SCIENTIFIC ABSTRACT BARTOSH, Y. Y. - BARTOSHEVICH, M.A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000203730013-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 31
• Document Creation Date: November 2, 2016
• Document Release Date: June 6, 2000
• Sequence Number: 13
• Publication Date: December 31, 1967
• Content Type: SCIENCEAB

BARTOSH, Tel., kv=d.tekbn.naUk
pickup characteristics of the gas turbine engines of locomotiver
with mechanical tranmission system. Trudy TSfin M no.241220-
35 162. (KM 15-.12)
(Gas turbines) (Locomotives)

PARTON, Y9.T.I.kand.tekbn.na:uk; SYUZYUMOVA, Ye.M.
Analysis of principal networks and thermodynamic characteristics
of the engines of gas ttzbine locomotives with free-piston gas
generators. Trudy TSNII M no.24195842 1622. (MIU 15:12)
(LOOMotives) (Gas turbines)
J C!"'AA
5'.
v

- BARTOSHI Ya,T., kand.tekbn.nauk
Tracticnal charaoteriatioo of a turbine with counterrotatitg
rotors. Trudy TSNII MPS no*2LI:36-5D 162. (MM l5zl2)
(Gas turbines) (Loomotives)

.BARTOSH, Ye ank
kand.tekbnuauk__.,__
Constraction of approximate cUracteristics of an a-dal
campresoors
T=dy TSNII M no.241&132-3-18 162. (NM 15,22)
(Ompressoril

BAR,TO.S.Hp--Ye*T*, kand.tekhn.nauk
Selecting the design parameters of traction tprbines for
gas-turbins
locomotives. Vest. TSNII MPS 22 no.2:9-13 163. (MIRA 1~4)
(Gas-turbine locomotive s-Design and construction)......

AMPq4,t-Ye.T,,, kand.takhn.nauk; KOLODYAZHNYYt NOVO., kand,tekl~qnauk
Prospects for the expansion of gas-thwbine traction. Zbel*dor.tx-a-nap,,,
43 no.2:23-28 F 16), (MM 16:2)
(Gas-t,.-rbine locomotives)
R5,

_YLev en raBovich kand. tekhn. nauk; KISELEVA, N.P.,
ARA M& iy Ta BovIchL
in vA
i
, . rep
rjzh., re .; I G.P., tekhn. red.
[Gas-turbine locomotives] Gazoturbovozy. Moskva,
Trans-
zbeldorizdat, 1963. 94 P. (MIRA 16:4)
(Gaa-turbine locomotIveo)

BARTOSH, Ye.T.p doktor toviim, nauk
Determinjug the characteristics of double-3haft gas-turbine engines,
Veste VIVU MPS 24 no.5319-22 165, (MIRA 18:9)

AUTHOR: Barto9b Ye. T. (Candidate of tecb-nical actenecs)
TITLE., Performance curves of radial centrinat-9 turbines Y
SOURCE: Moscow. Vaesoyamyy nauebno4solrdmat-a.] IsIdy Institut
zbc1eznodorozhn0g0
transportz. Mrud
no. 282, 1964, nezulltaty ias~uedovanly gazoturbovoiza GI-01 I
I lokomotivnykb gazoturbinnykh dvigateley (ResVs of research on (ho
glis turbine
i loccmotive, G1-01 and locometf-vo 9VS turbine engines), 65-75
rr
IT)PIC TAGS: gas turbine, radial turbine, ra;lio tientripetal turb
ic, turbine perfo oante
curve. locomoti-ve turbine
14
-stap In comparison with-an-Wal
drop 19
itage at simflar peripheral sput%l, wIdle the speed may be increased
by 30-40%. resulting
in lugher power. Loss of puwfir is highe.- In the cent ipetal stages
than in axial etages,
VhIle t1w losses at thn nnzz!eB and leakage am 1mver. Radial
turbines are mainly single-
stage. On the basis of the general theory of turbines, an expression
is given for the

A
diff6rent speeds'- The Mattm no*'-doofficlentsJor raffial stages Aure
calcul-ated on the

same basis as for axial onen. Mw analysis indicates that in
radial stages, as in axial

ones, nozzle adjusting by a byperbolic curve is
best clone at the same time the turbin,3 is

boosted, ensuring an increase In
the beat drop. A radial centripetal turbine has several

posidve features,
emuring a betttr future for gas turbine e-gines of medJurm and low

p,lwer for
',ocomotives. Orig. art. bas: 5 figures and 21 equations.

TIE- V1908
Uwmbw4wfledvvMdIqhb-IAsUtut zMethnodorothmp

ImUtube of %Ur6"
MOSOM *Uroh

A

Tra
ti
M)
ilaWAg
4

-
-
-
00 EIMM: 00 UB ,-Pn,-
UTTED.-
MTBb

.
_-

card 2/2

AddESSION IM: -AT400.524
AUTHOR: Partoiffi, Ye. T. (CanOldatwof technical sLqenceB)
TMM -'Zff 6PA c& 6~~ 6-1-rtwb-41haft-ps IlfbhE:4i 2A
PA Way.
"in, y%r. 01
M
L*id W. Wd6vad
~-l -0tive 01-01 and 16c -bublue-.4wou0s)'~-76-63-
TOP19 TAGS: gast~, gas birbine pickup.- ps tturblue volume. -16.ft'433t-
m-rDuve"
lociomotives gaB ttirb-Ine
being true for aviation and loc otive wrimes the simple direct-flow type.
flowemver,
there b a regeneratoror yre-ewl-ar, disragardinX inertia may leM tD
elpfficant errors
741=7
1/2

L
ACCEMON NR: ATR49524
-derived -equatimg proves that in twin-abaft locomotive engines, regenerators
of
v6lume may Imp;dr -the pick-up of the engine. lm-us, - inbvduouw of
regowation into
locomotive gas tuib1W(VWg0,"-
9 SbOUld
rageneration-in -gan UWAe loomotives Oztg. - arL hti~q 2 f Imes and 4 0
64i"4as D1

ASSOCIAITON: Vaes:)Yuznyy umbno-issledovaWkskly Institut
zhe1ezbnodorozbn",j

transporta, Moscow
(In-Union Sdentifit Rusuleb lmtltute of
hilmd

j~!ajj;pqrtA icn

__
SUBbErITED: 00
ENCL.' 00 BUB CODE: PR

NO REF SOV46 003
OTHER14 M

S

-

Cord 4i2

1~1 26128
-65 EWT(M)
ACCIk'%MN NR: S/2917/64/-000/28Z/OOW-0095-1;==
AU771011i., Bar!osh, Ye. T. (Candidate of teoWoal sciences)
......................
7b..
TITLE': Effect of performance features of locbmotive.~ae turbifies on the
trAnment____--
--processes off train motion
Moscow. Va"pyuzny-y nsuchno-i
SOIMCE.- sisledovatellaldy institut zheleznodor6zbn
transporta. Trudy, no. 2.82, 1964. Rezulltaty IsBledovanty gazoturbovoza
G1-01 f
lokomot3vnykh gazoturbinnykh dvigateley (Results of research on the gas
turbine
locomofive GI-01 and locomotive gas turbine engines), 84-95,
TOPIC TAW: gas turbine, locomotive gas turbine, turbine, performance,
railroad
locomotive. train motion
M
ABSTR~CT: 71, s principal performance features of the gas turbine,
distingnilshing it
from other lacomotire eingines, are the significant deviation of
performance curves from
hyperbolic ones and -insufficient pick-%T of the engine, requiiing time for
passage of the
turbo-coznpressor from Idling speed to ftdl power. On railroads, after p
ing to idling
ass
speed (at signals), the lo-comoUve must then change to full power. 7%e
differettial
equation for train motion shows thall the acceleration and spoed depend on
the specific -XI
tractive force, specific t-aln resistance and total resistance caused by
the grade and
Card 1/2

CCEMNmR-.-;-AT40496W'-z
b6r1zon61_cUr`Vas._ -Two- sol :-for -hyperbolic and-linear- performance.-c
Utter's nea-glyan
It was fo-wid tWv the decisive effect on s'pred for transient,
Comsidert* these solutions
-zW aWblaltralu motion Is the doi-434ion of tho-Por1brw=-ce,mrve from a
hyperbolla. The
--_-Pas the
senger and freight tridw.- Thtj-~~uatlons show that for medimn and-heavy
grades,
lowerog of speed as the r inci eases Is mp" marked wAb a linear performance
curve
-'F~-than vilfb-a hyperbolic curve. Analt:rils~fpew-. iii "-- C-0--features
of locoinotlvepDwer units
turbtm enginem showaAhe pl. OMSwz =LbbrAny"Uption-a the worki"
power-mait
bine th t sexabUes 0 0
0 an a 0, 0' J~
rim-
the- tivi6 force."bf.AW" - M- W61hei-40idut. 14(partiewer V
'AOM . Ary
Arse ~ ~ V '
M i-alm-Aurbihn
_k :appia AWN rm ce-curvet
-:Aacmoftes -with rect i1rive- i-_11S_-w4*S improvwnent--of -Pick-up
dl to
4
~-'of-xn tii;sl ti a arL- Mai 4 -figurii-and
turbin a,&
F4
lubw 61--- Q
=-AMOCUITOME-1
trawWrtis Mos6ow- (A
14tib
SUB Mle" PR
(YMIM ~000
-SOV.
NO RSF 003
-2/2
ctqd
-A

GUGOLn,', Nikolay YatveyevL:h; KURITS, Aleksujr-Jr Ariyevich;
VODOLAZHCff,IIKO, Vitaliy Vasil lyevlc~;
Tarasovichj SAWCOV, A.G., red.
[Internal combustion engl-Les ani gas turbines for diese'l
locorrotives] Teplovoznyo dvigateli vnutrennego sgoraniia
i gazox-je turbiny. Izd.2., perer. Moakva, Transport,
1965. 400 P. (MIRA 18:6)
Ki~
Y'

~ng ,~he nciple ri 7..r)e +-xz ~. L:,n cc -I-,
2hx-r. 9 no.'~-412-417 165.
M ILFA 3, F
-wf-

L i 11 _- i -
AR6014706 SOUME C -UiV62
AUTHOR.- Bartosh, Ye, T.
UTLE: Determination of the characteristics of dual-ahaft g"
turbine a
_SWP~3_
SOURM Ref. zhe Trubostroyeniye,, Abs. 11.49.66
REF SOURCE% Vestn. Vses. n.-i. in-ta. zh.-d. transp , no. 5,
1965, 19-22
TOPIC TAGS: gas turbine, gas turbine pertormance, turbine
ABSTRLCT: A graphical-analytical method for determining the
basic characteristics
of dual-shaft locomotive GTD's is presented. The method can
substantially simplify
the problem of determining the energy parameters of multishaft
engines preceding
their exact calculations based on the experimental aerodynamic
characteristics of
the turbine componentse ffranslation of abstraeg
SUB CODE2 3jr /0
Card UDCi 621.438.(

ACC NR. AP7005401 (A) SOURCE CODE: UR/0232/66/000/011/0034/0040
AUTHOR: Bart shYe..--T-_(Doctor of technical sciences)
ORG: none
!.'TITLE: Present state and prospects for the use of gas turbine
locomotives in railroad
service
SOURCE: Zheleznodorozhnv transport, no. 11,1966, 34-40
Y
TOPIC TAGS: gas turbine engine, railroad transportation, locomotive
engineering
ABSTRACT: The present state of gas turbine propulsion for railroad
locomotives in the.
USSR is reviewed and future prospects are discussed. In the USSR
the development of
gas-turbine installations for -locomotives was started in 1955. The
first gas turbine
locomotive had an efficiency of 10 to 12%, 1, e., it consumed 2.0
to 2.2 tines more
fuel than the diesel locomotive. However, the fuel was of a lower
grade containing
2.0 to 3.0% sulfur and its projected cost was 1.5 to 2.0 times less
than that of die-
sel fuel. The advantages of developing gas turbine propulsion' for
future high-speed
railway transportation are discussed relative to the following
schemes: a single-shaft
gas turbine drive with dc generaior and motor;* two-shaft gas
turbine drive with direct
mechanical power transmission; a three-shaft gas turbine drive with
ac synchronous
generator and nsynchronous electric.motor drive; and a combination
gas turbine drive L
UDC: 625.282-e43-8

ACC HRs AP7005401
with a free-piston'gas generator. A note by the editor states that
considerable sums
of money have been expended in recent years at the Kolomna and Lugansk
plants on thw
development of experimental gas turbine locomotives. However, the state
plans have
not been fulfilled and work at the Kalomna. plant in this direction is
being temi-
nated. Orig. art. has: 8 figures.
SUB ODDE. 21,13/ SUBM DATE: none
77-7-77-7 7,
. ~ -~-i 11 *

I BARTOSHEK11 V. [Bartosek, V.]
Transient states of a reactor during the recharging of
fuel
elements. Atom.energ. 16 no. 4:315-324 Ap 164. (MIRA
17:5)
1. Institut yadernykh issladevaniy Chakhoslovatakoy
Akadeadi neuk,
Praga-Rzhezh.

ACCESSION NR: AP4029693 S/0089/64/015/004/0315/0324
AUTHOR: Bartoshek, V.
'JPL&'jL LE: Transition atates of 'a reactor during reloading
SOURCE: Atornnaya energlya, v. 16, no. 4, 1964, 325-324
TOPIC TAGS: fuel element, radiation stability, equilibrium statel
neutron
flux, neutron distribution, neutron multiplicationg equilibrium trana-
sition . mixed transition
ABSTRACT: The change of a reactor from an initial to an equilibrium
state, as
I well as the most important phy:3ical indicators of various types." of
this
tmndtimwe discusiedbasWen the auunptk-A dut ft relmdkg. - -of one fuel
element pro-
duces an insignificant reactivity jump1h the entire reactor and that
the spatial
distribution of the neutron flux Is constant and does not depend on the
burn-up
fiactiorpof diefuel elawnt*.ata gt=-pDJnt, The routm-nuidplicatknfacbrs
In tfr*tr&v1d=-., state,.
N
Card', 1/2

ACCESSION NR: AP4029'693
the .1ifference between the old and fresh fuel elements, and the
equilibrium
r eloade d ai a constant rate equal to
transition whereby the fuel elements are
m equilibrium rat* am discumed in parda a The nepdve aspectof Me
eqLdirfun rewtor tza ft
is that the bum-up of the first fuel charge is half that of an
equilibrium burn-up.
This is because the fuel elements 4re extracted from the reactor as
soon as it is
started. Better efficiency can' be achieved by delaying the fuel
elements in the
reactoruntLI they ge irradiated to son dog, , and then extracting
them at a constant
rate which would prevent the reactor reactivity from dropping below
the required'
level. The other schemes include: the Ponstant reactivity
transition,;, the mixed
transition, and a transition with, a second degree reactivity
dependence. "The
author extends his gratitu de to B. L. loffe for his discussion of
this project.
Orig. art. has: 5 figures and 55 f orlaul &6o
ASSOCIATION: Institut yademykh issledovaniy ChSAN, Prague-Rzhezh
(Institute
of Nuclear Research, C echoKovak Academy of Sciences)
'JZ
S UB MITTED i 05Jun63 ATD.PRESSt M'50 ~4 ENCL: 00
SUB CODE t NO REF SOV 1 001. OTHERs 001

f
r- DWORTIE-1107-Ij )n~
%'r V"s
ACCESSION NR: AP4049539 S/0089/64/017/005/0380/()?84
AUTHORS: Bartoshek, V.; Lelek, V.
TTT-E: Burnup of natural uranium moving axially in a-reactor
SOURCE; htor.iaya energiyav, v. 17, no. 5, 1964, 380-384
TOPIC TAGS! -reactor buckling, reactor fuel, reactor operation,
nuclear fuel burnup
.. BSTRACT: The effect of continuous axial motion of the fuel elenzent
on the neutron flux distribution and on the burnup of natural urani-
um in a heavy-water reactor is examined. A simplified nodel in
which the variables of the buckling equation are assumed to be
separable is used, and allowance is made the dependence of %he.-
neutron multiplication coefficient on the burnup of uranium. Calcu-
latior.i� for 10 reaetat vaeiani-s are ecrnpare,]_ 14-- Is s~-.own that
motio" of the uranium in a single direction increases the burnup
Corti 1/2
-777~
ow
o
E~

element-s--are - continuotisly replaced,- -and -improves the rmody -
namd c
operating conditions of the fuel elements. A regime in wh' ch half
the fuel moves in oppvsition to the other half increases uranium
burnup by 40% without changing noticeably the ccndition5 of heat
-trans fer~f rom -the --fuel ele ts _has.i 1 f igure -26
formulas, and I table.
ASSOCIATIM, None
SUBMIPTED.-
13Dec63
FA;CL:
00
so CODE:
1~~ NR REk'SOV. -001

001

BARTOSHgVjCH..A.t-i,nzh.
d large-panal apartment houses. Ra stroi- Mosk.
EconomicallY Plann6 (MIRk 11:9)
1 no.6:3-6 Jo ,58.
cmogcow-Apartment houses)

BEKER, M. Ye. (Bakers, M.]j BARTOSHMCH, G.I.; V=TUR,
U,E. [Wenturs, U.),
LURE, Y&.YA. (TA7.e,.T. I I
Growing and drying of fodder yeast in the Milgravio
Distillery.
Farm. i spirt, prom. 30 no.7t29-33 164 (MIRA 18t2)
1. Institat mikrobiologii Ll latviyukoy SSR (for Baker).
2. Hil-
gravskiy spirtovoy zavod (for Bartoshevich). 3. Sovet
narodnogo
khozyaystva Latviyakoy SSR (for Viyestur, Lazha).

-s-fF 7
Radio' imtelile.-Ii
ou
19:- 8~4-"
ard VI
ossa,
Bartoshevich' I.
e3 of Peoples, bemocracies
In countri
aadio 6, 14 1954
three., gw4-,L -Art,ioles I.'-X& -*-ring to radio-
Abgt,--act 2. IkInder the above title, aiv.'given:
ictivi _trations.
tour- i - .. , 1~.~ary. i - -~ -
ijj~ Cj_jtrdtl- Bulga-ria ArA~j
M-21M.
A'A"
V:
R.
70
SW
qy_

BARTOSHIVICH, Htj,,--
klane-parallel fabrics of hypersurfaces. Doid. AN SSSR 124
nC095:
970-972 Y '59. (MIU M-3)
I.Moskovskiy goeudaretvauM universitat imeni M.V.
Lomonosova.
Predstavleno AlmAemikom P.S. Aleksandro-rrm.
(Surfaces)

3
16(1)

AUTHORt
Bartoshevich~ M.A. SOV/20-124-5-2/62
TITLEt
Plane
Parallel Fabrics of Hyperstarfaoes (Plosko-parallel.1nyye

tkani
giperpoverkhnostey)
PERIODICALt
Doklady Akademii nauk SSSR,
1959,Vol 124,Nr 5,PP 970-972 (USSR)
ABSTRACTt
The author obtains
three theorems with the aid of an invariant

-method of
investigation for embedded manifolds developed by

G.F. Laptev
[Ref 3,4) and A.M. Vasillyev [Ref 5,7 ; they contain

necessary
and sufficient conditions that a p-fabric.in the

n-dimensional
space be equivalent to a plane parallel p--fabrio

(see Blaschke
[Ref Ij ). In theorem 1 it '49 p - n + 1, n >2 9

in theorem 2 p
is arbitrary, n >2, in theorem 3 p is arbitrary,

n - 2 . The
author thanks Professor G.F. Laptev for his

assistance. - There
are 6 references, 4 of which are Soviet,

I GermanD and I French.
LSSOCIATIONs
Moskovski-y gosudars-tvennyy universitet imeni
M.V.Lomonosova

(Moscow state University imeni M.V. Lomonosov)
PRESENTED:
October 14,1958t by P.S. Aleksandrov, Academician
SUBMITTED:
October 9s,1958
Card 1/i

/W c 5, ~, or
6)91f14 A*
7~V
Avr~/
gW St1fY1Choo',#.,
/ ~4-
0