SCIENTIFIC ABSTRACT BESSONOV, A. F. - BESSONOV, A. P.

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• Collection: Scientific Abstracts
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• Sequence Number: 7
• Publication Date: December 31, 1967
• Content Type: SCIENCEAB

21220
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AUTHORS: Strekalovskiy, V.N., P_t~ ~A,1~., Vlasov, VG. and
Sidorenko, F.A.
TITLE: Phase Transformations During Reduction and Oxydation
of Uranium Oxides
PERIODICAL: Fizika metallov i metallovedeniye, 1961, Vol~ll,
No-3,

PP.400-403 + 1 plate

TEXT: The uranium-oxygen system has
lately attracted a great

deal of attention owing to the
possibility of using uranium

oxides (dioxide in particular) in
the manufacture of ceramic fuel

elements. However, the
experimental work has been mainly

confined to studies of
oxydation or thermal decomposition of

uranium oxides, and the
object of the present in-iestigation was to

study (a) the
kinetics of hydrogen raduction of' amorphous U03

and green U308
at 300 to 7000C, W the process of oxydation of

U02 in air,
oxygen and C02 at 165 to 860*C and (_-) the phase

transformations taking place during these reactions, The
results

of the study of kinetics of the reduction process are
reproduced

schematically in Fig.1, where the rate of reduction
(A in

arbitrary units) is plotted against the overall
--amposition of the

Card 115

21,220
Phase Transformations
S/126/61/oil/003/007/017
E193/E483
resultant product, i.e. against the oxygen/uranium (O/U) ratio.
It is pointed out, in this connection, that. neither the rates
of reduction of U03 and U08, nor the energy barrie:s during the
crystallo-chemical transformations of these oxides are the same;
thus, for instance, hydrogen reduction Of U03 begins at 350*C,
the
corresponding temperature for U08 being 4500C. In addition,
reduction of U03 at temperatures < 500% practically ceases when
the oxide reaches the oxide content corresponding to U02-33; at
higher temperatures, U409 and oxides with a still lower oxygen
content are produced. The results of the kinetic studies were
correlated with the results of X-ray diffraction analysis of the
products of the reduction of U308, and the following conclusions
were reached regarding the phase transformations, taking place
during the reduction process. In the initial stages, UiO8
gradually loses its oxygen, this process continuing unti the
starting material is reduced to 46.9% (100% reduction
corresponding
to complete conversion Of U03 to U02) which corresponds to the
overall composition of the product given by the formula U02-539;
at this stage. the X-ray diffraction pattern still shows the
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S/126/61/oll/003/007/017
Phase Transformations E193/E483
lines of the U308 phase; the lattice parameters of the initial
phase have changed but, no lines of a new phase have yet
appeared;
at 62 and 69% reduction, the lines of the starting oxide are
still
present in the X-ray pattern and lines of the cubic U407 phase
appear,, at 75% reduction, the U308 lines completely disappear
and
only the U407 lines remain; after a further decrease in the
oxygen content, the crystal structure of the oxide remains cubic
but the lattice parameter increases. Reduction of U03 takes
place in a similar manner, the crystalline U308phase being formed
directly from the amorphous U03 which does not pass through the
crystalline form during this process. The whole reduction process
can be represented in the following manner-.
Amorphous U03--JSolid solution, based on U02,6 -IU02.2_4UO2+x*
Regarding the process of oxydation of U02 in air or in oxygen, it
can be represented by;, -+Solid solution, based on U02.67,
U02 ' U02 + x U02-36 + 0.05
The tetragonal phases (U02.32 0.0.1, U02.35, U02.3?, U02A1)
whose presence can be inferred from the kinetics of the process
studied, are unstable and decompose to form U409 and U308, When
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Phase Transformations E193/E483
the 6xydation reaction takes place (in air or oxygen) at
temperatures >4000C, no formation of the tetragonal phases
occurs,
and the process proceeds according tot
U02-+UO2 + x_')'UO2,25-4Solid solution, based on U02,67
Finally, it was established that U02 does not oxidize in carbon
dioxlde~ There are 3 figures and 12 references,,, 8 Soviet and
4 non-Soviet,
ASSOCIATIONg Urallskiy politekhnicheskiy institut im. S.M.Kirova
(Ural Polytechnical Institute imeni S.M.Kirov)
SUBMITTEDi juiy A, ig6o
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'on rl'~n lli?n "Kh 'on
9
SUOT,417wjojguu-u asuqd
LTO/Z00/~00/TTO/T9/99T/S

24484
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0 7 10 E193/E483
AUTHORS: Bessonov, A.F. and Vlasov., V.G.
TITLE- Phase transformations during oxidation of metallic
uranium '
PERIODICAL: Fizika metallov i metallovedeniye, 1961, Vol.11,
No.6,
PP-957-959
TEXT: 7ne object of the present investigation was to study
oxidation of uranium in air and carbon dioxide. To this end,
specimens (4 x 2 x 15 mm),,were degreased, pickled in
concentrated
HN03, washed in alcohol and held for 15 minutes in air at
various
temperatures between 20 and'3500C, or in C02 at 400 to 9000C,
after
which the surface of the specimens were examined by X-ray
diffraction. The results are reproduced-in Fig.1, showing the
X-ray diffraction pattern of the surface of uranium specimens
after
(a) 8 days exposure to air at room temperature, (4) oxidation at
1000C, (8) oxidation at 2050C, (?,) oxidation at 3000C,
Cb) oxidation at 350%, (e) removal of the outer, loose, oxide
layer. An X-ray diffraction pattern of uranium, oxidized in C02
is reproduced in the paper. The following conclusions were
reached.
1) The phase transformations taking place during oxidation of
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24484
S/126/61/oli/oo6/m/oil
Phase transformations E193/E483
uranium in air at 265 to 4OO*C can be represented by:
Umetarl-ta U02-1W& U02+x-+P U09-*U307 -*solid solutions based on
U02.67
2) The constitution diagram of the U-0 system is repeated in the
phases which constitute the consecutive oxide layers of scale,
formed on uranium in air at atmospheric pressure in the
temperature
interval studied. 3) Metallic uranium, heated in C02, oxidizes to
U02 only. There are 2 figures and 8 references: 7 Soviet-bloc and
1 non-Soviet-bloc. The reference to an English language
publication reads as follows: Blackburn P., Weissbart J.,
Gulbransen E., J.Phys.chem., 1958, 62, 8.
ASSOCIATION: Urallskiy politekhnicheskiy institut im. S.M.Kirova.
(Ural Polytechnical Institute Imeni. S.M.Kirov)
SUBMITTED: December 15, 1960
Card 2/3

Phase transformations
Fig.l.
Ilb
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4,

S/ 2~485
oil/oWoli/oll
0 E073/E335
V~Tlqdig*
BessonQv. A.Fog.Borisov, B.S. aid Vlasov, V.Qq
TITLE: Investigation of the Structure of the Primary Oxide
Film on 'Uranium
PERIODICAL: F--*zika metallov i metallovedeniye, 1961, Vol. 11,
iio. 6, pp. 959 - 960
TEXT: --n studying the mechanism of oxidation of metals
invosti,:,ation of the structure of the primary oxide film formed
in air at room temperature during the initial oxid&tion'period is
of great importance. For some metals the structure of the films
.Lornod durinZ the initial period of oxidation does not differ
~rosn those formed during later stages of o.-idation. For a
.numoer of other metals, for instance, iron and its alloys,
a film of a particular structure (type J-Fe 0 ) forms during
2 3
i
t.:"e initial period of oxidation. The primary oxide film s
a -.1rotective one for most metals; it grows to some limit
thickness, then stops growing and prevents further oxidation.
'D
The kinetics of -rowth of the primary films depends on a
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24485
s/126/61/oil/oWoll/oll
Investigation of the Structure ... E073/E335
number of factors and so far no satisfactory theory on this
process exists. The authors carried out investigations on
uranium of 99.80,!l purity which, after rolling, was
annealed at
850 OC for six hours in vacuum. Plate specimens 10 X 5 x 3 mm
were initially ground with enery paper of varying coarseness
and lapped by a ring using high-grado alumina. After
polishing
the ring was moistened with benzol or ethyl alcohol to
prevent
access of air to the polished surface. Microscopic investi-
,gations have shown that the surface was peppered with fine
crystals and the number and size of the crystals increased
rapidly. For determinincr the structure of this primary film
electron-diffraction studies were made. For removin- the
scale films the specimens were etched in nitric acid for 10
rain
and then washed several times in ethyl alcohol. Oxidation was
in air at room temperature for durations of 10, 30, 120 and
240 min. In the socond series of experiments, the specimen,
after having been taken out of the alcohol (wet), was placed
im:11ediately into the chamber of the electron-diffraction
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24485
S/126/61/oll/oWoll/oli
investigation of the Structure E073/E335
apparatus from which the air was evacuated so that the
specimen
surface interacted only with the air which remained in the
cha,mber of the electron-diffraction camera. Part of the
specimens
were subjected to el ectron-dif fraction investigations
immediately
after poliohinr~ (i..ithoiat etching); bach reflection
pictures
'%-rere ta%en. The obtained interplane distances %.rere
compared
with X-ray data, obtained by the powder method for uranium
o::ides. TI-ie investigations revealed a cubic phase on
uranium
o:Ude with a lattic constant of a = 5A5 A for all the
specimens,
wIlAch corresponds to the oxide U02' In a second series of
experiments the electron-diffraction patterns contained
rcflwces'
.Lrom the metallic uranium in addition to lines of the phase
UOV
This indicates that in this case the entire thiclmess of the
oxide film participated in the diffraction and that the
primary
oxide film of uranium consists solely of the paase UOP. From
the widening of the Debye lines the size of the forming UO
-4 It. 2
crystals could be determined, which was about 10 cni. Thus,
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24485
suilulAcc Zin caps); Givea Na=s
Country: Yugoslavia
-7
Aca&*mic D_-E_~rees; /not given"/.
Af:eiliation. Veterinary Station CVeterinaraka stanica), Imotaki
Sourcet Belgradep .erivarski SjUnik No 6o 1961t pp 529-531.
Data: *Field Rminotow-in Nentraumatic Indigestion Just Before
Calvinsol
Authorst
BESTAL V.
E , D.
1.3f,

S/126/61/012/003/011/021
E193/E135
AUTHORS: Bessonov, A.F., and Vlasov, V.G.
TITLE: Concerning the mechanism of oxydation of
metallic uranium
PERIODICAL: Fizika metallov i metallovedeniye, vol.12, no.3,
1961,
403-40
TEXT% Effective measures against oxydation during the
preparation of metals or in service can be applied only if the
mechanism of this process is properly understood. Hence the
present investigation, in which the kinetics of oxydation of
uranium were studied by the gravimetric method and the
constitution of the scale formed on uranium under var.Jous
conditions was determined by X-ray diffraction, microscopic, and
electron diffraction analyses. The experiments were carried out
on 99.8% pure uranium specimens, degreased, pickled in
concentrated
HN039 and washed in ethyl alcohol. The oxydation tests were
carried out in dry air and oxygen at various temperatures and
pressures; some results are reproduced gra hically. In Fig.1
the specific increase in weight (&M/s x __t, mg/cm2) of uranium
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J

Concerning the mechanism of oxydation.. s/i26/61/012/003/011/021
E193/E135
heated in air is plotted against time (minutes), curves 1-6
relating to tests conducted at 250, 300, 350, 400, 600 and 760 OC
respectively. The kinetics of oxydation of uranium
in oxygen are
illustrated in the same manner in Fig.2, where curves 1-4 relate
to results obtained at 250, 300, 330 and 400 OC. It was
established that the effect of pressure (p, mm Hg) on the rate of
oxydation (v, mg/cm2) in minutes of uranium in air at 400 OC is
described by 4f T
for pressures higher than 200 Mm Hg, and by
v a2 P (4)
for pressures lower than 200 mm Hg. The oxydation rate of
uranium in oxygen at 300 OC under pressures ranging from 5 to
550 mm H9 is given by v = a3 0/--P.
The rate of oxydation was not affected at all by forced
circulation of oxygen and only to a small extent by circulation of
air at pressures > 200 mm Hg; at p < 200 mm Hg forced
Card 21.6.

Concerning the mechanism o -f oxydat-'on...
S/126/61/012/003/011/021
E193/EI35
circulation of air increased the oxydation rate, this effect
becoming more pronounced at higher temperatures. The activation
energy of the process studied was 18 and 4.6 kcal/mol, when the
reaction took place in air below and above 400 OC, respectively,
and 17 kcal/mol for oxydation in oxygen below 400 OC. The oxide
film formed on uranium in air at room temperature had a
crystalline structure and consisted exclusively of U02, The
constitution of scale formed on uranium in air at 26o-4oo OC was
determined by the present authors in an earlier investigation:
the composition of the consecutive layers starting from metallic
titanium (Umet) is
U(met)-.) a UO2 Ot UO 2+ UO2NO 9 U307 _> U 308
Although the molecular volume, U., of uranium oxide is larger
than
the atomic -volume, Um, of uranium, the oxide scale formed on
this
metal does not protect it from further oxydation. This is
attributed by the present authors to the coarsely-crystalline
nature of the oxide film formed at room temperature, and also to
the fact that large internal stresses are set up in the oxide
film
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Concerning the mechanism of oxydation ...
S/126/61/012/003/011/021
E193/EI35
owing to the large difference between the specific volumes of the
uranium oxide and uranium whose ratio varies between 1.9 and 2.6.
To determine the relative roles played in the oxydation of
uranium by the diffusion of oxygen and metal, tests were carried
out in air at 350 OC on specimens fitted with inert platinum
markers in the form of 0.02 mm thick wire; irrespective of the
duration of the test, the platinum marker remained on the surface
of the oxide scale. The results of the present investigation are
discussed in relation to various published data and it i3
concluded that diffusion of oxygen through the dense triplex
"02-73* aU02,x--)~ OU02(U409) layer of oxides with a cubic
crystal
lattice which adheres strongly to uranium, governs the kinetics
of
oxydation of uranium. There are 4 figures and 15 references:
10 Soviet-bloc and 5 non-Soviet-bloc. The English language
references read as follows:
Ref-5: N.B. Pilling, R.E. Bedworth. Inst. Met., 529, Vol.29,
1923.
Ref-7: P. Blackburn, 1. Weissbart, E.I. Gulbransen. Phys. Chew.,
1958, voi.62, 8.
Ref.10: F.I. Gronvold, Inorg. Nucl. Chem., 1955, Vol.1, 357.
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Concerning the mechanism of oxydation... S/126/61/012/003/011/021
E193/E135
ASSOCIATION: Urallskiy politekhnicheskiy inBtitut im. S.M. Kirova
(Ural Polytechnical Institute imeni S.M. Kirov)
SUBMITTED: February 6, 1961
Am to,' 1#01
Fig.1
Card 5/j9,,-
B,oe,w.q, NUy

BESSONOV y A, VLASOV , V, G.
Interaction of uranium metal with carbon
dioxide. Fiz. met.
metalloved. 12 no.5-.775-778 N 161, (MIRA 14-12)
1. Urallskiy politekh
t:lt tut imeni S.M.Korova.
(=heusk
m!~M~ i
lograpby)
(Carbon dioxide)

V.G.; SHAlAGINOV, V.N.; BESSONOV A.F.;
STREKALOVSKIY, V.N.
VLASOV, Z.-
Change of the design of a glass pressure regulator.
Trudy Ural.
politekh.inst.no.12L102-103 162. (MM 16:5)
(Pressure regulators)

39732
C
S/1 600/004/002/003
Aoo6/A lo 1
AUTHORS; Bessonov, A. F., Vlasov, V. 0.
TITLE: Kinetics of uranium oxidation with air, oxygen and
carbon dioxide
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Tsvetnaya
metallurgiya,
no. 4, 1962,. 137 - 142
TEXT: Oxidation of uranium metal was studied in aggressive gas
media at
various temperatures a;jd pressures of the oxidizing gas, for
the purpose of ob-
taining kinetic charact' ess. Com-
.Fristics and revealing the mechanism of the proc
mercially pure uranium.-Metal plates (2,5xl.5xl.5 mm) were
oxidized in a high-vac-
ii9m device. The true ratp of the oxidation process was
graphically determined from
t1Tp inclination angle of-the tangent to the"oxidation
degree-versus-time" curve.
The apparent activatioW~iqnergy was calculated with the aid of
the Arrhenius equa-
tibn. The average composition of the oxidation product was
determined by calculat-
ing the increase in weight of the specimen during oxidation
and the loss in weight
during reduction with hydrogen. It was found that the
oxidation process in all the
given ag4ressive media obeys the temporar7 linear law; the
rate of the process is
proportional to the square root from air and oxygen pressure.
The possible mechM
ism of the uranium oxidation is analyzed with the aid of
Soviet and foreign
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S/149/62/bc,0/004/002~003
Kinetics of uranium oxidation with air,... A006IA101
sources (Ref. 9; P. Chiotti, H. Klepfer, R. White.
Trans.Amer.Soc.Metals, 51, 772
(1959)). It was found that the diffusion of oxygen atoms through
a dense layer of
uranium dioxide was the decisive limiting stage. There are 4
figures.
ASSOCIATION: Ural'skly politikhnicheskly institut (Ural
Polytechnic Institute)
SUalITTED: July 25, 1960
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STREKALOVSKIY, V.N.; BESSONOV, A.F.; ZHUKOVSKIY,
V.M.; NEUYMINJ, A.D.
Electric properties of uranium oxides. Trudy
Inst. elektro-
khim. UFAN SSSR n0-3:155-159 162. (MIRA 16:6)
(Uranium oxides-Electric properties)

S/149/62/000/005/004/008
Aoo6/AlOl
AMHORS: Vlasov, V. G., Bessonov, A. F.
TITLE: Oxidation of uranium dioxide
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Tsvetnaya
metallurgiya,
no. 5, 1962, 113 - 122
TEXT: Since the opinions of scientists differ on the mechanism
of the
oxidation process of uranium dioxide, the gathering of
experimental data in this
field is imperative. The authors studied kinetics of uranium
dioxide oxidation
in different gas media and investigated simultaneously the
effect of the admix-
ture of alkali metal carbonates and Th03, ZrO2 and TiO2 oxides
upon the kinetic
characteristics of the oxidation process. Kinetics of
oxidation with air oxygen
was studied within a range of 165 to BOOOC, at 2.5 - 600 mm Hg
atmospheric p~res-
sure. The results are shown in Graph (2). Determined values of
the apparent ac-
tivation energy at different oxidation degrees range from 34.6
kcal/mole at 28%
oxidation to 39.4 kcal/mole at 9(Yo' oxidation. Kinetic
characteristics of U02
oxidation with pure oxygen were investigated in a range of 125
to 3300C and
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s/149/62/000/005/004/008
Oxidation of uranium dioxide Aoo6/Aiol
PO, = 100 mm 11g. The following schemes of phase transformations
are proposed:
C
U02.04 - U02+xmax _"02.25 .- U02-36+0-05 -"02.6-xmax ---)'U02.67
for the 260 to
3900C range, and U02.04 --> U02+x 111ax -*:~ U02.25 --P
U02.6-xmax -~,U02.67 for the 400 to
8000C range. The effect of different admixtures upon the process
is given in
Figures 5 and 6. Due to the liberation of considerable amounts
of heat in oxida-
tion Of U02 to U308' local overheating occurs In the solid
phases, entailing a
sharp increase in the process rate on these spots, so that
several phase transi-
tion's take place. This explains the jumplike evolution of the
process in the
150 - 2000C range. The inhibiting effect Of K2CO admixtures on
U02 oxidation
V
at 1850C is apparently due.to the fact that at t12s temperature
the migration of
potassium ions from the carbonate crystal lattice into that Of
U02 is little
probable. Simultaneously the admixture is in a close contact
with U02 and screers
a portion of its surface. As a result, the surface for oxygen
adsorption from
the gaseou3 phase is reduced and the total rate of the oxidation
process de-
creases. At 3300C the accelerating effect of alkali metal
carbonates appears on
those stages where a substantial reconstruction of the crystal
lattice takes
place. Apparently the catalytic effect of carbonates consists in
the fact that
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Oxidation of uranium dioxide
S/149/62/000/005/004/008
Aoo6/Aiol
their particles.are crystallization centers of a new phase which
eliminates the
induction period. There are 6 figures.
ASSOCIATION: Ural'skiy politekhnicheskiy institut (Ural
Polytechnic Institute)
SUBMITTED: April 22, 1961
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s/14q/62/ooO/oo5/0o4/0o8
Oxidation'of uranium dioxide Aoo6/Aloi
Figure 2. Isotherms of U02 oxidation with air oxygen (at constant
200 mm llg air
pressure) 2r. -
Zj.
,a!:
5
2jj .
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Oxidation of uranium d1oxtdc
s/09/62/000/0c)5/004/608
Aoo6/A i o 1
Figure 5. Isotherms of' UOn oxidation with air oxygen at 1850C
(1 and 2) and at
- 6) 'thout admixtures (2 and 3) and with admixtures of
3300C (3 wj
K2('03 (1 and 4 N Li
aOC03 2C03 (6).
U)
cd
0
zi
`4 ~;
0 4t
cu
0
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Oxidation of uranium dioxide
,3/14g/62/()00/005/004/008
Aoo6/Alol
Figure 6. Isotherms of U02 oxidation with air oxygen at
330OC-Without admix-
ture (1) and with admixture of ThO2 (2); Zr02 (3) and T102 (4)
cd
2.40
227
2 Q 4Je
~4
X
0
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S/126/62/014/003/021/022
E039/E42O
AUTHORS: Bessonov, A.F., Vlasov, V.G.
TITLE: The interaction of uranium with nitrogen
PERIODICAL: FiziXa metallov i metallovedeniye, v.14, no.3, 196z,
478-479
TEXT: The kinetic processes of oxidation have been investigated
previously by the authors. This is a continuation.and the
formation of uranium nitride is investi7gated. The apparatus and
method is described.in the previous paper, the nitrogen gas being
obtained from liquid nitrogen and purified by passing over
titanium at 8000c and CaC12- The basic investigation is carried
out at 200 mm Ng in the temperature range.400 to 9200C.
Initially the reaction pr .oceeds parabolically with time for
about 0.5 min and then continues linearly for all temperatures.
No reaction is observed below 400*C. At 590 and 710*c the rate
of reaction is proportional to the square root of the pressure.
Circulation of the nitrogen does not produce any effect on the
reaction rate. The activation energy of the process at 6300C is
16 kcal/mole and at higher temperatures 7 kcal/mole,
C~rd 1/2

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The interaction of uranium E039/E420
X-ray analysis of the nitride formed at 9200C shows that it has
a,
face-centred cubic lattice. The initial rate of reaction is
modified by the presence of the U02 layer on the uranium surface
and the linear part is associated with the diffusion of the
nitrogen through the nitride layer. It is suggested that the
square root dependence of the rate of reactiaii'on,pressure is
due
to the dissociation of the nitrogen molecules.into atoms during
the
diffusion process through the nitride layer. The decrease in
activation energy above 630'C in explained on the basis of the
.U a to Up transition. There is I figure.
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D202 302
AUTHORS: Bessonov, A. P., Vlasov, V. G. and Strekalovskiy,V.
N.
TITLE; Cyclic oxidation-reduction of uranium oxides
PERIODICAL: Zhurnal prikladnoy khimii, v. 35, no. 3, 1962,
657-0660
TEXT; The subject of this study was the elucidation of the
fol-
lowing questions: 1) Which phases are formed during the
oxidation
0
and reduction processes of active uranium dioxide and
urano-urani-
um. oxide? 2) Can the tetragonal phase be obtained at
temperatures
below 400 - 5000C? 3) The oxidation kinetics of active
uranium di-
oxide, unstable at room temperature. The work is a
repetition of
investigations previously published by Western scientists.
The
authors state -that their resulta Lire in good agreement
with those
given in Western literature. The following phases were found
dur-
ing the cyclic oxidation and reduction of uranium oxides in
the
temperature range from 20 to 5000C: U021 '02�Xl U02.25'
U02-36�Xl
UO 2.6�X' U0 2.67* The tetragonal phase does exist as a
stable one
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Cyclic oxidation-reduction ...
S/08 62/035/003/017/024
D202X302
at some definite temperature range between 5000C and room
tempera-
ture. There are 3 figures and 8 references; 1 Soviet-bloc
and 7
non-Soviet-bloc. The 4 most recent references to the
English-lan-
guage publications read as follows: R. W. Willardson, I.
1-loody and
H. Goering, J. Inorg. Nuclear Chem., 6, 19-38, 19~8; 0.
Runnols,
Nucleonics, 17, 104-111, 1959; A. Arrot and I. Goldman,
Phys. Rev.,
108, 948, 1957; F. Blackburn, I. Weissbart and E.
Gulbransen, J.
Phys. Chem., 62, 8, 12, 1958.
SUBMITTED: January 16, 1961
Card 2/2
0

STREVAU'VS.-K-TY, V.N.; NEU)TT, A.D.;
B:-,,"'SCN',,V, A.F.
Flectric conductivity of hIghor uranium oxides in a
hydrogen
stream. Zhur. fiz. khim. 36 no.6;:1355-1358 Je'62
17-7)
1. Institut elektrokhimii Ural'--kogo filiala V4
SSSR.

S/126/63/015/003/024/025
E039/E1135
AUTHORS: 'Besson2y,_A-_F,, Vlasovi V.G.
TITLE: On the 'question of the high temperature oxidation of
metallic'uranium
PERIODICAL: Fizika metallov i metallovedeniye, V.15, no.3, 1963,
477-478
TEXT,. Tho oxidation of uranium by C02 at temperattiros above
9000C
is investigated. The uranium (technical purity 99.8%) in the form
of plates is first degreased in benzene, etched with cold
concentrated nitric acid'and then thoroughly washed in ethyl
alcohol. Isotherms are ineasured at temperatures of 900, 950 and
10000C-for a C02 pressure,of 420 mm 11g. It is shown that the
dependence of the rate of.oxidation of uranium on the pre.saure
of
C02 is given by
v = ap n
C02
1
where n = 7 ; a is-a temperature consiant; PC02 is the
pressure Of C02- It is also shown that the rate of circulation of
C02 has practically no effect on the reaction rate. The
Card 1/3

S/.126/63/015/003/024/025
On the question of the high ... B039/F,433
-,,--disintegration of the as mple is caused by the phase changes
772* 6 2 Ua
UY -~,. Up which produces an inerease-in volume and -Up..~4
which produces a decrease in volume. X-ray diffraction analysis
shows that therels a layer of UO on the surface of the U02- This
is also detected chemically together with the mono-nitride and mono-
carbide in the surface scale of uranium oxidized at C02 at 10000C.
The catalytic effect.of U02 is demonstrated by comparing the rates
of oxidation of pure iron powder and a mixture' of iron powder and
U02 (205'a by wt Fe). The U02 produces a significant increase in
the rate of oxidation of the iron. 'When the temperature of
uranium is increased from'900 to.1000.*C the rato of oxidation
decreases owing to an increase in density.of the UO-. At
temperatures < 7800C the oxidation is accomplished by oxygen
diffusing through the oxide layer but at temperatures > 9000C the
rate of diffusion of the metal through the scale becbmes
significant, There are 2'figurea.
ASSOCIATION:,Urallskiy politekhnipheakiy institut im. S.M.Kirova
(Ural PolytechniSal Institute.imeni S.M.Kirov)
Card 2/3

S/126/63/015/003/024/025-
On they- question or the high ... r,039/B435
SUBMITTED: September 2,'1962 (initially)
October 6, 1962 (after revIslon)
Card 3/3

~,MCL Of Lbe E,Irface stal.e of 3ay~.--,s on
procosS of magmc~sftv powders. ljorosli. met. 5 1656
0-1-li"A 19~5)
1. VosLochpyr r,--,,jo'tini;-is--~iclovatellskiy j
prc,:fekLtiyy in---i
ogneuoornoy promps'niermost2, -S,.rcr6]ovsl,.

L 1253-66.. 3e(e)/31T(m)/T - Wh'
rWUC=0N NR: AP5021510 UR/0131/65/000/008/0030/0034
666.76.0012
AUT14OR- Bessonov A F U~nj~jev, V. M.
TITLE: Investigation of phase changes in the systems of
MgO-Fe2O3 and
MgO-FeO(Fe2O3) during heating and cooling in air
SOURCE: Ogneuproy, no. 8, 1965, 30-34
TOPIC TAGS: refractory compound, magnesium oxide, iron oxide,
electric
resistance, phase analysis, solid kinetics
ABSTRACT: The article considers phase changes and chemical
interactions under
nonequilibrium conditi ns, that is, under the actual
opLarating conditions of these
refractory materials7A special apparatus permitted
simultaneous measurement,.
6~_e!66irical resis' and X-ray analysis of the samples at
different tempera-
tures. The compositions of the samples were: 90% MgO and
10-'7j Fe2O3 and
90% MgO and 1016 FeO. The samples were prepared in tablet
forizi 3-4 mm thick
by mixing finely ground powders, with subsequent pressing.
The samples were
placed in a high temperature chamber which permitted heating
to 1500 C, with
r-M 1/2

i, 1253-66
ACCESSION NR: AP5021510
attachment of a URS-501 diffractometer. They were heated at a rate
of 0. 17 de-
grees/sec with practically no temperature gradient across the
sample. The
phase composition of each sample was studied by continuous X-ray
photography in
the angular range of 200-270301. For some samples complete X-ray
photos were
taken over the angular range of 11-410. The same measurements were
made with
cooling of the samples and subsequent reheating. Results for both
types of sam-
ples in the given temperature interval are shown graphically.
Basically, the
article gives a qualitative picture of the kinetics of phase
changes in the systems
MgO-Fe,03 and MgO-FeO(Fe 03) at atmospheric air pressure and with
continu-
ous heating to 1400 C. In parficular, it is shown that
magnesioferrite under these
conditions forms at 290 C. Orig. art. has: 8 figures
ASSOCIATION: Vostochnyy institut ogneuporov (Eastern Institute for
RefractoFY___,___
SUBMITTED: 00 ENCL: 00 SUB CODE: MM, IC
NR REF SOV: 006 OTHER: 005
Card 2/2

BFS'014OV, A.F*,t 1UTIVOTSEV, V.M,; !AROSLAUSEV, A,.'~,
:nvestigating the kinetics of phase transformations in
a 5peclmen
of magnesium and copper oxides. -Izv. vys. uctleb,
zav,,,~ tavet. met..
(~171j,lt 18~
,JV!
8 no.5~.49-53 165.
1. Vrallskiy politeklinicheskiy institut, kafe.3ra
mesta~bll:,~I-i
tyazhelykh t2vetnykh metallcv -., Vostochnyy institar,
ngneuporov.

BESSONOV,-.A.S.t kand.veter.nauk
Diagnoais of trichinelliasis. Voterinariia 41
no.10:85-86
0 164. (FJRA 18:1.1)
1. Vsesoyuznyy institut gellmintologii imeni
akademika
Skryabina.

~';T(i-IiVE'.:P(w) EPF(c'/F
St 1-;G 'E;'IAkZ- ViTI E!
Q
p7-
ACC55-'-J0?,' JUP.-5,012504 LPi~/0032/65/031/005/C&'O/C-,,21
5)9-:C6.07
:MUIIJIOPS?~ Devsonov, A. F,; Untlyantsev, V. H.
TIME: A device for the simil-taneous high temperature plotting of
cumes of
slectrical conductivity and x-ray patterns of solid oxidpA
SOURCE: Zavodskaya Iaboratorlya,.V. 31, no. 5, 1965, 620-621
r oxide electric conductivity, high tempara-
TOPIC TAGS: x ray diffraction stut
dnstrumvht. measuring apparatus
ture 3G I audio frequency gen rator, RNSH
autotransformer., 531M 220 0.75 voltage regulator, FSR 03 automatic
potentiom;rtor,
PP potentiometer, Ronionster URS 50334 goniometer
j O~SOA
-LOMMM, A devicq was developed Xor providing sim4;p=eDuS May
ana-l-v-sia/and
I~elsctrical conductivitz measurements of Solid Oxlded~~t high
temperatures.R'Dy
nt SI-M,11 I
B~alg--LHF t-wo types of r-easurems a- T'nnaously, th problem of the
ccnqgrue--~o
of these meaDurements at high temperatures has been eliminated. The
glectrical
conductivity meaaurenents are made with a standard 14heatstons
bri&,ge (Fig. 1 ot
the Enclosure) In which R is the regulated resiatance for
determining, ho
t
3
lance R x of the specimen., and R.4 ip the Bta nda=d resistance for
periodicaLly
C rd :L/

L 53592-65
ACCESSION IM: AP5012504
Calibrating ths bridge. A capacitor box (1) is connected to one
log. A 'G-1
audio frequemcy generator (IWO-5000 cps) in oro diagoiial
preventu pro-electrode
iT)o1arization. An oacillograph (3) in the other bridge diagonal
serves as a 7-ero
indicatlor. AD RIISE-55 autotransforner (6) controls the heater
located in 'Uia high
terperature chanber (5). A SME-220-0.75 voltage regulator (7)
elini-nates voltage
fluctuations. A FISR-03 automatic potentiometer (8) is used for
recording and
regulatinr7 the specim-an temperature, and a P? potentiometer (9)
is used for fire
+
1.-30 tenuerature neasuraments. The heater (7W,. Pt + 30% Rh) can
heat the hori-
-o temperatures
zontal tiibular furnace (attached to the vater-cooled casing) up
4V
of 1500C. The x-ray camera, uhich can be positioned in t%,T
dimnsions by tl,,o
lunners,, is nounted on either a LTS-501 or a UIRLS-50311
gonioneter. The corunda-r-
heater block has a 10-12-= hole in which the specinen is placed
for its conductiv-
Ry measuren-ent. no furr-ace is surrounded by lightweight bri-eks
and its ends are
_C,
sealed with therrizal insulation disks. ' 'Fhe x-ray beam slit's
are covered with
nickel foal. There are t-wo slit varia-tions: the side slit
Mrm-Ittimg an an.-alar
irange of 500; the end slit with an angular range of 720 with
unit URS-501 or of
821) with URS-501214. -In test masuremmants, in addition to the
Pt-PtRlh thermocouple,
tomparat-ares iTore controlled by otud~rizg the %-bray patterns
of platinum, uhich
vary with te=eraiturs in a Imown vay, Test measurements gave
excellent results.
Card 2/4

ACITESSION SIR: AP501-125OX
ov-ig. art. han: 2 figures,
AS 'MOULMCMI.- Vo3toohw nauchno-ImiledovatelloMy i proyoktTwy
institut
ogrEmpornoy prm7,shlor-n6sti, (I~Roterz) Scientific Rrmearch nnd
Doviryi ImolAtnto of
the RvLmot;n~y industx-1)
SMAJTIED.- 00 ENCL: 01 SUB GODE:TD,- &H
INO RU SOV., 003 OTHER,., OW

!,.F. ; STREKALOIK.~K FY, V..N. ; N~% UY!-!l IN,
Ilranium dioxide oxidation st-.icfled by thc, -f
alecAric conductIvIty, X-ray dlf'fr.,Ant~cm, and
Zhur.fiz.]~Illm. 39 no.7.~1708-1711 -JI lb5-
(MURA IL8:8)

9
L 1657-66 EWT(m)/EPF(r.)-2/~KG(m)/Wp(t)/W(W
__1JP CL) M JD WV1 JG
;,ACCESSION NR: AP5021417 UR/0076/65/039/008/1932/1937
541.13t541.17
AUTHOR: Bessonov, A. F.; Ust'yantsev, V. M.
TITLE: Study of certain oxide systems with the aid of a
high-tenperature device
zthe simultaneous measurement of the electrical resistance and
x-ray diffraction
'analysis of samples
!SOURCE: Zhurnal fizicheskoy khimii, v* 39, no. 8, 1965,
1932-1937
JOPIC TAGS: electrical resistance measurement, x-ray diffraction
analysis zirconi-
lum oxide phase analysis
iABSTRACT: The properties of ZrO - MgO and Zr02 - Y203
Compositions (taken in the
2
iratio of 73:25 and 93:7 mole % respectively), whicS-were
pressed and sinterred at
I
!16000C, were studied as a function of temperature by means of a
novel device which
ipermitted the simultaneous measurement of electrical resistance
and x-ray diffrac
analysis. A wiring diagram of the device is given. 'The phase
transformations
iof Zr02 were investigated, and the electrical resistance method
was found to be mor(
;sensitive than the x-ray method in the identification of the
phases formed during
Card 1/2

L 1657-"
iACCESS10N NR: AP5021417
~beating
or cooling, since it detected their formation earlier and was
sensitive to
i I
~their presence for a longer time. Furthermore, inflections
occurring at 5500C and
i4900C on the resistance curve had no equivalents in the x-ray
studies. It is con-
'eluded that the resistance method is highly sensitive to slight
structural changes
larising under the influence of external factors such as
temperature, medium, pres-
4
isure, or chemical reactions. The two all-important methods of
x-ray diffraction and
~electrical resistance measurement can thus be made to supplement
each other in a
';highly useful manner. Orig. art. has: 6 figures and 1-table.
;ASSOCIATION: Vostochnyy nauchno-issledovatellskiy i pmyektnyy
institut ogneupor_
J1
promyshlennosti (Eastern Scientific Rese-~,rch and Planning
Institute of the Refrac-
;tory Industry)
':SUBMITTED: 14Apr64 ENCL: 00 SUB OODE: GC, IC
:NO REr sov: 012 OTHER: 005
Card.,.2/2

10882--�6 h] A-11A
ACC NR% ATS028247 SOURCE CODE: UR/261/6~/000/006/0123/0130
q Zj
"THOR: Strekalovskly, V. N.; Bessonov, A Ustlyantsev, V. M.;
Burov, G. V.
ORG: Institute of Electrochemistry,_ Ural Branch, Academy of
Sciences SSR,(AkademtyA--,
nauk SSR, UraFskiy Mal, Institut Elektrokhimil) 114
Tff LE: High- temperature x-ray diffraction stud of oxide
ceramics e )W
%-7
SOURCE: AnSSSR. Ural P My filial. Inatitutelektrokhimit. Trudy,
no. 6, 1965, Elck-
trokhtmiya rasplavlennykh solevykh I tyerdykh electrolitov
(Electrochemistry of fused salts
and solid electrolytet), 123-130
T-
TOPTC TAGS: x ray diffraction analysis, oxide ceramic, cerium
Zompound, strontium com-
pound., zirconium compound, yttrium compound, nt2qymtum compound
7-1 117 -t 7
ABSTRACT: A description is given of high-temperature
attachments for x-ray diffraction
studies with photo- and Ionization recording of the diffraction
pattern (at temperatures between
20 and 1500C). Examples of high-temperature x-ray ana!yses are
given for sintered oxide
materials: CeO2, CeO27SrO, ZrO27-Y.03', ZrO.-M203, ZrO2-CaO.
The transitions
occurring in ZrOeNd~03 and ZrO27Y203 on heating and cooling are
determined. The x-ray
coefficients of thermal expansion of these samples are found to
be lower than the dilatometric
ones. It Is postulated that the difference in the change of the
lattice constant of Ce02 as

L 10880-66
ACC NR: AT5028247
studied in air and vacuum to due to the formation of a solid
solution of Ce in CeO.
203
In a vacuum. Orig. art. has: 8 (igures and 1 table.
SUB CODE: 071, 11/ SUBM DATE: none/ ORIG REF: 008/ OTH REF: 011
U C)
C,,,A 2/2

;C NR' AP6036904 SOURCE CODE: UR/0226/66/000/011/007;&iu,,._
AU THOR: Bessonov, A. F.; Taksis, G. A.; Semavin, Yu. N.
ORG: UralskPolytechnic Institute im. S. M. Kirov (Ural'skiy
politekhnicheskiy
institut)
TITLE: Investigation of solid phase reaC-tions with the aid of a
micrometric
dilatometer
SOURCE: Poroshkovaya metallurg~ya, no. 11, 1966, 72-76
TOPIC TAGS- chemical reaction, solid phase reaction, dimension
analysis,
micrometric dilatometer, dilatometer , calcium carbonate, cuprous
oxide, iron
oxide , material deformation, aluminum oxide, zirconium oxide
ABSTRACT: A schematic diagram is presented for a high-temperature
complex
micrometric dilatometer. Use of this dilatometer, makes it
possible to analyze
in addition to changes in linear dimensions the sequence of
processes which occur
. and ZrO2 + CaCO ort
in samples of MgO + FeO, M90 + Cu20, A120k Cu20 3
heating. The special characteristics of these processes are
determined for
temperature regions of existence of various phases, areas of
pronounced shrinkage'-

VLASOV, V.G.; BESSONOV,,A.F.
Oxidation of uranium diraide kv air in the presence of
added
carbonates and oxides. Kin.1 kat. 4 no.5;666-671 S-0
163.
(MUU 16:12)
1. Urallskiy politekhnicheskiy institut imeni
S.M.Kirova.

STRELOV, K.K.; BESSONOV, A.F.
Classification of porosities in refractory
materials.
Ogneupory, 28 no.10%1+69-471 163. (MIRA 16:11)
1. Vostochnyy institut ogneuporov.

28(5)
S/146/59/002/06/009/016

D002/D006
AUTHOR:
Bessonov, A.G.,
Candidate of Technical Sciences
-

TITLE:
____1
Determining the Kinematically and Dynamica~ly Ad-

vantageous
Parameters of OGyromotor Rotorfty the

Method of Dimensionless
Coefficients
PERIODICAL:
Izvestiya vysshikh uchebnykh zavedeniy.
Priborotroy-

eniye, 1959, Nr 6, pp 61-67 (USSR)
ABSTRACT;
This is a
mathematical determination of the rotor

parameters on which the
following rotor require-

ments depend: smallest possible weight,
maximum

possible axial inertia moment, smallest possible

aerodynamic resistance of the turning rotor in the

gyroframe, etc.
The proposed method of evaluating

the rotor shape for determining
the best relations

between rotor dimensions by means of kinetic
and dy-

~Jard 112
namic relations can, in some cases, be simplified and

S/146/59/002/06/009/016
D002/DO06
Determining
meters of a
cients
the Kinematically and %namically Advantageous Para-
i
Gyromotor Rotor by the iethod of Dimensionless Coeffi-
improved. The basic method can be applied to rotors
of any configuration. The article was recommended by
the Kafedra teoreticheskoy mekhaniki (Chair of Theo-
retical Mechanics). There are 3 Soviet references.
.TION: Leningradskiy institut aviatsionnogo priborostroyen-
iya (Leningrad Institute of Aeronautical Instrument
IMITTED:
September 25, 1959
ard 212

FESSON A
.-TY-1 - A-G.- -- -- - -
Aerodynamic --esistance of gyromotors and ways to reduce
it.
Vop. prikl. gir. no.20&-52 '60. (KRA 15:4)
(Gyroscopic instruments) (Aerodynamics)

28(5)

S/146/60/003/01/009/016
l(l)

D002/DO06
AUTHOR:
Bessonov
A.G.j
Candidate of Technical Sciences

TITLE:
On the Determination of
Aerodynamic

Resistanceland Friction in

the Axle
Supports of
a_Ryr?.motor by
the Coasting Method Using

a Vacuum
q

PERIODICAL:
Izvestiya
vysshikh uchebnykh zavedeniy. Priborostroyeniye,

1960,
Vol
3, Nr 1, pp 61-68 (USSR)

ABSTRACT: The author suggests a new method for determining the
coefficients
of aerodynamic resistance and friction for the square dependence
of both moments on the angular velocity of the rotor. The
possible relationships between the coefficients are discussed
in detail, and rotor-motion equations of the most characterist-
ic relationships are integrated. The method is based on ex-
periments-carried out during coasting under atmospheric con-
ditions as well as in vacuum. The article was recommende4 by
the Kafedra teoreticheskoy mekhaniki (Chair of Theoretical Me-
chanics). There are 2 Sovie-t references,
Card 1/2

S/146/60/003/01/009/016
D002/DOO6
On the Determination of Aerodynamic Resistance and Friction
in the Axle
Supports of a Gyromotor by the Coasting Method Using a Vacuum
ASSOCIATION: Leningradskiy institut aviatsionnogo
priborostroyeniya
(Leningrad Institute of Aviation Instrument Building)
SUBMITTED: September 29, 1959 C,/))
Card 2/2

AUTHOR:
87870
S11461601003100610061013
B012/Bo6o
Bessonov, A. G.
TITLE: Dynamic Axial Displacement of the Center of Gravity of
the:,
Gyroscope Rotor and Methods of Its Elimination
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy.
Priborostroyeniye,.,
ig6o, Vol. 3, No. 6, PP. 50 - 61
TECT: The results supplied by A..Yu. Ishlinskiy's (Ref.1) and
G. S. Santuryan's (Ref;2) papers are better defined and further
developed
here. The author studied the axial displacement of the center of
gravity
of the rotor in the deformation of the gyroscope rotor under the
action
of centrifugal forces. As in the two mentioned papers it is also
assumed
here that the external forces are negligibly small compared with
the
centrifugal forces, and secondly, that the theory of thin-walled
shells
is applicable. On the basis of the latter both the radial and
axial de-
formation are taken into account here. Also the effect of the
rotor axis
is taken into account, and a more precise form of ground
deformation, as
compared with papers (Refs. 1, 2) is obtained. Formula (42)
Card 1/3

87870
Dynamic Axial Displacement of the Center of
-5/146/60/003/006/006/013
Gravity of the Gyroscope Rotor and Methods B012/BO60
of Its Elimination
~Cg(R-p) R h, I
A 2 2 (A?hl+2 h I)J-r (42)
is derived. It gives the axial displacement of the center of
gravity in'
the case of a cup-shaped rotor. A series of calculations made with
thi s
formula shows that the latter is fairly well usable in the practice.
h is the thickness of the cylindrical shell, R is the radius of the
middle plane, a - is Poisson's number, C i are arbitrary constants,
Ki(x) are A. N. Krylov's functions, P is giVen by formula (4)
30 - 2 (4)
2 2
R H
Card

87870
D~namic Axial Displacement of the Center of
S/146/60/003/006/006/013
Gravity of the Gyroscope Rotor and Methods B012/Bo6o
of Its Elimination
P is the radius of the rotor axis, 1 is the maximum
flexure. It is shrwn
that if a cup-shaped rotor has been used, it is to undergo
a prior die-
placement of the rotor center of mass in the inverse
direction along
the z-axis. This displacement should correspond to 6z. in
normal opers.-
C
tion. Then, with normal operation of the gyroscope, the
rotor center of
mass will coincide with the center of the Cardanic
suspension. A complete
elimination of the rotor center of mass shift for all
modes of operation,
can be attained only with rotors having an equatorial
symmetry plane.
Mention is made of papers by A. I. Lurlye (Ref-3) and P.
F~ Papkovich
(Ref.5) as well as the tables of the functions by
Freyd-Puzyrevskiy.
The publication of this article was recommended by the
kafedra
teoreticheskoy mekhaniki (Department of Theoretioal
Mechanics). There
are 6 figures, 2 tables, and 5 Soviet references.
ASSOCIATION: Leningradskiy institut aviatsionnogo
priboros"V-royeniya
(Leningrad Institute of Aviation Instruments)
SUBMITTED: March 16, 1960
Card 3/3

20043
S/146/61/004/001/007/016
J3.252-0 B104/B215
AUTHOR: Bessonov, A. G.
TITLE: Effect of gaps between rotor and gyrochamber on the
aerodynamic resistance of a gyromotor
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy.
Priborostroyeniye,
v. 4, no. 1, 1961, 58-67
TEXT: It is the first purpose of the present paper to find a
mathematical term for expressing the dependence of the moment Ma
of the
aerodynamic resistance of the rotor rotation in the gyrochamber on
the
gap 5 between rotor and gyrochamber. Second purpose is to find an
optimum gap ~ opt by the function Ma - f(,5) with M abeing a
minimum.
Por the derivation of the function Ma = f(S) the author assumed
that the
power neoesuary for overcoming the aerodynamic resiatance, can be
expressed by the relation U - Ma (1). The author then derives U as
Card 1/ t

20043
S/146/61/004/001/007/016
Effect of gaps between rotor and B1041/B215
a function of S. He uses the relation dU, = 2nRHvq~Lv dv (2)
which
dh
represents the elementary power consumed by the elementary
cylindrical
layer of the gap. After comprehensive calculations, the author
obtains
the following relation: U(6) = R 2)22~ /Ak,& + 24B 1 (24),
3 (H + E
2 ~-3 T)
from which he obtains M nil 3 (H + /A k-; j+ 2vB (25) where
a 2 ~T
R is the radius of the cylindrical part of the rotor, H the
width of
this part, U the kinematic viscosity coefficient, dv the
difference
in the velocities of the elementary layers, and 9 the air
density. If
no air exchange takes place between gyrochamber and the
surrounding
medium (k~= 0), formula (25) takes on the following form:
me = 2nR 2(H + L)VqB "R (26). The dimensionless coefficient B
is
2 6
shown to give the ratio between velocity gradient in the
boundary layer
of the rotor, and the mean velocity gradient in the gap. The
experimental values of B ranging from 10 to 30 are dependent
on the gap.
Card 2/A

20043
S/146/61/004/001/007/Oi6
Effect of gaps between rotor and B104/B215
The values of A are approximately unit. Since the experimental
determination of A and B is diffioulto the author recommends a
previously
derived formula for the determination of Ida:
Ma = 2nR2Rpvq (dv/dh)p (27). The distribution of t he velocity
in the
gap of the Rn-5 (AP-5) autopilot was measured by a water
manometer.
A and B were calculated according to these results. Fig. 2
gives a
graphical representation of the values of Ma (Ma g.cm,,S in mm)
calculated by (25), i.e. by taking into account an air
exchange between
gyrochamber and the surrounding medium (k 0) and also by (26)
(k - 0).
It can be seen that 6opt is, the.sam'e for k 0 and k / 0. The
publication
of this article was recommended by the Kafedra teoreticheskoy
mekhaniki
(Department of Theoretical Mechanics). There are 2 figures, 1
table, and,
2 Soviet-bloc references.
ASSOCIATION: Leningradskiy institut aviatsonnogo
priborostroyeniya 2
(Leningrad Institute of Aviation Instruments)

25556
3/146/61/004/002/003/011
Displacement of the ... B124/B206
sistem. (Mechanics of special gyroscopic systems), Izd. AN
UkrSSR, 1952),
G. S. Santuryan (Ref. 2: Ukhody giroakopa, obuslovlennyye
deformatsiyey
rotora, imeyushchego formu stakana (Deflections of a gyroscope,
caused by
deformation of the cupped rotor, L., 1959), and the author
(Ref. 3:
Dinamicheskoye osevoye smeshcheniye tsentra tyazhesti rotora i
spoBoby yego
ustraneniya (Dynamic axial displacement of the center of
gravity of the
rotor and Drocedure for its elimination), "Izvestiya vysshikh
uchebnykh
zavedeniy SSSR, "Priborostroyen-iyell, 1960, No. 6). In these
studies the
theory of thin-walled envelopes is applied, which gives enough
accurate
results for the total deformation. It was shown that the
cylindrical Dart
of the rotor deforms owing to the effect of centrifugal forces
in such a
way that its radial displacement w is given by the equation
D - wIV + (Fh/R 2)w _(V/g)hR p2 (1).
z
The axis Oz is oriented toward the rotor axis (Pig. 1). In Eq.
(1) w
denotes the displacement of the points of the central cylinder
surface in
radial direction perpendicular to Oz, and D the cylindrical
rigidity
D =Eh3/12 . (1 _ 02) (2),
Card 2/ 7

3/146/61/0Q4,1/1002
Disolacement of the ... B1214'/B206
where E is Young's modulus, h the thickness of the cylindr-'eal
rotor part
U --c
R the radius of the centr cylinder surface of the rotor, 7 the
spec-,-~
gravity of the m~:Ve-riaal. Vthe angular velocity of the rotation
of" the ro".or
around its axis and a Pais.sorrl-G-P.9eff icient. A gene3~Ll
solution of (1)
is represented by the equation
(Z) + 7,2(3),
where Ci represents arbitrary integration constants '0o be
determined,,'Ili
the functions by A. Nt. Krylov, which are mentioned ---r Refs. 2
and 3, and
vit gives the special solution of Ea. (1), for rhich.the
correlation
W2' = TS~2 R3 /gE (4)
holds. For the displacement w of-the points of the central cylinder
surface in radial direction unler th'e effect of thb temnerature
field alone,
`3 = Rat -P(z) (5)
holds, where a is'-the temperature expansion coefficient. For the
total
disolacement w of'the points of the central.-cylinder sur'ace
under effect
Card 3/7
A

S/1 46161100411002 /C,.) 9/c 11
Displ6cement of the. 3124/32o6
of centrifugal forces as well as the temperature field,
expressed'as the
sum of the corresDon g displacemerts,
V? - NV 1+ VI3 Ci *Ki + vi2+ Rat - -o z) (6).
Fo'r the required displacement of the center of gravity,6z,
A Z" (R - P)- (C h, (R2 + p2)
2 2 + R a t (0" 2R-(Wh-, + 2hI)
2h (R - N, + N2)
7?-(R- -h. T-11-ily
is derived, vhich changes into form
Aze='-L~R-P), [C2+Rat-p.,(O)j - h, (R2 + p2)
*2 2R (I?hl +-')I,/)
2h +Rat- dx~p (x) dx +
R(Rhj+2hI)-pS - JW2- -0-L2) I
0 0
pi
Card 4/7 +fx-p(x)dx]+A,.C~+A,.C2+A,.C,+A,-C, (64),
0

inn in
S/ l Z. ') ,
, / 6 1 /00
D4snincement of the.... 3 12 4 /31 2 C DS
for the purpo3e of simolified comparison of the
center-o-f-gravity
ment rith and without 'OemDerature field, Aj being dete.rm-ined
from. equat-;ons
+a):K3; As K4 + I + K
Al 4
K,+,
A2=Kl a) - K4., A4-4 K,~
and t *he values of Ki taken for x =01. Ecs. (65) obtl-ined for
the deter-mina
tion of Ai-i -1...'4. are the same as in Ref. 3. The
establi'si,ed displace
9
ment*of the center of gravit' of the' rotor can also be
obtained by heating
Y 0
the rotor shaft. The values for the displacement i'-'zc of 'he
center of,
G-~avity of the Totbr with the parameters R 5- cm, h = 1 .22
c--, h0.4 cm,
3 6
1 = 3 - 0 cm, (5 = 0 - 3 , Y = 7. 8 g1cM,~'e = 3000 sec-' , B =
2. 1 , 10 kp,/c,-a are
given finally in Table 1. The experimental results "or ~zc
agree Aith
those calculated from Eq. (64) and results from previous
studies. The data
-mentioned in Table I characterize 'he disnlacement of the
center of gravity
of the rotor ozing to the effect of the rotor deformation
--*Itsel-L; they
cannot be used for the direct determination of the gyroscope
errors. The
Card'5/7

25556
S/146/61/0041/002/003/01 1
Displacement of t e ... B1241/32006
deformation of the gyro chamber and the bearings .-,could
have to be considerej
additionally. A. I. Lurlye (Ref. 4: Statika to-kostennykh
U,3rugikh
obolochek (Statics of thin-v;alled elastic envelopes),
Gostekhizdat. 10,47)
is mentioned. T~'31-~*"study has been recommended by- the.
Depar'tment of
Theoretical 'Ifechanics. 't'here,-:r-e,-2 fiCures, 1 table.
and 4 Sovict-bloc
refevences.
;'-SSOCIATIOIT: Leningradskiy institut aviatsionnogo
priborostroyeniya
(Lenin.-rad lnsti~ute of Aviation
SU-3111,=TED: June 27, 1960
6
Card 6/7

28958
8/14 61/004/003/007/013
S-~q 0 D217YD301
AUTHOR: Bs~seq~on y-k-Go
TITLE: The comparative advantages of some gas media in
gyromotor chambers
PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy.
Priboro-
stroyeniyep v. 4, no. 3p 1961, 68 - 74
TEXT: The gyrochambe* is either evacuated or filled with
gasp in
which case it must provide maximum cooling and not
introduce com-
plications into the chamber. It is necessary to find an
optimum
medium. The momentum of aerodynamic resistance
Ma = X xcr T R5 1_12
where R - rotor radiusp c,, coefficient of aerodynamic
resistance
per unit of rotor surface, - medium density, 11 angular
velo-
city,,)f - form factor. As Ma is proportional to the
filler must
Card 1/5"
I

28958
S/146/61/004/003/007/013
The comparative advantages of ... D217/D301
be of the lowest density possible. c T depends on Re and M
numbers.
For the analysis graphs c,, = c IT (Re ) and c.T = cIT (M)
where M is ta-
ken from an article by I.L. Povkh (Ref. 3:
Aerodinamicheskiy ek-
speriment v mashinostroyenii, Mashgizp 1959). From
Re = V (3)
where V - coefficient of kinematic viscosity, and the
graph (Fig.
1) the gas with the lowest 9 must be chosen. From
M = _Z_ (4)
v3B
and the graph (Fig. 2) the gas with the highest speed of
sound
must be chosen. Data are given In tabulated form for gas
fillers
at t = OOC and p = 760 mm.of Hg. For low F the best gases
are H
and He, ~The lowest viscosity is exhibited by a,-.monia
and methane
At Re > 106 the reduction Re 7 - 8 times hardly affects c.
. ?or
Card 2/R1

28Y58
S/146/61/004/003/007/013
The comparative advantages of D217/D301
~n air filled gyro with Re 'C~4 104 exchange of air for E or
He may
increase cl, 6 - 8 times. The reduction of aerodynamic
resistance
by changing from air to H, 14 foldt air to He 7 foldt may be
ob-
tained for high speed gyros, for which Re -;;_106* Ammonia
and metha-
nep if used at all, may be used for low speed gyros. It is
shown
that all gases are better than air. A comparison of Ma for
air with
other gases is also given. From the view point of minimum Ma
the
best gases are H and H v even at normal pressure. lieduced
pressure
produces reduced Ma but as this may increase the weight and
deform
the chamber it is not always recommended. It is produced a)
in the
stator and rotor of the gyrop b) in the bearing of the main
rotor
axis, and c) in the gas medium. Heat in (a) cannot be
reduced;
heat in the bearing can be reduced by approplate
construction;
heat in (a) can be removed by convection, conduction and
radiation,
It may generally be said that heat dissipation will be
improved if
a gas with a large specific heat Op and large thermal
conductivity
Card 31~r

28958
3/146/61/004/003/007/013
The comparative advantages of ... D217/D301
is used. The most advantageous is Ho and then He# In
concluAon, a
vacuum doe* not give great advantages compared with H or
He& There
are 3 tablesp 2 figures and 5 Soviet-bloc references.
ASSOCIATION: Leningradskiy institut aviatsionnogo
priboroBtroyen-
iya (Leningrad Institute of Aviation Instrument Con-
struction)
SUBMITTED: October 12, 1960
Card 4

AUTHUR: Bessonov. A,G..-
S/'146/()l/'L)04/ 004/ 009'u'. 5
D201/D306
TITLE: On computing the aerodynamical res-Ls-cance of a gyro-
motor
PERIODICAL: IzvesTiya vysshikn uchebnyjch zavedeniy. Priborro
stroyeniye, v,, 4. no, 4., iq6i., 61 - 7u
TEXT.: In designing a gyroscope system it is necessary To know
the
moment M of the motor and its aerodynamic resistance together
wa-~h
the coeRicient C of the moment Ma and coefficient Ox of tbe re
sistance of the elementary area dS of the rotor surfaced. The
acithor
derives a more accurate expression for Ma, The formula
reflects The
interdependence between the geometrical dimensions of the
rotor,
the width 6 of the gaps between the opposit'ir faces of the
motor anci
the body of the gyro, the angular frequency of revolut-ion i-L
of
the rotor and its max, radius R. the division of surfaces of
the
rotor into I'disc" and "cylindrical" domains and the
properties of
the fl-as trilling the gyro chamber,, The formula is derived
for a par--
Card 1/,'~

2 ~_,, t; 1; --1
S11 14 6/61'/004/004/ 009/01 -5
On computing the aerodynamical D20!/D30b-
ticular shape of the gyromotor, The motor is taken as having an
equatorial plane of symmetry~ For such a motor t-he expression
four
the toTal aerodynamir, resistance of the motor discs Mad !~'7
aerlv,~41
as
~0.2 r 4.8
5a-
M 1.2 R,
ad
where Re is the Reynold~a number,, a OoOll. and gaps,
Formula (1-7) permitz evaluation of the part. of h e 'r c) a 1
'mm
of the aerodynamic gyromoTor resistance due L (1 4- j
d_Lsc pa. s
the rotors To find the Total value of Ma - thF~ c) Tri p (',
r. T;' ;:.,
the moment must be determined which represents th e r ~r- ci a
s t ;~,ned
to cylindrical surfAces of the rotor. 1% is pointed :m~-: that
rhP ex,
pression for Ma does not include 'the eff-e,--,t of the
res_istan~,e, "1"i!
to the inner cyiindric.al surfaces of the ~-otor and cannot-,.
the~~El,:.,
re, be used. The expression for -.his total momenT
-a-Be 2 -X,
Card 21.3 Ma lc25

29645
S/146/61/004/004/009/015
On computing the aerodynamical D201/D306
4.8 H [(_I_cz_i -0.2 ri. 108 -0.2 1
R) R + k- (-R
2 5
p.a R (31)
is derived which is the required solution of the problem, It
must
be remembered that the ratios WR) should not exceed 0.05 -
0.10,
More exactly, if (6/R)opt is the value of the gap
corresponding to
the minimum aerod amical resistance, then the derived formulae
are
vali,". for 6/R -,< (F/R) opt and for larger values of 5/R
wouid cj.,)duce
erroneous results, It is stated that the present work does not
Sol--
ve the problem of the optimum value of gas (6/R) and of the
minimum
aerodynamic resistance & a min. This article was recommended
by the
Kafedra teoreticheskoy mekhaniki (Department of Theoretical
Mecha-
nics). There are 2 figures and 5 Soviet-bloc references.
ASSOCIATION: Leningradskiy institut aviatsionnogo
prioborostroyeni-
ya (Leningrad Institute of Aviation Instrument Construc-
tion)
SUBMITTED: October 14, 1960
Card 3/3

/-3, ;Z.,~-;?,O
3cssonov, A.G.
T 1 T'4 -2, Vacu-,,M in the cyroscopic
acrocILYI-L---ilical resistance
1,--vestiya vyschilch uchebayl-.1i
stroyeniye, v. 5, no. 3,
3 906 3
S/146/62/005/003/011/014
D234/D-303
chamber and the problem of
of gyroscope motor
zavcdc-,liy. Priboro-
1962, 91-98
of the T,)aT)cr is to prove that the intro
duction, Of vacuum i:-l thc gyroscopic cham 'Der. does not
solve the prob
0
lcm 0~-' acroclynczli'cal resistance, and to -Eind the-most
suitable way
-1 vin,, 4t. The author ~--nds ~rozi the
': s ol 11 - j. -- L formula of mean free path
o
0!:
-lc molecules tile oressurc at -71hich the acrod-namical
resistance
-.-)ractic ally disaln?ears. It is concluded that vacuum
leads to an in-
crcao,- of -7L,.-ihcro.-,"cncitv offf tCr,,-,Cra~jjrC whic-h
causes defornia-
tions of all -,?arts o.-"': the motor; the chx,,.bcr housing
must be made
stro-n-,-cr for the -%racuum, which increases the weight of
t: 1ac cla:-::6ber a-..d -its mozicz,.ta o-f iner-cia, cmd
t1herefore decreases the
accuracy O-LE, tl,-,c 1-strume-at. Me author discu sible
improve-
Sses Pos
Card 1/2

S/146/62/005/003/011/014
Vacuim in the gyroscopic ch=ber ... D2.54/D308
-ents sur,'rested by him, in previous publications a-Lid
concludes that
OL~
azi a a
-D-Dropriatzc solution is to -Fill the chLan,!Der with H or He
at hIf
the 'ai-Mospheric --)ressure and to i)rzovide -for a rational
shape of the
rotor, optinal -,a,,)-- between the rotor and the chamber and
adequate
fi-iiis'laing of the rotor'surface. There are 2 figurcs.and I
table.
ASSCO lz'~Ticjiq.
S j.T,.'1TTED
Leninrradskiy institut aviatsionnorlo priborostroyen-
iya (Le-riingrad institute of Aircraft Instrument Con-
struction)
December 25,. 1961
Card 2/2

393U
S/146/62/00.5/004/010/013
D295/D-:'?03
zTMOR: Dessonov, A.G.
T I TIE: Determining the optimum clearance between gyro-
chamber and rotor and the optimun smootluxiess of
their surfaces
.)E~~'IIODIC.E: izvestiya vysshilth uchebnykh zavederdy. Pr~iboro-
stroyeniye, v. 5, no. 4, 1962, 63-70
=-T The optinium clearance 6 ODtI between rotor and gyro-
chamber of given georretry is defined as the value.that minimizes,
0
-ror a given gapeous medium, the aerodynamic resistance of the gyro-
C~
motor. As theOretical formulae give contradi(~ting -figures, an ox-
porliric-ntal x3 roach to its determination is su--csted, op. the
assum-p-
tion that a pr t t gyro-motor is available havi achiev-
es; o ype ng M.-Imum -
able smoothn of the rotor surface. For values of 6 of the-order
Of opt Lhe aerodynamic resistance torque, Ma Iis considered to
be a -Lcunc;ion ~f 6 of the type Ma . A -1 + BS + C. Three measure-
Mants Of Ma 14iji,l suffice to determine A, B and C and hence
Card V2

__10 2 AWT (1) A-wT Lm)A-,',-0Xk~-2 /3w r'
L -EWTjd #SS- (c) IJP(c) JD
ACC-M., AR6o16445 SOURCE CODE: UR/0124/65/000/012/AO07/AOOB
32
AUTHOR: Bessonov. A., G.
TITLE: Relationship between the acceleration parameters of a rotor
for the case of
pulsed,gyroscope starting
160uRCE: Ref. zh%ekhanika, Abs, 12A60
iREF SOURCE: Tr. Leningr. in-t eviats. priborostr., vyp. 44, 1964,
105-110
TOPIC TAGS: gyroscope system, motion mechanics
ABSTRACT: The author formulates, solves and analyzes differential
equations for ac-
,celeration of the rotor in a pulsed gyroscope. Consideration is
given to the reactive
moment, aerodynamic drag and friction in the bearings caused by
dynamic reactions fro6
imbalance, as,well as variability in the axial moment of inertia of
the rotor in the
general case. A rather simple interaction is established between
the basic accelera-
tion parameters., S-ary. [Translation of abstract]
;SUB CODE: 17

L 42V4_6~
Pn-4f'Po-4/Pd-I'Pe-5'Pa-4,,'P---"!PR-4/PI-4 BC
ACC=ION NR: APS006643 S/0146/65/006/001/0113/lOIZI
AUTHOR: Bessonov, A. G.
TITLE: Fundamental interrelations between the design and
aerodynarnics of
spin motors
SOURCE: IVUZ. Priborostroyeniye, v. 8, no. 1, 1965, 11113-121
TOPIC TAGS: gyro spin motor, aerodynamics
ABSTRACT: Three tables sho-whig the interrelations between
aerodyTiarnic-
resistance factors, spin-motor operating conditions, its application,
its manu-
facture, etc., are presented. The aerodynarnic resistance depends on
the rotor
angular velocity, rotor shape and size, gaps, gas medium, drainage,
and rotor
surface machining. The spin-motoT characteristics connected wilh its
aero-
dynamic resistance are: required gyro accuracy, time of operation
(frequency o.f
use), power consumption, external medium characteristics. pressure,
Card I JZ

L 47474-65
ACCESSION Nn: A.PS006643
manufacturing facilities, economic requirements. Possible designs
include these,
factors: rotor shape (equatoriaUy symmetrical, asymmetrical); &yro
chamber
(sealed, draine~d); gas medium in the housing; Saps between the
rotor, housing,
and stator; screws, balancing countersinks, nozzles; internal baffle
plates. 'TI-c-
above three tables and auxiliary curves facilitate designing spin
motors for
minimal aerodynamic resistance and comparing the variants. Orig. ari.
has.
2.'rIgUreS and 3 tables,
ASSOCIATION- Leningradskiy institut aviatsionnogq
-priborostroveniya
(Leningrad InBtitute of Aviation Instruments)
SUBIaTTED: ISDec63: -ENCL: 00 SUB CODE: NG
NO PLF-F SOV: 006 OTHER: 000
4
C*rd'2/2.,

L 04444-67 EWT(d)/Fsg~.Z/E*T(1)/EWP(m)/EW-.(*)/EEC(k)-2 JD
_46/_
ACC NRt AP6022061 SOURCE CODE: UR/61 66 009/003/0093,0099
AUTHOR: Bessonov G.
ORG: LeninKrad Institute of Aviation Instrument Construction
(Leningradskiy Institut
aviatsionnogo priborostroyeniya)
.5.
TITLE: Methods of approximate calculation of aerodynamic losses
in a gyromotor
SOURCE: IVUZ. Priborostroyenlye, v. 9, no. 3, '1966, 93-99
TOPIC TAGS: approximation calculation, gyroscope, aerodynamic
drag moment, rotor
ABSTRACT: The aerodynamic drag of a cylindrical rotor is
determined by the additive
method, proceeding from the fundamental formula for the drag
coefficient of cylindrical Bud
disk-shaped surfaces. The dimensionless factor appearing in the
expression for the coef-
ficient of the moment of aerodynamic drag of a real rotor is
determined for the following casesi
1) taking Into account the rotor-stator unit, a) for the
laminar-with-vortex regime b) for
turbulent flowpast; 2) taking into account the tapering-off of a
real rotor; 3) taking into account
the increase in aerodynamic drag due to the presence on the
initially smooth surface of various
imperfections (bolt sockets and heads, balancing countersinks,
etc.); 4) taking into account
drainage of the gyrochumber by the surrounding gas medluni; 5)
taking into account Increased
ii-ioment of resistance due Lo acceleration of the rotor by
impulses deviating from the flow rate.
Card

L 044-44-67
ACC NR: AP6
It is concluded that these Individual factors may be expressed
with an accuracy on the order of
10-15%, especially with regard to Case 4 and perhaps case 3.
On an average the accuracy of
final results is completely satisfactory and the calculation
time required Is extremely short.
Orig. art. has: 17 formulas, 3 figures, and 1 table.
SUB CODE: 17, 20/ SUBM DATE: 21Apr65/ ORIG REF: OOG/ OTH REF:
002
Card

ARTOBOLEVSKIY, I.I., akademik, doktor tekhr. nauk,
red.; LEVITSKIY,
N.I., doktor tekhn. nauk, prof., red.;
KOZ1!1n11I1.OV, s.I.I.,
red.; KOB-HINSKIY, A.Ye., dolrtnr te-khn. nauk,
red.; P-ITROKAS,
L.V., doktor tekhn. nauk, prof., red.; GAVRIL124KO,
V.A.,
Uoktor tel'in. nauk, prof., red
~Y, A.I_.,,kand. tekhn.
.jj.AES�M,
nauk, red.; SIIEKIIVITS. E.I., kand. tekhn. ii~uh,
red.
[Theory of autoratic machines and of hydraulic and
pneumatic
drives] Teoriia mnshin-Rvtoniatov i
L!idro-pnevr,.opi-ivoda; sbor-
nik statei. Moskva, Mnshgiz, 1963. 327 p. (Its:
Trudy)
(1-111RA 17:10)
1. Soveshchaniye po osnovnym problemam teo-rii
mashin i irekha-
nLzmov. 3d, Moscow, 1961. 2. Chlen-korresponuent.
AN UkrSSIR
(for Kozhevnikov).

--Pa- 4e'Pr"4,-s-;4/. Nab- I W/
ACCESSION N-19- AP5012099 UR/0191/65/000/00~/0003110004
,71
AUTHOR: Bezsorov, A. I.; Vitushkin, N. 1.% Glazunov,-P. Ys,-~ ;7
Kar ap e t 'rfanoviShjL B. 14. Ry~~bchi-koy-a, -G.-C.
~aii Jch, A. A.
TITLE: Unit for gaz-phase radiation-induced I
_graft Poly-erization:
SOURCE: Plasticheskiye massy, no. 5, 1965, 3-4
ITOPIC TAGS: graft polymerization, gas phase graft polymerization,
Iradiation induced graft polymerization
1ABSTRACT- A -nilot-olant unit bas been built for producing various
graft polymerIzation Droducts (combining the advantapes of the con-
stituents) by the technique of gas-phase radiation-induced graft
~polymzerization in quantities sufficient for technical testing. The
lunit is suitable/for grafting polymer molecules tothe slurface of
-F~ics, and HIns"
!mineral powders'! and s~ntbetic and 'mineral fibe~s~,-`
by irradl-a-t7-nE~-them with fast electrons in an atmosphere of
gaseous i
monomer and inert gas. The unit is designed to operate e-itn-~-I'
with
monomers whose boiling 'point In above room temperature (Fig. I of
thel
Enclosure) or 2) with monomers which are normaily gaseous, In the i
t Card... 11.11

44*63=45-
ACCESSION TIR: AP5012099
first case, to prevent monomer vapor condenstion in the reactor a~nd
the pipe, the liquid mononer temperature in the feed tank is"alwP110
maintained 30-50C belov the working gas temperature. In the second
case, the gaseous monomer is fed directly fron a pressure cylinder.
Two reactor types are available: one specifically designed for fibers
!filnr,, and fabrics, and the othor, for powders. The exverimental
re-
sults shown in Table I of the Enclosure were in good agreement with
results obtained in glass ampuls, indicating the feasibility and ex-
~
'pediency of the scale-up of this process to full-5cale plant equip-
Iment. "The authors expres3 their appreciation to B. L. Ts-etlin for
I
,participating in the discussion of the project and for valuable
advite~
~during startup, and to N. V. Mikhaylov, 40' G. Tokareva, and Ye. V.
Yegorov for valuable advice on design problems. Orig. art. has-
I figure and I table.'
ASSOCIATION: none
!SUBMITTED: 00 ENCL: 02 SUB CODE:00)GC
~NO REF SOV: 005 OTHER: 000 ATD PRESSt 3246
214__

IQ-qn11QW1 116; GELIBUKH, L.A.; YELISTRATOV,
I.F.; SMIRNOV, V.A.;
TARSKIY) YU.S., kapitan 2 ranga, red.;
CHAPAYEVA, R.I.,
tekhn. red.
[Underwater search] Podvodnyi poisk. Moskva
Voenizdat,
1963. 93 P. ~MIRA 16:10)
(Diving, Submarine) (Underwater television)
(Underwater acoustics)

USSR/Engineering - Soil'Mechanics
Ca~rd 1/1 Pub. 4,1-12/17-
FD-1458
Author Artobolevskiy,-I. L Bessonov, A. P., and. Rayevskiy, N.
P., Moscow
Title Dynamic curves of soil pressure on a pile driven by the
vibration
method
Periodical : Izv. AN SSSR. Otd. tekh. nauk 7, ll6-l2l,.10kj$11
Abstract ! Describes apparatus used and gives results obtained in
an experimental
investigation of the effective pressure of-soil on a pilC- under
cbndi-
tions of vibration pile-driving.- Obtains curve of soil pressure
on the
butt o~ a pipe and a curve of the displacement of the-pipe during
proc-
ess of vibration p~le-driving as,a function of time. Oscillogram;
dia-'
grams; graphs. Seven references
Institution
Submitted September '3, l9r-4

124-1957-1-161
Translation from: Referativnyy zhurnal, Mekhanika, 1957, Nr
1, p 17 (USSR)
AUTHORS: Bessonov, A. P., Dubrovskiy, V.A.
TITLE; On A. 1. Taynov's Paper "Kinematics of the Assur
Groups of the
Second Class, Second Type" (0 stat'e A. 1. Taynova
"Kinematika
grupp Assura vtorogo klassa vtorogo tipall
PERIODICAL: Izv. AN BSSR, 1955, Nr Z, pp 143-146
ABSTRACT: Instead of applying the well-known method of
geometric loci
to a kinematic investigation of the Assur groups of the
fourth
class, A, 1. Taynov (RZhMekh, 1955, 47) attempted the
develop-
ment of a simpler and more direct method of investigation.
The
Authors have shown that A. 1. Taynov's methods appears
erroneous
in principle and, therefore, that it cannot be used.
1. 1. Artobolevskiy
I. Mathematics--Critic
Bessonov, Al P.] kandidat tehlinicheskikh nauk;
Card 1/1

ARTOBQIXVSXIT,1.1., akadsmik; BMCIWOV A.P.0 kandidat
tokhnichoskikh nauk;
9 0
SHLYAMMIN,A.Y., amULIT 1&srXHcS'8~ uauk; KITDi,V.I.,
redaktor;
YM r I I P.A.. akademik. redaktor; PAVIA)VSKIY,A.A.,
tekhaicheskly
redaktor
(Vibrating machines] 0 mashinakh vibratsionnogo
4Lqjgtvii&. Moskva,
Isd-vo AkmAemii nauk SSO, 1956. 45 p. (MLRA 9:3)
(Vibration--Industrial anlication)

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