coding initial information in network planning
and administration, Trudy LIEI noo55t89-95 165.
(KRA 18:11)

III I I WIt i4 11 1. 1' 1. ,1 a J4 IS "s ", )j " It IVIII out, J'I 0 it po
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; DV
.
,
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palsovoya 1"0. No, M. An 1widthy
00 old) pdady -00
Ms. awad)ic WWI, jbq blood I*Yrt siws on tfw;trmi,f&y soid
$."I. Sarki frvri I-Alwitim, at the

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hab to ralor thr blood bo
.

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the diftsm WMIM
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-LIVSHITS, T~. ..-[Livshyta, TS.A.J. kand.med.nauk: ZEWSOVA, N.O. ; FWZHOLI,
~ -: -N.N.; SHVABOVSKIT, V.A. [Shvabovalkyi, V.A.]
Intraoseeous drip infusion of saline solutions for infants. Pad.,
akush. i gin. 19 no-3:28-29 157. (MIRA 13:1)
1. Llvovskiy nauchno-iseledovatellskly institut okhrany mterinstva
i detstya (direktor - I.D. Tashchuk) na baze Oblastuoy klinicheskoy
bollnitey (glavnyy vrach - I.A. Iraragodin).
(INJF,CTIONS, SALINN)

N.M.; VIM'HSKIY, L.I.; GORBUITOV, H.G.; GUBSKIT, V.N.; GURVICH,
M.D.; LA7TSI&V, Tu.M.; UVOIRIN, L.I.; LIVSHITS, T.G.j LOGI-
NOVA, M.K.; RMIT9, D.A.; LTAMMS, G.ff.-;' MIROSHNICHWO, G.K.;
MOGILIVSKIT, B.Ya.; NEWOVSKIT, M.I.; CRLEA11SKIT, Ya.P.; SA-
VITSKIT, A.H.; SIMMA, S.F.; SURKOV, G.Z.; SIWGULI, B.P.; SHUBIN,
V.P.; DONSKOY, Te.Te., red.izd-va; KALINITSKIT, R.Ta., red.izd-va;
ZAMAKHOVSKIT, L.S.. takhn.red.
[Mechanization and automation in the machinery industry] Mekhani-
zateiia i avtomatizataiis v stankostroenii. 1harIkov, KharIkovskoe
obl.izd-vo, 1958. 119 p. (MIRA 13:2)
1. Kharkov. Inatitut "Giprostanok.* 2. Direktor instituta "Gipro-
stanok* (for Orleanskiy).
(Machinery industry--Technological innovations)
(Automation)

~-LMHITSI-T.P., prepodavatel, detskikh bolezney
Conducting a practical conference for the student6 at Hloscow IiBdica2
School No.3 Felld. i akmah. 26 no.9:60-62 3 161. (IMA 14:10)
iMOSCOW-I,IEDICAL COLLEGES) (PNEMNIA)

E,s T t d I
F : AT ~'~ 10601
Ir
'i-F, /314 34 IfA 3 /000/00d7/0,"0
A 1-7-111 (_ FLivs~iits, V. A.
I -, _'E ;Simple mathematical models of tlissue
U
SOURCZ: AN SSSR. Institut evolyutsian~(DX__Lizjq1oZii._ runktsii organizma v
_lLinvi"dA 2:,wriennoy gazovay sredy, v. 1, 1964, 87-90
f
TOPIC TAGS: simulation test, tissue, mathematical r-o-Jel
ABSTRACT: The Haldane mathematical model.of tissue defined by equatiorn
ab 1.(P P)
-r a
~which states that the rate of tissue saturation with inert gas is dira-ctiy propor-
tional to the differ-ence between the partial pressure of gas in the lungs and its
te--icn in tissue has been used to develop a anve-thod for comput-ing =1! inur"j-
ascociated with the treatment of -aissro-i disease. N,-i
4ith trapezoidal puises w,j~-,
~Ln,l observe on an oscilloscope the saturatior, a7j deso3-'I:--it I
tissues. Simulation can also be achieved by using a simp1e nyarraulic mode.L
[Cards J/2

4,31 C64 - ~L, 5
ACCESSION HR: AT5010603
CC-nS-;!jt'-n1- of, two vessels filled with a viscous fluid and connected at the bottom
a capillary tube. Ozi--t vessel simulates the ILmgs, the other. aimulates the
le. the vissous fluid simulates the inert gas. The hyririvilic model is
'han the electric model but is lesa convPnient to LL341 -md' r-quir--s more.
~.,rLg. art. has: 3 equations, I figure.
ASSOCIATION: none
SUBRI=D: 00 ENCL: 00 SUB CODE. LS
NO REF SOV: 009 OTHER! 002
kV
W2

RAMN, Yualb, inzh,; lnzh.
Installation of the boiler of a 1,000 Md. block in the Ravenswood
electric power plant In the U.S.A. Teploenergetika, 10 no.9:
85-87 S 163. (MIRA 16 t 10)
(New York-Electric power plants)
P4, J.

I
AC.:~' /,;C,01
AWHOR: Livshits. V. B.
TITLE: The Effects of Bijilt-jJp Edg,~ or, ,he Quality of tht~ Surface Finish
of Aluminum Alloye
PERIODICAL: Stanki i Instrument, 1962vt No, 11, pp. 29-29
TEX1% ThA Laboratory of `,,itlting Prn,,~P-.'zs~3 cf' th~3 TOmskI7 P01itek-~=ichesily
inst1tut (Tomsk Polytech-nio Ins-VII.-ate) c-arried out inves-.1gations of the
of a built-up to91 dge c- th- ~iurfa,- fir.~sh of a a-zobc-r of a .zmIn-xii alloyE,
AA A6 A" ~~AA8 (AVqar~d- AA,'OB
viz. 4 A 4T( ih-11) t' Th5 tests werl~
carried out with BK8 "'IKU) tx-g3ten-car~,Ide-lpped ':~:)ls, with a rak- ar4lti
250, an end couttizng edge &%gl-? 20 a nos,~ radll-s 9. 11 - 0.2 mT,
t-001 No. 1) and r = 1,5 mm (tool No~'2),
r
without cooling in a speed range of 2 - '(~O eni f-J5 fr.:.7i 0.07 to 0,3
revolution, The surfase finish was rated ti- tz,iwht nf on -tv'.
machined surface, which was w.~-,isunid wltn ttc mcd-!
microscope with a magnifi.:aticn cf 81 a:-,d -'45-51- --n tne cf~ 1-he -Zuttlas
process the built-up edgg forratlc7-~ wa~~- a:-J the hvmight ,,f growth h9was
Card 1/4

The Effects of Built-Up Edge on.
Allovs
measured with an -,h, d-! AL a
of the inve stigat' or s I tv wa s fvun, J f,"ti&4. 41'h,~ 17 C, f t- 11 tn
A. L ge or itz
absence depended on a 3,Ertal- ~,,..ittfrg th,~, 2i-vr:,:, rilloy (--La
Table 2)
Temperati.,re
A Al Al. i0 V
CorrespondIng "~o the "o-matior-
of bIA41t-Up edge and 41-f-
'75
greatest height. of Ineq,-- a c
(t,)
At wh!~,h no tuilt-up edg;~ ii
.2 9-~
290 320
-C" 270
2
260 290
3
Cand 214

S/121/6o/ooo/on/010/013
A004/AOOI
The Effects of Built-Up Edge on the Quality of the Surface Finish of Aluminum
Alloys
Figure 1: Figure 2:
PA
Mor MA C#,ieg Ax4f
60 - 41
A,
C ~,a�M
Rre
Figure I ahows the range of cutting
speeds at which growth did not origi- :-407
nate. The higher the heat conduction -0.3
-07
coefficiency A of the alloy, the higher 0 0 to 160 140 NO to
the cutting speeds at which no built-up remnepamyCir Pejellms
card 3/4
FU~
f
P, R 'M
vu

S/121/6o/ooo/oil/010/013
A004/AOO1
The Effects of Built-Up Edge on the Quality of the Surface Finish of Aluminum
Alloys
edge forms, other conditions being equal. Figure 2 shows that the activity of
built-up edge formation at given temperature conditions can be reduced by decrea.--
Ing the feed and by increasing the rake angle of the tool. To determine the
effects of growth on the surface microgeometry, the height of the residual crests
Hmax was compared with the theoretical microroughness Htheor for the tool of the
given geometry. Based on the investigation results obtained, the author draws the
following conclusions: When selecting the feed and magnitude of tool radius for
finish operations, the condition s 2r sin should be observed, which ensures
a microroughness profile approximating the theoretical one in a wide speed range,
except for the zone of the most active built-up edge formation. In that way the
necessary class of surface finish can be attained. When cutting is carried out in
the zone of active built-up edge formation (in the case of s _:~.2r !.0 ) a reduced
feed will result in a better finish of the machined surface, Opt4ulm results are
obtained at cutting conditions which exclude the built-up edge formation, I. e.
those conditions given in Figure 1. The lower the thermal conductivity of the
aluminum alloy, the narrower Is the zone of the built-up edge formation and the
lower are the speids at which no built-up edge forms, There are 5 figures, 2
tables and 3 refeiences.
Card 4/4

LIVSHITS), V.B.
Problems in the economic substantiaticn of 3tandiurds. Standartizatsi,la
29 no.1;39--42 Ja 165. 11~14j

KOKORFV, V.A.; LIVSHITS, V.B.
Types and dimensional series of reeling and warping machinps.
Standartizatsiia 26 no.1:35-39 Ja '62. (YJRA 15:1)
(Textile machinery-Standards)

XURENKOV, N.V., kand.skonom.naukj KOKOREV, V.A., inzh.;.LIVSHIT,Sj inzh.
'L
Standard %rpe8 of'k aving equipment. Mokh.i avtom.proizv. 16
no.1209-41~ D 167 (KRA 16 t 1)
(Textile machinery)

LIVSHITS, V.B., starshiy prepodavatell
Some characteristics of the process of aluminum alloy cutting, Izv.
vym.uchob.zav.;mashinostr.no.1&140-IU 163. WRA 160)
1. Xr*onoyarpkiy politekhnichaskiy inatitut,
(metal 90ting) (Aluminum alloys)

A
Soo
fe c
Soo
00
of
be
a mWW ior wwwok "udmk.
md L T. ZmumvA
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age
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a v -0 &$1;
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!Was
%saw *"$#IV
111161111 m a" ill
1 ow a 0 11 1 ff Ill 9 a4 3 0d"I
0 0 0 0 0 0 9 0 4 0 0 0 0
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A-t-1-A-L-E L -On 6.0
A - --- ---- - -JiT
a a a 46
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-17
A Oct
"MAWIOX Of CATALysT'FM AMMOb.U SYNTMWIS
00 C nOM UM XAMMITZ. V. & JeWolkin ard V. D.
!L(j, Chom" inds ,us#*# 1930P 13* 390-401).-
1A -as fingly.1)qw4gred &"tit*# coaftining 2.5%
Of 8102: in subjected to magnatic conan.j, thereby reducing
the SIN content to 1.1%j the produat Is dried# fuso,;
Oot with 1.5% of JL% mW 2% of A1203p tbo mass powdered,,
Iii WW'seperation fron Si% in a matuttle field repestode
!' ~
The dried product Is mind with sufficient Yo to oorre-
spond with the cOxPOsItIOn and again fused. sh*
W mass, containing 0.26-O.U% of 810 # to broken up
and used far synthesis. T.
a U
Ord
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in tub* Ps , Old Pramum.
and ifl~ivsrnwoy tamp. off"t w due to am
awm of t1w ywhods d deamp. 01 the A mw coo
coo
of ihw pieducts hao tho gmnujw; for ihis
rooWes the oiisa oi bwp Sma=Wwrimenowded when
the ps is growly owt&Mh*W With C& R. T.
A I a. I L JI 11111101"NOMM" LMINA"'" ""MC"tm

,Ljif~5-#H-Z~j jK-,P
SIDOROV. I.P.; LITSHITS, Y.D.
rinstles of ammonia synthesis
21 no.10:1177-1181 0 147.
1. Gosradaretyenrq7 institut
in laotharmal conditions. Zhur.fiz.k:his.
1, (KLRA 7:1)
,,, ~ "", I ;,~- ~~
azotn.oy, promyehlennosti, Moskva.
(Ammonia)

U /Chemistry - Annonia Synthesis Apr 52
"Kinetics of the Synthesis of Ammonia Under
Iscithermic Conditions," V. D. Livshits, 1. P,
Sidorov, Moscow
"Zhur Piz Xhim" Vol )=, No 4, PP 538-541
Imestigated kinetics of ammonia synthesis at
pressures of 10, 100, 200, 300, 4oo, 5oo atm, and
Vol velocities of 30,000, 60,000, 90,000, IM,000
br -1 at 5000 under strictly isothermic conditions.
Demonstrated that the velocity consts k. ceLled
bY means of M. I. TemId n and V. M. Pyzhev I a eq
(using the form vhicb is applicable to low
pressures) drop as the pressure is increased. The
dependence of k an pressure is in agreement with
X. I. Temkin's theoretical eqs of the kin ties of
ammonia synthesis at high pressures. Values of k
recalcd under consideration of the pressure effect
show a satisfactory constan y at changing pressures.
217M
E-

L 17438-63- EPR/EPF(_c)/EW?(q)/EWT(a)/BD8 AFFTC/ASD- Ps-4/Pr-4
B'd/RM/'%&/JD
~ACCESSION NHI '.AP3004299 S/0064/63/000/005/0024/002574~
AUTHORSt Moray-'
=1&&M ,._(Candidate of technical sciences
I* Po(candMar-9 or technical scienoes)z Beskova, A. P*
TITLE: Effect of methane~ nd its admixtures upon ammonlak
.synthesis 1-1
SOURCEt Xhimicheskaya promy*shlennoott, no. 5, 1963, 24-25
TOPIC TAGS: methane, ammonia, ammonia synthesis
ABSTRACT: Authors studied the effect of methane and some of its
admixtures which are contained in a nitrogen-hydrogen mixture
upon ammonia synthesis. Natural gas from the Saratov and Dashansk
beds was tested. The effect of methane in the gases from each of
theso fields was studied with one and the same catalyst in three
series of tests. The ammonia yield in a pure nitrogen-hydrogen
mixture of stoichiometric composition was determined in the first
series. The.same mixture with an admixture of methane was
-analyzed in the second series. The pure mixture of stoichiometric
rard 112

ACCESSION NRtAP3004299
composition was tested again In the third serles. The effect of
Pure methane was tested at a pressure or 300 ttm.,, temperatures of
450, 475 and 500c, space velocities of 15,000-90,000 hour-'
and concentrations of 5,16 and 30% by volume. Authors found that
eiren a maximum methane content (30~6 by V0113me) does not have a
negative effect upon the performance of the ammonia catalyst
(ammonia yield In first and third series of tests was Identical).
When methane is added to the nitrogen-hydrogen mixture, the
ammonia yield is noticeably reduced. The assumption that this is
caused by a reduction In the mixture's partial pressure on account
of methane rarefaotlon was not justified. Authors conclude that
presence of methane inhibits ammonia synthesis. -Orig. art. has:
3 tables.
ASSOCIATION: none
SUBMITTEDs 00. DATE ACQt 15Aug63 ENCM~ 00
SUB COM CH NO REF SM 002 OTHERs 00
2/12

LIVSHITS, V.D., kand. tekhn. nauk; SIDOROV, I.F.~ kand. tekhn. nauk;
'^~WA, A. P.
Effect of methane and its Impurities on the process of
ammonia synthesis. Khim. prom. no-5:344-345 My 163.
(MIRA 16:8)

RMENBERG, A.M.1 RHOVAKH, N.1.1 LIVSHITS, V.I.
,1-1.1-1--l-, "'.
Dynamometer for measuring cutting forces up to two tonao Stanei instr.
35 no.900-31 S 164* (MIRA :L7tlO)
k -

N AP6ol9933
ACC R SOURCE CODE: UR/0l22/66/ooo/oo06/0073/0074
AUTHOR: Kufarev, G. L. (Candidate of technical sciences) Livshits, Y. 1. (Engineers
ORG: None
TITLE: Workability of deformable bigh-manganese steel
SOURCE: Vestnik mashinostroyeniya, no. 6, 1966, 73-74
TOPIC TAGS: manganese steel, tool steel, cutting steel, honing, metal machining,
microscope, vibration, cast alloy 14
ABSTRACT: Data are given from a study on We marhininir properties of various grades
of tool steel used for planing 54Gl7Yu3 I&nd.45Pl7Yu eeel. These grades of steel
were machined on the 7M37 planer. Cutting edges were ifidchanically attached to the
cutters being tested. These cutters' ere ground on the K346SM2K abrasive disc and
honed on a cast iron disc. The "Mir" microscope was used for m7rs-urinrcuttprvearyi,
The foebwing grades of tool steel were tested as cutters: '18, R9K~, R9Kla R18F2
R14F4--'hard &kloys type TK (T5 10 K115, ?14K Id VK (VKX-703-vKP,~~.d o- Mer
IL ~a~o
141
est.,
hard alloys.,*Whe cutters t r 3 Ecs and c~tt le's. The tests shcru
d Val
that cutter shapes with negative angles are not stable. Negative angles cause cutting,
stresses and vibration. The most stable cutters were those made of A type rant Alloy.)
with the following chemical composition: 45-50% Co, 27-32% Cr. 14-19% W 2-4% C, 2-71;
Ccrd 1/2 uDc: 621.9.oil:669.15'74-194

ACC NR% AP6019933
q~-3%
ZAIP Mn and 2-5% Fe. Cutter stability as a function of cutting speed is given
in the form of a diagram for all tool materials used. Orig. art. has: I figure,
2 tables.
SUB CODE: 13, 1l/ SUBM DATE: none/ ORIG W: 002
Card 2/2

VORONOY Yu.yu. rof. (deceased]; RUDY101, O.D.; LIVSHITS,V.L.
.0 .9 p
Skin preservation by deepfreezing; preli,,dnary report.
Probl. gemat. i perel krovi 8 no-5:30-32 My'63. (MIRA 16:8)
1. Iz laboratorii konaervatsii organov I tkaney Kiyevskoeo
nauchno-iseledovatellskogo institutu perelivaniya krovi i
neotlozhnoy khirurgil (direktor - dotsont S.S-Lavrik).
(TISSUM-PRIBERVATION) (SKIN)

LIVSHITSP V*L-; inzh.; SIMAYOVP I.K., inzh.
h. 10 no-3:22-25 mr 165.
The SKB-2 loaders. Itroi. i dor. mac (141RA 18:5)

LIVSHITS., V.M,
Self-contained buoy stations in the United States. ',Ieteor.i gidrol.
no.8:51-53 n Ei.e,Ag.] 162o (.,.aRA 15.7)
1, TSentrallnyy institut prognozov.
(United States-Oceanographic research-Buoys)

LIVSHITSR,V.M.; YEFIMDV, V.M.; SUURKIVI, E.R.; DOYLOV, S.K.
- 9 a ZA4K~-
Remdta of a balance test of the remodeled gas generators of the
shale-chemical Kivioli Combine. Kh1m. i tekb. gor. slan. i prod.
ikb perer. no.llsl26-135 162. (MIRA 17:3)

HEIFETS, L.B.; LIVSHITS, V.M.
Utilization of sow methods of statistical evaluation of unit
morbidity index. Zhur.mikrobiol.,, epid, i immune 42 no.9s86-
91 S 165# (MIRA 18%12)
1. Moskovskiy institut vaktain i eyvorotok Imeni Mechnikova.
Sizbmitted September 8, 1964.

L
ACC NR;
AT6022346 SOURCE CODE: UR/0000/66/000/000/0057/0066
J~
:;AUTHOR: Livshits, V. M.
!ORG: None
iTIVjZ: A receiver for differentiating binary random signals
ISOURCE: Vsesoyuznaya nauchnaya sesBiya, posvyashchennaya Dnyu radio. 22d, 1966.
1
1Sektsiya teorii i tekhniki peredachi diskretnykh signalov. Doklady. Moscow, 1966,
57-66
TOPIC TAGS: binary code, signal reception, random noise signal/Aj--
iABSTRACT~ ~The author considers a radio receiver with an input voltage which is a ran-
1dom function of time and belongs to one of two sets having identical Gaussian distri-
lbution and different correlation functions. It is shown that a receiver for differen-i
itiating the set to which a signal x(t) belongs must calculate the expression
U X (S) X Y) h (s, 1) dsdi
Pard-

L 46
ACC NRt AT6022346
;where the weight function h(s,t) is given by the integral equation
rro (S. U) [~I (v, t) Nro (v,t)] h (u, v) dudv jr, (st) - r', (S"M
S N+I
0
jA block diagram is given for the optimum receiver capable of calculating the quantity
1V consisting of a filter with variable parameters We-,t), a multiplier and an integra.-
itor where the voltage at the output at time T is proportional to the quantity U.
IFormulas are derived for calculating the specific parameters of this type of receiver.
10rig. art. has: 4 figures, 22 formulas.
SUB CODE: OQ1-2 SUBM DATE: 09Apr66/ ORIG REF: 003/ OTH REF: 002
V
Card 2/2

(3)
AUTHORS: iiv_~~~Xatveyeva, N. K. SOV1105-59-6-9126
*TITLE: The Consideration of Resonance Phenomena in the Overhead Contact
System During the Performance of Rectifier Engines
PERIODICAL: Elektrichestvo, 1959, Ur 8, PP 41 - 45 (USSR)
ABSTRACT: This is an investigation of the distribution of the non-sinuso-
idal feed current of a rectifier engine in the overhead contact
system based upon the following articles. The theoretical and
experimental investigations presented in reference I resulled
in the determination of the amplitudes of the harmonics in the
primary current of the engine, not accounting for the capFs-~ity
of the contact wire. Other investigations (Refs 20) showed
that the distributed capacity of the contact wire mod1fies the
amplitudes of the primary current harmonics only to some extent,
but effects considerable changes in the harmonics spectrum of
the traction substation current. It was shown that in the sub-
station the amplitudes of the harmonics are much greater zhan
those of the primary engine current, which can be expluined by
the resonance phenomena occurring due to the distributed capac
ty of the contact wire. The method devised by M. P. Kostenko
Card 1/3 (Ref 4) may serve as a basis of theoretical investigation of

The Consideration of Resonance Phenomena in the SOV/105-59-0-9/2e
Oierhead Contact System During the Performance of
-Rectifier Engines
resonance phenomena. According to this theory, the rect5lfi-~r
installation is considered a hypothetical generator of " !..-heT
harmonics electromotive forces. By applying this princinl�~..,
Jotten and Lebrecht (Ref 5) have found the harmonies
of the substation for two cases: the engine is close tc ;i~fs'ib-
station or at the end of the line. In this article, the more
general case is investigated in which the engine is at any distaacz,
1 from the substation, that is 041-4'-l end* The equivalent
cuit shown by figure 2 is the starting point of a calculatioa
of the distribution of the n-th harmonic of the current over 'ohe
line. Formulas (9) are derived for the equivalent di3turbance
current, formula (10) for the amplification coefficient k of
ampi
the n-th harmonic, and formula (11) for the calculation of the
resonance frequency of an existing line. It is shown that the
results derived from f ormulas (10) and (11) dif f er considerably from
those obtained from formulas (12), 0A and (14) setup by Jstte:.-i
and Lebrecht. This is ascribed to mathematical inaccuracy ia
Card 2/3 the derivation of formulas (12) and (13) by Jotten and Lqb:echt.

Th'e Consideration of Resonance Phenomena in the SOV/105-59-8-9/28
Overhead Contact System During the Performance of Rectifier Engines
Finally, the general method is specialized to the cases of the
engine being either near the substation or at the far end of
the section which is fed from one end. The calculations showed
for the first case that the mean amplification factor can be
determined approximately from formula (16) for existing traction
systems, the mean error not exceeding 1-5%. There are 3 figures,
1 table, and 6 references, 7 of which are Soviet.
ASSOCIATION: Institut kompleksnykh transportnykh problem AN SSSR (Inatitlite
of Complex Transportation Problems of the AS USSR)
SUBMITTED: October 20, 1958
Card 3/3

LIViNIT6, V.1'.____
Princiul.o -'c-, --. ~i.; n,,-,in- 'ar!; - oil -.,,-rioi;.;
typet; Of C..L:. ~;,rud C-.or. z.o. '1-
11 8 1 ~0. (- L u*, 14: ! *1
IO,.~0rOtjv,-.;;)

-ALIV6HITS V "
Somi p~-olulcmj o--' th-3 1. vf LA-I~ .-,c' troll ard pow--r i t-lizaticL
o' a.c. Auctric locomo"~-.,13 o;,"-; ~ * -1 --' ~r:l
A. L:-nL: on -o=erc--al -'.-,. --:..
: - N
Slek. L,:.al (!or. no. 2:IC~-140 IiX. L" .)
(E!,;ctric locomoLivos)

'IVSHIT-S, V.N.,inzh. (Moskva)
'Lj
Consideration of the service life of equipment in cost
calculations of power engineering systems. :,'lektrichestvo
no.9:18-23 3 160. (MIRA 13:10)
(Bledtric power distribution-Uquipment and supplies)

LIVSHITS, V. N., Cand Tech Sci -- "Results of the study of
UA IL (n I :~
certain problems of/-,eleotrIcA& vz~ -ki%- -the single-phase
current of _~--malpme-AR frequency." Mos, 1961. (Min of Higher
and See SDec Ed RSFSR. M-os Order of Lenin Power Dig Inst)
(KL, 8-61, 245)
- 263 -

-LIVSHITS, V.N., inzh.; POZAMANTIR, E.I., inzh.
Economic comparison of variants in planning railroad lines.
Transp. stroi. 10 no. 12:50-51 D 160. (MIRA 13:12)
(Railroads--Estimates)

SI SHEN-LYAN; LIVS9ITS, V.N.
Effect of longitudinal compensation devices on the characteristics of
rectifying locomotives at normal operating conditions of the traction
power supply system. Elek.zhel.dor. no.31U9-158 161. (MM '14:7)
(Electric locomotives) (Electric railroads-Current supply)

LIVSHITSI V.N.
Rsoonan e effects in the contact network and methods for considering
them in evaluating the effe 'ct of electric traction systems using
single-phase current on wire comminication systems. Elek.zhel.dor.
. no.3:187-222 161. (MMA 14:7)
(Electric railxoado-Wires and wiring)
(Telecommini cation)

-LIVSHITS, V.N., kand.tekhn.nauk
Using electronic calculating machines for analyzing the effect
of the overhead system current on communication lines. Vest.
TSNII WS 20 no.5t54-58 162. OURA 15:8)
1. Institut kompleksynkh transportnykh problem Gosudarstvennogo
nauchno-dkonomichookogo soveta Soveta YAnistrov SSSR.
(Railroads-Communication systems) (Electronic digital computers)

PETROV, A.P., doktor tekhn. nauk, prof.; TULUPOV,.I...P., kand. tekhn.
nauk; KRYUKOV, N.D., kand. tekhn.nauk; GUNDOBIN, V.N., inzh.;
VASIL'YEV, G.S., kand. tekhn. nauk; GRISHIM, Y.S., kand.
tekhn. nauk; MOROZOVA, K.N., inzh.; ROZE, V.A., inzh.; 11WHIS,
G.L., inah.; BERNGARD, K.A., doktor tekhn. nauk, prof.;
BIKCHENTAY, M.A., inzh.; BTJYANOV, V.A., inih.; ILOVAYSKIY,
N.D.J. inzh.; MUKHAMEDOV. G.A., kand. tekhn.nauk; MIROSHNICHENKG,
A.P., insh.; ANDRIANOV, V.P., inzh.; BUTS, V.D., insh.; KAZMV,
A.A., inzh.; KIREYEV, O.P., inzh.; DYUFUR, S.L., kand. tekhru
nauk; USTINSKIY, A.A., kand. tekhn. nauk; MIKHAYIDV, S.M., Inzh.;
NESTEROV, Ye.P., kand. tekhn. nauk, retsenzent*.LIV3HIJJ_Y_~1.,
inzh., retsenzent; PREDE, V.Yu., inzh., red.; WFOYRTWOVA, 1.
tekhn. red.
[Control of transportation processes using electronic digital
computers] Upravlenie perevozoehnym protassaom 9 primeneniem
elektronnykh tsifrovykh vychislitellnykh mashin. Pod obshcbei
red. A.P.Petrova. Moskva, Transiheldorizdat, 1963. 207 p.
(MIRA l6s8)
1. Chlen-korrespondent AN SSSH (for Petrov).
(Railroads--Management) (Electronic digital computers)

GORINOVO A.V., prof.; KANTOR, I.E., dots.; KONDRATCHENKO, A.P., dots.;
REPREV, A.I., dots.; TURBIN, I.V., dots.; LIVSHITS, V.N.,
kand. tekhn. nauk; AKIYOV, V.I., kAnd. te i~uw
retsenzent; GURSKIY, P.A., prof., retsenzent; ZAYTSEVJ, P.F.'
kand. tekhn.nauk, retsenzent; LISHTVAN, L.L., inzh.,
retsenzent; PRUSAKOV, M.B., inzh., retsenzent; SHINKAREV,
F.S., inzh., retsenzent; SHULIPENKOV, V.M., inzh.,
retsenzent; MEDVEDEVA, M.A., t4khm. red.
(Design and planning of railroads] Proektirovenie zheleznykh
dorog. [By] A.V.Gorinov i dr. Moskva, Transzheldorizdat,
1963. 308 p. (MIRA 16:9)
1. Chlen-korrespondent AN SSSR (for Gorinov).
(Railroad engineering)

LIVSHITS, V.S., inzh.
-------
Determinatior of an effective number of electrical power recipien-s
in the calculation of electrical loads. Izv. vys. ucheb. zav.;
energ. 6 no-10:36-43 0 163. (MIRA 16:12)
1. Institut "Belpr6mproyekt*.

LIVSHITS, V.S., inzh.
Determination of peak current in designing electrical net-
works for shops. Prom. energ. 18 no.12:30-34 D 163.
(MIRA 17:1)