SCIENTIFIC ABSTRACT SHAVYRIN, V.N. - SHAYDEROV, V.A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001548720019-4
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 9, 2001
• Sequence Number: 19
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

2~6;~ 26016
S iy 6 1/000/008/005/011
On the problem of breaking tests ... AKO A101
-~-,rength of izlue-welded specimens exceeded almost by a factor of 2 that of welded
spa :!n~~ cf th,~ s-a~
-ne design and by 83% that of glue-welded standard cross-zhaped
pe~'-.,nens. The strength of the rew welded specimens was by 30% higher than that
of &tandard cro3-z.-s,'haped specimens and the strength of the new riveted specimens
wa.,,~ n-
y 10 - 12% be-Low tha-,. of riveted standard aross-shaped specimens. A partif-
.,ularly hIgh d�fference was observed during uniform a.-Lid non-unifor7n break of glued
spec'-mens. Exp6riments confirmed the conception on the high strength of glued
Jc-Ir-:;s under cwd-'-A4-cns of uniform breaks, exceeding even that of glue-welded joint4
a--6 on the ver-j low strength of these joints during non-uniform break. The ex-
c~7-.Pents lead t.-) the fali-owing conclusions, The breaking f,)r~ae of welded; glue-
ive::iei and rive-ad specimers depend on their ria-lditj and the syFtem of loading.
Ina -)f sorrf- -authors that the glue layer in a glue-welded JoLit does not
fts breaking stre.-ig--h is not correo-~. in structures whose aomponents
arc- sxp~-;-?--i t-) u-nif)rm break, the use of glue-welded joints is effis-,-ent to the
same degrl=e as in structure par-ts subjected to shearing stresses. 'Inere A-re 2
t-'ablc-~E5 an--4 4 figures,
-a7-" 212

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ACCESSION VR Am5ooO999 BOOK EXPLOITATION
A-.j:ier G#ggrI7 GLi 17eviob (E ngineer) jM!=,n, lay Nik ;h
_qdr Kg2j211cojaZ Khrloto OTT
iandidate of Technical 1)
Sciences) j A~
,'drididate of Technical Sciences)- Feltdman, Lev Semenovich (ftgineer)'.
j-'a lied jo in mechanical engineering (KleyesvarMS SOYOdineniya v
--tas'l-u-nostroyenii)., Kievf Izd--vo "Tekhnikan]y 1964., 199 p. i1lus-j, bibliao
-P600 copies printed
16s
TOPIC TAGS: glue welding., spot reldin . quality controlp alumi 3-10
51FIRPOSE AND COVERAGE: ~he book reports the results of scientific nd experimenta.3.1
iiork on the use of glue-welded joints in structures made from high-strength
alinninum alloys. Basic attention. is given to the technology of fabricating
glue-welded jointes, development of glue composition.9 glue applicatioup preparat-,
Ion of =face for welding# anticorrosion protection of glue-welded jolats',
mechanization and automation of the glue welding process, and its technical-
economijeal indicators* The book includes a comparison of the strengil of
welded and glue-r-n-Ided joints under static and cyclic loads under conditions
r normal and elevwbed temperat-wes. The book is intended for engilmlerg,
aesigners,) and researobars in various branches of machine buildings
Ca -d 1/2

L 41775o-65
ACCESSION NR AM5000999
TABLE OF CONTENTS (abridged).

a 1. Permanent joints in aluminum alloy structrwes 7
Il. Spot welding of almdutm alloys - 13
.,%o III* Olues used in-glue-ovelded joints - 30
Ch. IV. Technology of spot-ilue-welded joints -' 41
V. Strength of welded and glue-velded Joints - 51
iho VI* Defects in glue-ovelded Joints and methode of.inspection 116
Cho VII, Mechanization and automation of glue welding - 3.66
L,r,, VIII0 Recommendations on designing glue-welded jointe 186
.-,,-:)endix,194
-
A
bliography - 197
SUH4r= s 29Apr64 MM CM, M,
NO REF SOTt 031 01MMI MO

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J -2A"

ACC NR1 AT7007351 SOURCE CODE: uR/oooo/66/000/000,/0099/0105
AUTHOR: Shavyrin,. Y. N.
ORG: None
TITLE: Mechanizing the process of making glued and welded joints
SOURCE: Soveshchaniye po av-tomatizatsii protsessov mashinostroyeniya. hth, 1964.
Av-tomatizatsiya protsessov svarki i obrabotki davleniyem (Automation of welding and
ipressure treatment processes); trudy soveshchaniya. Moscow, Izd-vo Nauka, 1966, 99-
;105
'TOPIC TAGS: glue welding,' industrial automation, welding technology, automatic
1welding
jABSTRACT: A technological process has been developed for making joints by a combina-
!tion of resistance spot welding and cementing of metal structural elements. The ad-
dition of special structural glue to the joint increases the strength characteristics
and provides anticorrosion protection. Two methods are used for making glued and
welded Joints: 1. conventional welding followed by application of the glue (penetra-
ition by capillary forces) and 2. welding over a fresh layer of liquid or paste cement.
The author describes the universal VUS-1 welding manipulator designed for mechanization'
,of the spot welding process on large structures with compound curvature. This manipu-
'lator lines up the panels normal to the electrodes of the welder, automatically moves
Card 1/2

ACC NRI AT7007351
the workpiece through the proper spacing along the seam and makes tack welds at these
points. An eight-channel programmed control unit for this manipulator is also de-
scribed. Closed-circuit TV may be used for remote control. The operation of the BPU-,
1 programmed regulator for automatically welding elements of varying thickness is dis-I
cussed. Mechanization of the electrode cleaning process is considered and it is
pointed out that the GZP dressing unit based on the UD-2M angle drill may be used for
,solving this problem. Finally, an automatic machine for applying the cement to the
.welded joint (capillary methocl) is described. Orig. art. has: 2 figures.
SUB CODE: 13/ SUBM DATE: None
LCard 2/2

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DF,MIDOVA, L.S., SHAVYRINA. A.V., KUZIMA, Z.M., FADEYEVA, 0.1.,
LEVIN, V. L.
Results of using geobotanical methods in hydrogeological
investigations in Charnozem regions. Trudy VAGT no.1:61-70
'55. Mak 9:11)
(Phytogeography) (Chernozem soils)
(Water, Underground)

AUTHOR: I-Sh, a v Y r i n a , hV SC7;
T ! T L The Utiliz.:tion of Geobotanical Symptoms in tne Search For
_~r on Virgin Lands of tie Kustana- ".blast kispoll-
t
zovaniye t;eobotanicheskikh priznakov Pri poiska"ch vody na
tselinny"ch .;emlyakh Kustanayskoy oblasti)
i ': -,IUD DCAL; 1Razvt_-Jka i okhr:ina nedr, 1959, Nr 1, pp _-11--141 (U'ZISR)
AB S T RA C'P Numei ous shallow depressions occuring in th;~ ~;outhern -,n-,rt
of the Kustanay oblast very often indicate that under-
ground water is to be found there at a slight depth,
especially when the quack .-rass (..*igropyrum repens) and
other moisture-loving plants are growing in these
depressions. There are three ~*oviet references.
S SC) C i A L"! C, NVS;~"Gi_'.'GEO
Jard 1/1

SHAVYRINA, A.V.,
P0031bility of predicting the mineralization of underground water
from the chlorine content of phreatophyte plants. Sov geol. 4
no.3:1-11-11-3 Mr 161. ~MDbl 14: 5)
1. Vseso*yuznyy nauchno-issledovatellskiy institut gidrogeologii
i inzhenernoy geologii.
(Phreatophytes)
(Water, Underground)

VOS'.,'OKOVA, Ye.A.; SHAVY-RIVA., A.V.; LA,,ICfE-VA, S.G.; V1KO"~OV, S.V.,
doktor geogr. nauk, nauchnyy red.; FEDGROVA, L.N., red.izd-
va; IYE;USIJIl,,SKMA, Ye.S., teklm. --red.
[Handbook on indicator plants for gruund waters and soils in
southern deserts of the U.S.S.'~ .]SpravochnLk po rastenii~ir_
indikatorar. g--untovykh vod i Dochvo-gruntov 6lia iuzhr-.y.,-Ii
pust,yn' SSSR. Fo~_ red. S.V.Viktorova. .'oskva, Go-..geoltekh-
izdat, 196". 123 p. plates. (MIU 15:12)
~.Wssia, Southern--Indicator plants)
(~tussia, Southern--Desert flora)

SH.A.VYRIPIA, A. V.
Possibility of using the geobotanical method in the search
of fresh water in southern deserts.Trurlr~ %K~7 P 8:27-31 164.
, I I
(MIRA 17: 12)

1.
. . ; ~ 1 1, 1 . ~ I- 1 7 ~ . - :
- 7 p-i:*- :.~ ". , "":. , . . . .I . . : , 1. : .. 7 ; , . - . . !
7 . . ; - - ; .. - 1:~ , ! i . i . . ; L . .- . -. , , 1 . : . .
.(-; : -, :. 4 1 f n ;~ " ;: :'. ~ - ~ '- - -- ~. : , . I . - - - - - -, - -, --
I .. .: , ri : : : . : f", . ~ j 1 , I . 1 " ; .:( . ; .
r . 1 .1 - . I ~ , . .. t :
- -' 3 ~` -4'- 3 5 1',- ,k 1 , -, .
;I - ~i : - --: ,;

AFBU.;*C'V, Yu.A..: FFDYUKY.', '.'.L.; -SHP-,VYRlN`A, V.v -
Dienes
Interaction of di-(cyclohexene-l-yi-l~, 2, 3-dimethyl-butadiene-1, -1 and 1-phenyl-
butadlene-1, 3 with nitroso compounds. Uch. zap. Mosk. un., No. 132, 1950.
Monthly List of Russian Accessions. Library of Congress October 1952. 'JiCLASSIFIED.

Sf;,VY,dI6A, V. V.
The reactions of dfenlc hydrocarbons with nitroso com-
pounds. Addition nf 2 A-dirn,thyl-I -3-baWlene, I-phenyl-
Chemic,d Abst. 1,3-butadlene, and )Ff-i-cycloheren-l- aromatic nitroso
Voi. 48 No. 9 compou u.,/A. Arb ov, N. L~CFed ina V. V.
Y Z 7~x_ :F - - '77-
aa.*
V c, . 7.S.YY,
~~IaY 10, 1954 L)rv.* Chem. &s. 1952, 539-42(Engl. translatian)-Sce
Organic Chemistry C.A. 47, 4342f.

'ay/j till 5",
"Ti-e
3-1)i ut'a,; and DJ-(C-,rcIchcxene-I-y1-!)
tc r ol,.u .-S, l. -_ a ,%,r. V. Shavyr- na ,
Cc; ~O rbu,,.ov L. Fcdy,
w Stat- ime i
Incil of 02g Ci.ein, Acad Sci U~-~R; ,.csc.- 2 U n
t--e rcact-~,oris _- 2 dieric-
-thyiloutadiene_!, 3, trans- 1-plic, i.vlhuta
'ic n!'roso c~_-.i:z:ds. Ottairled t.he
-and C:.i- (cyclo i!e ~:e ne- w_-Lth aroi-alu i
Ll,,,+a ene-1, 3 w4 + h ni- roso e,,zcr-e and L.-
-_.ro
3 with nitrosrDienzene, 0-r-iturc-
ycohexene-l-yi-l) wIth ni~rcsc't.enzene
s~~'Uolu.cne an,i anO of ~i-(c, -

CHEXCHIKOV.n. 1;.P. SHAVYRINA, V.V.
Some data on the sporocidal and bactericidal effects of 1-3-dichloro-
5,5-dimethylhydantion. Zhur.mikrobiOl.eDid. i i-mun. 28 no.8:78'81
Ag '5 7 (KT
IRA 11:2)
1. lz TSentrallnogo dezinfektsionnogo institute.
(HYDAIROINS, effects,
1,3-dichloro-5.5-dimettiyl kvdantion, bactericidal &
sporocidal eff. (Rus))
WITISEPTICS. effects,
same)

and -sl~e,'a 0
~O 10~~,Y. Lfull IrseCtV3 ?
.13
Ztl,-~ of
t ):t 1'~.c a:: i
2-1-ol., JO 1J,
X-Z Mor
Ccnti,al jc~c~a--ic 2oi-jarz~', imtitute fcr L`11_9~'.~-Ufoc;"~-!-i
1e '--.oect'c'de ~!rL)-ort`;!s 3f '.0t:1xyCi1.1Or
Oxig Pub : Tr. Tront!, - n i -i - dozin~cekft~, i n-ta, 19"17, vyp.
211-216
Abstroct : ~Io abstrac-t --i U."
N
V/
J
USSR General and 3pecial Loology. Insects. Insects P
and Arachnids. Chezical Method of Controlling
Harmful Insects and Arachnids.
Abs Jour: Ref Zhur-Biol,, No 21, 1958, 9~5503.
Author Vashkov V. I.; Klechetova, ~,. Y.; Shavyrina,
V *V,;/3hilova, 3'. A.; and Kalu6ina, T. 1.
Inst Cent al'86i-ehtific Research Oisinfection Inst-
itute.
Title The Activator's WC Influenca on the Insecti-
cide Effectiveness of DDT Preparations.
Orig Pub: Tr. Tsentr. n.-i. desinfects. in-ta, 1957,
vyp 10, 198-204.
Abstract: ':hen. 11-aY/a of the activator Mv!C (4.41-dichlor-
diphenyl.mathylcarbinol) is added to DDT the
ef2tict on the DDT preparations against flies,
buqs, lice and roaches is accelerated and the
Card 1/2

i'l 2, 12) 3ov/i6 -59-6- 2,.,,/1,6
AUTHORS Cherichikova, E. P. and Shawjrina, V.V.
TiTLE~ Some Data on the Snoricidal and Bactericidal ProDerties of
Trichlorisocyanuric Acid
P FTi T OD I CA L -ZhUrnal mikroblologii, epidemiologii i Lmmunobiologit, icy~91-1"Nr 6~
pp 82-86 (USSR)
i'lB3TRACT The authors performed tests to study the bactericidal and spor-,I-L~Ial
properties of trichlorisocyanuric acid with a view to 1-~z no-zEit-I-e- use
as a disinfectant. The investigations were performed wiln Cambr,.-,
test objecis. The microbes were; Staphylococcus aure-us, Escherichia
coli, and a spore culture of Anthrax. Ghloramin-~- was used as the
reference disinfectant. The results showed that ri.-hloriso--yanuric
acid had a bactericidal effect on Staphylo~occus aureus 511, *-J.-~Illes grea-ter
than chloramine, and on Escherichia coli - 10 times greater. A
solution of trichlorisocyanuric acid killed anthrax spor=-s in.
minutes, whereas lQ-4 chloramine showed no disinfe--ting, effects in 6
e h orin.- -r.--r=
hours action. Trichlorisozyanuric acid loz,, itS activ - i --.- -~-
o~ul--kly than ?riloramlne but lefiz quickly -har --hloride of lim-e and
--alcium hypochloride. However, solutions cf it lle~~ F-a--le -n-3r,

`,V/ If) - IZ)q- 17/146
:om
e Data oq the "poricidal and Bactericidal Properttes of Tri,-hlori~oc-(anurtf, kid
any of the chlorous solutions used f-)- disirif-t.ion. A rl~~e in ~em-,erature
boo~,.~d the efficacy of ~he -~-id -on
the spore and the vegetative fo,mF G.M. -:~iozburw. a-nd
m i in -.a i ned that ,-,rc%tem dops not n I av -3 ,~,v n r i-; r
r'hloramiyl~ --i:~ t-.r other d-i-,LnfectFints, ln~ a
priDteini 2.omewna, leng,~hen~~ the time .-.E
or Sporcirla-I effe-t , A,-,-,--,,dinL,
Koval-, 'I.F. Mavnr~,vu ard
-,I,-,rinIn- -ir,d chloride of lima- may L-- u:~~d `7,
r
_I 5 LP,hrax an-I o'her inf~-*ion-- A A I
aiid so,-j-ionq wish ammorium
of thi-z

sov/16-59-6-17/46
-Eome Data on the Sporicidal and Bactericidal Properties of Trichlorisocyanuric Acid
There are: 4 tables, 1 graph and 10 references, 6 of which are Soviet
and If English.
ASSOCIATION: Tsentrallnyy nauchno-issledovatellskiy dezinfektsionnyy institut (Central
Disinfection Scientific Research Institute)
SUBMITTED: August 13, 1958
Card 3/3

17(6) SOV/16-59-9-.3/47
AUTHORS: Alekseyeva, M.I., and Shavyrina, V.V.
TITLE: The Use of 1_chloro-~-naphthol for Disinfection in Tuberculosis
PERIODICAL: Zhurnal mikrobiologii, epidemiologil I immunobiologii, 1959, Nr 9,
PP 13-18 (USSR)
ABSTRACT: 1-chloro-P-naphthol has not been widely used in disinfectant practice
because of its low bactericidal activity (Ya.L.Okunevskiy). Vashkov,
Chadova, Shavyrina and Ramkova have observed that it has a marked
selective action on bacteria of the typhus-enteric group. Subject
authors synthesized the substance by chlorinating P-naphthol with
sulfuryl chloride in chloroform. A water-soap emulsion of the dis-
infectant was prepared and tested in concentrations ranging from 0.025
to 2% in the laboratory and under field conditions. The disinfecting
action of the emulsion was tried out on gauze test-objects, soaked
with fowl tuberculosis bacillus or with tuberculosis sputum, and on
wooden, painted and plaster surfaces contaminated with Mycobacterium
tuberculosis. The results proved that 1-chloro-p- naphthol is effective
In a concentration 10 times less than that of chloramine. Its other
Card 1/2 advantages are that it does not discolor linen and has no obnoxious

SOV/16-59-9-3/47
The Use of 1-chloro- -naphthol for Disinfection in Tuberculosis
smell. As far as can be observed, it has no toxic properties, although
gloves are recommended when handling it due to the inaremed skin
sensitivity it may provoke. For the disinfection of surfaces, crockery,
utensils and linen in tuberculosis nidi it is recommended to use a
0.5% water-soap emulsion of 1-chloro-p,-naphthol and to allow it to act
for 60 minutes.
There are 3 tables and I Soviet reference.
ASSOCIATION- Tsentrallnyy nauchno-issledovatellskiy dezinfektsionnyy institut
(Central Disinfection Research Institute)
SUBMITTED: September 29, 1958
Card 2/2

SHATf RKIDT., Yu.
Processing corn for mixed feeds at the 14elekess Milling
Combine. Muk.-elev. prom. 29 no.8:24-25 Ag 163.
(MIRA 17: 1)
1. Zamestitell glavnogo inzhenera Melekesskogo mellnichnogo
kombinata.

in7h.;
R A. ,
Ll-
~31LVEIIKAYA, L.B., inzh.;
M.
1.1 RA

I'sJ
Agalmatolite as a Valuable Raw Material for Refractories
of * h Refmcloriness. A. L. Shavzi& (Liminoe.Proizvodsivo,
1953, (7), 31-32). [In RUSrt-A-nT-=waa found that agalmoto-
lito firod at 1100' C. forme a white, porcelain-liko MGM with
high mochanical strength and refractorinew of the ordor of
1900* C.-S. X.

GOLOSOVK&R, S.Ya.; SHAV,,IS, F.Ya.
Xtiology of pyoderma in the nfjwborn. Vop.okh.mst. i det. 3 no.l:
33-36 Ja-F 158. (MIRA 11:2)
1. 1% kafedry mikrobiolo~;ii (zgv. - prof. V.K.Berman) i kafedry
kozhnykh bolezriey (zav. - orof. S.Ya.Golosovker) Leningradskogo
pediatricheskogo meditsirskogo institutua (dir. prof. N.T.Shutova)
(SKIN-DISRhSils) ( Ili FANTS--D ISEASES

A'~.MOIL.
Biliamll.h, G. N.
SOVi7'-14-4-310~30
SeCtlass Of -~:hzziztt`7 4f thQ T-1:1 ~9-!Cl~.ttv
Camara.. .. G.-L noi Applied Chemistry
PCILIDDICL.I., Zh--l amILtL.h..k., kbiall, 19~9, Vol 14, fir 4, Py 511-512
(USSR)
Cl
A.11311TACT. IPPrazimet 300 persons parttolp4tad it the ark a.- the
DOP~tmant of Anstlytical Chomistry, among them repronontAtIT0.
0f various scientific research institute., higher school. and
Industrial enterprises in Hussia, ciontlet. from China,
DWS-i-, the I!SR. Poland, Nungary, and Italy. 1pproxinat:ly 70
rapor-a waro, heard. In him opening speech J.P~_All-"- port*4 ~-J~D
- the maht-d r,mults and on modern probl,tv f nalyti-1.
h IV_ "N" ' r' ~*rt,l a"ll, I IT
't__ _'l . ..1.
h::' Ino u my .f r tso t 0
-a-ma 11.1. ~in-Nr., It.
..rise of probl... of -1~-tl zo-1-
reported a modern &I=. I. the of
_t~~t:hoc.ed at the example of he' Ida mad th"',
rr.l.tl.. Wis.- it..atttlIty or -d
,:,Positimn of th.Z;orr..p cling ... t,.1 at... 1. the p.ri.11-
1/4 am. T,-X.PAAhka and _7=D_2tkMa lectured a. the t.bility
of.mist of Cu, Co, and It a. d.;ending on th a at to cturo .f
lectured on hub
th:r:.i- Isola t a do
r:4.
%I.. C._.%
at r Of ac,I=-,,I,,.In, I;n.,f
It .1pyll at a '" I,
,I. Th . prohI.t':.aI,
a,malyti-I chemistry a.. dealt with in Zho lectures or
.7. 1- Shkh,e, .ad -workers, -I ~. I,_xoYQx_.I1 ..1 .1, . A.
JaJ23AJAM. A large number of lecture . dealt with the oag of
;-7.t I a-
rt.d ato thpI.. of lkyl ad di.ry-l dithi.-
phosphoric &old for the separation of elements, used
"71 r.a.I. aid and ryl ;d,:,;hi.Ia ..td. R. P. Lest. .1,1y -d
hlaoa-~manrlmmrw ra at ad ... propnrtlea of now a,mp 1:_n. The
I* at - or f- - N-arghko. q~R. Shitareva, and 4, Xohononk,,
4the ph,,,,*trlc -olo-t.
.:ilt -ith
.gfI-ri A. 1. -h.1k ... m led 'U'od the u,. of
hAlghromation In Aam,lytITWT chards.-Do k
"I tita lectured on the
diffeInentI&I spot tropho tome% r7.
prt.d .. ..a highly It"-It
C" 2/4 toraviol.t microulope. S::*1rl l:.1t1.1ly dealt tth
methodical ad theoretical problem. of .;,-t rum ..... ly.l.
.1"i rY.,
-.dPaj AE-1"h"_TD
S. kto, -;1 1, Ulk, 1:'",he
oral 'M ':7'
rfaction of flema photometry. Sov Imlr. I..ll with the
M.-i-tion of elements by-1
d
Z,I,-R.zu* t,,njkMA mad -L. A. L.1--12Y Ihahis _~n.; !I..
in mine fi-4 olactrodam -ore r't.1 b; 1. D.-
Lyallkov and co-vorka- -.!to locturo ,f
the .or
titration with two s5cE_roTaT*In tho chom 1.t~.ror.. I umand
tharium 11,U, Sny::Ia,;.Io,.,d p.. il~t~.. of predtcti
""I tiar-trbation of elements ba:~,,%-.
ch Ith, P:I
th" Ir po:tt%- In the periodic system. rep-1-3
.. th: us. of to. Itchang. I. the In-tig.tl..II`: -state ,f
subs t ne.. in -al-ti.... adVon'
I~:,tur. d on the chromiatoerc.1hic s.parat1,,,,*f
41 at., ~. G. r.,-.rt.d a 'd.,os rti..
Or Lt. :.ob^ g.r -in., Y- M. Zh.my_tkin and associates -port,4
.0 th . hromatoCraphic proof of mUlfn~ilmx:lde prnparntionu In
Card 3/4 liquid& of the organi.m. Staroblaets and associates trooto!
the Ipp 11. In. Of high P.I~m,rs In chromatographic Analysir.
I..ur:tr It L.Tylloi~, -d VI14.jurkel-tatub, G.
a
tI, ._2~=
4stal t with no chromatoj..Fhy. Several act r. rdAtOd tl~l UdF-
r.dl O..tl,. for th, chrommtoCraplAc In-ntleittion or
.0.9 lot formation U.J..Ej_n~c~lkov and &-,cimtev), for tI.,
f""I:' 'h at" am
Lov
4
th h:
if
I.A
.1 .... to b mean. ofIrka,
jjllpayuhl . In th u 1,11 f v1--tarl oz-,:,nlcmi 1, 1.) a I .
.." a, r. 11
If y_o_v_j_Z. r.,, -1 V,_s* KII!,- wlth
aaaI'll 'o to "ho tti to ol"ur"tt"', "r
rapid t.rovatb.d. far IL, Imul t"Tu" " I
.n.o.t. 1-ca. ~,ad
'Y

KISTFR, E.G.; ZLOTNIK, D.Ye.5 FOPKOVA, L.M.; NAZAROVA, V.D.; SHASKOL'-
SKI~YA, T.P.
klombination chromate reagents for flushing fluids. Burenie
no.9al7-18 165. (MIRA 18:10)
1. Vsesoyuznyy nauchno-issledovatellskiy institut burovoy
tekhniki.

.SJfAYAKBMOV, N-Sh.
Automatic control of the operations of waste dump winches. Ugoll
35 no.11:34-35 N 160. (MLEA 13:12)
1. Rudoupravleniye Tadzhikugf,"'-
(Autom tic control)
(Coal minee and mining-Equipment and supplies)

MUKMIEDOV., Ya.Yu., rentgenolog; SHMAKINEDOVA R.59) red.; AKSELIROD,
M.B.., red.; TSA7, A.A., t629-.red.
[X-ray diagnosis of dyskinesias of the gall bladder) Rentgenodiag-
nostika diskinezii zhelchnogo puzyria. Tashkent, Yedgiz, UzSSR,
1961. 120 p. (MIRA 15:6)
(GALL BLADDEH--DISEASES)

PARPIYEV, K.M.; SFAYAKF-WEfjOVA, H.S,, red.; AGZAM-CV, K. tekhn.red.
9
[Chronic colitis]Khronicheskie kolity. Tashkent, Medgiz.
UZSSP.Y 1962. 22 p. (MIRA 16:3)
(COLITIS)

r C,
3 t:

KPAKIYOV, Khadzhl A-kbqravich, kand. med. nauk; SHAYAKRfETlOVA,H,t
red. - - 1. -
(Hood transfusion and donorship] Perelivanie krovi
donorstvo. Tashkent, Meditsina Uzbekskai SSR, 1965.
U P. (MIRA 18;12)
4

ACC NRt AP6021605 SOURCE CODE: UR/0020/66/1&8/005/i01iJ/iU!)i
AUTHOR: Kovylin, V. M.; Karp, B. Ya.; Shayakhmetov, R. B.
ORG: Institute of Oc anology, Academy of Sciences $SSSR (Inst1tut okeanologif Aka-
demii niiuk-SSSR) L!~_ - /
ITITa -. Structure of the earth's crust'land sedimentar-j strata of the Sea of Japan on
!the basis of seismological data
SOURCE: A11 SSSR. Doklady, v. 168, no. 5, 1966, 1048-1051
TOPIC TAGS: earth crust, seismic wave, ocean acoustics, wave propagation, seismographl
ABSTRACT: The cross section profile 500 km in length located in the middle and south-
ern parts of the Sea of Japan was investigated using shot points at depths of 90-150 m
brcad-band geophones, and an analyzer for recording bottom reflections. Sea depths
and. sedimentary bed structures were studied by recording reflected waves when the ves-
sel. was in motion. The study of the seismographs indicated the presence of two typas
of reflected waves P4 and PM at the distance intervals 10-43 km and 37-81. km, respeci'~_
ively. For the construction of the P* wave type, it was assumed that its near velo..r,
city of propagation in the sedimentary beds was 2.0 km/sec. For the construction off
the )I wave type, using the method of time fields, it was assumed that its velocity'of
Card 1/2 UDC: 550.834

MAKWUOV, No.-"-.Iw,--izhtt F. odzl-.ay,--v,,h, kand. biol. nauk; POGCTRILKO
1,F., -.".)ktor --.ed. nauk. red. --ceased!;
SHAIAKEN:EDOVA, red.
(Produc t4 ial oils (terpenes) ,in(d their use in
ion of essent
urolithias-'Ls] Pciuchenie e -riykh mase-l (terpenov) i --kh
primenenie pr-~4 -,..ochekanennoi bolazni. Tasl-&,-ni lzd-v(D
"Madit,ninall UZSSIR 1964. (m ,
-135 p. IU 180)

SOV/92--59-3-12/44
AUTHOR----Shavban, D.A., Senior Operator
TITLE; Remodeling of Standard Processing Units (Rekonstruktsiya
fipovykh ustanovok)
PERIODICAL: Neftyanik, 1959, Nr 3, pp 14-15 (USSR)
ABSTRACT. The author refers to Neftyanik, 1958, Nr 5, in which
E.B. Khesin raised the question of improving designs of future
processing units. The author maintains that another question
of importance is the standardization of methods to be
followed in remodeling units now in operation. Every re-
finery solves this problem in its own way. It is desirable,
however, that the planning organizations develop a standard
project for remodeling existing units. The reconstruction of
the two-furnace cracking units of the Nefteproyekt type should
be carried out on the basis of a standardized design. In the
opirdon of the author, a furnace and atmospheric columns
should be added to the above-mentioned unit and placed ahead
Card 1/2

Remodeling of Standard Processing Units SOV/92-59-3-12/44
of it,.. In t-hfs case t,ha yields and the processing capacity
of the entire unit will become equal to those
obtained froser bcth Mae -nracking unit and the atmospheric-va-
cu,jm p-1pe stil';'. It is also advisable that the standard
prr-jer:t provide for the installation of a
wit.1i the goudron flowing to the mild crackir-g
P,jrrva:7e, and t-h.e vacu,.-,z gas ail flowing to the deep cracking
furna-.e. Mild !,,ra3k14-g furnaces should be equipped with
s1de-reac-ors. Bil-h f-Arnaces will have to operate on narrow
Petrele-am- fraaticns and, as a result. a higher yield of
~~ra~.ked gaZ(',7'pr_
will be ensured, provided proper operating
conditions are maintained. From the economic standpoint a
reLonetruct-~'on- of existIng ur-it-s is highly desirable. Funds
and eq-,Jpment be made available to refineries for
this purpose.
ASSOCIATION-. 1,Uier3o---,.skiy NPZ (The Kherson Refinery)
Card 212

SWUM#`, K.A.
3598. SHAYBL~KOV, K.A. Oplata Truda Kolkhoznikov-Zhivotnovodov Kazakhstana
(Po Sovetskowu Zekonodatel!stvu). Alma-Ata, Izd-vo Akad. Nauk Kaz SSR, 10,54
95s. 20sm (Akad. Hauk Kazakh. SSR. Sektor Pravs) 5,000ekz. 2r 50k.-
(54-57164) P 331.20:636 (584.6) 4kn. Let No. 3.
SO: Knizhnaya Letopis', Vol. 3, 1955

SHAYBEKOV, Kimalkhan Asambekovich; TVERDnV, A. `~., -ed.; KOSAIRURVA,
Ye.N., tekhn.red.
[Wa-,es of collective farmers engaged i-:, '--'i -rop cultivation]
ODlata truda kolkhoznikovo zaniatykh . - --- Mosk-va,
Gos.izd-vo iurid.lit-ry, 1959. 85 P. (MIRA 13:1)
(Collective farms) 1% W a -..F- 3 )

Vi Ii Y 6 E K 0,/,
PANKRATOV9 I.F., kandidat yaridicheakikh nauke
Legal problems concerning wages of collective farm cattle breeders
in Kazakhstan ("Wages of collective farm cattle breeders in Kazakh-
stan, according to Soviet legislation.0 S.X.Shaibekov, A.G.Ashcheu-
lov. Reviewed by I.F.-Pankratov). Vest. AN Kazakh.SSR 11 no-3:94-97
Mr 155. (HIRIL 8:6)
(E:azakhstan--Collective farms) (Kazakhstan--Wages)
(Shaibekov, S.K.) (Ashcheulov, A.G.)

SH,IYBrK?-)n, ~-.A. ~L:SIA:t
m,,, e o e .g s ,.17 ri s p
Inf i
-3 n a~.
cf t-f3 man -jA-7,. ess 4-tre T)-.

gMbL,t, David Solomanovi,-,h; G~-,,`j H, A' K. , red.
[111 trrt.3t;ni-,- f- a w r;i-tec,--,i,)nj It''I I trazv-ukoval a 'efektoskop- Ia.
L j , a f- -
'Moskva retallurgilaY 91 P. 0, li-,A lg:i)
J, 1 3,

L.24787-66 EWT (1) /E14P (m) /EPF (n) _?_1&dA (d) /'ETC (m) - 6 JKT/W'W
N AJ ~,o14221 09) /0198/66/00270-0-~-/-ol-W2-70-lIi3-
N
CC-k SOURCE CODE: UR
1 F7~:Op
P-,:;c'aenkov, A. N. Lukashenko, A. N.
~i J-; None
TITLE: Scientific conference on the hydrodynamics of a submerged foil
SOURCE: Prikladnaya inekhanika, v. 2, no. 4, 1966, 142-143
TOPIC TAGS: hydrodynamics, fluid dynamics, flow analysis, cavitation, cavity flow,
boundary layer flow
ABSTRACT: A scientific conference an the aerohydrodynamics of a foil near a free
surface and a. solid surface was held at the Kiev Institute of dromechanics of the
USSR AcadeaV 2f_~ciences from 28-30 October 1965, with 106 delegates from 45 Soviet
institutions participating. The following scientific institutions were represented:
Central Scientific-Research Institute im. Academician A. 1q. Kryl Central Institu~-Q_
ypamics; Institute of Hydrodynamics, Siberian Branch, USSR Acadenu of
-ad _c EuFle of Water ransporua-
--l-Sciences Leningi ShlZjjt~~! n tute; eninCiaa n~ I
Lion Enrineers, Central SciontiPic _M,-TFi'0 :Cm-e
__!-7arch Insti7t7ute LeEi,
Novosibirsk and Gor'kiy instlitul~.f-s of Wat ,er Transportation Engineers; Kazan' and i~Lvg_l
[jell it e- r 's" i-t iF 6 te S_ 1i1v_:!rs Kf~_eV__t_n_'s1Eff_uYF_
S t ate a e.
r"T rleet Kharlkov Aviation Institute. Forty-one papers were Dre-
of t1v, Civil _; and
1-se-ated'-which-dealt with actual aerohydrodynamic probler-s of high-speed objects, among
I

ACC NR: Ap6ol);221 0
which were the following: A. 11. Panchenkov discussed problems of the unsteady motion
of a foil at a variable distance from a surface, and the hydrodynamic boundary-value
problem of a cavitating submerged foil. K. K. Fedyayevskiy presented an approximate
nonlinear theory of a rectangular low-aspect-ratio foil moving near a fluid surface
at high Froude numbers. V. I. Rudomanoy reported on takeoff (lift) and landing
(settling) ;tnamlcsof craft utLizing surface effect. V. M. Ivchenko- reported on unsteady
hydrodynamic problems of supercavitating bodies and the use of electronic digital
computers in propeller design. G. A. Ryaz2jiof2_,paper dealt with electric flow simu-
lation around foils of infinite span, and magnetic flow simulation around foils of
finite span. V. V. Ko eyetskiy irleported on the use of a magnetic simulation method
for estimating the effect of blade thickness in the design of a propeller with a
given blade pressure differential. V. A. '.Yanov and G. N. y_yeported on
_Ezj~~_ ____Eoyarski
investigations made on electrohydrodjn~~Y~ flows and on boundary-layer control along
a foil profile. Ye. D.-Udartsev reviewed methods for the laminarIzation
of the boundary la-~r-e-r--o7-eTe-c-fr-oSydrodynamic flows. Yu. K. Biktimirov reported on
specific features in plot+,ing the potential of velocities caused by a source moving
in a fluid. R. B. Nudel'man discussed bodies moving in a multilayer fluid, and
V. T. Tok-arer_____
'Leported on a quantum-hydrodynamical analogy and its application in
hydrodynamics problems. In a final statement, it is mentioned that the conference
J
emphasized the importance and urgency of problems in aerohydrodynamics of a foil near
a surface. 'Bie lag of Soviet science in the study of supercavitating foils was also
mentioned, and a more intense study of three-dimensional cavitation problems was
reco=nended. It wp-- agreed that the proceedings of thiB conference be published. GE
SUB CODE, 13, 01, 20/ SUBM DATE, nonq ATD Pre ss F 6-
Card

SHAYBOJ, N.V. [Shaibo, M.V. ]
Motion of s-ips cm mderwater wings. Visti Inst. gidrol.
i gidr. AN URS: 27:34-,46 160. (MIRA 14:8)
(Ships)
, -.
I

SHAYBO, Nikola- lSlavovi--b[Slialbc,- 11 V.1; FAVLM'10, 0 Ye,,
I vlenko. 11 M- j-,- akadei,-A.1- D-t-v,red, FECHKOVSYAYA 0.114-
p.
iechkovslkr-. 0 M ], red. ind-va LIB-rlba-~W, T,R,, tekhn,
r
red,
[Ships on undeniater vings] Suldna ria oi(dvod-,ykh ki-,,lakh,
Kviv.1 lyd vo Akad nauk U:I.SP., 1962 53 P- (MIU 15:7)
l-, Akademiya nAUk MqSffor Favlenkc)
(Planir,g liulls)

10(3); 1(2); l(9) PHASE I BOOK EXPLOITATION SOV/2538
Moscow. Aviatsionnyy institut imeni 3ergo Ordzhonikidze
Issledovaniya v oblasti teoreticheskoy i prikladnoy aerogidrodinamiki; sbornik
statey (Research in Theoretical and Applied Aero-and HydrodV~0_8 ; col-
lection of Articles) Moscow, Oborongiz, 1959. 92 P. (Se ries: Its: Trudy, vyp.
-1-11) 2,650 copies printed.
Ed. (Title page): N.S. Arzhanikov, Honored Worker of the RSFSR in Science,
Professor; Ed. (Inside book): A. S. Ginevskiy, Candidate of Technical Sciences;
Ed. of Publishing House: E. A. Shekhtman; Tech. Ed.: V.I. Oreshkina; Managing
Ed.: A. S. Zaymovskaya, Engineer.
PURPOSE: This collection of articles is intended for scientific workers, engineers,
and students of advanced specialized courses.
COVERAGE: This collection of six papers is concerned with the aerodynamics of
wLngs and shrouded prope-12jers, hydrodynamic lubrication of bearings, and such
fundamental problems as t*rj-- -,riBcosity of fluids and pressure losses due to
local drags.
Gard 1/4

TABLE OF CONTENTS:
Pre face
1. Biryukov,. Ye.A., En6l~i,:!er. Dawrpi-ng Due- to LaF, Z tne Do,,mwaih
Behind a Wing of Finttk- Span 5
This artir~le the ~:ffect of a ac,astationary vortex
sheet on the aurpli*,tde and lag of the dovawash of a flw behind a
wing of finite span. 2 Sovlet.
2. -Sadekovp.,-~G.S.., Candidat,2 of Teclh-uioai CaIc---LIatirjn of the
Ler~dy~mi,
Chara,tristics of a Sweptba-zk Wing 1!i a Bounded Flow 14
This article invest-iga-tes the effect cf the flow ba:i-ridari,-s
on aerodynamic cna-z-ac-ter-is--ics of sweptback wingTs- of arbitrary
plan fom. RefereL2es: 2 Sowlet a-rd -2 Je--ma--n.
Nikitin., A.K., and V.S. Kc.-Z-2hagir) Candidato-s ~jf Tt---haicai Sciea,2es.
Twodimensional Nonlinear Problem of the Motion of the Lubricant in
a Journal Bearing in the Case of Uniform Rotation and Constant Load 29
This article discusses the problem of the motion -~f a Journal
bearing under the assumption of constant load and uniform
Card 2,/ 4

Research in Theoretical and Applied (Cont.) SOV/25135
rotational velocity, the entire space between journal and bearing
being assumed to be filled by the lubricant. References: 4 S3viet.
4. Shaydakov, V.I., Engineer. Aerodynamic Investigations of a "Shrouded-
Propeller" System for Hovering 41
This article attempts to obtain a theoretical solution for the
load-supporting characteristics of a shrouded propeller. The
paper is of great practical interest because a shrouded rotor-
propeller is both the load-carrying and propel-ling element of
a new type of aircraft--the so-called "flying platform". Aerodynamic
investigations made by F.P. Kuzvchkin,, Candidate of Technical
Sciences at MAI are mentioned.
5. Levkoyevax N.V., Engineer. On the Problem of Determining Pressure-
Losses Due to Local Drags 71
This paper presents a critical synopsis of current knowledge
regarding pressure losses due to local drags in aircraft hydraulic
systems. References: 17 Soviet, 5 German, 2 English, 1 French. 84
Card 3/4

Research in Theoretical and Appiied (Cont. ) sov " f-~ ~ ~'~i
6. Reshetnikova, A.D., Candidate of Technical Sciences. Variation of the
Viscosity of Certain Fluids With Pressure 85
The results presented in this paper were obtained in the co-ars~-=
of an investigation of the solubility of air in various wr_:z-king
fluids used in aircraft hydraulic systems. This phase of tne
work is an extension of the research started by Candidate of
Technical Sciences i-M. Krasov. References: 4 Soviet, I
lation from Englisn.
AVAILABLE: Library of Congress
-~Sjlfai
card 4/4 11-3-59

s/147/59/ooo/o4/007/020
E022/E435
AUTHOR.~ Shaydakov, V.,I.
TITLE,- A New Method for Computing the Vertical Velocity of
Climb of Helicopters Y
PERIODICAL4 Izvestiya vysshikh Llchebnykh zavedeniy, Aviatsionnaya
teklinika, 1959, Nr 4, pp 64-69 (USSR)
AbSTRACT? There are several methods j-n use at present. They are
all based on the approximate expressions for the thrust
and the turning moment of the rotor and are obtained
either from the vortex theory or from the impulse theory.
The most popular method is that due to L.S.Wieldgrube
on account of its simplicity but it has a fundamental
shortcoming in that it is based on the approximation for
the induced velocity. This article presents a new
method free from the above shortcoming. The thrust and
the power of the rotor are given by Eq (1) and (2)
respectively, the coefficient CT and mK in these
equations being computed from the blade element theory
as given by Eq (3) and (4) respectively. The meanings
Card 1/6 of the symbols in the last two equations are as followv.--/)
(Y--,)

S/147/59/ooo/o4/007/020
E022/E435
A New Method for Computing the Vertical Velocity of Climb of
Helicopters
CY7, Cx7 mean values of cY and C. for a blade
taken at the station r = 0-7 R
C1.7 coefficient of solidity of the rotor at
that station
XT and Kp thrust and power coefficients for the
given shape of the blade
coefficient of non-uniformity of the
induced velocitv field
x (~40.94) -- coefficient of end losses of the rotor.
The values of KT, K and I may be taken from the
table and Fig Ili t9e blades being trapezoidal~ having
a contraction i1 and a negative linear twist (- Ay).
The mean reduced velocity of the air in the plane of
rotation of the rotor-, based on the impulse theory
(see Ref 1) is given by Eq (5) which, for the case of
hovering (Vy = 0), reduces to Eq (6). The power required
is then given by Eq (7) where Lp is the power lost in
friction of the blade in the air. When the motion is
Card 2/6 steady and the power L... weight G and wR are given

5/147/59/000/04/007/020
E022/E435
A New Method for Computing the Vertical Velocity of Climb of
Helicopters
then V, Ls given by Eq (8). Assuming now that the
induced velocity v, is independent from V y and is
always equal to its value at hovering (vi.) then,
by Eq (8), the vertical velocity of climb so obtained
is underestimated. Giving it the symbol V y
Eq (9) follows. All velocities are now refMed to
the induced velocity, this being denoted by a wave sign
over the symbols, T hen by Eq (6) and (9), the Eq (10)
is derived, where Vy~ is given by Eq (11), this being
derived using Eq (1)~ (2), (3), (4), (6) and (9). In
this last relation V is the coefficient of power losses
which, according to Ref 2,mav be taken as equal to 0.811
to 0.64 for single rotor-and 0.89 to 0.91 for double
rotor-helicopters and qM is the specific load per unit
hor-se-power. The method of evaluation of the velocity
of the v-Prtical climb when the follcwing values are given.
H (height of flight), P (specific load kg/m2 of the
Card 3/6 rotor disc)~, a-/~ wR-1 i1 and A TO is as foll

3/147/59/ooo/o4/007/020
E022/E435
A New Method for Computing the Vertical Velocity of Climb of
Helicopters
1) From the graphs take K K
16P Ts p
2) Determine CT = -
(wR)?-
3) Find CY7 and CXP7'~
4) ComputevlB
5) Evaluate V yf~ from Eq (11)~
6) Find the true vertical velocity from Eq (12).
This is repeated for several different heights, which
enables the graph Vy = f(H) to be drawn. When designing
a helicopter, it is often necessary, in order to decide
the choice of some design parameters, to be able to
compute quickly the velocity of the take-off from the
ground. This can be done in the following way-,
transform Eq (11) to read as in Eq (13), where TIO is
Card 4/6 given by Eq (14) and represents the relative efficienc 0

S/147/59/000/04/007/020
E022/E435
A New Method for Computing the Vertical Velocity of Climb of
Helicopters
of the rotor. For modern rotors it may be assumed
tha t I = 2, 6Y = -50~ KT = 0.96, K = o.923, ~ 1.03 -
p
Then a graph of
110 = f(cy7a?)
x 3/2
may be constructed as shown in Fig 2 (which is for the
profile NACA 230-11) and used for evaluation of VY4.
in Eq (13)~ If some further assumptions are made,r
viz no = 0.7., w = 0.94, the graphs of Fig 3 are
obtained which will make easier the choice of the
parameters in the preliminary stages of design of a
helicopter. Finally, the author computes some data
in order to compare his methoi with that of
L.W.Wieldgrube. Three different crafts are considered2
(1) medium weight class (P = .16 kg/m2., wR = 200 m/sec etc)
(2). li-ght class (P kg/m2. frR = 130 m/sec etc)
(3) a model (P = 2 kg/m2. wR = 75 m/sec etc)
Card 5-/6 and the results are shown in Fig 4. The two methods OV/

s/147/59/000/04/007/020
E022/E435
A New Method for Computing the Vertical Velocity of Climb of
Helicopters
agree pretty well for the medium weight class of
helicopters but the lighter the craft, the greater
the difference between the two methods.
ASSOCIATIONg Kafedra C-2 Moskovskiy aviatsionnyy institut
(Chair- S-2, Moscow Aviation Institute)
SUBMITTED3 May 19, 1959
Card 6/6
(0

S/535/61/000/142/003/003
61) E191/E4811
Sha yda ko v V,I, Candidate of Te-lini-al S-
TITLE I iivesLlgaLion of vertical des,-ent stale-, of ;ri
he I i c op t er
SOURCE Mo s C ow Aviatsionnyy instILUt Tr udy N 1
Vopt osy aerodinataLki neSUSli---hLkh vntov vey ci,-- t
81 141
TEXT- The vertical descent of a helicopter pro--eect5 tn h~
~O :alled ',vortex ring" and Ilivindmill brake" ~~tate-~ in whi-h ri-,
-leL]tl,,- defined slipstream exists but viscosi--y for,e-, p~ -du~'L
:.~ r-haracteristic circulation of air around the rotor. MD S L
previous work devoted to these states of operation was purely
-~.~Zppiiniental Certain earlier theories applicable to windmi-115
do not fit the vertical descent states of a helicop,e.- rotor
In ~he Present paper, a theory is advanced covering the -:)rtex
r ing ond w indmill bralie states which agrees wi th exper imenta I
re-~Ults, Consideration is given to the Newton model of
P, -irti-1-le5 of air approaching the boundary of the real ilip~-tream
terminates due to viscosity) from belo%,~ entirely 1,DZe their
C a r d (~ ~/a)
Vi

S/-35/61/000/'-I'jL'/00-z/003
ion of ver ticai El I /E481
1, int, t i c ene r gy . The pattern of an "ai-r- bod~r` surround-Lno the
lo"ir I, given, The total thrust in the vor!A-x ring
of the reaCtive thrust due to the zhanve of ri~)menttijn
tn~idt, the associated body of air moving ivith th,~! ;,D'o- ar:1-1 '.h~
1 ii, li--;t hic- to he drag of the body of air, Tlie r t-a !- , , ; t I ir ,ttr,?
I Itio. un the hl--i ~is of the usual analv-~i S rh- -I I I a of
th,~- ej i-- ~ ~~,d a ir body is e -a lua ted by the a ziumpl i n ia
referred to the rotor dinn, at ~i -L:~
f f L,-, i ent
::,-j It 1; On this basis the exper'manl,'il r n
I v P Brothe~hood (British ARC R. nno M N o 19 5
t1-,- vej,--ity of descent. and the lo-sl
:t,,e- at the dis- and far behind it ;i,rrpe toi-l% -1 1
-ed
-~,l ities deri, in thc- pr~-zen' popf.-
t:)I i I i t v of motion in the i cr r I r,
occurt -in the :~tat, of
J I II L -S I T d
e xper
confirmed by
I gh~ s on British and Amt~r t --r-t h~- I
in t~ -1 ri r T p t
~f the rotor Ln e ri - fiv
sra~e begln~ when rhp

S/535/6i/ooo/-I",2/003/003
In il-e,;i. i Qa t ion of ver t 1,_3 I E191/Eq8i
the dis, is directed upwards, A pattern c," flt~t,
h~i - cj - i r- i ~ ti; of Lh-Ls -ondiLion is sugge~tecl, Tfi,~ t (; r'-I ~hru6
cWlli-,.~,Zed Of L%,;-O pirts, one due to the influx of a~SOI--la'.ed
of iir irito the slipstream and the othei part due to tli~
ex-han-ce of momentum with the main slipstream passing 'hroi;~gh ~IIE
di-i,:- The development of this assumption iS shown to lea:1
on a za 1 n to relations between velocities whi,h agree ,ell t.,~ith
experimental results- On the basis of' the heortez~ -~.() dt-s~ribed
the aerodviazimic- characteristics (thrust and torque . oefficients)
ar-- derL%ed. for vertical descent stateS, A deri,ar.ion ~- given
Cor -:oriiputing the vertical descent of a helicopter a! n3rtLal
a 111t. f- A fantily of curves, each for a -- e:- t a i n d i. 0a di. ng
relato-z he velocity of descent to the per--entage of Ii-i(.-er-ng
p o w At a disc loading of about 3 lb/ft2 at r a t e cf deScent
of 30 fps is reached already at 8030' of holrer ing powe.- I The
autc-roto t ion of a helicopter rotor with jet engines- nea r the
blade tips is examined by the method of the chara - bladc
t i on It i-s shown that the assumption of a ~hara. #.-sr L-Q~i-
e T I o I Ia r 705o of the blade radius is ~,ali-d also in aul-orot;.~, t ion
C.-) r d 3

s/53=/61 /'000/142/003/003
n --.- c- zs t 1 ~~; i i ti- on D f v e r 1~ I _- a I E191/E481
The 1-1 ty of autor,otation is invest igj te,1 for blades %vi th jet
Pu~ian rest s wirli. models have ~11L~ble aW -;t olat ;ort
u; n t I ve bla de pi t ch of 8 so thar 9 --in ~.afel~ 1-
-d -,ri -1 full _~-zile rotor- Thp computati(n of h- r,-.1- f
Y I- I _o -t auickrotation is given Lin~l ~urflF~ Fllr a.,~ I
d e r I The drag c.oef f i, ien, ut th~ r c- or- 1-1
t I I aut of u~a t= I e dv, s -_ Pnt 1 s comput ed rin-1 q I .-n E)
T*,-,e I rig :.I .-, h-2 I Dp t er- by sudden in-, r e.) t
3 11 Of Ota t Lve desc ent i t~xatnin,
11-'! file .~T _~vlnd III
1 1k I on f i~,r a landing f rom ver r I ii
t 1) r ~ !_i i h;:- t %,;t~ en I-- !~inet I, energy of the r : lie
:n~ i r f 1,il`lding ~an be T! t
I - t 1 o a z; a f un c t Ion t; f t: 1 ? .
t r ~ 1 - 1) 1., de s e - ~ i on I S S I e-i r a h e
j the blade t p ~
t~ angine at nd
fi 01_,1_, ~he fOrMer is shown I c w f i
T tranz5f.tion between fLf. ri) aril
In
it. I o rl:i I d Numef I I e
~J 1;" -

S/535A 1/ 000/ 1 if z/003VO03
i o.-i n C. f V(-- r t L - D E 19 1 /E I
ransi t ion periods of 1 olld~, and 'I
1 o:-; ~ e -, c, 't I ~O a n (1 8 5 ni have bec-n -(jmr,u~.e,A f
w-en hovering and steadv state
Th and It tables.
C,-~ I ~-l 5i

69316
S/147/60/000/01/005/ol8
1 o'cooo 1-4000 E191/E581
AUTHOR: Shaydakov, V. I.
TITLE: Thoeti,, _rn-,,s~tigation of the Working of a Lifting
Helicopter Rotor in the State of Vertical Descent
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Aviatsionnaya
tekhnika, 1960, Nr 1, pp 43-51 (USSR)
ABSTRACT: An elementary theory is proposed for the working of a
lifting rotor in vertical descent with engine-on which
includes the vortex ring and windmill states. The
theory is based on the application of the general
theorems of hydrodynamics. In power-on vertical
descent, viscosity forces cannot be ignored. The
induced velocity variation upstream and downstream of
the rotor shows an acceleration towards the rotor,
further acceleration downstream and subsequent
deceleration. Superimposing the descending motion of
absolute velocity
are
the rotor, surfaces of zero
found both above the rotor and underneath the rotor.
Card 1/6 Joining these surfaces around the rotor, an air "body"
Vl(

69316
S/147/60/000/01/005/ol8
E191/E581
Theoretical Investigation of the Working of a Lifting Helicopter
Rotor in the State of Vertical Descent
is obtained surrounded by the relative approach flow.
The drag of this "body" is expressed in the usual way,
based on a drag coefficient and the cross-section of
the air "body". The rotor slipstream opposes this drag
by an equal drag. The power to overcome this
slipstream drag is supplied by the rotor. The total
rotor lift is the sum of the drag opposing that of the
air "body" and the reaction due to the impulse created
in the circulating flow inside the "body". In the
analytical expression for the total lift, the assumptions
are made that the velocity distributions are uniform
across the disc and in the region of deceleration of the
slipstream its energy is entirely converted into heat
so that the pressure remains constant. It is shown that
the absolute velocity in the rotor is half the absolute
velocity in the throat of the slipstream. Certain
considerations lead to the assumption that the drag
c
Card 2/6 coefficient of the air "body" reduced to the rotor dis ~)r

'09316
s/147/60/000i'01/005/oi8
E191/E58i
Theoretical Investigation of the Working of a Lifting Helicopter
Rotor in the State of Vertical Descent
velocity is large so that the retarded velocity is much
smaller than the velocity of approach, turbulent
conditions exist (roughly so long as the induced velocity
is more than half tile velocity of descent). Otherwise,
an orderly flow prevails. In the computation of the
total: rotor thrust, a cross-section of the rotor wake
above the rotor is chosen, where the absolute velocity
is a minimum, The induced velocity at this point is
expressed by a formula, due to Sabinin, G.Kh. ("Theory
of the Ideal Windmill", Trudy TsAGI, Issue 32, 1927)-
By this formula, this terminal induced velocity is
less than twice the induced velocity in the rotor disc
itself. The reduction factor is larger than unity
by the ratio of the induced velocity in the disc to the
velocity of descent. With these assumptions, the
absolute velocities and the induced velocities are
Card 4/6 computed. Their comparison with other investigations

69316
s/147/60/000/01/005/ol8
E191/E58i
Theoretical Investigation of the Working of a Lifting Helicopter
Rotor in the State of Vertical Descent
shown to be inversely proportional to the velocity in
the rotor plane and directly proportional to the velocity
of descent. This derivative is in fact the rate of
change of profile loss power with respect to the velocity
of descent. Since this rate of change is small,
instability occurs at small rates of descent. This
limit of in5tability is stated to have been observed in
the experiments of Stewart and the loss of control
experienced by many helicopters.
There are 6 figures and 4 references, 2 of which are
Soviet and 2 English.
ASSOCIATIONz Kafedra C-2, Moskovskiy aviatsionnyy institur
(Chair S-2, Moscow Aviation Institute)
SUBMITTEDz April 14, 1959
Card 6/6

Bo,)59
S/147/60/000/02/00':!/020
E191/E48i
AUTHOR. Qaydakov, V.I.
TITLE-. The Effect of the Depth of Fan Position in a Ring
Duct on the-Aerodynamic Froperties of the System under
Hovering Conditions I
k,ERIODICAL, Izvestiya vysshikh uchebnykh zavedeniy, A-iatsionnaya
tekhnika,, 1960, Nr 2, pp 22-30 (USSR)
ABSTRACT-, A ducted fan~-"operating as a flying platform is examined
with a deep ring duct having a flared entry of senii-
circular profile. Ideal fluid, uniform distribution of
velocity across the fan disc and an absence of losses
due to tangential velocity components are assumed. The
total thrust is the sum of the fan thrust and the ring
thrust., In an earlier analysis of a ducted fan with a
shallow ring duct, the ring thrust was expressed as the
product of the mass flow and the velocity in the fan
disc multiplied by a factor. This factor is plotted in
Fig 3 as a function of the ratio of the flare radius
to the fan radius (relative flare radius)- The factor
is unity when the ratio is zero. The curve for a deep
duct lies below that for a shallow duct,, When the ratio
Card 1/4 1-; 0~2; the factor for the deer) (11-t is C.-.6 and f'cr the

80959
s/147/60/000/02/003/020
E191/E481
The Effect of the Depth of Fan Position in a Ring Duct on the
Aerodynamic Properties of the System under Hovering Conditions
shallow duct 0.72. Comparing the thrust of an
unshrounded free propeller with that of a ducted fail of
the same diameter, Fig 4 shows the ratio of thrusts
against the relative flare radius for the same power
input. As the flare radius increases, the thrust of
the ducted fan increases towards a limit of 1.26.
In the case of a shallow duct, the ducted fan thrust
for zero flare radius (plain tube) is tile same as that
of the unshrouded propeller, but the thrust of the fan
in a deep tube is 80% of the free propeller. When the
profile losses and the tip losses of the fan are taken
into account., the lifting efficiencies of the free
propeller and the ducted fan are compared. Fig 5 shows
tile ratio of tile ducted fan to tile free propeller
efficiencies plotted against the relative flare radius
for different free propeller efficiencies, both for di~ep
and shallow ducts, At a flare radius of 0.15: a free
px-opeller with an effi-clency of 0.-7 gains 16% in
Card 2/4 efficiency when pla,:.ed in a deep duct and 10*i~ in a

8095~
s/147/60/000/02/003/020
E191/E481
The Effect of the Depth of Fan Position in a Ring Duct on the
Acrodynamic Properties of the System under Hovering Conditions
shallow duct, Fig 6 shows the ratio of thrusts of a
ducted fan and a free propeller plotted against the
relative flare radius when the free propeller
efficiency is 0.7, and the same power is absorbed.
The curves for both deep and shallow ducts tend to a
limit of 1.4. Below a relative flare radiusof 0.15,
the shallow duct gives more thrust and above this flare
radius, less thrust than the deep duct. When the thrust
of the ducted fan is compared wxth that of a free
propeller, of the same diameter as the outside diameter
of the duct flare (equivalent propeller), the ratio of
thrusts is plotted in Fig 7 agaInst the relat3-ve flare
radius, In the range of radii between 0.15 and 0.4,
the ducted fan develops the same thrust as the
equivalent propeller,, Outside this range the ducted
fan has a sinaller thrust. Experiments were carried out
at the Moscow Aviation Institute with four-bladed single
and contrarotating aircraft propellers, The slipstream
Card 3/4 had almost no contraction when the flare had a lemniscate

r-'ILP.YD,I,K(;V . '! - 1 ~ , kand. tekh n - nauk
1-n-vestigating ccnditicns of the vertical de6-ent of a
helicopter. Trudy MAI nc.lUj2::Sl- *!Al 161. (,T-IIRA 14:12)
(Heli

TUR'YEV, Boris Nilcolayevich, akademik [deceased]; LESNIKOVA, N.P..,
kand. tek-hn. nauk; SHAYDAKOVA, V.I., kand. tekhn. nauk;
ARTOBOIEVSKXY, I.I., akadernik, otv. red.; BRATUI99N, I.P.,
prof., zam otv. red.; GORSHKOV, G.B.9 red. izd-va; LAbT, V.G.,
tekbn. -red.
[Selected works] Izbrannye trudy. Moskva, Izd-vo Akad.nauk
SSSR. Vol.l. [Propellers, helicopters] Vozdushnye vinty. Verto-
lety. 1961. 551 P. (MIRA 15:1)
(Propellers) (Helicopters)

ACC NR: AP6030250 SOURCE CODE: uR/0147/66/000/003/0043/0049
AUTHOR: 5haydakov, V. I.
ORG: none
TITLE: Application of the method of ring vortices to aerodynamic design of lifting
rotor systems I-P
SOURCE: IVUZ. Avintsionnaya tekhnika, no. 3, 1966, 43-49
TOPIC TAGS: aerodynamics, aerodynamic design, aerodynamic lift, vortex flow, heli-
copter rotor, helicopter, circulatory flow
ABSTRACT: The method of ring vortices, as it is called by the author, used for
aerodynamic calculations of lifting rotor systems in axial and oblique flows is
described. It yields the same accuracy as ideal rotor theory and is intended for
investigating the regime of steep descent of an helicopter in the first approximation.
'This method uses the Zhukovskiy formula for lift of an airfoil and consists in sub-
stituting the vortex cylinder produced by the rotor by a system of discrete ring vor-
tices which is equivalent to the decomposition of a vortex cylinder into ring and
longitudinal vortices used in the vortex theory of rotors. The longitudinal vortices
are neglected here. The effect of nonlinearity of the axis of the vortex cylinder on
the inductive velocity of the rotor is evaluated and found to be less than 2.4%. This
Card 1/2 UDC: 533.695

L L3761-66
method may be used for rotors with variable circulation along the radius. Orig. art.
has: 4 figures and 24 formulas. -(ABI
SUB CODE:O/ SUBM DATE: 03Mar65/ ORIC REF: 007/ ATD PRESS: 5076
atm j
L,3
Card 2/2

, ~: 1 ,, Y *." A 1: (, ~' . " , . : .
~ ( , ';%,F..l of ', r. `Iur~ rug ef!*ect of 13 -1 rrad~ ati on )!' i" 9~d
i i
-1-ol. see-is with t~,e help of physiologically act4ve comp-olinds.
k-,,)sin. t4-ol. 1-:469-473 165. 1
(PaRA 18:9)

T3V-F,TKOVA, a' V . ; ~ Y:i. I. ~ il i~-)YJA , V . M.
Cherricterist-I.,!F of ttr- nmtd t-1-7 ol plarit3 prawn dn an air
.1 U I
culture for a closed sy-cv~mi, I'volvib kosm~ hdol, 4,670-
675 165. (MIRA 18:9)

1112-94-66 EWT(M)/EPF(n)-2 GGIRD
ACC NR: AT6003881 SOURCE CODE: UR/2865/65/004/000/0469/0473
AUTHOR: Shaydarov, Yu. 1.
ORG: none
TITLE: Elimination of the injurious effects of beta-radiation on the seeds of
cultivated plants by means of physiologicaUy active compounds
SOURCE: AN SSSR. Otdeleniye biologicheskikh nauk. Problemy kosmicheskoy biologii,
v. 4, 1965o 469-473
TOPIC TAGS: beta radiation, radiation plant effect, plant genetics, plant growth,
phosphorus, radioisotope, agriculture crop
ABSTRACT: All form's- of i6nizing radiation characteristically depress the gr.owth
and development of plants. This work investigates chemical means of
eliminating the injurious effect of increased doses of P-radiation on
.seeds of corn, lupine, turnip, and spring wheat. Radioactive phosphorus
p32 was the A-radiation source. The following preparations were used as
XY-
protective agents: N -(2-pyridy1)-N4-(2"-bydro V, 4"-naphthoquinon)-
'4-ylsulfanilamide (designated P-46); di- (para- trichloroacetylaminophenyl)
-sulfone; and 2-ketbnonanoic acid. Half of the seeds were soaked for 2 days
Card 113

L 14294-66
ACC 14R: AT6003881
in a solutioii of radioactive phosphorus, lightly dried, and then soaked in
a 0. 01% solution of the preparations for 2 days. The other half were-kept
in the preparation solutions for 4 days. Seeds soaked in water served as
the-control. All seeds were then grown in normal soil.
Treatment of corn seeds with radioactive phosphorus lowered the
weight of the green mass of corn plants. However, application of the
preparations not only eliminated the injurious radiation effect but even
increased the harvest as compared with the control. Under these
conditions lupine was -less responsive than corn to the effects of either
ionizing radiation or the preparations. p32 clearly exerted a negative
influence on spring wheat seeds, and the preparations had the
opposite effect. Most effective in this case was P.-46, which signifi-
cantly but not completely decreased the injurious effect of radioactive
phosphorus on wheat seeds.
To study the aftereffects of treatment with radioactive phosphorus
and P-46, seeds obtained from treated wheat plants were sown.the following
year. It was found that the harmful effects of ionizing radiation are re-
Card 2/3

L 14293-66
ACC NR: AT6003877
and also the absence of a significant change in the intensity of metabolic
ndicate, that Ionizing radiation,. in the dose used, does not
'processes,
damage oxidizing systems in the tissues. Orig. art..has: 3 figures.
[ATD PRESS: 4091-F]
SUB CODE: 06 SUBM DATE: none CRIG REF: 008 OTH REF: 008

L 14258-66 M
ACC NR: AT6oo3go6 SOUECE CODEt UR/2865/65/004/000/0670/0675
AUTHOR& Tivetkove, 1. V.; Sh -Yu. I.; Abramova, V. M.
37
ORG: none
:TITLE- Special features of plant feeding under conditions of aeropo;-d:c extivation:;
for a closed system
,SOURCKI- AN SSSR. Otdeleniye biologicheskik# nauk. Probleagr kosmicheskoy
.biologii, v. 4, 1965, 670-675
TOPIC TAGS: aeroponics, plant physiolog~r, metabolic waste, fertilizer, sodium
J chloride, closed ecology system,-test chamber, toxicology, excretion, plant-growth
ABSTRACT: In order to grow higher plants in closed ecological systems it is nec-
essary to use -mineralized products of human wastes. The danger of this
procedure stems from the presence of excessive amounts of NaCl in min-
eralizedwastes. In order to. evaluate the hazard of NaC1 toxicity, experi-
Pents were performed at the Artificial Climate Station of the Institute of
:Plant Physiology of the Academy of Sciences, USSR. For this purpose
Cardl/3

L 14258-66
~ACC NR: AT60039o6
sprouts of Chinese cabbage were grown aeroponically. Their roots, Sus-
pended in air in a closed compartment, were automatically sprayed mrith
nutrient solutions for 30 see every 20 min. Acroponics, with its absence
of a substrate, has weight-saving advantages for spaceflight purposes.
Three types of nutrient solutions were us:~d: a normal solution without
additional salts, the same with NaCl added (0. 02-2. 016 Cl ions), and solu-
,tions composed of mineralized products of human metabolism to which
corrective-.amouhts of nitrogen, phosphorus, and calcium were added. The
.:pH of the solution was maintained at 5. 8. The temperature of the chamber
,.ranged from 20 to 25C, _the humidity from 70 ~tcl 8016.
Not only did the us Iiiineraliz-e-d- hu-m an wa�tes not- hav-d any- toxic
effects, but it brought about a stimulation of growth, as indicated by a
higher rate of absorption of basic elements of mineral nutrition. On the
other hand, the standard nutrient solution used turned out to have toxic
:properties. But nutrient solutions to whf ch up to 0. Ila NaCl had been added
did not manifest toxic properties. Apparently, the presence of NaCl in the
nutrient solution prevents the accumulation of soluble toxic products of the
Card 2/3

L 2.4-258-66
ACC NRi A%omo6
root metabolism or those of the microflor a. The addition of NaCI to the
:mineral nutrient solution caused a sharp increase in absorption of sodium
and chlorine ions by the plant. Additions of NaCI of up to 2% did not have
any adverse effects on plant growth. On the contrary, the addition of NaCI
to the nutrient solution caused a significant increase in the raw weight of
the plant although the dry weight was approximately equal to that of plants
grown on nutrient solutionwithout addifioaal NaCl. Apparently, the addi-
tion of NaC1 causes the plant cells to absorb more water, resulting in
extra succulence.
'-Plants grown aeroponically have been-sho'wn to possess a higher
degree of resistance to salt, apparently t ecause of better aeration and
water supply of the root systems. Tests have indicated that even signifi-
cant concentrations of chlorine in aeropottic culture do not have a toxic
effect on the plants. Cons equ ently, the high amount of chlorides in the
mineralized products of human metabolism will not 'result in death of the i
-_ i * ' - I
plants, provided they are grown aeroponi--ally.;' brig. art. has-5 tables.*
fACTD~ PRESSi 4091
suBj com o6 fs~UBM_
DATE: none 0 UG REF: 010 OTH REF: 005
3/3

VIASOVI I.I., kando istor. nauk, dots.; ABEYDULLU], S.K., kand,, ist.nauk'.
dots, polkovnik; KOVAlEV, S.S.', kand. ist.nauk., dots.~; polkaynik,
SPAYDAY7-,_- M.G,-. kand. ist.nai~:.9 dotts., polkovnik; SHCHEDRUNOVq
V.F.., kand. ist.nauk, dots.,- CIEBUSHEV, I,V-,, polIlcovnik. red.;
KUZIMIL, I.F,. tekhn. red.
[Party and political work in the Soviet Armed Forces; a textbook for
r.ilitary schools] Partiino-politicheskaia rabota v Vooruzhennykh Si--
lakh SSSR; uchebnoe posobie dJia voennykh uchilishch. Moskva,. Voen.
izd-vo M-va oborony SSSR, 1961- 294 P. (MIRA 14'~~12)
(:Iussia,4rmd Foices-Political activity)

SHAYDATEVA, T.A.
Qjia(lrature formulas with leas-, remainder estimate for certain classes
of functions. Trudy mat. inst, 53:313-341 '59. (MITU 12:9)
(Calculus, Inte,-,ral)

-JIIAYI)F,NKO, A.
A book about an exceptional lussian gun deeigner("Designer
S.I.Mosin" by V.N.Asburkov. levieved by A.Shaidanko). Voen.
znan. 25 no.9:24 S 149. (MIRI,. 12:12)
(Mosin, Sorgoi Ivanovich, 1849-1902)
(Ashurkov. V.N.)

n n
-10 -r:

S/003/60/000/307/0012/002
B023/BO77
AUTHORS: Petrukhin, S. S., Shaydenko, A. Ya., Candidates of Technical
Sciences, Docents ------
TITLE: Intercollegiate s::ientific conference
PERIODICAL: Vestnik vysshey shkoly, no~ 7, 1960, 40-43
TEXT: In a number of technical institutes (the MVTU, the Moskovskiy
energeticheskiy institut (Moscow Power Engineering Institute), Moskovskiy
avtomek.~anicheskiy institut (Moscow Automechanical Institute), Moskovskiy
Stank,)-instrumentallnyy institut (Moscow Institute of Machine Tools and
Instruments), the Tullskiy mekhanicheskiy institut (Tula Mechanical
Institute), the Odessa, Tomsk and Donets politekhnicheskiy institut
(Polytechnic Institutes), the Moskovskiy institut. stali (Moscow Steel
Institute), the Khar1kov, Tula and Sverdlovsk gornyy institut (Mining
Institutes), the Vsesoyuznyy zaochnyy energeticheskiy institut (All-Union
Correspondence Power Engineering Institute) research has already yielded
important results, By the order of the Ministerstvo vysshego i srednego
spetsiallnogo obrazovaniya. RSFSR (Ministry of Higher and Specialized
Card !/5

Intercollegiate scientific conference S/00 60/000/007/002/002
B023YB077
Secondary Education of the Russian Socialist Federative Soviet Republic)
an intercollegiate scientific conference was held in Tula on automation
' production and on automatic machines, 350 conference participants
:n U
representing 76 industrial organizations and institutes in Moscow,
Leningrad, Khar1kov, Novosibirsk, Gor1kiy, Chelyabinsk, Penza, Sverdlovsk,
Vladivostok, Kiyev, Perm', Rostov and other cities were present. The
participants worked in six sections- Over 60 lectures were given. 115
persons took part in the discussion which followed, S. I. Artobolevskiy,
Doctor of Technical Sciences, Professor lectured on "Theoretical princip-
les of comprehensive automation of production processes", D. V. Charnko
(Moscow Institute of Machine Tools and Instruments) spoke on "The
structural system of the development of technological operations and its
principles", B. M. Podchufarov, Candidate of Technical Sciences, Docent
(Tula Mechanical Institute) lectured on "Dynamics of the cyclic automa-
tion", A. A, Andronov, Academician spoke on dynamics of machines in
g,--~nerai, as f-,)und in studies of cyclic automation, L. N. Koshkin,
Candidate of Technical Sciences, Docent, 'Lectured on "Automation of
produ.ct:on methods, based on rotor lines".. At the Odessa Polysechni~
Card 2,15

I rite rco 111e ic i en t if i4c c--rif erence S/003/60/000/007/002/002
B023/BO77
Institute under A. P. Voloshchenko, Candidate of Technical Sciences,
Docent, studies are being conducted aiming at the analysis of the theory
of mass operation. V. F. Preys, Candidate of Technical Sciences,
Docent at the Tula Mechanical Institute spoke on bunker charging of
automatic assembly lines, Results of studies of automatic rotor machines
(constructed by L. N. Koshkin) were discussed by I. A. Klusov and
V. F. Preys, both instructors, Candidates of Technical Sciences
(Kafedra "Oborudovaniye shtampovochnogo proizdvodstvall (Department for
"Equipment for Stamping Production")). Ye. N. Frolovich, Aspirant,
spoke on automation based on rotor lines in the field of synthetic
products. A. I. Zimin, Doctor of Technical Sciences, Professor, and
A. S. Yezzhev, Engineer, (MVTU) reported on problems in 'the automation of
synthetic pressings. I. M. Kratenko, delegate of the Tula economic
administrative rayon reported on the mechanized protection devices in the
mines of "Tulaugol" Combine. The studies of the Department of Calcula- I/
tion and Construction of Mining Machines of the Tula Mechanical Institute,
conducted in cooperation with Kopeyskiy mashinostroitellnyy zavod
(Kopeysk Machine Building Factory), were discussed. Furthermore, the
results of the studies of the Sverdlovsk gornyy institut (Sverdlovsk
Card 3/5

Intercollegiate scientific conference S1100316010001007/0021002
B023/BO77
Mining Institute), Donetskiy politekhnicheskiy institut (Donets Poly-
technic Institute), Tula Mechanical Institute, Gornyy Novocherkasskiy
politekhnicheskiy institut (Novocherkassk Polytechnic Institute of
Mining) and of the Institut Ukr NIIPROYERT Gosplana UkrSSR were checked
with respect to automation, V. N, Podurayev, Candidate of Technical
Sciences, Docent~ talked on "Vibration loops of metals in automatic
productlon lines and automatic workbenches". I. A. Koganov, Candidate
of Technical Sciences, Docent, (Tula Mee-: 4'cal Institute) treated a
similar subject- At the last general meetag 0. A- Chukanov, Docent,
Secretary of the Tullskiy obkom KPSS (Tula District Committee cf the
OPSU) lectured on the possibilities of automation and mechanization of
the Tula raycn, A resolution established that the success does not
fully sa?,igfv 'he daily needs- There are not enough laborator:es and
Construct4ve s-_,ggestions
--'Killed -.,torkers all the district institutes,
were made by E: A. Satelf, Doctor of Technical So-lences, Professor;
B~ S. Balak-shin, Doctor of Technical Sciences, Professor. The delegates
decided 1) to improve the training of engineers in this f_4eld; 2) the
Ministry of Higher and Secondary Specialized Education will be -asked t,-
Card 4/5

Intercollo6iate scipntific conference S/003/60/000i"--1,371/00 2/0C
B023/3077
convene a methodical conference to check all problems concerning 1.1,i2
subject, On the day the conference started all participants a
special edition of the magazine "About Manpower". (Chiei Editor
0. N. Vinogradov). It contains contributions of the Director of the
Institute, S. S, Petrukhin, Candidate of Technical Sciences, Docent,
Al, A. Yamontov, Ya, M. Khaymovich~ Professor, M; I., Slobr'dkin, Doctor
of Technical Sciences, S. A. Ragozin, Candidate of Technical Sciences,
Docent, I. A, Klusov, B. M. Podchufarov, both Candidates of Technical
Sciences, and A. Ya- Shaydenko, Candidate of Technical Sciences, Docent.
ASSOCIATION: Tul'skiy mekhanicheskiy institut (Tula Merhanical Institute)
Card 5/5

ALITMAN, M.Z.; SHAYDERMAN, A.L.
Floating vibration-damping collar plate. StanA Instr. 31 no. U:
38 N 160. (MIU 13:11)
(Lathee--Attachments)

,SfLAYD-4N1()V, B.~I,.. redaktor; NAGORNTY A.A., redal-tor; SAVINA, Z.A.,
r ; POLOSINA, A.S., tokhnichaskiy redaktor.
[Results of operating and maintaining equipment in the petroleum
industry; based on data of a meeting of chief engineers of the
Ministry of the Petroleum Industry] Opyt ekspluatatsii i renonta
obortidovaniia v neftianoi promyshlennosti I remont oborudovaniia
v neftianoi promyshlennosti; po materialari soveshcbaniia glavnykh
mekhanikov Ministerstva neftianoi promyshlennosti 15-22 aprelia
1952 g. Moskva, Gos.nauchno-tak-hn.izd-vo neftianoi i gorno-
tnplivnoi lit-ry, N53. 299 p. (MLRA 8:11)
1. Vspsoiuzwye nauchnoye inzhenerno-tekhnicheskoye obshchestvo
nPf t;ranikov.
(Petrolewm industrv--Eqnipment and supplies)

SHAYIEROV, B.M.; TUDOLOVIGH, M.Ya.
[Oil-field mechanic's handbookJ Spravochnik mekhanika neftepromyslov.
Sostavili B.M.Shaiderov i M.IA.lUdolovich. Vol.2. LDrilling] Burenie.
Moskva, Gos. na-achno-tekhnicheekoe izd-vo neftianoi i gornotoplivnoi
lit-ry. 1953. 539 P. (MLRA 7:2)
(Petroleum--Well boring)

GAYVOROIISKIY, A.A.; SHAYDIMOV. B.M.
ClassificaTion- of-a~b-a~orption zones. Neft.khoz.34 no-7:15-18 JI '56.
(Oil wall camentinc) (KLRA 9-10)

NAGORNTY, Aleksey Afanaslyevich, MALYSHEV, Konstantin Nikolayevich;
redaktor; BBXXAN, Yu.K., vedushchiy redaktor:
~W
TRGFIMOV. i.T.. te-hnicheskiy redaktor
[Organization of preventive repair of equipment used in the
petroleum industry; a reference manual] OrganizatBila planovo-
predupIreditellnogo remonta neftepromyslovogo oborudovantia;
spravochnik. Moskva, dos.zisuchno-tekhn. izd-vo neft. i gorno-
tiplivnoi lit-ry, 1957. 269 p. (MLRA 10:7).
(Petroleum industry--Equipment and supplies)

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ACC NR, AP6033448 SOURCE CODE: UR/0413/66/000/018/0028/0029
INVENTOR: Arkad'yev, V. I.; Shayderov, V. A.
ORG: none
TITLE: Device for introducing solid inhibitors into oil. Class 12, No. 185849
SOURCE': Izobreteniya, promyshlennyye obraztsy, tovarnyye znaki, no. 18, 1966,
28-29
TOPIC TAGS: lubricating oil, propellant inhibitor, oil inhibitor
An Author Curtificate has been issued describing a device for intro-
ducing, Solid hillibitors inte) oil. It has a body with intalke and outlet connec ing
pipes and a mA. T(--) incrcase Qic inhi-bitor interaction with tile oil, to impr ve
Liie fine, dispersion of Lhe inhibiLor in 'the oil, and to' prevent the deposition of resin
on ltnt2 il-ilhI'lii'Lor surface, Lhe connecting pipe for lead in oil is fastened to the body I
tangen'Lially and -is provided with a nozzle, while the connecting outlet pipe is
proLecte.d by a beaker and net (see Fig. 1). Orig. art. has: I figure. [Translation
-Card---l-/-2 UDC: 67-8.-053. 3:66. 097. 7