SCIENTIFIC ABSTRACT KHARLAMOV, P.V. - KHARLAMOV, V.P.

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• Collection: Scientific Abstracts
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• Document Creation Date: November 2, 2016
• Document Release Date: September 17, 2001
• Sequence Number: 18
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

Ignt AkIUV4-1-4
Tharlemov, P. V. (Novosibirsk)
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-7-
AIJ-HOR Kharlamov.-P. V. ~3
-T L-F - A case of integrrbility of equgtlons of' -zotio-I .7,r -a ~iegvy so4A-~~
liquid filled carities
SOURCE AN SSSR, Doklady, V. 150, no- 4, 1,06.3, 759-76P
TOPIC TAaS: equations of motion, liquid filled cavities, elliptical integral
-7 A A golid body vith a fixed point and civP,ies
Wl',~ I(Je3- liqllld Was stud! ed. In a Foneral :~s-, ~-i*,er j,!:, a v iy,
6 sy~3tem does not coincide i4i-Ah tne 2ap-nort poin'. C a s
;:)e a V-dy -1 "out liqiiid f iiied cav-A by B,jt) 1 imi n -
Wa9 Used i-n or-d3r to find 'Uie ei~.rtl~ql
i 9 equati(=S.
A -S-So~"J.A.TTC~4 ~ -iit a- " Sit n
In,;tit Ridrodin, mil., i r 3'~, of-
Card

KIWTMIOV) P. V, (NovosIbIrsk)
"On the solutions of equations of solid dynamics".
rep,)rt presented at the 2nd.All-Unir!-i Congress on Tbeoretical and Applied
Mer!hanics, Moscow, 29 January - 5 February 1964.

I A r.
TI FLE:
Extuations
-77 -,T
r r r, i 1 4

KHARLAMOV, P.V. (flovosibirok)
One nolution to the problem of the motion of a body having a
fixed point. Prikl. mat. i mekh. 28 no.1:158-159 Ja-F'64.
(MIRA 17:2)

RIAMOV9 1'.V. (Nrvosibirek)
KRA
-
Kinematic; inter;vAt'v0~10f, of the motlon of, a b--,dl with (ril-I
fixed point. "rikle mut. I me~kh. 28 no.3a~kj2-,;O17 Mlyb-z~-'Ul

KHARLAMOVI P.V.
Two particular solutions of the problem of the motion of
a body havinga single fixed point. Dokl. AN SSSR 154
no.2:287-289 JaI64. (MIRA 17:2)
1. Institut gidromakhaniki Sibirskogo otdeleniya AN SSSR.
Predstavleno akademikom P.Ya. Kochinoy.

!ntx--rpn~tat-,'Li -,f a snl-iLion to a pr~blam concerning the mcr%ioil
L, body with ono fixul t~clir-A. TD)k-1. 111 SI:SR .1.58 nc~.5?1W,8-1050 0 '64.
(M!R~ 17.-1 -0)
Lr;3t!tut. g-ldndinam"i". c-Ade-i(-n-~*.ya AN S,~.ZR. Fredotavlene
ak-demJ~.c,m F.Y&.Krjr:h-'r-,f,)Y.

Llt-VegUrjV ej_ne~q
Witil the
it
U~zf c e I Ld 1,71 ll~

'hat in based Lmon
Liu
cloo
WN

C -40F
IM110 5 6 7/0 ~1

1 P.0- i L 2
t it ovoin in ilow I
'nu mvn,
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SOURCE
dP29
ii 19rq 947- -7

Of. 4?

tral Nnwtnnian fev~~ -ii-L-a ul a uo-Lia in a con-
a
d
%m
d
o

'ffiia gull, lit irm
Sr
CCDE-

KHARLDIDV, S.A. (Moskva)
Rigidity of a radial thrunt Pall bearing with
Izv,AN S$3R.Otd,tekh*nauks%~h.i mashinoatr.
(Bail bearings)
an axial tmuion.
noOtI39-W S-0 162.
(Ku 15:10)

MIR
I , --
Reciprocation of Routh:s theorem. Veat. Mosk. un. Ser.1 -,
mat.., mekh..16 no.6-.62,-66 N-D 161. (11IRA 14%11)
1. Kafedra prikladnoy mekhaniki Moskovskogo univeraiteta.
(14echanks. Analytic)

S/02o 61 139/002/007/017
B 1 04A O~
AUTHOR: Kharlamov, S. A.-
TITLE: Movement of a gyroscope suspended on gir3bals in the presence'
of a moment about its axis of auto:rotation
PERIODICAL: Akademiya nauk SSSR. Dbklady, v. 139, no. 2, 1961, 327-330
TEXT:- The eauation of motion for the system shown in Fig. 1 reads
[d dT dT 6q, - 0. The kinetic energy of -the system is
-aT) -
j-1 dt CL
given by
2T. [At + (A,.+ A,) cos! + C, sin' P) IiI + (A + Bj~ ~2 + C (j +Sir,
where A and C are the equatorial and the polar moment of inertia, respective,
1y, of the rotor; A,, B1, and C, are the moments of inertia of the inner
frame of the gyroscope relative to the xj, y,j and z, axes; and A2 'a the
moment of inertia of the outer frame of the gyroscope relative to its axis
Card 1/7

5/02 61/139/002/007/017
Movement of a gyroscope suspended B104YB205
of rotation. The system
JA2 +(A +Ai) coO P + (C +Ci) sln~ 01
2(A +Ai-C-C,)LOcosPsInP +
+110COSP +C(A-,'sIn,-P-+sOCoSP 0,
di
(A + B.)*~ + (A, + At - C - Ci) ~' sin P cos P -11 ~ cos PCsa cos 0- 0,
CA (s + ~ sin P) + X9 - 0,
rAe H = CwO. I aq., .
is set up-for the equation of motion. Ilere,tic, is the angular velocity of
the rotor at which the torque and the moment of,regietance as functions of
the number of revolutions are equally large; H - C(j A 'dQ- lag q
0 Y Y
is the sum 02 moment of resistance plus torquef a 6)0.The first
integral of this equation of motion roiads
.Card 2/7

7
S/020/61/1 39/002/007/017
Movement of a jyroscope suspended ... B104/B205
A + (A + A,) coo 2P + (C + Cj) sinPI& + (H + Cs) sinp k. 116xt, the
2 %
f
author contemplates the particular solution to the equation of motion,
which corresponds to a steady rotation of the rotor about its axis with the
angular velocity ci 0. In order to investigate the stability of this motion,
the author studies the perturbed motion of this system and shows that, in
accordance with a theorem of Lyapunov,.the unperturbed motion is
asymptotically stable with respect to ands - As is known, the
nut&tion of a free gyroscope causes it to deviate systematically. In the
presence of torque, however, the movement becomes'asympt Iotically stable
ev
With respect to &- This indicates that a gyroscope 'd"iates under the
influence of nutation. To determine this deviationp the equationsof motion
are solved under the initial conditions, a m a of a r'SZ1 0 " POI P2 01
s = 0. The solutions a, 0, and a are sought as power series of.2 The
first approximation reads
(A + (A + A i) cO Do + (C + Q sin' Do I -~t + if cos pool +,C sin Pon =0,
(A + B,) H cos Do&, 0, (3)
T (;-i + ~t sin Do) + Si = 0.
Card 3/7

25 7
5/020/61/139/002/007/017
Movement of a gyroscope suspended ... B104/B205
which is aolved under the initial conditions 01 0, s I
The bolutions are
Hcos Oq e-A, 0 Cos WO,
e-nt Cos Wt, ~-A + B&I
S1 sin PO e-f Cos flit e-n' sinwti
+
where the damping n and the frequency o of vibration'are given by
k' C st n*4 0. H cos 5,
U;r, .(10 ~ --
Y' (1, +
A, + (A + At) cO Po + Ct slri~ Po,
C.
1, A, + (A +A i) cos2 r5o + (c, + "
These resultb are substituted in.the second.,approximation:
Card 4/7
(y) .

s/o2o/61/,,-Tq/c,02/007/017
Movement of a gyroscope suspended B104/13205
IA,s +(A +At-) CO PO +(C +CI) SiT13 Pol (L2 -, It Cos N~-. +C sin POS2
2 (A + Ai C - Q) cos Po sin flo (~ipt + (it PI)
(SIPI) Cos 00,
+ 11 PIPI sill PO - C Tit
+ Bi) ~s H co's Po~i (A + A, - Ccl)'al Cos Po sin N
H alpi Cos PO + csiLl Cos P0.
T (is + ~s sin ~o) + s.. T cos ~o A (a'IPI) 4r#
dt
From this, the following expression is obtained for the limiting angle of
the deviation of the gyro's body axis un,I,~-.: t~e influence of nutation:
skipm I C 01
kAs + C, + A*
,'(40~2H cos'p.
Card 5/7

S/020/61/139/002/00~/01 7'
Movement of a gyroscope suspended 31 Q4/B205
A. Yu. Ishlinskiy (Mokhanika opetsiailnykh girookopicheakikh aietem
(Mechanics of apeoial gyronoopio oyatema), Kiyev, lc,,r)2) is mentioned.
Theme are 2 figures and 5.referencee: 4 Soviet-bloc and 1 non-Soviet-bloc.
PRESMITED: January 6, 1961, by A. Yu. Ishlinskiy, A'cademician
SUBMITTED: January 5, 1961
Card 6/7

AlMiUR: Kharlamov, S-.A..
r~
371143.
S/179/62/Goo/ooi/oIG/027
(Moscow)
TITLE: Particular solutions for Reynolds' equation of the
hydrodynamic behaviour of lubricant in ball bearings
PERIODICAL: Akademiya nnuk 35SR. Izvc5tiya. Otdaleniye
teklinichaskikh nauk. Mckhanika i mashinostroyeniye,
no.1, 1962, 77-82
TEZf To explain the mechanism of the creation of an oil
f ilm in a COMbihCd journal and thrust ball bearing and to determine
the forces exerted by the fluid film in the area of contact it is
assui-aed that the balls and the race rings are geometrically ideal
and absolutely inelastic. All equation is derived for the thickness
of tile oil f ilia. Hydrodynai'aic equations are derived from the
Xavier-Stokes equations by assuming that inertia forces are
negligibly small in comparison with viscous frict-4on, that the
main component of the viscous friction is proportional to the
square of the distance along the normal to tile surface, and that
the pressure in the oil film is constant throughout its thickness.
Card 1/3

Particular solutions for Reynolds, ... S/179/62/OOG/001/010/027
E 111kIE181
1f the pressure distribution function is known, it is now possible
to determine velocities and calculate forces acting on the ball
due to the oil film. General equations for the force and couple
acting on the ball are determined and can be solved if the
pressure distribution function is known. It is proved that pure
rolling is not possible in a ball bearing and a case is considered
of combined rolling and sliding. The sliding velocity is found to
be a direct function of the oil film thicknes's. The equation for
the force due to the spinning of the ball with respect to one of
the race rings - which always occurs in the case of combined
journal and thrust bearings - is found to be in the form of a
divergent integral, as in the case of combined sliding and rolling.
That is, frictional forces due to spinning will significantly
depend on the thickness of the oil film. The frictional couple
due to spinning is found to be proportional to the 4/3 power of
the bearing load, which is in good agreement with experimental
data of G.S. Reichenback (Ref-3: The importance of 5pinning
friction in thrust-carrying ball bearings, Trans. ASAME Ser. D.,
J. Dasic Engineering, 82, no.2, 1960, 295-301).
Card 2/3

Particular solutions for Roynolds'...5/179/62/i~uo/uol/01()/()2,7
L-1111/E161
Forces tending to bring the ball into a direc-t colitact with the
race ring in a static bearing reduce the separating film of oil
along an %~xponcntial time curve. By neglecting the assumption
that the ball and the race rings are completely inelastic, a
formula is derived for the starting torque of the combined
journal and thrust ball bearing as a function of the journal
loading. An attempt is made to generalise the equation to allow
for viscosity which is not constant but varies with pressure,
There are 3 figures.
SUBMITTED: October 3, 19061
Card 3/3

360h5
S/040/62/026/002/019/025
13,2,500 D299/D301
.i'.UTHOH: Kharlamovp S.A. (Moscow)
TTTL": On t"Le motion of a gyroscope, mounted on ball bearings.
in a Cardan suspension
P3RIODICAL: Prikladnaya matematika i mekhanika, v. 26, no. 2,
1962, 3 5 - 369
TEXT; In the theory of free gyroscope-motion, it is assumed th,,!.t
the ,osition of the momentary axis of rotation with respect, to the
internal Zrip-bal-rings, is fixed in a coordinate systerq connected
to the ring. In the present article, this assumption is riot made.
The relative motion of the gyroscope is determined purely kinemati-
cally, by giving the law of motion of its center of inortia and the
orient--tion of its figure of rotation. The inertia forces of the re-
lative notion -oroduce S-,all oscillations of the gyroscope about its
st'atio.nary notion, forcing the gyroscope to precess about the axis
of t.-.e external ring. Pirst, the equation of the hyperboloid of ro-
a 41,
t
-ionp described by the axis of the figure, is derived. Then the
equations of motion of the gyroscope are set up by the method of
C--rd 1/3

S1040V601026100210191025
On tile motion of a gyrosco-pe, D299/ ,301
T,agran~ye. If the --uler angle 80 between the z- and `-axes is zero,
I L)
then the equations of motion allovi a particuiar solution which cor-
responds.to station----.ry motion with respect to the support. The mo-
ii,entary axis of rotation is shift
-ed, describing a cylindrical sur-
~ace, whose axis coincides with the z-axis. The ternis in which 80
r' Op are considered as si,,iall perturbations. Thereupon the solutions
of the eauations of motion ar~
cc = a + Ut + ~Mf i9 + t Ir = /it + "--T- + ,c ( t ) j
0 0 0
where u is the constant rate of Drecession. These exnressions lead
,,o a syste:ii of nonhomogeneous Linear differential equations o-' mo-
tion. After inteLrating this system, it is ncssibie to -Nnd the
precession rate by the j-,ethod of Mgnus. The obtained reSuit ooints
to the need ~or making the z-axis coincide exactly wit-li the princi-
,)al axis of inertia of the internal ring. 2'arther, it is shovin that
a disnlacement h of the center of inertia of the Eyroscoje, lead--
L
to add it4 onal reactions in the resistances of the axes. ~_Ihe j-enera-
.Lized reaction forces were determined A.I. Lurlye's method. !'arther-
t'ole displacement of the gyroscope figure under the rotation of the
Card 2/3

S104O1621nV2Q'_1UG21V1r,1O25
Or. the i~,.otion. of a uroscopep D299/D301
ball be_-rin,~-sp is analyzect. The obtained formuias for 'U'.--o rL)te ol~'
,~01'1 eC-4 o.- -utati cnal osi-il -I, tions
V_ , of the t;:;'ro~,cope under
of a -Yro--co-oe on ball bear-irl, s, ii, the -orese-nce of a
sl_ift ir. tlie axis (with resuect to the axis of sy=etry of the e7-
serral rin-s), is aanaaloEous to the motion of a dynanically unbalan-
ccd '~-roscope, whose polar moment of inel-tic. is k ti:::es lar-er, the
az-%c--le betv:aen the axis of dynamical sy=etry and the axis off proper
r o -t_ tion beinG equal to 00, and the velocity off rotation - ktimes
S'Marl -1 er. In the above analysis it was assumed that the ca-es of the
ball becarin-s are rotating synchronously; in practice, however,
this condition is not ri-orously fulfiiled. Hence more accurate in-
vc2tilgations are still required. There are 2 figures and 6 referen-
ces: 3 Soviet-bloc and 3 non-Soviet-bloc (includin,- 1 transl'-.tion).
The reference to the English-language public-rtion reads as follows:
T. Y_-mamoto. On critical speeds of a si~aft supported by a ball
bearing, J. Appl. klech., 1959, 206j no. 2v 199-204*
SUMIITTED: July 10, 1961
Card 3/3

3h822
S/020/62/142/005/011/022
B104/B102
AUTHOR: -q-
14holir-1.
TITLE; Effect of elasticity of the axle bearing of the outer gimbal
of a cardanic suspension on nutational oscillations and on
the gyroscopic deviation
PERIODICAL: Akademiya nauk SSSR. Doklady, v. 142, no- 5, 1962, 1054-1057
TEXT: Ye. L. Nikolaile equation of motion of a gyroscope (Tr. po mekhanike~
M-, 1955) is applied to study the reaction of the axle bearings of a
cardanic suspension. Two coordinate systems fixed with respect to the
ou~qr and inner gimbals are introduced, and the moments of reaction of the
bea~,ings are determined from Eulerts equations for the outer and inner
gimbals and the gyroscope (A. 1. Lurlye, Prikl. matem. i mekh., 21, no .6,
759 (1957)). The kinetic energy of the system is determined, and-from it
the Lagrangians are derived where-the momenta of reaction forces in the
bearings are taken into account.
PZ2 - (A2 + Cl)a-tg P + (C1 + B, - Aj)dA'. (1)
Card 1/3

S/020/62/142/005/011/022
Effect of elasticity of the ... B104/BIO2
is obtained for projecting the moment of reaction of the axle bearing of
the outer gimbal onto the Oz2 axis (Fig. 1). A2 is the moment of inertia
of the outer gimbal with respect to its axis of rotation, A,p B1v and C,
are the moments of inertia of the inner gimbal, a, 0, and y are the angles
of rotation of the outer gimbal with respect to the fixed base. The
precession velocity of a gyroscope is approximated by means of the moments
of reaction forces. Elastic deformationect the bearings are taken into
account by introducing further degrees of freedom whose number equals that
of the non-varnishing moments of reaction in the bearings. In general,
five more degrees of freedom must be introduced. Calculations were
conducted by X. Magnus, R. Gudsteyn, D. S. Pellpor, Ya. L. Lunts et al.
S,, S, Tikhmenev (Izv. Vy9sh. uchebn. zaved., ser. Priborostroyeniye, 2,
no- 5, 63 (1959)) and A. Yu. Ishlinskiy (Mekhanika spetaiallnykh
giroskopicheskikh eistem, Kiyev, 1952) are mentioned. There are
2 f.gures and 4 Soviet references.
ASSOCIATION: Moskovskiy gosudarstvennyy universitet im, M, V. Lomonosova
(Moscow state University imeni 14. V. Lomonosov)
Card 2/3

,JKHARLAMOV) S.A. (Moskva)
Motion of a gyroscope suspended on ball bearings in gimbals. Prik.
mat. i mekh. 26 no.2:365-369 Mr-Ap 162. (MIRA 15:4)
(QVroscope)

41332
S/020/62/146/003/004/019
B172/Bla6
AUTHOR: Kharlamov. S. A.
TITLE: Nutation and drift of a gimbal-supported synchronous gyroscope
PERIODICAL: Akademiya nauk SSSR. Doklady, v.*146, nu. 3, 1962, 550-')53
TEXT: A Eyroscope spinning with great angular velocity is driveh
electrically in such a way that the inner frame of the suspension
constitutes the stator and the gyroscope itself is the rotor, so as to
eli~ninate losses due to friction and resistance. Lagrange equations are
set up to determine the effect of the maEnetic. field in the non-perpendicular
frames on nutation and drift. Two caset~ are discussed- 0) Nu'tation and
drift when the external frame performs ishort-Verm, rotations. (2) Forced
vibrations when the geometric axis of the gyroscope do6s not coincide-with
the Dolar axis of inertia. There-are 2 figures..
.ASSOCIATION: Moskovskiy gosudaretvenny:r universitet im. M. V. Lomonosova
(Moscow State University imeni M. V. Lomonosov)
PRESE7,T:D: April 6, 1962, by A. Yu. Ishlinskiy, Academician
SUBMITTED: March 30, 1962
Card 1/1

-(engineer)
.3ome proolems of the xrmmics of z, g7roscop-) with c.n electric -~r:ive
installed in a 67mool suspenslon.11
report presented at the -jcientlric-techalcal Uonference on Yoaern Gyroscope
Technology 1-iinistr7 or Higher and Jeconaary 4pacial zdu-Ai.on fLiFSh, held
at the Leningrad Institute of Precision Mchanics and Uptic3. 20-24 klovember
1962.
(Izv. vysshikh uchebrorkh zavedemy. er:worostroyeniyet v. b, no. Z, 190j)

Mann
AID Nr. 990-6 june
IL ",'T 11_-TC
TECHNICAL CONFERENCE ONT MODERINT GYROSCOPE TECH-
NQ~LOGY (USSR)
q
Izvestiya vysshik-h uchebnykh zavedzaiy. Priborostroyeniye, v. 6, no. 2. 1963,
S/146/63/006~002/010/010
Confere.nce or, Gyroscope Technology. sponsored by the Y[inistry
~Z~-3:~_tary Spec-al Edicatian RSFSR, was a' :he Leningrad
-cs anc' O?tics frr -n 0 4) 24 Nove:~,,ber '962.
a-.-=~ed by repr-~!senta,,;ves irorr 43 (-)rgar__.a-,,Or!S ,n
ed,,;cat~onal es-at'!~s.'=,ents, s c; e n i., e s e a r c,i i rt -
-cncerns e r"A, -e sorne
a:
C 7: S S S,~ con,e:-ence
w"..~-i a mw,-a~-,e S 7~ S: a o - r-n
Z 'Acre e:- nn Dr o g
n
Sedoy, Sen4or Sc.,
c".a:-acleristics of some gyro instruments ana devicc~s. ~L. _v'. 1:tepr,.kov,
of Technical Sciences; some prob:eins of the dynamics of a
W.
an e'ect,-;c drive installed in a gyrnbol susDensi:,r.. S. A.
Card 113

-AT-D. Mr.- 990-4 24 JVMIO
CMZ=MZ- (Cout'dj
kh_,rIa=_-v. Engineer; problemg of the theory of the inertial method for measur-
a..-craf- acceleration: 1. 1. Pomykayev, Doccnt. Candidate of Technical Sci-
-es ~__-cr-n~ning the drift of a floated-type integrqting gyroscope without the
--mic s*and: G. A. Slomyanskiy, Doceni, Candi,:ia-- of Techni a!
7, --,-al d~,-,-)`ng of nutational vibrations of a gyrosco-e N' V Gusev,
%&-.h vertically
n a not, q*,ii,,e symmetrical
N i3o-suva, t-: e e T- c) r
s y- a r es,
V. A. S,~r
'netween, rhannels in triaxial gyro- stabi' izea' -,,Ia*,:-c'r-rn L N
theoretical proposal for the possibie ces,.gn 0~ a generalized
gyro instrument: M. M. Bogdanovich, Docent, Candidate of 7(.-chnical Sciences;
pro~D:ern of drift in a power-type triaxial gyro stabilizer: V. N. Karpov. Engineer;
methods of modeling random disturbances in gyro systems: S. S. Shishman, Senior
rnethod of noise functions for investigating a system subjected to random
Card 2/',!-

AZ NIz. 990-6 14 June
colv=11"CE [Convdl
kov, 'date of Techn: --a' S,7 er_- i. in a gy-o-
o'o Docent, Cand
.:r, ;, s a :-es- _- of the e~fec-. an d r an -
slab'
Nazarov,
Docent,
a S` -: n d e r
C, n-I D g tr E:o U sl N, T- 1 jT I C: ;f,;
Cherniko-., -net'loc-s with
au."~pznat,.c iatlwde and course corrections- A. V. Till, Candidate of Technical Scien-
ce-4; use o7 asyrnptotic methods in solving problems of the motion of an astatic
S 5P en s , n r. nn o v, Ca7~-:,-Ja't- P-+-.-s:,-,-.: a7.d %lathe-
ard 3

Nutational Vibrations and drift of a synchronous gyroscope in
gimbals. Dolk. AN SSSR 146 no.3:550-553 S 162. (MIU 15:10)
1. Moskovskiy gosudarstvennyy universitet im. M.V.Lomonosova.
Predstavlenu akademikom A.Yu.Ishlinskim.
(Gyroscope)

KHARLAMOV, S.A. (Moskva)
Theory of an astatic gyroscope in gimbals and with an electric
drive. Izv. AN SSM. Mekh. i mashinostr. no.6:45-54 N-D 163.
(KIRA 171l)

""gidity 1y
no.? - p4
f MIRA 17:4)

S./0179/64/000/002/0050/0060
AUCESSIM NR: AP4035059
AUTFOR: Kharlamovj S. A. Moscow)
TIME: Application of Resal's Theorem to Detcrmining the Dynamic
Departures of a Gyroscope in a Cardan Suspension..-..-.
SOUPCE: AN SSSR, I:westiya. Mekhanika i mashinostroyeniyo',' no.2, 1964j.
50-60
TO?IC TAQSr gy-roscopti, Cardan suspension, vibration, gyroscope oscillations
precession, Resal theorem
r
ABSTRACT: Dynamic departures of a gyroscope in a Cardan suspension a're
defined as tho departures caused by small oscillations of the axis of the
figure of the gyroscope& This article considors dynamic departures that, are
caused by nutation oscillations, oscillations of a dynamically unbalanced
aroscope, forced oscillations of the gyroscope,, and ouQi1lations of a
p_7roscope attached to a vibrating base.,
It is shown that departures of a gyroscope in a Cardan suspension for
1/2

P.1.9pam
kww-NR--Al
:-,L ; Ai~404487 I
. - ; I. .
I. -,I t, ,

Sh' MA)%, Yu.A., inzh.; Prinimali uchastiYO: KHARLANOVp S.Kh,, izizh.;
DIRYULEVt V.G., inzh.; TAMUTSEV/t, 1-.-S-.# imb.; IGLITSYN, I.L.,
red.; LARIONOV, G.Ye*, tekhn.red,
[Study of ignitron characteristics and design of firing circuits]
Issledovanie kharaktorintik zazhigatelei i raschet aldien zashiga-
niia ignitronov. Moskva, Gos.energ.izd-vo, 1960. 57 p. (Moscow.
Vaes,oiuznyi nauchno-issledovateliskii institut clektroenergetiki.
Wormatsiormye materialy, no*56)* (MIRA 24t12)
1. Voonoyuzriyy nauchno-looledovatellakly institut elektroenergWki
(for Kharlamov, Biryulev,, Tamantseva).
(Mercury-are rectifierB)

SMWRI, Yu.A., kand.tekhn.nauk; KHARLWOV, S.-Kh.,-Uzh.
Regulation of the ignition interval of an Ionic current conrerter.
Test.elektroprom. 33 no.12:44-45 D 162. (MIRA 15t12)
(Electrio ourrent convertero)

Of PhOto--milsions. The
--ater

x1ttMAYOVY V.I., X=41m A
"tri v O.V., LARTONOIA, V.0.
"Photoproduction of Negative74 Mesons on Deuterium," paper
presented at CERN Symposium, 1956, appearing in Nuclear Instruments,
Ho. 1, pp. 21-30, 1957

AUTHORS: Adamovich, U. I., Kuzlmicheva, G. V., S07/56- 3-5- 1 -31/59
Larionova, V. G., Kharlamov, S.
TITLE: The Photoproduction of n -Mesons on Deuterium Near
the Threshold (Fotorozhdcniye r,--.,nezonov na dezrterii
Y"3lizi poroga)
PERIODICAL- Zhurnal eksperimentallnoy i teoietichoskoy fizAki, 1958~
Vol 35, Ur 1 , pp 27 - 38 OISSR)
ABSTRACT: In several earlier papers (Refs 1-4) th.-, ratio of
the cross sections of the proceose8 y+d 4 pfp+n and
y+d 4 n~n+n+ has already been inv,- ,,-,tij~,ited ; Watoon
(Vatson) (Ref 4) sholved that c-/al for deuteriu-Li
correaponds to that for free nucleons. The authovs
of the present paper inventioated the reaction y+d 4 pp+r
on the 265 MeV synchrotron of the FIAN (Fizicheskiy
institut kkademii nauk SSSR - Physics Institute AS USSR)
with NITM-R photoemulsion plates which -sere enriched with
deuterium ~as D 20). (Plates: 3,2.1022 deiiterium nuclei
per cm3). The maximum enerjy of the y-quanta. announted to
Card 113 250 and 200 eV for a magnetic field with il=7000 09 in

The Photoproduction of n--Veaons on Deuterium Ne~ir SOV/56-35-1-3/59
the Threshold
the evaluation of the platn3 the microscope MBI -2
was usedIfor the determination of coordinates in the
--age, of multiple scatterinb MBI -8. For the dependence
of the cross section of meson production on photon
enerey (54 E