SCIENTIFIC ABSTRACT SHATER, YU.G. - SHATILIN A.L.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001548710017-7
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 9, 2001
• Sequence Number: 17
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

SHATENSHTEYN, V.G., LEYTIMAN, Ya.7,, TEMNIK, V.G.
Ell"fect o' the I'E wetting agnet on the increase of the buLk densit7y
- (MlRA 17-.4)
of the coal charge. Koks i khLm. no,2,11-13 164.
1. Kc-mmunarqkiv kcksokhimicheskiy zavod (for Shatenshtey-n, Ley-tman),
,~. Kommunarskiy gerno-metallurgicheskiy institut (for 'remnik',l.
2

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L 41248-65 EWP(k)AwP(z)AwT-(-d)A-wT(m)AWP(h)/EiWP(b) ./EWA wiiPk
Pf-4 MjWlb S/2563/64/000/2
ACCESS AT4042606 33/0030/003.5
Ion NR:
AUTHOR: Shaterik, M. A.
TITIE: Drilling of heat resistant steel E1787
SOURCE: Leningrad. Politekhnicheski-i institut, Trudy,.no. 233, 1964. Avtomati-
zatsiya i tekhnologlya mashinostroyeniya (M~o tion_and technology of machinery
manufacturiqg.pToceBses),, 30-35
TOPIC TAGS: drilling, steel drilling, drillingispeed, drill angle, drilling
steel E1787
lubricant., drill durability, drilling,coolant
ABSTRACT: Drilling is one of the most.difficult technological.operations, and the
heat-resistant steel E1787 isi in this respect, one of the most difficult materil-
of the austenite class. The aut4pr studied techniques for drilling this steel on.
the vertical drilling stand 213511powered by a 4.6 kW motor. Graphs show the
dur-ab1lity of -vario drills'as a function of 1) the lubricant-coolant compositioni.
us
2) the magnitude of the cutting point angle; 3) the length of the working section;
and 4) the magnitude of the back angle at the periphery of the drill. Thebest * -Y
drilling lukricant was found to be industrial oil 20 with admixtures of LZ-M-2.- J
Card 1/2

L 41248-65 -
ACCESSION NR: AT4042 606
(a chlorine-,containing ohosphinic acid eater), or sulfofrezol mixed with 10% kero-
sene. The article concludes with data on the geometry'of drills-recommended for---,
the processing of 91787 heat-resistant steel, and with the * cutting.rates of the
recommended,tools. The cutting rate,V in w1min. is determined by the following
formula
'-V 1.31 d o.44
S U- WMUH,
where T, d ind a are the stability of thedrill (in minutee)i~its d1tameter (in
MM) and bite (mm/revolution), respectively. prig* art. has'.- 1 fbimula, 5 figurest
and 4 tables.
ASSOCIATION: Leningradskly politekhnicheskiy institut-iment M, 1. Kalinina (Un.
'ingrad polAechnic Institute)
SUINITTED: 00 EUCL: .00 SM CODE,.. 1E
RO,REF SOV: 000 OTM: -000
Card, 2/2

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LIHATER-1
waiding cl, tools. Svar. Pro'-~'v-
Au,OIu--,,,-4-- wn~1,0- ~,.,Mk 2_4 - 12
rc,.j,2-,2,>-28 D 161.
Veskova.
instrumentalln-,i zavoc.
teei-A..elding,
oontrcl)

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SFIAT'ERKOV, V.I., Imb.
` jilty ef rail% w1thin nwitchoo,
Invest igqtir~v Jatr)ral rig
Trudy DIN no.27:290-300 1 58. (Mla 12W
(Pailr-ads--Raila) (Railmade-Switchoo)

.and. :.-ekhr ~Tl I I v.
S0111C, Tyrjb2erft6 in the cf Fwitc-he2. Trudlf
DIN nc.30-209. .2-14 160.
(Rai lroad.~- - -Switches)

FRISHMAN, M.A., doktor tpkhn.nauk;.SBATERKOV,-V.- I., kand.tekhn.nauk;
SHKODA, Ye.G., inzh.; LIPOVSKIY, R.S., k~~d.tekhn.nauk
Eliminating the causes of crack formation in switch rails with
squeezed out heels. Vest. TSkI HPS 20 no.5:50-52 162.
(MIRA 15:8)
1. Dnepropetrovskly institut inzhenerov zheleznodorozhnago
transporta.
(Railroads-Rails-Defects)

SEMENCHENKO, F.Ya., Geroy Sotsialisticheskogo truda, starshiy dorozhnyy
master; ISAKOV, I.F., kand. tekhn. nauk; KOBETS, N.G., starshly
dorozhnyy master; VOLOSHKO, Yu.D., kand. tekhn. nauk; CliERKASSKIY,
_t!,HATERKOV V I -kand. tekhn. nauk LIPOVSKIY, R.S.,
M.M.5 inzh.; S
kand.tekhn.nauk; FRISHMAN, M.A., prof., red.; POTOTSKIY, G.I.,
inzh., red.; VOROBIYEVA, L.V., tekhn. red.
[Current maintenance and repair of tracks]Tekushchee soderzhanie
i remont puti; opyt puteitsev Nizhnedneprovsk-Uzlovskol distantsii
Pridneprovskoi dorogi. Moskva, Transzheldorizdat, 1962., 55 p.
(MIRA 16:1)
(Railroads-14aintenance and repair)

FRISHMAN, M.A., prof. (Dnepropetrovsk); SHXrERKOV, V.I., dotoent
(Dnepropetrovsk); VOLOSHKO, Yu.D~., A6~sent (Dnepropetrovsk);
ORLOVSKIY, A.N., inzh. (Dnepropetrovsk)
Performance of switches laid on reinforced concrete slabs. Put'
i put.khoz. 7 no.7:11-12 t63. (MIRA 16:10)

SHATEMIIK,S., urach
I ,
New methods in treatment for worms. Rab.i sial-31 no.!(~:23 0155.
(MIRA 8:12)
(worms, Intestinal and Darasitic)
I
!' I
f
- I.

-7
, ~,. I,%
Beki (:IJ 1 Wr-fl
Sto:-kiu ~ep, llreaO.
Pchr--107rorlstvc; 29, N(3. J,., 1-115;,.
%~oirt IED.
I . . -h.!,t List of Russian Accessions, Library of' Congress, November 1952. UNIG LAS6 IF I

/v lk6' V r1
TURPAYEV, T.M.4 SHATMIKOV, V.A~
Role of acetylcholine on the negative chronotropic action of the
vagus nerve on the heart. Biul.eksp.biol. i med. 38 no.8:3-8 Ag 154.
(MLRA 7:9)
1. Iz laboratorii obshchey I sr~vntiellnoy f*iziologii (zav. chlen-
korrespondent AN SSSR Kh.S.Koahtoyants) Instituta morfologii zhivot-
nykh imeni A.N.Severtsova (dir. chlen-korrespondent AN SSSR G.K.
Khrushchov) AN SSSR, Koskva.
(AGETYLGHOLINIC, effects,
on vagus nerve negative chronotrople action on heart)
(NERVIS, VAGUS, effect of drugs on.
acetylcholine, on vagus negative chronotropic action on heart)
(HEART, physiology,
eff. of acetylcholine on vague nerve negative chronotropic
action on heart)

SHATFMIIKOV, V. A.
"Disturbances of the Processes of Absorption in Small Intestine
During Radiation Injury of Animals Maintained on Various Food
Rations," by V. A. Shaternikov, ?4editsinsLmya Radiologiya,
Vol 1, No 4, Jul/Aug 56, pp 61-67
Tests were conducted on 18 dogs who were subjected to a preliminary
operation whereupon the extreme end of the small intestine was isolated
and a metallic fistula inserted. The experimental animals were then sub-
jected to 350, 400, and 500 r and then r.~aintained on "physiological,"
"hepatic," or "milk-egg" diets.
During the acute form of radiation sickness in dogs that bad been
maintained on "Physiological" and "hepatic" rations there were observed
acute wavelike changes in the absorption rate of glycine against a back-
ground of inhibition of the absorptive capacity of the small intestine.
During the subacute course of radiation sickness in dogs that had
been maintained on "physiological" and "hepatic" rations, there was observed
a general increase of the intensity of absorption against a background in
which acute wavelike disturbances of the absorptive activity of the
small intestine occurred.

After the action of ionizing radiation food stimulation of animals
led to additional decrease of the rate of absorption in the small in-
testine.
The "milk-egg" ration exerted a normalizing effect an the processes
of glycine absorption in irradiated animals.
Enriching the "physiological" and "milk-egg" rations with vitamin
P, PP,and C exerted a positive effect in normalizing the absorptive
activity of the small intestine.

7

SHATFIRNIKOV. V.A.
Mechanism of' the disruption of intestin,91 absorntIon of glycocell
following x-irradiption [with summnry in 14'ng'Lish]. Mpd.riqd. 3 no.3
37-42 My-Je 158 (MIRA 11:7)
(GLYGINN,
intestinal nbsorp., eff. of x-rays in animnis (Rus))
(MBSTRIBES, physiol.
glycine absorp., eff. of x-rays in animals (Rus))
(ROENTGEN RAYS, effects
on intestinal glycine AbsorD. (Rils))

SHATERNIKOV, V.A.
Metabolism of lip-ids in radiation sickness. Med. rad. 5 no.12:
61-68 160. (MIFA 14. 3)
(LIPID, METABOLISM) (RADIATION SIGIGIESS)

') 1. ~,s oo
17,5000 69512
AUTHORS~ Smirnov. K.-V.,, Shater ikov, V~ A- S/020/60/13-1/04/067'/073
B011/B002
TITLE: Acetylcholine Appearing in the Blood Under the Influence of
Ionizing Radiation

PERIODICAL& Doklady Akademii nauk SSSR, 1960, Vol 131, Nr 4, pp 961-963 (USSR)
LBSTRACTs This paper is ment to explain the participation of small intestine
and liver in the metabolism of acetylcholine in the action of
T-irradiation. The experiments were made with three dogs
angiostomized according to Ye. S. London's method (modification by
the authors). Isolated sections of the small intestine were used
as tubules. Stomata were fixed at vena portae and hepatica. 18 hours
after feeding, blood was taken from arteria femoralis and the two
veins mentioned, For 5 minutes, 2 ml of this blood were extracted
with 8 ml of Ringer's solution (PH Of 7.6) and eserine (2.10-5)
under heating by means of a boiling bath. The extract was tested
in a muscle of the back of the leech. The difference between the
muscle contraction in the experiment and in the control (control
with addition of active cholinesterase) corresponded to the
contraction achieved under the action of acetylcholine contained
in the blood. It was found that the arterial peripheral blood
Card 1/3 flowing off from intestine and liver in all three dogs not exposed

69512
Acetylcholine Appearing in the Blood Under the
Influence of Ionizing Radiation
Card 2/3
S/020/60/131/04/067/073
B011/B002
to irradiation, contained only traces of acetylcholine. After this
has been found out, animals not treated before, were completely
exposed to r-rays of C060 (dose of 300 r, dose intensity of 450-
46o r/min). Table 1 gives the amounts of acetylcholine contained
in the individual blood vessels. Already 2 hours after irradiation
on empty stomach, acetylcholine appeared in the blood of intestines
and livers of all dogs examined. Acetylcholine however, was complete-
ly stored by the liver. On the second day even more acetylcholine
was secreted by the intestine into the blood stream, its con-
centration in the vena portae increased up to 10-151Ag%. In two dcgs,
acetylcholine not only penetrated the liver, but was also found
in the arterial blood. Six days after irradiation, the content of
acetylcholine in the vena portae become somewhat lower in two of
the dogs, while the liver of one of them, still let it pass. This
dog soon died. Another dog showed such an escape of acetylcholine
on the 9th day after irradiatioa~ The vena portae of all dogs
contained acetylcholine until the obaervation was terminated. The
constant transportation of acetylcholine into the liver cannot be
ineffective. A certain favorable influence on the metabolism of
the liver seems quite possible. A negative influence is also
possible, but special investigations are necessary to find this out.

69512
Acetylcholine Appearing in the Blood Under the S/020/60/131/04/067/073
Influence of Ionizing Radiation Boll/BO02
N. Ye. Kuznetsova, Ye. N. Petrovnina, N. N. Deming A. F. Platonova-
Pokrovskaya, N. Ye. Ponomarenko are mentioned in the paper. There
are 1 table and 19 referencesq 14 of which are Soviet.
PRESENTED: November 199 19599 by L. S. Shtern, Academician
SUBMITTED: November 18, 1959
Card 3/3

SMIRNOVP K.V.; SHAT ERN IKOV, V.A.
Effect of external ionizing Irr4pation on heptic and intestinal
participation in lipid metabolAam. Vop.med.khim. 6 no.5:464,7468
S-0 160. (MIRA 14: 1)
(LIPID METABOLISM) (LIVER)
(INTESTINES) (RADIATION SICKNEqS)
I ,

DEMIN, N.N.; KORNEYEVA, N-V-; SHATERNIKOV, V.A.
Effect of ionizing radiation on acetylcho*ine metabolism in Macaca
rhesus. Biokhimiia 26 no-3:494-498 My~e 161. (MIRA 14:6)
(CHOLINE) (RADIATION-PHYSIOLOGICAL EFFECT)

SMURNOV) K.V.; SHATERNIKOV, V.A.
Cholesterol metabolism in radiation sickness of dogs. Radiobiologiia
2 no.2;194-195 162. WMA 15-4)
I
(CHOLESTEROL 1 THTABOLISM) (.-LADIATIO17 Sjr

SMIRNOV, K.V.; SHATERNIKOV, V.A.
Angiostwy b7 means of an isolated loop of small intestine.
Biul. eksp. biol. i med. 51 no.6:105-106 Te 161. (14IPj- 15:6)
1. Rredstavlena deystvitellnym chienom AM SSSR AN.
Lobedinskim.
(BLOOD VESSELS-STIRGERY)
(IRMTIM--JMMPPANTATIO,11)

SHATERNIKOV, V.A.; SAIWICHUK, L.A.
Determination of the content of free fatty acids in blood
plasma by the colorimetric method. Lab. delo no.10:598-
599 164. (MIRA 17-12)
1. Klinika lechebno&o pitaniya (direktor - prof. I.S. Savoshchenko)
Instituta pitaniya (direktor - chlon-korrespondent AMN SSSR prof.
A.A. Pokrovskiy) AMN SSSR, Moskva.

8LI
14.
I f
R 18
.1-IMIN ESSR

ACC NR., AR6034975 (,'V) SOURCE CODE: UR/01"72/66/000/008/005910060
AUTHOR! Bykhovskiy, Yu. S.; Shaternikov, V. Ye.; Nerubay, M. S.
TITLE: Nioncontact measurement of ultrasonic oscillation amplitude in
magnetostrictive transducers
SOURCE: Ref. zh. Metrologiya i izrneritellnaya tekhnika, Abs. 8. 32. 475
REF SOURCE: Nauchn. tr. vuzov Povolzhlya, vyp. 2, 1065, 117-126
TOPIC TAGS: oscillation, magnetostriction, eddy currents, ultrasonic
machining
ABSTRACT: The measurement of ultrasonic oscillation amplitude has become a
prerequisite with the introduction of ultrasonics in cutting heat-resistant titanium
alloys. For instance, in machining EI-437B high-temperature all-Dy the tool
resistance may increase twice as much or be reduced by a factor of 1. 4, depend-
ing on the amplitude A to 0. 0015 up to 0. 005 mm, respectively, all other conditions
being equal. Amplitude measurements are necessary in the 0. 5-20 range and
frequency range up to 40 kilocycles in the presence of a high-tensity magnetic L
~L-Card-IJ3 UDC: 534. 838:538. 65. 083. 8

A,CC NR: M1603497-5
I'ield ind variable dielectric loss in the lubric ant -coolant fluid. Under Shop
condiLions only eddy current transducers are found to meet the reqiiirements. In
these transducers, the reverse effect is measured on the primary coil by eddy I
cut-rents generated in the conductive surface induced by the transducer's electro-
magnetic field. Another concept of eddy current transducers design features gaps
commensurable with the dimension of the coil. The method makes it possible to
calculate both the active resistance and insertion impedances. Calculations show-I
ed that tile inserted active resistance markedly depends on the conductivity of the I
surface as well as on the gap, while the inductance depends on the gap alone. Tile
maximum sensitivity range of C transducer lies within the rangeof the ratio of tile
gap to the coil radius 0 to 0. 35, while the inductance sensitivity remains constant
in the frequency range of 0. 3 to 10 Me. The relative reactance Change for small
displacements is just a few percent which determines the selection of the measur-
ing circuit imbalanced bridge, which is used for comparing the transducer
impedance against a standard; the measuring instrument responds to the difference'
of currents passing through it (109/,kamp corresponds to a gap change of 10/ e&'
the total gap being 1. 5 mm). The sensitivity can be increased Q2 times Q is
the quality factor of the transducer coil) by supplying the voltage of the eddy
current transducer through a cable whose capacitance resonates with the coil. An,
instrument based on this design concept has been built. Basically, it is a high-
Cara

ACC NR; ARG03,1975
frequency oscillator with rated power of 7 watts and a frequency of 2. 5 !Mc-
It rneasurcs quasi-static and dynamic motion. The effect of test-stand vibrations
are filtered out by a bandpass filter with a frequency range of 2 to 50 kc. Static
calibration is accomplished by a micrometer with an error of 0. 5 T e
h
device provides readings which are almost linear for gaps between 1. 0-1. 65 mm.1
Orig. art. has 4 titles and 12 illustrations. [KPI
SUB CODE: 20, 14/
C.rci 3/3

Clof
Micromethods for the detennination of autta in Evony-
mus. A. N. &u(amkuv.t aml I V. Mrg. S-wi. Hotax.
j5, mi-XI917); CAm /rmll. 1447. 11, 757.-Kud-~
,hrva (Cf. C .1. 35, (;-M~!') h4, rv,.mumen-h,d StAillillit w 1,
All WI. tini'ttift 411 1. 111 ti- C- the IIIUC-IltUCk CUII
11~42 'd the 'I.m h gr.in' I he '1~%,h CO !"I
"it he removed 1AMe the VrIlOW 0449 44 the gututrA"Mr
jppcar~ by cxtg. for I mottilt with Ac. A twtta prIwc-
du- is li-tti,ig ~jzh JL5 X; 11,Sf), for 3-4 min. at -54)-
tN) '. which cotivert, the urch into mom-icchArulc.
tb.,t cadv th,- Kulta I, t micil with the 1. M. G. M:

SHATERNIKOVA, A. N.
23108 Anatomicheskiye issledovaniya stroenlya smoloobrazuyushchey sistamy
listvennitsy. V sb.* issledovaniya po les. Zhoz-vu. L., 1948 (Na
oblt 1949),, C. 175-97. - Bibliogr: 7 nazv.
SO: LETOPIS' NO. 31, 191,9

SHATERNIKOVA
Using Crimean pine for establishing highly resiniferous pla-11tations.
Gidroliz.i lesokhtm.prom. 10 no.4:18 15?. 04W 10:7)
1. TSentral'nyy nauchno-issledovatellskiy Institut lesnogo
khozyaystva.
(Pine)

SHATE1G'IPO_VA,,_A_11_____
Condition of tapped pine stands in the Central Urals. Gidroliz.
i lesokh1m. prom. 11 no-5:10-12 '58. (MIRA 11:9)
1. Leningradskly nauchno-iBsledovatel'Bkiy institut lesnogo
khozya.rstva.
(Central Urals--Turpentine) (Tree tapping)

AKIFIYEVA, K. V.; BELINSKIY, V. A.; DRY-UKRMOV, A. V.; VLADIMIROVA,
G. A.; MAKHOVA, Yu. V.; MALINOVSMA, N. M.; MYAGKOV, S. M.;
NOWAN 3E. A.; SEMEMN, Y-a. V.; TARASOV, G. K.; TUSHINSKIY,
G. K.; UTYAKOV, P. A.; FAMINTSYN, % M.; SHATERNIKOVA, I. S.;
SHAMHIYEV, K. M.
Estimation of the danger of avalanches in high mountain areas
designated for development. Inform. sbor. o rab. Geog. fak.
Mosk. gos. un. po. Mezhdunar. geofiz. godu no.8-.27-163 162.
(MIRA 16:1)
(Caucasus-Avalanches)

RUMYANTSEV, N.V.; SHATERNIKOVA, T.M.
Contemporary data on leukemia in cattle. Ifeterinariia 40
no.4:20-26 Ap 163. (MIRA .17:1)
- - -.1h IQ

S AN
If ,_.T., BOAGOV, YU. A., DZHELEPOV, V. P., DZ14AKOV, N. I., IV OV, N. E.,
LEPTLOV, V. I., MOSKALEV, V. I., FLYAGIN, V. B.,
"ne One-Fleter Provane Bubble Chamber in Magnetic Field"
paper presented at the Intl Conference on High Energy Physics, Rochester, N. Y.
and/or Berkly California, 25 Aug - 16 Sep 1960.

k., -
Y--RO1?-r'Yh-V,, B.N. -, SHATA-LOV, Ye.T.
For an indissoluble union of geological surveying and prospecting
for mineral resources. Sov. !,-eol. no-53:3-21 '56. (MLRA 10:4)
(Prospecting) (Geological surveys)

SHATIK, V.Pl~
,, e genus Gandida ~ffider tne
Variability in the yeastlike fungi of th
influence of mycerin and vel.iutinin., Eksp. i klin, issl, po antibi.,;,Li
2:21-1-216 160. (CAI.MSDA) (ANTIBIOTICS) NIRA 15:5)

SI(MAL) V.N.
l4uantitative determination of the activity of antibiotic 26/1 by
the agar-diffusion method. Antibiotiki 6 no.12:1123-1127 D 161.
(I'ilAA 15:2)
1. Leningradskiy nauchno-isoledovateliskiy insti-Eut antibiotikov,
(kNTIBIOTICS)

SANBONOV, G.V.; VEDEITEYEVA, V.V.; SHATIK, V.V.; VIKHOREVA, T.A.
---- - I - . -... I.,
Study of the conditions for the reversibility of the sorption of
penicillin sorbed in the presence of sulfates and phosphates on
the nonselpetive sorbing EDE-10 anion exchanger. Trudy Len.khim.-
farm.inst. no-15:75-80 162. (MIRA 15:11)
(PENICILLIN) (1uK EXCHANGE) (SORPTION)

lamatAc factors of
nd tl,-,e oceurrenrv- ~,i n n'*~- r
rm~12:111-114 0 164.
KIZA ipt]
,ya tK.,l I ni t. sa im, cl L-, ;7 ai-
gorodska
.0. Migalk'nl
4 , .

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CDAL 11-1:A 10
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CR PULVERIM. 11

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'ITHAIR C00010 AND OV7FUiEt%D (=- OUTLL Katanelson, - B.D..,arM ShaTill A#A
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resulta on an experimental -vorriedl oyn3ore camhlrtiri~~dh
amher with ovarhepA

r -
ta on the oporatlon.of the bh=bc'
Cas outlet provide da r VIM
air toolirz o
the flue walls which are of Interest In cases Mare this arrangej~onit--Is 1:
ciTployed In gas turbines using p1mlzed coal. h6chanloal:undercombustion

onj,-i
was 2.2-7,55o Fuel flnone.~s, co -r-re sponaing to. lwast value, of 'underooz-busti
lay vilrbIn the range R88 20-35,oe Slag removal coefficiefit-was 65-7COP.

, ye, yu.
-a,T - ;__
41re etrain F;al~pes used in RutomtIc recording -,f tenatca drops.
ler-, tak-11 - r - - --.1-*-~"7 Yv-je '57- %MTM 10~8)
Otrain gauges)

kand Wat ri-valp.. "H~T 1 A-
ent eachange in an air-aool;.--~~
IF; exhwast throu_-)-, the to7--.
7"lentrallnrl kotloturbinn.;j
(Combuq -.
cycir.ne combustion chamber wl-.h
--e-oloenerigetikp 4 no-'?:713-75
insti-~lat.
icni'l ~Furaaces)

A Tr "LO'n 3
A.A.
T ITIF, 'li j3es o~ a Thr,,)+-~le Flow-me~er for Dus+-
U U
C.Q '. 1 - . e no ; .. -hodomera)
Rasn -t-- drossel' o pylerask~_
PERIODICAL: Te3,, -rj
prget4 10 (U6SR).
1~)58) Ar 5,
A; STRACT
-i,ea~~urin- dust
ntc" 1
1v t~-- USSR and a-road. er e
T_ i.z'
for devices of ti-is Zivtd.. TL e
IbaEd~; aloe _-Cor;pulated and a formula is _-given for 'L'-r-e
fa-~t:.)i- that rela~'-es the rate of flow to the pressure chanr-e
in-the throt-blinG device. Results of the calculation of the
vc-Loci,tj dis'uribution and, additional pressure drops ca-,se(_--~ b'y,
a frac-'Gion, of dust c:.)nsistin--,- of she es ol one size
are sho-~7i 2.
n in
-L'A' iJhe dust-, -;*)a.rtj.-_1-_s o~' a-.sorted sizes are accelerated
independe-atly of one another, the total loss of head in the
constriction will not be the same as that occurring with
uniform particles. HowevIer, experimental data show that in
pri~_;ctlce the motion of an assor-ted dust in gas cannot be con-
sidered as independent motion of individual particles. In
fact, the -particles interact so that, within certain limits 01'
Lneness of millinG,, the aerodynamic properties of dust with
d
.L L, L -1 U i:~ n
'fferen~ s4zes of oartcles are the saLie. Hence, calcu'a

SOV/96-
C, D, Vottle Plow-me~tev for Dust
B _L - -
of the L-ate of flow LhrQULL, throttlirir~ equipmer,t; -1-s Con-
::;kbr,abiy simpiified. TI,is is illustrated rra,phically iii
r_i
shovis tk,e calcul,~.-tted curve for sphericz,_!
I-Irticles of 20 ji dia. and. for an experimental assorted
Aus'. It vi'll be seen th,,,t in '-he covistrictiLn, ~-.hich -S
U L LI _L
~:he r)j.* -)ractical ii,,,.portance, 1;-'L-.e curves OrtlIctically
-ide xr -i
n
c 13impler e. _,iessiota ran, tierefore, I- L'I~LVeL'
t-he factor in the, fOTmula.
't ,-cnt--i deta !.~as In'therttzi ',-en ;_)ublished z;r.L
~,L tie exoeriL .1. 1 1.
-I.-Ilrottle-tyne flo-i.-.-meters. The table rives valoes of the
,, ~n L.
eff'icient fox, -t- El seven 'U11--rottlin- devices illustrcted in
Fic~-ure 4. TI,,e d-rst four ..ere testea in the TsKTI (Central
y
Bro,iler 'I'l--bine inistitute), the fifth -if, the ~13I (Llosco7, Pov!er
I-~astitute) and the remaiain.- two by Farb_= in tli~e USA. 9_11e
as-ree_-I.ent bet-,,veen the calcul~-,-ted and test values of the
coeffic.ent is s,~tisfactory. T-h-ere al-e .7~ fi-ures, 1 table and
ref=-n-re-ac~. 5~: Cf 7-:1--ich are Soviet,
-r:,an and 1 En~,i-lish.
Fiowmeters--De-5ig~_-., 2 Flowmeters--Test results 3. Particies
'.A;__-b(-j.--ne'--VeJ.oci_Ty

--f
S
,.;iTIL', A.,, , Inzh.; KALISHEVSKIY, L.L., inzh.
Using the Ventury tube in measuring the consuription of pulverized
cnal. rTrudyj M.U no.94:78-85 '58. OMIR& 12:3)
(Coal, Pulverized--Measurement)

SHATIL', A. A.., Candidate Tech Sci (dies) -- "Investigation of the throttle
method of measuring dust consumption in pneumatic transport", Leningradv 1959.
11 pp (Min Higher Educ USSR, Leningrad Polytech Inst im M. 1. Kalinin), 150
copies (KL, No 24, 1959, 143)

S 0 111~3 6 - --) 9 - 71 2 6
A U, T H C-) R,- Shatill, A.A., Engineer;
TITLE, Letter to the Editor (Pis'mo v redakt-siru)
PERIODICALg Teploenergetika, 1959, -Jr 7, pp 92-94, (USSR)
ABSTRACT-. This is a discussion of -the loss of head when 5~, flow of
dusty gas passes a local resistance in a pipe, The losi
of pressure with a dusty flow as comppred with a clean
flow is given by equation (1). In t~Lis equation the con-
centration of dust is allowed for by a factor k numeric-
ally equal to 0.8. _w~n nrticle by Tsygankov in Teploener-
getika Jr "~, 1958 proposed an method ef deter-mining the
flow of dus-.y air in which this constant- was 'used, His
method of successive approximntlon is valid~ but -~he graph
that was given in the article to illustra-te the good
agreement between the theoretical and expe--rimental curves
for pure air is not; the same agreement can be obtained
for any value of the coefficient k. American authors and
the present nuthor have shown th,-~t a sharp diaphragm is
not sensiLive to the Dresence of dust in the f:;Low,- Figur~~---
1 shows graphs of st-ati-. -oressure-dro-os across- a- sJoarp-,
Card 112 edged thro-Ocling device- wish vario'us ~~onoentratilcjns of

SOV/96 - 59 -.7
Letter tc, +-he -,-'ditcr
g,,-.s in the flow. Figure 2 p '.ots the coefficient k a'
culated from the results of Zigure 1 :~s a fun-ction of lie
position of the referer,.,:-e holes in the throt-,Iin- devi-I-e
with a sh,--irp-edged di-n-phragm. it will be se~!ii Oia- 1-h--
value of k does not ex:~eed -'-n ex-oian~ t,-,)n i s
Of'Lered fcr these findings, it is cor-cluded; t-i,--T, fur-ter
tes-ts are reouired -to deterra'Lne the value (,.t fde fict~-,r k
for sh;-~rp diaphragms,
There are I figures and 6 reCerances, 5 cf wl-.-i,ch a-r,~
6oviet and 1 Fngl-ish~
Card 2/2

S 0 V
AUTHORS Ka.~.,On a! Bl~ - D. (C a ndidat a of Te~!:Lnil -,a-', 3,~:ert a
.-Shatill. A.A. (Ertginee-2)
.7,
L !-gatin:-, of an Expe-!~--'
--l, q~est4~ ' '- .1 -
TITLE; A menta".
Com'--,us-tion (,'narb-r AD., Ccc-l-ing
PERIODICAL,, Ni- 9~ pi, 39--V (USS
ABSTRACT; ~x.,mbu.:~t.j.on. :tan,- e -,s w-1- tb. ii:5 s.,*" a g T- isn-)
app~,~a'~, for )u-r, tin r1g, ~Oli-ld for C-a:~
wo-king on ar, op-~n -e.
Tu,~"hine Iristi`;u~e ha3
j-
Ct 0 mb,,- s r~ n am 3-~, s, *-ri ---,n -.-n(-,, co aa us r, wit"L a .:.., ''. .- I
3 e o . - +- - -F-
gas Am ob..e~-.,
of us-ing a
da !~- a
Lig t1h 1, -L , - raton,
was install.a(f on a tL~st 7- a s i 1 -..,,7 z- t
d f
mati-call~y ix, The :r. bias J,
jr .,7 :
'L ~, f
_Lg 4
-er 000 =
-mum and the dialflete',--- o the vltlet a 0 f -a: a
I
rt,:,a a 1, e
the c.;--l-mbustior. chaml,-, %.,r-a.
~;~,z~ uxhaus t ga S Gs a rl 7, a tdu --a F, 11 ~? 4L
~,ard s,71- -
,(, t'he throat c~f tl-ue
o rn, e i -a tu ii: e v

An Investigat-ton of an Experimental, Ho-z-Jzonta2, Cyclone
Combustion Chambe-- with Air Cooling
Hence, the gases pass to an air heater in which the
secondary air -is heated to a temperature of -)50-L~00 OG~
There is no ash arrester on the test rig and s~D a steel
Sc2een was installed to trap enough ash to prevent
excessive damage to the air heater. Liquid slag retained
in the (,-ombustion chamber drains off and falls -into water
f.-or. which it -is periodically removed. The -:!!a- II-.ap hole
is heated by some gas from the r~ombustion cl-,armbe:~. To
ensure urLformity of delivery the coal was supplied
L t-. I-
through a wcrm oon-,reyor. r-oal dust del-'vered a' the ra'e
of `50-250 kg/hr is taken nr, by the primary air- and may be
delivered either t~iiough a burner on the central a-x--I*s of
tirie c,.)mbustion chambe--.- or through one Of SOVeral slits
round the end. Previous work has usually shovm ttat';
axi 'a]. delivery of coal dust did not give gaoa results,
tangential delivery being necessary to obtair. --atisfa,~t-ory
crimbi-'stion and ash removal in ~iorizontal cyclone
crj-'u'zt~on ~~hambers, The tests were made with Donet-13
_L; - - - t.- L'
,lard 2/7 gas cnal, the cliara-teristics of which are given, Da ta
I-
'Dr- the vi-soosity oIF' the ash of two grades of '~-'-,al u---e(,' as
- I - -

SO V/96 - 50 - V 42L-
An Investigatic,,ri cf, ari Rk-perimental, Horizontal', Cyclone C-umbuOt.1-on
Chamber with Air Cooling
Pwlflc-ticn of flemperature are noted in Tabia -1. D,9
Pril'l,~,.ipal teSt 31'eslal ts are given in Tab-le, 2; :12.1 i,_-f ttLLn,
1;,,) str)a-_--,y Ope ating Conditions aftqr
L - 4 - mentE.
had been ma,lo. Hovever, the table does juel".'-de i-rta On
Dr! E; L
p-_,el'J.mm.!-,ry f.E.-sts to determino ~.C-v
thE, fuel t-) the. charmber. D Pj y e y, y t
IX a 3"L
cez-jair, slits did i-ot; givp- the best
Pai,ticulal-_-7 stable- The mosl~ sat_Jsfa,,ito-_r-Y were
o b ta J rl- - d toh e -1 _', ve~ _ ~t,
- 11 - - - L _,51 t*
.f,GU~-h 4,W,::, 041 1 Ir
J. t ~,,ae
er.-'
er, -.i.T
"a Inc -p,i e
Axi a I dali-,/ery of the fuel Twar
las" F,:..St iia3 s ?,-, e a
e 1 1E,- _'~~u a ground to '~.(I% rcsirlu~=
-1 - I - - _-, n 7
s i f:" v e s Th-EI main (.haracteris tic,,; oi~ i*.tlis a-L--
The f-.- wore niuc-h better than when burnir-,g t- 11,
fir-
J
e d c c, a J_ a nd e a 3 1-1 c- mm. c, va:L c: t o r wa s 3 C, "Irl e "'; lll~_ I
oe,ter tk~lan 0 c." . isi th,~-refo-_-'e, some rea5,:ln to
3UPPOS-e -Lhai.- a.31! rMoval w"I'll bu, arpfec'-La"lD"lL-,--
Usin-7 relativejy 1-11,1-irj~, Al
- I I _ 1"'lough
'lard start,,:.~d ur. ,,nany zimes
an at vez-y h-;:7'--
tul-es, it was ni)4.- ~aTa-,-1. Du-ng t' ' es'
-16 -1 s, !;nT~ ,)a!-'

SOV/96-50, --q-- "J/'2 ""
An Investinaticn of an Experimental, Horizontal., Cyclone
0
Chamber with Air Cool-:ng
)0 01, t!~~C-ujfL- 5,)me-
temDeratures usually did not excee,-I 7C
t4M
es they reached 750 CC. Durina the tests the fue!
consumDtion ranged frorr 144 to 258 kg/hr, the lower value
representina the minimum rate for stable combustion and
the upper being limited by the draught facilities
available. Mechanical u-nder--oombustion, that Js, fuel
actually left unbupned, ranged from 1.17 to IO.',7%o, and
was greate-r than 6% in about half the tests. This figui-e
is high because the chamber is small and the rating
relatively low. In-;rpasing the coarseness of milli-n-a
red-tices t,--e mechanic-al under- (,, om bustion, as will be seen
from, drI2 9-.aph plotted in Fig 2. Differenc-3s betureen ".his
~:,ffect- in and vertical combusti-on -~ham'hez-s ai;~
d 4-1 s cu s s &-i The amounb of unburned fuel emitted with the
exhaust remained apprcx-imately constant, most c-f the
Variation beinb- in the amount contained in the slaz.
Th-e graph plotted in Fig ~ shows the particle siZe compo-
sit-ion of t~ie coal dust and of the ash b-'.(iwn out tha-uEf
Card V7 the exhaus I.- in a ticular test. It W 11 be sr-on tha~-
pa--tic-I e sises above 2.0 nicrons (Whi.-.4i are the m-,,st

SOV/96-501-9-77/2z-
An Investicration of an Ey_;)er1menta;1, Hcrizont-al, Cyolf--- r-r~M-U~~.Z-cn
Chamber w'J-I'h Air Cnol-ing
dangerous for t~he gas turt'-fae) cc-isti'-ute about of -,--.he
ini-tial fuv,-! bu-L on-1v `r 1~ie ash. In tt,~
cloal dust zlie slag rerrv-)-.-al faf.1to-Y ranged from 6() to w%,
and -In t`ie t:1--st wlh. ,,oarse milling -it was areatel- than
90%. The graph of slav remc.,~al facto:n as a 1*.'u,-.c-.t--n of
finene3S of milling, given, in Fig L, shows that "very fine
4s un-r vourab29, The same f -,tor -s plot'ed
MI. - -a .-a _L t, .
against t h r. t-r~ e 1- ma.. 1- 1 o a d 41. n 5- c) f t h e m b u s 'L, i o n ~l ha M. 1- e -, 1, u1
Fi 5, ar, k L.
pi 3-ows slac, -emo-val t-Lds b- e s s
-J-.rry a' low corubustli-on rates. -.s 1~
satisfa, Iq the test
Samplao of slag and as~, vie-e oaken every hou_-. T'he slag
."lowed c:ontinuously fo~-. tlae eight hours of tht? test, The
resuits are plotted "n Fig 6 from which it will. be Seen
ti-iat the slag remo- ..al factor ~Ln this -test wa_-1- 9,01%,
The air -_,-esistance of the chamt~er increased du'ring tb_~
,.est because of 'he unsatisf'actor-
v y operatio- cf t.',te o- tiet.
throat, whi-c-h ne;3ds mo d _i f -'L,,;a t i ca. The excess ai.r
in the combustion ~_hamber ranged from 7-06 to 1,42. T t
will be seen frcm the graph plotted in Fig that the
Past meclianii~al under. combust-ion oorrespo!ided to an
,.lard 5/7 excess ai-7 fac-.to--- Df 17.15 to 1.15. In sorme tests aa:z

SO V/96- 5u, -0/ --:7/2-2
An Investigation of an Experimental, Horizontal-, Cyclone
Chamber with Air Cooling
analyses were made across the diameter and along the
length of the combustion chamber and the results are given
in Fig 8. These tests confirmed the importance of the
mixing effect of the outlet throat cons tri~,,tion in
ensuring that all the gas i-s- fully oxidised, Graphs of
the temperature distribution across two sectic'ns of the
combustion chamber are shown in Fig 9, at distances of
1,'~O mm and 415-0 mm from the top of the chamber. TI, will be.
seen that the flame temperature differs little ao.~Toss the
chamber arid is of the order o--.' 3-500-1600 oc~
Circumferential and axial gas speGis across three sections
in the chamber are p! -otted in Fig 10. Graphs of tKe
resistance of the secondary air duct as a func-tion of the
per tur e of t- lie s1 i ts are plo t t ed in Fig 11 Da ta on the
resistance of the secondary air duct including the
resistance of 'the grid and mixing 2hamber are given - n
Tablie 2, which also includes air speeds in the Zlits.
The abo-~,-e results show that a horizontal pulverized-Due'L
Card 6/7, 1-yclone combus-tion chamber with air cooling and liquId
sia-;-,, removal --an be used --'-rL open ... cycle gas turbines,

3OV/G4-59-9-7 292:w
An Investigation of all Experim-antal, HGrizontal, Cyclone Comb-IstiOn
Chamber wit!a -'.J.r
TYie beSt -,ombustion and slag removal is obtaineJ -vi-th
"Lied fuel Further investigatior-~) may, show
cc-arse-y-m i L
how far tbe- increase in resistance that inevitablY
ac~,-,,)mpanies .3oarse milling i -, ec:onomi:~aliy jjust~_._-,`-Je~-' by
a t 1,F
redu-,--tiori -in mi.!'Ling cost, and imprcvemen4- in cP,~.!r- i--
There are 11 'Ligures, *-;' tables and 9 re--Pprerices,
8 a7-e and --- En,clish-).
ASSOCIATION: Tsentral-Inyv 1(--otlo11u:E-bin-ny-y Inst-itut
i.Central Boiler 'LUrbine Institat-~)

PHASE- r BOOK KXP LOITATION SOV/5519
Kramlevskly, P. P, , Candidate of Technical Sciences, ad.
Teploener get ich eaklya I khimikotekhnalogicheakiye pribory I regulyalor
y
'(1natrurnents and Regulmors in Heat-Power and Chemical Engineering)
Moscow, blastigiz, 1061. 207 p. Errata alip inserted. 8, 500 copies
printed.
Ed. of Publishing House: G. A. Dudusova; Tech, Ed. : L. V. Shchetinina;
Managing Ed. for Literature on the Design*and Operation of Machines,
Leningrad Department. Mashgiz: F. 1. Fetisov, Engineer.
PURPOSE: This book in Intended for engineers and technicians who construc,
design. and operate Industrial Instruments and regulators.
COVERAGE. The book deals with new investigations In the field of automatic
checking and regulation of heat-power and chemical Industrial processes.
The following problems atre discussed: improvement of two-position
control operation: effect of mass action and damping on proportional
control. new proportional plus integral and programming electronic
regulation systema; complete automation of open-hearth furnaces;
aulDmation of boilers with variable load capacity; measurement of
pulsating now: neasurement of dust flow; ultrasonic and magneUc-
Induction flowmeters; pneumatic compensating differential manorne-
tars. aggressive-nuid nowmaters, new magnetic and optical-acaus.
Ucal 'an analyzers; concentration meters; and chlorine and coagulant
regulators. The book is the fifth in a series containing reports on the
investigations carried out by the Section on Heat- Engineering Control
Instrumientation and Automation of the Leningradakoye otdclenlye
Nauchno-tekhnicheskago obahchestva priborostroitel-noy promystilennostl
(Leningrad Branch of the Scientific and Technical Society of the Instru-
ment-Building Industry.) Ali the articles presented In this book were
discussed elthker at sessions of the above section or at the conference on
measurements if mechanical quantities called by the section, the
VNEN (Vaenoyuznyy nauchno-inaltdovateliskly inatitut metrologil Lm.
D.L Mendelayeva -- All-Unlon Scientific Research Institute of
Metrology imenI D,1. Mendeleyev), and the Leningradakly dom
uchanykh Im. A. M. Clorikogo (Leningrad Home for Scientists iment
A.M. Gorlitly). No personalities are mentioned. There are 65 ref-
arences: 41 Soviet, 20 English. and 4 German. References accompany
most chapters.
TABLE OF CONTENTS:
Foreword 3
PART L AUTOMATIC CONTROL
OF INDUSTRIAL PROCESSES
Ch. 1. Kaimpe-Nemm, A, A. Two-Position Automatic Control and
Methods of Improving Its Properties 5
J, 1. Methods of Improving properties of two-poaltion control without
changing the block diagram of the system 5
2. Discontinuous two-position control
3. Introduction of additional pulses to the rule of relrulsting
according to the lot and 2d derivatives 10
4. Increasing the number of inflow steps (three-position
control) 13
5. Application of exponential feedback$ (two-poaition static and
two~positlon proportional plus Integral control) 14
Ch. IL Kate, A. M. . Lnd N. F. Conek. Investigation of Proper-
tional Control. Taking Into Account the Mose of the Sensi-
tive Element and Damping in the System Units 23
1. Equations for a control system with variable speed of the
servomotor and Inertia of the sensitive element 24
ow'"te-

4
Instruments and Regulators (Cont.) SOV/5519
2. Limit of system stability 2'd
3. Formation of transients 32
4. Equations for a control system with pure time delay 36
Ch. M. Stra un. A. Z Automatic Regulators 42
L Baafc-iypes of regulators 42
2. RV4-01 and RU4-06 regulators 44
3. HU4-15 regulator 49
4. RIJ4-16A regulator 51
5. RU 5-01 and RU5 -02 programming devices 54
Ch. IV. Demboyakly, V, V-, , and S. V. Yurovetakly. Complex
Automation of Open-He4rth Furnaces 5

1. Programming elements of the circuit
5
:
2. Automatic correction of the programming of the thermal
operating conditions III
3. Automatic regulation of name angle 63
4. Regulation of fuel oil conaumption 64
5. Correction of fuel oil consumption by the frequency of
throwing over the valved as
Ch. V. ShUrin. M.St. Building Up Control Circuits for
ShipboaFT-Baller System$ 68
L Regulation of boiler water-oupply system 72
2. Regulation of combustion process in the boilers 73
S. Regulation of air and steam pressure 75
PART IL FLOW RATE MEASUREMENT
Ch. VL Kremlevsklyy, P.P. Criterion of Puls&Ung-now
Damping
Ch. VIL Shatill, A.A. Avolication of Narrowing Devices for
JWRiRWMst Flow Ina Pneumatic Traffic iyatem 00
Ch. VUL KliLmunin A. S. Ultrasonic Flowmeters 101
L Phase 101A
2. Pulse-Ume method 110
Ch. M. Zasedatelev S M V A_ Rukhadze . and K. A. Savell-
~nsatTn i rentiaYiXi-nometers 115
1. Errors In compensating differentW manometers us
2. Means for increasing operating reliability of membrane
differential manometers 124
3. Differential manometers with pneumatic power compensa-
uan 126
Ch. X NIkltin B L L D, Vel't, and V. K. Rukavishnikova, 111-
i~d..ji.4,TEle~tr;magnetic7-Fro-w-m-e-tiro-- 134
Ch. 11:iach 0 eyrie ana-i~rpe Flowmetero
for Sulphurte Acid 141
1. Measuring average flown 142
2. Measuring high flows 146
3. Measuring low flows 150
Ch. = Mikhaylov. 11.1p, Measuring the Flow of Aggressive
EIquids 151
L Inductive no,emeter for registration of quick-changing
liquid news 151,
3. Tachometric wane-type liquid flowmeters 154
3. Measurement of ertremely low now& 154
PART UL MEASUREMENT OF TIFE CONCENTRATION OF
JNDlV`WUAL COMPONENTS IN GASES AND LIQUMS

23464
S/114/61/000/007/003/003
1~6 E194/E455
11 117 0
AUTHORS: Polyatskin, M.A., Candidate of Technical Sciences,
-~hatill, A.A., Khaynovskiy, Ya,S., Engineer and
Babkin-, V.N., Engineer
TITLE, Natural gas burners for gas-turbine combustion chambers
PERIODICAL: Energomashinostroyeniye, 1961, No.7, PP-34-36
TEXT: In designing the combustion chamber for a gas turbine type
PTY-5o-8oo (GTU-50-800) burning natural gas, insufficient
information was available about burner design. Accordingly,
TSKTI and KhTGZ made a joint investigation of burners in an
experimental combustion chamber which was described in an article
by M.Polyatskin and Z.M.Svyatskiy in Teploenergetika, 1959, No.2.
The main object was not so much to find the best burner for
burning natural gas as to study the main features of certain very
different types of burner. Accordingly, besides studying complete-
ness of combustion, an attempt was made to study the influence of
the burner design on flame structure. As the process of mixing
gas with air governs burner operation, three types of burner,
illustrated in Fig.2, were tested. The first of these (Fig.2a)
Card 1/4

23464
S/114/61/000/007/003/003
Natural gas burners ... E194/E455
uses a conical swirler, which allows preliminary mixing of gas and
air in the actual burner. The second (Fig.2b) has a flat swirler
with hollow blades, gas being delivered through holes in the blade;
it allows only partial mixing of fuel and air in the burner, In
the third type (Fig.2B) the gas and air are mixed in the actual
combustion chamber. A number of variants on these basic designs
were tested. The usual kinds of measurements were made and, in
addition, gas samples were taken for analysis at various places in
the flame tube and measurements were made of the gas temperature,
Curves of completeness of combustion and of temperature
distribution were plotted and the influence of various minor
design modifications on the performance were studied with such
curves, With natural gas, combustion was most complete with the
burner with conical swirler but it could operate only over a narrow
range of excess-air factor. The burner with flat swirler with the
gas delivered through hollow blades was more stable, particularly
-when there was no preliminary mixing of gas and air. Studies of
temperature distribution and gas analysis distribution were made
with various design modifications and, in general, the following
Card 2/4

1
R~61
S/114/61 0/007/003/003
Natural gas burners ... E194/E455
conclusions are drawn. When burning liquid fuel, it is desirable-
to have a fairly strong axial return flow of hot combustion products
to heat up the liquid fuel and to stabilize combustion. However,
when burning natural gas, the axial return of a large quantity of
heat to the root of the flame usually gives inadequate oxygen and
can lead to soot formation. 1--'ith natural gas, quite a small
return flow, required to ensure stable ignition of the mixture, is
sufficient. None of the burners tested was good in respect of
completeness of combustion; the main reason for this was that
methane was carried away along the walls of the flame tube where
the temperature is lowest with high excess-air factor. if
preliminary mixing of the fuel and air is reduced, the range of
stable operation is widened. It is expected that the experimental
data on flame structure will be useful in designing the
distribution of air and fuel over the chamber section. There
are 5 figures and 4 Soviet-bloc references.
Card 3/4

Natural gas burners ...
aj
23464
S/114/61/000/007/()03/003
E194/E455
;TJ I
z z ~J;,
Card 4/4 Fig.p_.

- SHATILI ) A.A.
Meesuring the flow of a two-phase current by means of a
Ventury tube, Izm.tekh. no.9:46- 48 S 161. (MIRA 14:8)
(F.Ioi,meters)

an - e Idul . n "11-01.
chrorato Uaphi~- gao analyze- 4"or studying the
s ra3 -bi r n, -omashinostroenie
-r. il,er, Of 2 t,- e systainx L r~
RA I
Ar~ (ML -4:7)
,.!~as turbines!.) ('Cias-Analysis)

POLYATSM., H.A., kand.teklm.nauk; SHATILI, A.A.; HHAINOVSKIY, Ya.S., inzh.
RABKIN, V.M., inzh.
Torch tips for burning natural gas in the combustion chambers of
gas turbine systems. Energomashinostroenie 7 no.7:34-36 J1
161, (MIRA 14:8)
(Gas turbines)

POLY-ATSKINI M.A.1 kand.tekhn.nauk; SHATILI,_A.A,,,_kand.tekhn.naiik;
FHS",YI'OV--KIY, Ya.S.,, inzh.; inzh.
Certain data on heat exchange in the combustion chamber of a gas
turbine system operating on natural gas. Teploenergetiki) 8 no.7:
68-72 Jl 161. (MMA 1-4:9)
1. 'I'SontralInyy nauchno-isoledovatel'skiy kotloturbirinyy in-
stitut imcni I.I. Polzunova i KharIkovskiy turbogeneratornyy
zavod.
(Gas turbines) (Ifeat-Transmission)

POLYATSKIN., M.A., kand,teY-hn.nauk; SHATILI, A.A., kand.tekhn.nauk;
KHAYINOVS-1KOY., Ya.s.., ir-zh.; SE01M, A. T. , inzh.
Testing the experimental GTU-50-800 combustion chamber fired with
natural gas. Teploenergetika 9 no.l.-20-24 Ja t62.
(vaRA 14~12)
1. TSentrallnyy kotloturbinnyy institut im. I.I.Polzunova i
Khartkovskiy turbinn7y zavod imeni Kirova.
(Gas turbines-Testing)
(Gas, Natural)

,-_ _~UATIL_',_A._A.. kand. tekhn.nauk
Simplified method of heat caluclation in the multiple-stage
burning of natural gas and liquid fuel. Teploenergetika 9 no.11:
91-93 N 162. (MIRA 15:10)
1. TsentralInyy kotloturbinnyy institut.
(Fuel-Combus,tion) (Boilers-Design and conati..ction)

~ffEVLEVSSKIY, P: F- ; SFATIL , A.A... lciind. tekhn.nauk,,, retsenzent;
KRYPSK lY !.L., inzh,, retsenzent 111ITARCHUK, G.A., red.
y
lzd-va., SP-'(-?l(-V"'-'KIY, IN.Z. . rp-(',izd-vaj SHCHETININA, L.T ,
tek.hn, re~-
r[Flowmeters', Raskbodomery, Izd.2,., perer. i dop. Moskva,
I
f,'ashgzlz, 1963 IS55 p. (MIRA 16~.Ll)
(Flowmeters)

S/096/63/000/005/002/011,
E194/E455
AUTHORS: Shatill A.A. Candidate of Technical Sciences,
Khaynovskiy, Ya.5., Engineer
TITLE: A~! investigation of heat exchange in an experimental
combustion chamber of a gas turbine type r'TY -50-800
(GTU-50,-800) burning natural gas.
PERIODICAL: Toploenergetika, no.5, 1963, 30-35
TEXT: A study was made of radiative and convective heat-transfer
in a large combustion chamberl-installed on a test bed in the
Kharlkovskiy turbinnyy zavodJ(Khar1kov Turbine Works). Hitherto
~little work has been done in this field for gas turbines running on~
natural gas fuel. Radiative and convective heat-transfer could
not be separated by the usual procedure of having calorimeters with',
different degrees of blackness because of heavy contamination of
the calorimeter surfaces by'dust and oil in the air delivered by
the compressors. Eight water-cooled calorimeters with blackened
surfaces were installed in'pairs in four different sections of the
combustion chamber. The calorimeters were calibrated by hot-air
blowing tests. Corrections that must be made when combustion is
Card l/ 4
q

s/o96/63/000/01)5/002/011
An investigation of heat exchange ... E194/E455
present and the calorimeter surface is at a different temperature
from that of the surrounding casing are explained. A special
eight-position thermocouple rig measured the temperature
distribution near the flametube. Hemispherical radiation radio-
meters were also used to determine the incident radiant-heat flows
in the first, third and fifth~casing shells. This device is water-
cooled, and ventilated with dry air. The heat-absorbing sphere,
4 mm in diameter, is located at the focus of an ellipsoid with
diameters of 100 and 60 mm. The instrument is calibrated in a
furnace and its sensitivity is 1200 kcal/m2 hour per degree of
reading. The temperature distribution in the combustion chamber
studied is trapezoidal. There is a sharp fall in temperature near!
the walls. Near the core of the flame the temperature remains
approximately constant over a considerable proportion of the flame
length. In this large flame tube the flow temperature near the
walls was less than that*of the walLs throughout their length.
It follows that the flame tube is cooled from within as well as
from without. The following expression gives the approximate
criterial relationship for convective heat-transfer between the,
Card 2/ 4

S/09b/b3/000/005,/002/011
An investigation of heat exchange ... E194/E455
-flame tube and the flow on the inner side
M
Nul 0.0111Re1 (6)
In some of the tests the radiant and convective components of
heat transfer were separated by means of calorimeters and hemi-
spherical radiation radiometers. Calculated and experimental
results were in agreement within 20%, which is considered
satisfactory. Graphs are plotted of the relationship between the
effective blackness of the flame and the excess-air factor,
of the spectral 'blackness' temperature of the flame in the wave
length range of 0.8 to 2.61L,which displays the typical wavy
spectrum of triatomic gases, and curves of the spectral. intensity
of radiation of black, grey and actual flame for a flame tem]~erature
of 1823*K. The data obtained can be used to draw up a beat-flow i_
balance on the wall of the~fiame tube with accuracy sufficient for
practical purposes; similar calculations can be made for other
combustion chambers of similar design burning natural gas. - In
making these calculations it is recommended that the coefficient
Card 3/4

There are 7 figures.
ASSOCIATION: TsKTI - KhTGZ
Card 4/4
s/096/63/000/005/002/011
An investigation of heat exchange ... B194/E455
of thermal effectiveness should be calculated by the following
expression
Tct I
t9)
Ect
TF CT
and the degree of blackness of the furnace radiation ET Y
b
ET EF (12)
C + W
F F
where E,t and cT are the degrees of blackness of the wall and
the furnace radiation respectively, EF - the effective idegree of
blackness of the flame, Tct - wall-temperature and Tp - flame
temperature. The heat-transfer coefficients from the outer and,
-inner surfaces of the casings should be calculated in the
following expressions
Nu. = 0.043Re 0.8 NU O.OllRe o.8
-2 1 1

SiLATILI, A.A,., kand. tekhn. nauk
Effect of heat supply on the hydraulic characteristics of the
combustion chamber of a gas turbine system. Teploenergetika
10 no.9:15-19 S 163. (MM 16:10)
1. TSentrallnyy kotloturbinnyy institut.
(Gas turbines)

ACCESSION NR: ep S/0096/6
API,0346;)4 4/000/005/0048/0053
AUTHORS: Shatill, A. A. (Candidate of technical sciences); Murashko, V. D.
(En,,inear)
TITLE: Application of characteristic method in gas turbine combustion chamber
investigations
SOUFCE; Toploonergetika, no. 5, 1964, 48-53
TOPIC TAGS: combustion process, combustion chamber, pure diffusion, heat
balanco:p adiabatic limit, heat capacity, excess coefficient, diffusion time
ARST,RACT- Several characteristic combustion processes were investigateq.and
applied to combustion chamber studies in CTU gas turbines. Combustion types
considered were: pure kinetic, pure diffusion, and an intermediate method de-
scribed by L. A. Vulis (Teplovoy rezhim goreniya. Gosenergoizdat, 1954). A small
and a large combustion chamber were studied with both plane and conical type con-
structions. The heat balance equation for the combustion chamber becomes
+ 40 CP. (r TJ1
where coefficient characterizing the adiabatic-iiiite of the chambei
L
C.-,d 113

ACCESSION UR: AP4034654
H
(0.85 4- ~ -