FOIA
SCIENTIFIC ABSTRACT FR:BOLSHAKOV, A.S. TO:ZAZHIGIN, V.V.
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP86-00513R001964100003-6
Release Decision:
RIF
Original Classification:
U
Document Page Count:
99
Document Creation Date:
November 2, 2016
Sequence Number:
3
Case Number:
Publication Date:
December 31, 1967
Content Type:
SCIENTIFIC ABSTR
File:
| Attachment | Size |
|---|---|
 CIA-RDP86-00513R001964100003-6.pdf | 4.78 MB |
Body:
UpL~~pV, Anato~.iy Stepauvv'~,ch; S1t~~N, Va7~e~r~,y i~var~o~vich;
S~V'AYHSHTL~YP~, Boris 3~onovioh; FOttt~~:iEV, ~'.5., inxb.,
rdt~dn~e~~; ZA~~V~T~.~,,f iri~h.~ ret~dnxent; -'.~m".ARGV,
M.S. ~ ~.nzh. ~ rae~i~d~~t; ~'a~#~' j C.V. ~ ~.~~h. ~ ~~dt~dr~~;~r~t;
~U~'hAfi4V, ~..I. y 1`~Gt88n~-Ylt; 14T~'A"~$~'A, ~i,A. , 4n7ih. ,
retsenzdnt; SDOI3~t~OV, Yt:. F, , rdteen~ent; lipVALEV, A. K, ,
inxh., rdtslenzdnt; ~{L: AR~~Y, ~ rP. ~ inch., retsenzent;
~ KIS~LE"f1A, N.p., ~.nzh., r~sd.; C~.Ot~aV, S.A., kend. tekhn.
Weak, grad.; SHC~~tB~CHEV;~C~i, G.S. ~ ~.n~h., rid.; US~`tKQ, L.A. ,
tdkbn. add.
[Shunting di�sel locomotives]Manavrovye teplovozy. Moskva,
1962. 3g3 p� (MIl3A 1.5:6
(D9.Irad1 locomotives)
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AUTHORS
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~a~arr~k~y~~.,~� ~�; Shivxin, 0. N.
~asaiq etruoture of metallic polyaryatal~- and extinatian exfeate. ~
~'~. ~iz~.}~ca, no. 6, 193, ~5~9~ ,
~ 20FIC TAGSs extinction effeot, mi.arogxanularet omain ~ x-rsy irradiation,
powder, radiograpk~,y, diffraatometE~r, c,oh@renc d
aoaree
j 1~5T."t11CT; The extinction effeot ~.n ooarse and miorogranular tunggtEn powder under
The coarse povrder averaged
copper and molybdenum x-ray irradiation was studied.
0.2M0.~~ curt in sire, ~vhereas the fine specimen had a mean size of 10~u � Plane
s eaimens were prepared from both types of powders with B~'~2 bond, and~ae radi-
. p
o~Ap~y was oarri.ed out on diffraatameter UR5-50-1 in filtered coppe
m~o~ybdenum. ~'ha measurements ind;lasts mat the aaeheerwi~he~ deoe ass i~s~adiation
evaluated .from prir~arY exoitatian affects, deaarea
wave: lex~gth� Measurements on the miorogranular powder, however, show a very creak
extinatian from both Cu- and ~fo~r,a;diationg, ` Fund even with a nonuniform coherenaa
i doa~a,i.n the ~esu7.ta do not Shaw ;the expected values. Renae, on],y a general
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US~Ch~mical. ~echzi�~1ogy ~ Ct~.~n3c~1~ T'rt~du~~~ anc~ '~~i,e~.r App1.~.~at~~.ari, ~+x~niet-~ak:lr,rr
Industry, I~27
Abet 3ourba:ls Referat Zbw.~ - Kh.�m~.ya, .Ho 19, 1956, 63559
Authoxs Mal'teev, P. M., 7~zirnaya., M. V., Velikaya, Ye. I., Vyal'ko, Ye. F.
4
xnstit~utirn~ t None
Titles Effects of Separat3.on on ~ual.itative Composition of Beer Wort
Ux~~,gina:l
Periad~,ca:~s Tx. Kievsk. takhnal. in~ta p~,shchevoy prom-s't~., ~.9~3, No 1.3, l.G~.-x,05
Abstracts Studies of qualitative changes in turbid beer wont on y�minute centri-
fugatian in laboratory pr~rclpitation centrifuge at 2,OOQ RPM. The
~deac~+s thur~ abtaixred are compaxed with these of Glean wort (CW) col
lected From outlet of f~.lter-preen after fil.tratian off' turbid. liquar
tthat was cc~acurrentlye,,,/ub,.~e^tct�~edr~toy eejp~arya~t~,on. tt1R~.e,,s,~tdue of.pinaoluble~ae
/ir~~~~ t~ wa~~ th~ ~~Q~ ~ytj~.~tJ ,{p/.Wl"'Vs1J~ 45! ~.tl1J m~r ,LU,[b.6L4g1a~i~/,po.L y~Qp~~~atCTLi
lsli ~1.~~~or~t ~ t~~~ 1.~ie~ UiL~~ to ~~.'~ ~wQ~Qp~~~ ~~~.~.1~J. ~.`Qol.~,o~de ~3o~ih
pr~.ar to and aftex hop treatment oP the wort . Color and pH of C'W are
the same. Protein content and dextrin content of CW arP practically
the same.
Caxd l~~~l
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i~ e~~a~~~tEld by the au~thcr ghat ran nvae s~~g~:~~:~ng ~, g~.ver~ ~ta~~ ~~.th
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~au1d b~ abta~.ned~ H~'uvevFax� ~h~ c~~t7an~i~ta~~v~ p~~~r~~c rr.P ~rhe in~e~ti~*a~~
t:~.an ~ihau.ld x~~nt~.~n bart~rh~~nga~h~
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23950
s/o9b/fi l/ooo/ooh/o01/00;,
>~x94/1rx55
An experimental study of a radial compressor stage with ~~ new
type off` spa.ral guide vane
somewhe~t the Compressor stage slhou~.ri operate stabl~- over a wide
range ~r~' f~,ow w~,th ,~n eff~.ci.en~,y of ab+~t~t ~1~~9U~i, 'I'ha design
des~r~lbi~d i~ pa.t~~~.r.ul.~r:l~y sua.tct;ly:l,~ tt~~' s~t~g~,e-stage cc~ruj,rcjt~r~~~~~s~
The guide vane assembly for multi-stage compressors will require
speci$~. adjusting devices whatch may be similar in design to that
described here.
There s~,e ~ 1~`~.guxes,
ASSI~CIA7C~ON: Krymskiy pedagogi.clieskiy insf;itut
(Crimean Fedagog~.cfil Tnatitute)
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23950
S/o9b/6 ~./ooc~/t~c~~/ool/005
E194/E355
An experimental. study of a rr~di.al compressor stage with a new
type of spiral guide vane
concerned with the design. and study of the discharge guide vane
equipment, interest centred upon the dowcalled two-.ink cvmpressvr
stage cc>nsi.sting of an inlet duct rr~.nrier aricl discharge guide vane
ey~tem. Test resix~,ts with tw~M aracl three-linlc s#~ages ~irtr jit.r~t~~~d
in ~"igs� ~ and ~. ~`ig.~ gives the statl.a tieacl as a f~xiictJ.aii c,i" t1YC~
dischar~se factor, and ~ig.3 the efficiency ae a func~tivn of the
discharge factor. The index ~ relates to two-link, and index 3
to threw-la.nk stages. Each curve corre,egonds to ~- certain angle of
blA~de in,~tal~.at~.on during the conduct of the f:eets, The bold
curves correspand to two-link, and the dotted. curves to three-link
e~ta,~e,~. ~,t will be seen that av�r a fairy pride range of t'Iow-
fac~tors high static hez~ds avid effit~iericies are obtained. The
design of the guide vane assembly is still somewhat imperfect and
the header chamber beyond the back guide vane equipment is rather
large. Consequently the efficiency was affected, and the maximum
efficiency of the three-link stage wa,~ not greater than a6~o.
However, the results confirm that when the design has been developed
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/ . a
~3~No
/a~6/Fil/c~u~/~~ts/t~~~/uo1
pn ~�xper~,mental rstudy of a race-a1 cc~rt~p.ressar stage with ~~ new
typle of spiral guide vane
con,igists of the inlet section 7 witlY dowel ~ and mas.n paz�t 9.
The blades swing about the dowels $ wh~e~~bladesnaretrotated key
su~.table apertures in the lawer da.sc. Th
the handle lp and draw bars 11 which are screwed to the main
part of the blade. The construction of a mechanism for simul-
taneous adjustment of all blades is shown in Fig. 12. The equipment
may be designed with any number of adjustable blades. The maximum
number dgpands an thv r.nng+e off' vrariatian of the angle of attach,
rand they am~-~.].sx~ this range i:he g~re~-~'Fer thRa number of l~1.atles. The
experimental equipment wr~:th ad~usl;r~l~1e gu~.~18 vt:~x~r~e was tnste~i can
the rig of the TeKTx (Central ~~oiler and Turbine Institute). Igo
particular difficulties were encountered. The equipment is easy
to aseer~nble and discn+~ntle. pn the basis of previous experience,
l~ guide vanes were used, and lfhe tests ware made at a runr~.er'
speed of 12 OOq r. p. m�: giving a peripheral discharge speed of
16g m/.sec. The air flow wag varied from maxlraum to minimum and
the ra~xge of stables opcratian was ccyvcred. As the work vas m�~~-nly
C~r~ci 2/ 8
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~, .. ;
2395Q
/A9~/~ 1/c~00/oot~/o01/005
AUTkxgR: ~a7~.mka, p. A., Cund:ldnte off:` Technical ac~.ericr~r+
. _.,,..y.e..-
m:tT~;~: An e~c~~ex~~almntxtrxl st~.tdy cif a radial cc~mpres:~or ~ctage
with a nevi ty~-e of spiral guide vane
PER:I~aUTCAL: T~,plo~nergetika, 1~Er1, No.a- PP� 23"z7
TEX^I`: The main losses in radial compressoes thanrratedhe
sta~i;ionary guide ducts and guides vanes. At oth r
conditions the angle of discharge of flow from the runner differs
froaa the angle of installation of the guide vanes, When turbines
are required to operate at vary~.ng loads the characteristics of
the compressor stage may' be improved by arranging for the angle of
ins'~al].ation to be adjustable. Anew design of this kind is
described in the present article. The general view of an $-duct
guide vane system with adjustable blAdes is g�recovering~ disc T1e
aseernbly Consists cif five main parts t an upP a guide 4, and a
a g'~,aped guatde ring ~' aathsclonee'.stsaofsthe~apiral ducts as-bb,
ls~wer d;;i.s c y . The flow P
tkre~ atr~-ight lame diffusers b~--CC and the trans iti.on sections
cc-dd. The constructf.on of a ~:-lade is shown in F~.g.l4+ and
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~7~;~
An eacperiinental investigation of ths, , . ~~~'~~/~~//oa2Jr~c~~/c~o~
A~71A 1~G
The mounting angles of, the blades at the outlet from the wheel changed within the j
litpit,s of 1~+ 9a�. The present article deals with the results of tests on the
step 'with a wheel caf ,q 9Q�. The exper~.mental, data could not confirm tha aasump-
tir~n thd~t ~~he periphe ail s +~ed was av~~~a
p ly distr~.but~ld along the width of the coif-
fueex~, as aCaepted in than calculations . Tnveatigations showed that the flow iTE
the bladel.e:ss diffuser, vrhen working with different types of wheels, is rather com-
plex i~nd depends on the c:ondl.tiot~ of the work of the stage, the stru~:ture of the
flow d9.t tfE1~ outlet of the! wheel, the a:ff'ect of the transient section and the re-
verse~;ly=directing apparatus . The existing method raf ca.lculatian of the bladeless
diffu.iser, base}ci oA the assumption that the flow is uniform at the outlet of the
wheel and in the cro$s~eeations of the diffuser, only oacaeionally offer satisfac-
tory a�esul.ts, corresponding e],osely to the experiments], values , In order to per-
fect ~I,he calculation method, it is suggested aeoumul.ating data on the structure of
the f1.ow in the diffuser cross-sections when ~.n wark, in stages with various types
of reri~ersely directing apparatus and wA~^king wheels. There are $ figures and 1
table,
ASSOC7;ATlq~'; Krym$kiy p�dagogicheskiy ~.nstit~ut ~`.~he Crimean Teacher�s Co:llage~
~U,~MI~!TEUs AprJ.l 5, 196a
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off/ 1~~/~+~~/GC~/4~.~~,/dG6
AtITRDRs Zazimko, D, A� C~didate of Technical Scienoes
Tl~ItiEs An experimelntal investigation of the. flaw structure in aE bladeless
diffuser of the centrifugal compression stage
PE1~Ti~DI:CAL; Energetika, no. 2, 1~1, 79 - 88
T~XTs The author points out that the structure of the flaw in the diffuser
~.ep~nds can thb fdllowing factors; ~torking conditions of .the stage and tape of
working wheel., the relation of ahantiel width of the diffuser bd to the width of
the ,work~~t~ wheel. b et the outlet, th� design of the transitional section of the
diff~czser, An inveg~igation was carried out at constant peripheral, speed u~ at the
outl,~~t a~` the wheel and within a wide range of the field consumption of full and
stat:~.c pressures, rates and flow angles in several cross-sections of the diffuser.
A ntu~ber of compressor stages were tested (Fig, 1). Each stage consisted of a suc-
tion funnel 1, bladeless diffuser 3, reverse direction apparatus ~, collection
eham'k~er ~, pumping pipe line with a throttle valve and various tapes of working
wheels 2. The working wheels had the ~sa~~ne inlet rl and outlet r~ radii. Some of
the wheels had the same angle of the blade mounting at the inlet ~1, equal to ~+0�.
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APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138001964100003-6
APPROVED FOR RELEASE: 06/23/11: CIA-R~P86-OO5'13ROO1964'1OOOO3-6
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APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138001964100003-6
APPROVED FOR RELEASE: 06/23/11: CIA-R~P86-005138001964100003-6
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APPROVED FOR RELEASE. 06/23/11 CIA-RDP86-005138001964100003-6
APPROVED FOR RELEASE: 06/23/'1'1: CIA-R~P86-005'1 3 8001 9649 00003-6
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