SCIENTIFIC ABSTRACT PARFENOV, V. A. - PARFENOV, V. P.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001239220007-5
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 99
• Document Creation Date: November 2, 2016
• Document Release Date: June 15, 2000
• Sequence Number: 7
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

AID P - 4383
Subject USSR/Power Engineering
Card 1/1 Pub. 110 a - 9/17
Author Parfenov, V. A., Kand. Tech. Sci.
- -----------
Title Conditions of the surface of equipment parts and resistance
to high tempe:satures.
Periodical Teploenergetilca, 5, 43-46, MY 1956
Abstract Experimental research on the behaviour of the surface of
equipment par*,s made of two heat-resisting alloys on a
nickel basis :is reported. The influence of the plastic
surface deformation upon the fatigue strength of the
parts reportedly depends upon the test temperature and
the teMperatu,7e of re-crystallization. Five diagrams,
5 Russian references, 1932-1955, 1 American, 1951.
Institution : None
Submitted : No date

PARMOV. V.A., kwididat te)dinichookikh nau)r.
vm~ww bmwn*aw
Indium. N=MmL i zhimil 23 no.n:63 N 156. (Km 9: 11)
(Imdi=)

137-58-6-13334
Translation from, Referativnyy zhurnal, Metallurgiya, 1958, Nr 6, p 312(USSR)
AUTHOR: Parfenov, V. A.
TITLE: An ~Inve`stigati~oo ~e Process of Fatigue Failure of Alloys at
Elevated Temperatures (Issledovaniye protsessa ustalostnogo
razrusheniya splavov pri -vysc)kikh temperaturakh)
PERfDDICAL: V sb. : Issled. po zharoprochn. splavam. Vol 2. Moscow,
AN SSSR, 195 7, pp Z I I - 2 2 7
ABSFRACT: The process of fatigue failure of alloys subjected to high-
temperature cyclic deformations was investigated. The kine-
tics of oxidation occurring during fatigue tests of refractory
alloys EI-617 and EI-437 B was studied on cylindrical speci-
mens (S) which were subjected to rotary flexure on machines
of the Ya-8 type at temperatures of 750-8000. It is shown that
voids formed within slip planes of surface grains accelerate
the oxidation process by diffusing OZ atoms in a direction
opposite to that of the atoms of alloying elements which are
diffusing toward the surface of the S. The properties of
oxide films thus formed exert a definite influence on the cy-
Card 1/2 clic strength (CS) of the metal. The adverse effect of

137-58-6-13334
An (nvestigation of the Process of Fatigue Failure of Alloys (cont. )
oxidation of alloys involves a lowering of the recrystaIlization (R) temperature
of the layer just underneath the film and the creation of stress concentrations
whenever surface defects undergo oxidation. Structural changes in the sur-
face layer at phase-transformation temperatures were investigated by means
of electrochemical dissolution of S' s made of the alloy EI-437B after they
had been subjected to various processes of mechanical treatment and isother-
mal aging, as well as after aging processes combined with cyclic stresses.
It is shown that the CS of the alloy at temperatures corresponding to the
beginning of R is a function of the initial structural stability of the surface
layer of the S. After investigating the effect of plastic surface deformation
on the CS of the EI-437B alloy, it was established that work hardening in-
creases the CS provided no R takes place during the tests and the compres-
sive stresses introduced at testing temperatures have not yet been removed.
X-ray analysis performed on 5's of EI-602 alloy, which were subjected to
fatigue tests with asymmetrical tensile-loa.d fluctuations at temperatures of
700-8SOO, revealed a blurring of the doublet and a reduction in the intensity
of reflection lines. The widening of lines is explained by the crumbling of
grains and disorientation of blocks. The reduced intensity of interference
lines Avith a concurrent increase in amplitude of cyclic slips is attributable
to the formation of defects on the slip planes in the form of associated voids
and micropores. 1. Allo-ys--Fatigue 2. Alloys--Temperature factors V. N.
Card Z-!12 3. Alloys--Test results

I- 17f-- f'lVV
SUBJECT: USSR/Chemiatry
25 -4 - 32./ -4
AUTHOR-. Parfenov, V.A., Candidate of Technical Sciencee
TITLE% The Rare Metal of Lithium (Redk:Ly Metall Litiy)
PERIODICALs Nauka i Zhizn'~ - April 1957, # 4, p 63 (usn)
1BSTRACT: It is the lightest of metals and does not exist in pure form.
For industrial purposes it is used in the form of chemical com-
pounds. Caustic lithium is ueed to fill high power electric
batteries which last without charge three times longer than
ordinary ones. Lubricants, in which lithium forma a part, re-
tain their 9 roperties in extremely low temperature and in as
high as 100 C; they are successfully used to reduce friction
among machine parts. Lithium compounds containing chloride and
bromide decompose carbon dioxide and are employed for purifying
air in submarines during extended submersions, Lithium compounds
are also added to the fuel of jet and rocket engines as lithium
given off considerable heat when exposed to oxygen. The range
of application of lithium is becoming wider every day.,
Card 1/2

0
j S -- ~L - 3 -.2-1
/ --~ V
I
TITLEa The Rare Metal of Lithium (Redkiy Metall Litiy)
ASSOCIATION:
PRESENTED BY:
SUBMITTEDi
AVAILABLE: At the Library of Congress.
I
Card 2/2

AUTHOR: Parfenov, V. A., Cand. Tech. Se. 657
'R-el:a-~n ~etwe`en the fatigue and the ultimate strength
of alloys at elevated temperatures. (Sootnosheniye
mezhdu vynoslivostlyu i dlitelluoy prochnostlyu
splavov pri povyshennykh temperaturakh).
FRIODICAL: "Netallovedenie i Obrabotka Iletalloy" (Metallur, and
Metal Treatment), 1957, No.6, pp.IT-73
ABSTRACT: On the basis of test results and evaluation of
published data (1-5), the fatigue limit and the
ultimate strength is compared for a number of heat
resistant alloys at 60D to 850,0. In the analysis
of experimental data the author attempted to elucidate
certain phenomena relating to the complex process of
fatigue fracture of alloys. At elevated temperatures
the magnitude of the rupture stress for nickel base
alloys is determined by the duration of the stress
application; this is illustrated by the data of
Tapsel, R.I. (2) relating to nimonic-80 for 700 and
750 0 for which the 10 000 hour fatigue limit is half
the value of 100 hour fatigue limit. Fig.1 shows the
fatigue limit and the ultimette strength values at
800 C for the Ni-Cr-Ti alloy with tungsten and
molybdenum, 9W517. The results were obtained on
smooth specimens of 5 mm dia, (ultimate strength) and
8 mm dia. (fatigue). The fatigue tests consisted of
Vir

f
Relation between the fatigue and the ultimate strength
of alloys at elevated temperatures. (Cont.)
alternate bendiag in all directions of the stationary
specimen with a frequency of 50 C.P.s. It can be
seen from this Xigure that for test durations below
20D hours fatigie failures are more likely than
failures due to loss of static strength. The
intensity Of strength reduction at phase transformation
temperatures is higher for static loads than it is for
cyclic loads. Figs. 2 to 4 give the fatigue limit
and the ultimate strength values for 600 and 300 hours
respectively for the alloys M395~ DW43 and $M617
at 600 to 850 C.; the values expressed by full line
curves relate to smooth specimens, whilst the dotted
line curves relate to notched specimens. Usually the
notch brings about a considerable reduction in the
fatigue strength but no change and even an increase
in the ultimato strength of the alloy. The magnitude
of the relative plastic deformation amounted to
fractions of percent per hour; fractures observed
during this pri,)cess are attributed to the diffusion
of vacancies La the crystal lattice which accumulate
at grain boundaries and develop into cracks owing to
the diffusion flow of new vacancies to the grain
boundaries. Ttte relative deformation of the alloy in
the case of constant specimen dimensions is much
Cmd 2/4

657
Relation between the fatigue and the ultimate strength
of alloys at elevated temperatures. (Cont.)
higher in the case of fatigue stress than it is in the
case of long dxr:,ation static stress; alternate sliding
along the slidiag planes of the weak grains bring
about intragranilar fractures,, It can be seen
clearly from the included mic~~o-photographs that the
width of the areas deformed by sliding surfaces grow
from cycle to cycle. Even slight discontinuities
forming during cyclic shifts as a result of cyclic
loads will not heal at relatively low temperatures and
load, even in the case of relatively low cyclic
stresses, to a rapid loosening of the material; at
higher test temperatures (above t ) a part of the
forming loosening vacancies and iKs the beginning of
fracture will occur later thtm in tests for ultimate
static strength at which the plastic deformation
proceeding at low speed brings about diffusion
processes aloq~ the grain boimdaries and the healing
of sub-micrOBCI)PiC fractures is less effective than
in cyclic streiis. Investigating the intensity of
the processes 3f disintegration of the solid solution
the author fouad earlier (10).that cyclic stresses
accelerate the process ofdeCOMPOBition of solid
solutions. The fatigue limit and ultimate strength
curves plotted in the same coordinates of stress
against time to failure intersect. For test durations

657
Relation between the fatigue and the ultimate strength
of alloys at elevated temperatures. (Cont.)
of 200 to 500 hours fatigue fractures are more likely,
whilst for longer test durations failure due to static
stresses are more likely. It was established that
for each alloy a temperature t exists under given
conditions at which fatigue fraPture is more likely,
whilst above that temperature failure due to static
loads is more likely; the temperature of equal strength
of deformed nicicel base alloys for smooth specimens
varies between '760 and 800 Ct whilst for notched
specimens it v&cies between 800 and 850 C. The
difference of t'Ae position of the fatigue limit and
ultimate Btrengbh curves for a given temperature range
is attributed by the author to the sharp difference in
the magnitude of the relative deformation of the
specimen and the difference in the speeds of plastic
deformation and also in the unequal intensity of ageing
of the alloy during fatigue tests and during ultimate
strength tests. It is stated in an editorial comment
that the quantitative relations between the ultimate
and fatigue strength as a function of test duration or
the temperature given by'the author are valid only for
the speeds applied by the author and are likely to vary
as a function of the loading speed. 10 figures, 10
references, 6 of which are Slavic.
AVAILABLE:

AI~V /1/0 L-11 71
Ilk
Ax kand.tekhn.reuk; IANI L.L. red.;
,r:~
Ar' r-d.
e
Pe ta Is of progress],Netally progressm. MDBkVS. 12d-vo *Znanie.l
1958. 31 p. (Vaesciuznoe obahchestvo po rasprostrananiiu politi-
chaskikh I asuchafth znanii. Ser.4, tic.1) (MERA 11:2)
Oletals)

1?9-?-4/*ll
AUTHOR:-Parfenov, V.A. (Cand.Tech.Sc.)
TITLE: Features of the Process of Fatigue Fracture of A-11oYs at
Elevated Temperatures ( Osobenrosti protsessa ustalostnogo
-razrusheniya splavov pri vysokikh temperaturakh)
PERIODICU: Metallovedeniy,B i Obrabotka Metallov, 1958, Nr 2,
pp'.19-22 + 1 plate (USSR)
ABSTBACT: The heat resistance of alloys is being evaluated on the
basis of results of long duration strength tests and creep
tests without taking into consideration fatigue character-
istics of the material. Very little experimental data is
available on fatigue of alloys at elevated temperatures.
For some steels and alloys results obtained in TsNIITMASh
have been described by Aleksandrov (Ref ,.1) and Shishkova.
The fatigue characteristics and the notch sensitivity of
alloys after various heat t6eatments were investigated up
to 8000C on the basis of 10 loading cycles. Analysis of
data published by Aleksandrov and also by other authors
(Refs.2 - 4 ) allows certain general conclusions on the
fatigue of high temperature alloys at test temperatures up
to 0.7 Tabs of the melting temperature; some of these were
experinentally confirmed. Absence of a fatigue limit at
Card 1/5 elevated temperatures is attributed to the fact that due to

1?9-2-4/11
Features of the Process of Fatigue Fracture of Alloys at Elevated
Temperatures.
relaxation, hardenirg caused by plastic deformation is
eliminated; disperse hardening has practically no influence
owii~g to accelerated disruption of coherent bonds between
the lattice of the separated out phases and the bazic lattice
and also owi.*ng to coagulation of the separated out phases.
Sliding processes are accompanied by breaking up tile grain
into blocks and development of" sub-micro cracks. Therefore,
specimens subjected to fatigue tests at elevated temperatures
have lower high temperature strengths than the specimens in
the initial state. The softeni7pg effect of cyclic stresses
is always larger than the effect of long duration static
stresses at the same temperatures. Micro-plastic deformat-
ions duri.-ipg alternating stresses accelerate considerably the
processes of structural tran formations on slidirg planes in
grains of the alloy and make it possible to investigate, even
by optical methods,certain phenomena of fatigue of austenitic
alloys . Metallographic analysis is inapplicablefor studying
creep phenomena but can be successfully used for studying
Card 2/!; processes of fatigue. In specimens subjected to cyclic

1?9-')-4/'ll
Features of the Process of Fatigue Fracture of Alloys a6 Elevaled
Temperatures.
bending at elevated temperatures a difference can be ob-
served clearly between the str~acture of those surface grains
which are most highly stressed during the tests and the
grains located in the centre of the active cross-section;
considerable deformation can beobserved in the surface
grains, as can be seen from Fig.IA(Plate); particles of the
second phase of lamellar shape are formed in the sliding
planes. The geometrically regular distribution of these
lamellae enables detection of the planes of facilitated
sliding in the grains. No process of plastic deformation
is observed in the grains of the core of the active cross-
sectionp i.e., grains which Exe not highly stressed during
bending tests. If in the calse of riiekel-,-,Lrom-Lum-ti--6-anium
alloys the surface grains show twining, the plastic defor-
mation is usually developed mainly along the twining planes
which represent loci of reduoed strength of the metal; the
twining planes of the surface grains bec*me gradually
thicker during fatigue and only one of them develops into
a micro-crack, Fig'.2 (Plate). The effect of cyclic stresses
accelerates tile formation of lamellar phases from the sliding
Card 3/5 plane and particularly on tLe twining planes. With increas-

Features Of 'L
Temperatures.
ing test duration the lamellar separations become increas-
inglY isolated (Fig-3), their tlaiickncss may reach 1,,u and
jaeir length several tens Of '/L- . In the case of ageing
7,Dlaase transformations may be observed only after test durat-
'~ons exceeding tens of times the duration of fatigue tests.
*Differing operatinC temperatures require differing initial
I:ieat treatment. Fatigue test data show that up to 0.5 T
point abs
of the melt inir/temperature austenitic alloys are less
:3ensitive to notches after be'j.ng liardened to. form a solid
solution, which. at these temperatures still has a high
-Dlasticity; at test temperatures (0'.6 to 0 7 T the
:3ensitivity to stress concentration is lower As the same
alloy after stabilisation since at this temperature range
:stabilised alloys have a high plasticity although their high
-temperature strength is lower,, In evaluating the hLigh tem-
-Derature characteristics of alloys it is important to know
1he i~elations between the fat.f.gue limit and the long duration
Strength for each d1loy. As an example, in Fig.7 the curves
4/5 ;3-re graphed of an W-37 type alloy. It can be seen that for

129-?-4/-il
Features of the Process of Fatigue Fracture of Alloys at Elevated
Temperatures.
300 hours the probability of fatigue fracture at
7500C is higher than of fractures caused by static loads;
with increasingtest durations (applying lover stresses)
Tatigue fracture uecomes less likely. There are 7 figures
Mgs .1, 2, 3 and 6 on Plate), and 6 references, all of which
are Slavic.
AVAIIABIJ-',: Library of Congress.
Card 5/5

ADTHORs Parfenov, V.A.9 Candidate of Technical Sciences 25-58-4-.25/111
TITLEt ln the Plasmatron Jet (V struye plazmotrona)
PBRIODICAL: Nauka i Zhizn', 1958, Nr 4, n 67 - 68 (USSR)
ABSTRACTs The heating up of fast moving bodies in the Earth's atmosphere
is a great problem, the invoBtigation of which requires the
artificial creation of temperatures over 4t5OO - 5,0000. For
this purpose, foreign scientists have devised a plasma gene-
rator, the so-called plasmatron, developed on the basis of
an improved electric are. To carry out rocket tests, the
plasma jet is placed into a aerodynamic tube. Plasma tempera-
0
ture can exceed 100,000 . Information on some American plas-
matrons is given. There are 2 sketches.
AVAILABLE: Library of Congress
Card 1/1 1. Aerodynamics 2. Thermodynamics

3OV-129-58--o-8/17
AUTHOR: fenov, and.Tech.Se.)
~q~ ~-__ V ~~C
TITLE: 'Protective Coatings of He'at Res-istant... Alloys (Zashchitnyye
-pokrytiya zharoprochnykh splevov)
PERIODICAL: Metallovedeniye i Obrabotka Metallov, 1958, Nr 61
PP 33-37 (USSR)
ABSTRACT: English and American work (Refs.1 and 2) has shovim that
accelerated corrosion of gas turbine blades made of nicicel
base alloys is caused by vanadium and sodium, micro doses
of which exist in certain grades of fuel. In this paper
the results are described of investigations of the strength
of specimens made of the alloy E1437B (20.10% Cr; 2.401%.Ti;
0.71% Al; 0.04% C; 0.45% Si; 0.20% Mn; 0.005% S; O~006% P;
0 60516 Fe; 0.05% Cu; 0.05% Zr; the rest Ni) and of the alloy
H617 (composition as per standard spe,;ification); the
active neck of the specimens was of 8 mm dia. On the basis
of results of tests of chromated and enamelled specimens
the following conclusions are arrived at: (1) A 0.1 mm
thick chromium layer will bring about a 16% increase in the
fatigue strength at 75000 of the alloy E14~W. A 0.1 tc
0.2 mm thick chromium layer will bring about a 14% increase
in the fatigue strength at 8000C of the alloy E1617 (50 -
Card 112 106 cycles). (2) Wi-th increasing number of test cycles,

SOV-129-58-6-8/17
Protective Coatings of He4t Resistant Alloys,
the effectiveness of chromating from the point of view of
increasing the fatigue strength of the alloys EI 43?B and
E1617 increases. During the tests at 8000C the electrolytic
'Layer . 'recrystallises . with an appreciable speed and there-
.Core application of chromium-as a protective coating of com-
,-~onents operating at temperatures above 8000C is inadvisable,
0
4) Enamelling increases the fatij~ue strength of specimens of
.~he alloy EI617 at 8000C (300 his) by 15% compared with the
fatigue strength of reference specimens. Apparently, for in-
(.reasing the effectiveness of enamelling, it is necessary to
reduce the baking temperature of enamelled components.
There are 5 figures and 5 references, of which 3 are En-lish,
'D
I French and 1 Soviet.
1. Heat resistant jaloys - Coatings 2. Heat resistant alloys
Corrosion prevention 3. Vanadium - Corrosive effects
4. Sodium - Corrosive effects 5. Chromium - Applications
Card 2/2

AUTHOR: Parfenov, V, A. BOV/126-6-2-27/34
TITLE: gation of the Plastic Deformation of Metals
During Cyclic Loading (Issledovaniye plasticheskoy
deformatsii metallov pri tsiklicheskom nagruzhenii)
PERIODICAL: Fizika Metallov i Metallovedeniye, 1958, Vol 6, Wr 2,
pp 359-362 (USSR)
ABSHULCT: The aim of the here described work was to study the
process .of formation of twin crystals of deformation.
This was done by a method of investigation of the plastic
deformation during cyclic loading which is described.
The experiments were made on the nickel alloy EI602.
The alternate bending (from two sides) of flat specimens
was interrupted after each fourth cycle for the purpose
of observing changes in the structure. For convenience
the cyclic bending was effected at large values of
residual deformations. The 50 x 6 x 2 mm specimens were
deformed by impact loads in a special test rig.
Individual specimens were subjected to 0cyclic bending by
an angle equalling 2.5; 7.5; 15 and 25 . The progress of
Card 1/2 twin crystal formation in the surface grain of a specimen
was investigated with an increasing number of cycles of

SOV/126-6-2-27/34
Investigation of the Plastic Deformation of Metals During Cvclir-
Loading
alternate bending of a specimen of the nickel alloy EI602
with a face-centred lattice. It is shown that durin,z
investigation of the ultimate strength of specimens
of an alloy witha face-centred lattice the plastic
deformation is effected not only by sliding but also as
a result of formation of twin crystals.
There are 4 figures and 4 references, 3 of which are
Soviet, 1 English.
SUBMITTED: August 201 1956
Card 2/2 1. Nickel alloys--Deformation 2. Crystals--Metallurgical
effects 3. Nickel alloys--Crystal structure 4. Nickel
alloys-,Ti#t-m&thods-5. Crystals--lattices

PARFE"OV, V.A.ML kand. takhn. nauk
W. t5pll- -.-
V~- ~-, ^-q
Airplanes without rivets. Nauka I zhiznl 2.5 no. 6:6.9 Je '58.
(MIRA 11:8)
(Airplanee-Shect-metal work)

PA]UnKIV9 V.A9q kandetakhnanauk
HYP&raonlc f21ght. Naulm I zblznl 23 no*B.,69-70 Ag 158.
(MIRA '12:9)
(Aeredymmics, Supersonic)

AMS ~Mj 2(10) FW1 I a= nyw1jaylew 3OV/2;10
Atelmnarm snerglys v aviatell I rokketney tommiker sbornsk statey
(AtOMIe Iner t Collection
a In &via lon and Rocket loginver
r Aftleles) Unease, Vqvon. lad-we 14-ve abor.1"Ma 1959. 500 p.
.73 a bibltatelos) ft. eagles printed
*riseI Vauehao-papulyarnay al?I
Not given. I
Zd,g;dCamVIl,rv ?.I. Astashenkov, Ingla"P, Lt.-Call U. o Va. M.
erg Tech. ad., "T
PVRPMXI this book is intended for errieffre or the Soviet Armed
Varoo:,,,waboro of DOSUP, and the general reader Interested In
the u or stowto ensersy and in the development of aviation and
rookst eagizaarlall.
Co"Mazo This ealleettan of %G &rt&also, compiled by 28 Soviet
scientists and based chiefly an non-Soviet materials, discusses
various aspects of the use of &taste ongergy In racLetry and avia ;r
t4on. The took surveys the development of atowle am therwonuels
weapons and weapon cg"Lgrg. Isyl dome the ortneIVIes of anti-
steel$ defense, and *valuate* the appIlestlon of nuclear snaergy
in aviation am reaketry. Pug, avid construction natorials, as
wall 06 actual OW818-1 and technological processes Involved, &Va
treatoof briefly. Fundamental* of Ltc"e werfur% and combat t&Q-
ties are discussed at some length. MM book In divided late four
of %hlGJA the last consists chiefly of &Rtl-Wg~torn grape.
306tica I IN devoted to nuclear weapons and their use In
aviation- S*Otlcn rr Is On &Ati-atemle defense. especially the
dsts"99 and decontamination of airfields and aircraft, and do-
r6Rs9y4f:i1n~t radiation. Section III im-en the use of nuelv&r
sO4dVn arlaraft and rocket technology mod flight tech-
lnftludl;!tQcfts GROulstlons an space travel and an the
energy a he U" . r0 `1" 126 r1gures and 35 non-3orlet
r0f%r0n :.f to~ In Russ jag
n Translation).
TABLE OF o0rMMj
aiporeft and Rocket* as C&F_
sal Ru IQ Weapons 48
Petrov, A. flnginser-U. Col"011- ftid0d Missiles With an Atowle
M&M 18 Aviation and Uti-aipcraft D~Ion~g T8
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NuVlfav, V, arrootiven~ss of Rocket Weapons 104
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Arkh_LPOT, N. (Docent, Candidate Of Technical 3sionces, Inginoor-
Lt- MOD811. Contemporary Atcale Paub. am Rocket* 144
Arkh1pov, X. CO"tff"OPAr? ThOrmOnu&20&r Bmbs &ad Rpek&t. ITI
LrkiPOT, M. The @"called 'Clean" RYdrOton Nmb IT9
Card 4/ 9

SOV/25-59-1-36/51
AUTHORt Parfenov V A Candidate of Technical Sciences
I
TITLE: Reactive Wings (Reaktivnoye krylo)
PERIODICALt Nauka i zhiznl, 1959, Nr 1, p 69, (USSR)
ABSTRACTs The article is based on a publication in the journal
"Aviation Age", 1958, Nr 8. There is one drawing.
Card 1/1

-2
29( SOV/25-59-7-32/5./
AUTHOR: Parfenov, V.A., Candidate of Technical Sciences
TITLE: A Thermo-Electronic Generator
PERIODIC:J'i_L: Nauka i zhiznl, 1959, 111r '?, p 69 (USSR)
ABSTRACT: This is a description of a project of a thermo-electronic
generator for artificial Satellites for both the earth
and moon published in the western press. The project
features direct conversion of thermal power into elec-
tric energy. The generator consists of 2 netal plates
separated by only several thousandths of a mm and built
into a vacuum tube. One p;ate is to be heated t8 the
temperature of about 1,200 C. the other - to 500 C. :~Iie
electrons,due to the process of "boilin- over", tr,,~vel
u
from the hot to the cooler plate. Connected up by a
conductor, electric current can be thus produced. T-Icr-
mal energy for the generator will be supplied eithur b.-,.
U
an atomic reactor or by the sun.
Card 1/1.

1(
SOV/25-59-9-31/49
AUTHOR: Parfenov V.A., - Candidate of Technical Sciences
TITLE: Rocket Aircraft
PERIODICAL: Nauka i zhiznl, 1959, Nr S1, pp 68-69 (USSR)
ABSTRACT: The article is based on the following journals:
"Aviation Age", 1958, Nr 21 and 8; "Aviation Week",
1958, Nr 17, 22 and 24 and. "Missiles and Rockets",
1958, Nr 4. There are 2 French and 4 English-language
references, and 4 diagrams.
Card 1/1

69735
S/025/60/000/05/027/044
DD48/DOO6
UTHOR: Perfenov,-V.A , Candidate of Technical Sciences
TITLE:
PERIODICAL: Nauka i zhizn'. 1960, Nr 5, p 67 (USSR)
ABSTRACT:
Card 1/2
I.D. Kulagin', Candidate of Technical Sciences and
engineer I.V. Nikolayev both from the Institut
metallurgii Akademri~nauk SSSR (Institute of Metal--
lurgy of the USSR Academy of Sciences) have deve-
loped a plasma burner which develops a temperature
0~ ature of plasma inerea-
of 15,000 Since the temper.
ses-when subject to lateral pressure and the passage
0
between cathode and anode is narrowed, the electric
are is placed in the barrel of the welding pistol.
The most powerful plasma burners require a current

69735
'L)/025/60/000/05/027/044
D048/D006
A Plasma Barner
Card 212 of several 100 amp and a 30-50 volt tension. L~(

80820
'2q,1000 3/025/60/000/06/08/- 12
AUTHOR: Parfenov. V.A. Candidate of Technical Sciences
J_ il~
TITLE- Return From Space
PERIODICAL: Nauka J. zhizn', 1960, No. 6, PP 31 - 33
TEXT- This Is a brief popular review of four foreign (nation not stated)
design proje-2ts of space vehicles, capable of returiing to the Earth without burning
in dense atmosphere, 1) A "winged gliderJ'I, 2) An Inflatable triangular vehicle
whIch would descend on a spiral path with no more than 360 km/hr and for which
specialists In many countries are trying to create elastic carbon-metal material
with sufficient heat resistance; A. %, r, d
_3) "ballistic capsule" with braking rockets
parachutes, -wrning its wider end about when entering the atmospher -,, 4) "Sputnik
with aerodynamic brake", it is said that foreign specialists are working most
Intensively )n the "ballistic capsules" and the "splitnik with aerodynamic brake",
which botb could be brought already now Into an orb.~t by the existing rockets.
Card 1/1

84891
2- 2 D2, 2107, 2307, '1712 S11,004/60/000/010/001/008
A00VAGO-1
AUIHOR! Parfenov, V_ Candidate of Teahnical Sciences
TTTLEt Space Vehiole Returns to !-he Earth Penetration intc the Unvers~
PERIODICAL, Znaniye - Sila, 1960, No~ 10, pp. 1-3
TEXT,-- The article gives a general Informattion on the problems crnnected
with the p,anetration Into the universe by a space vehicle anJ the temperaturez~.
arising in the vehicle'g. nose cgn~_Iand carrying components, Me following tc..
pics are considered! 1) the nose-cone problem; 2) behavior of metals in 41%e
cosmic space; 3) the family of hig:h-melting metals, 4) evaporation of metals,
and 5) magnetic cooling. The consIderations refer specifically to the man.
carrying space vehicle and the ret).2rn :;4P Tran to the Earth, i.e., the re-entry
problem under cosmic and atmospheric conditions, - The pointed stream-1.1ned
nose c:,!ne gives rise to a thin boundary layer, verr high temperatures sl_nce
W X
weak shook waveslreflec~.Into the atmospbere only about 50% of !he thermal ener-
gy, The 1:.lLintbodv coneWausez- a high-intense shook wave reflecling -InTc, the
atmospherc- more than 90% of the tncrmal energy, decreases sharply its speed
when reentering 'the atmosphere, and affects Intena-zly the man A braking f%n-
Card 1/5

84891
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A005/AO01
Space Vehicle ReturnE to the Earth - Penetration Int.-D the Univers~
may decreaE;e the deceleration forces. Ihe known effects are described t--l
which the ~!ngineering materials are sub~eoted in spaced meteoric showerr, ' nuc
lear particle showers, sharp temperature contrasts, *t-hermal ' vibrational . a-
COU5tical offects, the plasma in Uie Earth's atmosphere, DegaEsed materials
must be used. - High-melting metals beryllium, columblum, molytderum, tan*.a-lunl,
and tungsten are aonsidered In detail in respect of weight, me-Iting pc'int,
rigidity arid resistance to high temperature-c' heat absorpt-lon, ductility. forge.
ability, 9xidation stability, alloying property, ac1tt resistance * ba5e re-nFlance
electrochemical corrosl-~n resistance, heat conductancie, The alloys are -on-
sidered,c, -~antalum-tunjzsten, and on the mol.ybden base, which give the most C"K
pedient. cc-inbinat-Jon of properties for the operation under high- temperature cc-n
d.itions. The molybdenum oxide forms rapidly and is volatile and evaporates.
Alloys are required having more expedient properties than the known all,:~y.A
Therefore, investigations on solid physics, metallurgy, and metal teol-incl)gy
must be c&rried out. High alloys are required with high heat. capacIty and -_:ow
beat oondu2tance, and seifs-ablimating materi-als are needed for eliminating 'he
heat wnen the vehicle re-en'ters 'the atmo5chere. the latt.er prcblem is mcs'.1y
Card 215

84891
S/004/60/OOo/ojo/Ooj/Oo,R
A005/AO01
Space Vehiale Returns to the Earth - Penetration Into -the Universe
promising in the opinion of the non-Soviet investigators because the transilli-n
of a solid Immedlately Into gas requires a huge amount of heat, Vb1ch .-an be
eliminated with the metal gas, Only the heat conductance must be low enough
for avoiding the heating of the cabin, Scientists of the USA considered tne
conditions of the re-entry of a satellite from the altitude of 160 km with the
speed of 6,4 km/sec, assuming for the sake of simplicity that the trajectory of
landing is perpendicular to the Earth's surface and the total kinetic and poten-
tial energies are transformed into heat at the instant of attaining the Earth'E
surface, According to these data, about 5,500 kcal of heat will be emitted per
each kg of weight of the satellite. Therefore, the metallic walls 6f the
satellite must have an unacceptable thickness, due to the intensity of this
thermal flw:. Circulation cooling is also insufficient for eliminating the heat
emission, Beryllium oxide is an expedient refleotory and sublimating material
of low weight, which evaporated into the gaseous state at abcut 2,5000C, which
is not harmful for the structure and equipment of the satellite because the heat
exerts durirg a short time, and the heat conductance of beryllium oxide Is low
In the same manner, tantal, molybdenum, tungsten, silver and also plastics can
1-15
Card 3/5

84891
S
C 4/6o/ooo/o lo /oo 1/ooB
AO
A005/AOO I
Space Vehicle Returns to the Earth - Penetration Into the Universe
be used; the latter has low heat conductanoe, elasticity, and resistance t,')
heat shocks. Such sublimating materials can be used for covering the main
elements of the space vehicle such as the fuselage nose and the leading edges
of wings, and the empanage. The Pigure 3 shown a hypoth.etic wing profile ami
cross section before and after re-entering the mosphere. The slTucture co_m-
k. b
ponents loaded are covered by a heat insulation layer of asbestos"or quartz and
a sublimati-ng material layer, The sublima~.ion of the nese cone and the wings
increases the drag of the vehicle and leads to decreasing temperature - Ther-
mal radiation can also be applied to protection against superneating, It 1_--
estimated that up -1: 40% of heat ~_oming in"c, the vehi,le surface f-om the
boundary layer can be zeflec~ed intc the atmosphere, ihe reflecting proper*Ie-Z
can be increased by enlarging the.reflecting _zurfal~es and burnishing them -
I -io
In the opinion of non-Sovl=lt scientists, the dissociat n and ionization of
the gaz- in the shock wave and the boundary layer of the s-'reamlined body can
be utilized for heat dissipation when applying an electromagnetic fleld, wh-1--n
mcves aside the charged particles and reflec.-S the ionized gaB (plasma) -
In the opinion of non-Soviet sclentists, ,he minimurr. weigtit ~_-f the heat-dissipa-
card 4/5

84891
S/004/60/00O./cio/00 I '0G8
AD05/AO01
Spaoe Vehicle Returns to the Earth - Penetration Into the Universe
tion equIpMent, will resilt from the methcd of Sublimaticn of the ~-irfa-e 13yer
which will be "Eacrificed" - There are three floares.
Card 5/5

PARMOV, V.A., kand.tekhn.nauk
I. Returning a sWe ship to earth. Vost.Vot(I.Il. no.llt65-68 1 060.
(MIRA 13:11)
(Space ships)
f.

PARFENC7 V lmra.tekhn.nauk
-Itz ~-- ;--W "
Wings. Gr-azhd. av. 17 no. 11:28-29 N 160. (KRA 13:12)
(Airplanes--Vings)

PHASE I BOOK EXPLOITATION SOV/5653
Farfenov, Vasilly Aleksandrovich
Vozvrashcheniye iz kosmosa I~Return From the Cosmos) Moscow, Voyenizdat
M-va obor. SSSR, 1961. 67 P. (Series: Nauchno-populyarnaya
biblioteka) 75,000 copies printed.
Ed.: V. L. Stdrligov, Engineer, Major; Tech. Ed.: M. P. Zudina.
PURPOSE: This booklet is intended for the general reader.
COVERAGE: The booklet deser4bdng the entry of space ships Into the
atmosphereis based on information from popular-type scientific
open publications. Certain projects of the entry of space ve-
hicles into the atmosphere, deceleration systemq, and selection
of construction materials are discussed. No personalities are
mentioned. There are 33 references: 27 English, 4 Soviet, and
2 German.
Car.4-41~5-

FAILFENOV, V.A... kand.tekbn.nauk
A feat worthy of the land of Lenin. Vest-Vozcl.Fl. no.3:7-10 Mr
161. \1 (Astronautics) (NIU 14:6)

8 5~5 IL 7
19.22tb
S/129/61/000/004/009/012
E073/E535
AUTHORa Parfenov, V, A., Candidate of Technical Sciences
TITLE,., Change of the Bt~_e_ngth and the Structure of Metals
During Cyclic Loading
PERIODICA&vr~"Vetallovedeniye i termicheskaya obrabotka metallov,
r 1%)61, No.4, pp.40-44
TEXTt - The author studied the changes in the strength and
structure of some metals and alloys after cyclic loading at room
and at elevated temperatures. Specimens 0.5 + 0.01 inm thick,
10 MM2 cross-section were subjected to alterna-ting bending tests
and to tensile tests. Specimens of the alloys AAQ'. .(.ADI) and
JZi(D 016) were annealed for two hours in vacuum (10-'mm Hg at
300*0 and specimens from the alleys M3, -_'16~1 (L62) and CZpO-1) (Br,OF)
were annealed at 600*C. one batch of the bronze specimens were
not annealed and were tested after plastic deformation. Various
groups were subjected to a differIng number of load cycles
(1, 10, 100 and 1000 cycles). The service life of the specimens
from ADI and D16 materials was 1200-i500 cycles and that of
copper and copper alloys was 1400-1600 cycles. Most specimens
Card 1/6

S/129/61/000/004/009/012
Change of the Strength and E073/E535
were subjected to cyclic bending tests at 20'C. For obtaining
comparative results, a part of the Al alloy specimens were tested
at 3000(; and a part of the copper specimens at 6000C. After the
cyclic Roading the specimens were electrically polished and
subjectod to tensile tests at 200C, microhardtiess tests and also
X-ray structural analysis. Flat specimens of the alloy
(E1602) were subjected to fatigue tests under asymmetric tension
at 700,
800 and 850*C, making X-ray exposures in the zone of
maximum stresses and In the clamping zone where the stresses were
half the maximum stresses. Circular specimens of the alloy
(EI437B) were subjected to fatigue tests under symmetric
circular bending at 7500C. Following that, they were cut along
the axia, the deformed layer was etched in the cutting plane and
the exposures were made from points with differing stress
conditions during the fatigue tests, i.e. at the centre of the
neck and its periphery. Some of the results obtained are
plotted in the graphs, Figs.1-4. On the basis of the results
the following conclusions were arrived at;
1. The strength of metals and alloys as a result of cyclic
Card 2/6

S/129/6i/ooo/oo4/009/012
Change of the Strength and .... E073/E535
deformation does not change in accordance with the same pattern.
Commercial aluminium and partly copper will harden somewhat at
first and then soften appreciably with increasing number of cycles.
The strength of annealed duralumin and brass,increases with
increasing number of cycles. Cold-worked bronze softens as a
result of cyclic loading.
2. The strength of alloys, which have been cyclically loaded at the
relaxation temperatures, changes in the same way as they do in
c
o.
mmercially pure metals.
3. The change in strength of metals with increasing number of
cycles of alternating plastic bending is influenced by the LX
irreversible processes of loosening in the slip planes. Slowing
down of the process of loosening by preliminary work hardening can
be achieved only at temperatures at which the processes of reversal,
and particularly recrystallization, are braked.
4. At a certain stage of its development defects in the crystal
structure cannot be eliminated by annealing. This is the main
difference between the effect of repeated plastic deformations and
that of a single plastic deformation.
There are 4 figures.
Card 3/6

Change or the Strength and ....
8 9,6 P2 7
S/129/61/ooo/oo4/009/012
E073/E535
Fig.1 Legend:
Stretching of the specimens of the
alloy DIIS as a result of cyclic
bending, load, kg vs. deformation,mm.
Graphs a - test temperature 20*C
(from left to right 1,100,1000 cycles)
Graphs b - test temperature 3000C
(from left to right 1,10,1000 cycles)
Card 4/6
too
0 1 M 0 1 Ij 4
50
30- LL-L--L- I U a
jrl- 1) -1 1 --1 f4j
Of 254 f Ij 4NIV
-
V~

Change of the Strength and ....
Fig.2. Legend:
Stretching of the specimens subjected
to plastic bending tests at 20*C,
load, kI; vs. deformation, mm.
Graphs et - copper (from left to right
1,1,1000 cycles)
b - cold-worked bronze
(from left to right
1,1000,1000 cycles)
Art
1 2 J 4 of 2 J a
?J 4
IX.1
Rt F 9
11 ard 0 1 1 J Iffs.
C
S/i2q/6i/ooo/oo4/oo9/012
E073/E535
Fig.3. Legend:
Relative change in the
streng:th of Al and dural-
umin as a function of the
number of bending cycles
and test temperature.
Change in a % v9. cycles.
b*
1<
0 ~~fvo
t
)AI

Change of the Strength and ....
Fig-4-
Legend:
'RelaUve change in the strength
of copper, brass and bronze as
a function of the number of
bending cycles and the temperature,
change in strength V % vs. number
of cycles. b~
(black dots - tests on cyclic
bending at 20OC;
dots - tests at 600*C).
white
8 "': 6 2 -1
S/129/61/000/004/009/012
E073/E535
%
-Q IF
I

of

Card 6/6

V.,. , I , . I
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I- -~ . -r . - ~---C:S.
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cc. MR A
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UNOTi. INIC)Aip Ne & aifenv~ T. A Semenavj~
J
A. v F
7777 - 777.1771
5 an& Coviittee.ov-tbe Ifse of At6mic Efiergy.,85SH,
COG, Lca:_ PmerInititute,.. State
ches po.~ Is-p`OMF';wn-
Lki;:eni eti E691 -at
It
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TLE:` "Oe -a eriba of sl&O-
Ightion 6f elastI6 catt 0% cim tirconium bydridt
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6kryp - a Ow neutiojm~- scattering cross, sectialij -di ial cross section
t
_t'".Ahe art cle describes rons scatt
f ered by
measurementof the-ape ra o n
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49D *band 2DC. The
gle of t6 the Incident,bes* at t6werstures. C
tvwe - 4 iiiti;. a- slv4 t
VA rpeu rqn'double ape roveter'.described by 1. 1.
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and qu
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ge .00
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Ahe Oustlc-~xcatUrir -,v- 72i Imiewlty or the mono-
t 0-1~ n rons at h a -van - %25 Nev.
e I&IkWa -N"NWN~ 04,'OiWii~ it,-energy
or. iwdrom'- vAb
~tx -vere enav 0.02 Mmjo: the total re-
'mmn
Ir
rd

F. K. ; PP-11 IJXICHM' , R.R. [Pbu I a VI P-1 1:,g P-"i"FF N C'
A IEYNTKC)V
SLIMS, V.A. [snizys, V.1)
Effect of heat. tri,-atment. on some phy,-:c:umechn-n,c,--' and
stnicture of silicate glasies. Part 1: I-Ile-chanical jrcperties.
Tnidy All Lit.S-S-R. Ser. B. no.12:97-109 16-5.
2. Instittit khiTO 'i i khimi~,heskoy t,,kiinologli M; ',,'Tovq'wOy
Submitted Auf-,,st 6, 19r',4.

PAMNOV, V.A.; AIEYNIKOV, F.K.; SLIMS, V.A. [S3.izys, V.
Use.of the therzographic mthod for the determination of vitrification
temperature. Trudy-AN Lit. SSR. S&r.B no.103-38 065. (MRA 18s7)
I. Institut khimil. i kbinicheskoy tekhnologii AN Lltavskoy SSR.

BONDARENKO, I.I. (deceased];-LIFOROV, V.G.; MMOZOV, V.N.; NIKOLAYEV, M.N.;
PIRFENOV. V.A.; SEWNUI, V.A.
Wiasurement of neutron spectra in nickel, iron, and stainless steel.
Atom. energ. 18 no.6:593-601 Je 165. (MIRA 18:7)

-PARFENOV, V.A.; SLIMS, V.A. [Slizys, V.]
Effect of the conditions of synthesis of dicalci= silicate on
its physicochemical properties and processes of hardening. Trudy
AN Lit. SSR Ser. B no.3:143-166 162.
(MIRA 18:3)
1. Institut khimii i khimicheskoy tekhnologii AN Litovskoy SSR.

PARRNOV, V.A.; SLUES, V.A. fSldz,,,,s, I,.)
Utilization of concretes,, unu--Pble in constructicn-, as a
agent in the mayufacture of autorlave products. Trudy AN 5,31;.
Ser. B no.4:197-202 162. (MITIA IF:3)
1. InstiLut khl3mii i khimicheskov tekhnologii. P, L-itovskoy SSR.

MT G-r-

PARFEWOVP V.D.; KOnDRAT'DV, V.A.
Characteristics of the formation of shifting dislocatione in
the Karamazar Momtaine. Geotaktonika no.D68-79 ja-F 166.
(MIRA 19:1)
1. Mookovskly gosudarestvennyy univereitet imeni loomonosova,
geologicheakiy fakulltet.

N:-4
loond'

PARFEFOV V.I. [Parfionau, V.I.]
Intraspecific variability of the Norway spruce at the southern
range of its massive distribution (in Polesye). Vestsi AN BSSR.
Ser. biial. nav. no.4:16-22 164. (MMA 18:12)

oreBt-forming role of spruce and the characteristics of spnuce phyto-
cenoses In Polesve. Bot.; issl. Bel. otd, VBO no.6sll9-131 964.
(WRA 18s7)

PARFENOV J. V.I.
New biological forms of the Norway spruce in White Russia.
Dokl. AN BSSR 8 no. 3:18F-192 Mr 164. (MIRA .17:5)
1. Institut eksperimentallnoy botaniki i m1krobialogii
AN BSSR. predstavleno akademikom AN BSSF I.D. Yurkevichem.

YURNEVICH, Ivan Danilovich.; ~,taflancvich;
"-- I
I-D., akarlemik,
red
alder f3rest~, axid ttieir economic use] Seroollko-
,ye 1, . -' -1
'kh ,hoziaistvenrioe isprillzovanie. tllinsk~ Izd-
vo AN BSSR, -1963. 142 (141riA 17.10)
1. ~Lkademaya n;71-uJ, ~for NeGterovAch)-

)0V V.I. (Parrionut Val.)
PAPW - P.- - -
Typological and goobotaniml ~hsraatariatias of spruce forests
tt the southern rango of apme (in Polosye). Vest$ j AN MR,
Sort bilaL navo noe~j2l-26 165. (MIRA 18,11)

PARPENOV,,V.M.; ZVORYKINA, L.N., red.; BDRDVNEV, N.K., tekhn. red.
NOWNION'" igz-
(Safety manual for the driller in open pits] Pamiatka po
tekhnike bezopannoBtl dlia burillahchika (na otkry-tykh ra-
botakh). Izd.2., perer. i dop. Moskva, Gosstroiizdat,
1963. 24 P. (MIRA 16:8)
(Boring-Safety measures)

PAgnMr.,~.CMKHOVffAT4 T.P., red.lsd-val RUDAKOVA, N.I.,
tekhn.red.
[Handbook of safety regulations for the driller In open Pita]
Pamiatka po tekbnike bezopasnostl dlia burillshchiks (us
otkrytykh rabotakh). Moskra, Gom.izdv* lit-ry po Ntroit.,
arkhIt. I strolt.materialemi, 1961. 19 p. (MM& 14:12)
(Boring-Safety measures)

FARFENOV, Ul.; CIIEKHUVSKAYA, T.P., red. izd-va; DOROWIEV,
tekhn. red.
[Guide to safety measures for blasters (in open-air operations)]
Painiatka po tekhnike bezopasnosti dlia, vzryvnika (na otkrytykh
I rabotakli). Moskva, Gos. izd-vo lit-:7 po, stroit., arkhit. i
stroit. material=., 1961. 21 p. (MIRA 15:3)
(Wildirg-SafeV moasures)
(Blasting-Safety measures)

PAEMOV, V.P., kand,tekbn.nauk
- 1, 1 1 ~ - I ~e -d~-;;-. 4-
Experience on the design of statiams in sections of a heavy~-duty
min line. Sbor. trud.LT-IZHT no.22:lt:120-:150 164,
(MIRA 18:8)

5/1 2Y60/000/010/008/016/XX
A033 A133
AUTHOROSs Gellperin, N.-'V.1 Zvolinakaya, V. V.; Parfenov, V. S., and
Sherman, A. D. I
TITLE& Technological process of casting crankshafts for the AB-30
(DV-30) engine at the Vladinorovskiv traktornyy zavod (Vladi-
mirov Tractor Plant)
PERIODICALz Litsynoye prdzvodetvop no..10,,.1960o 16 - 17
TEXTs Based on the experience of the-Kharikov "Berp i molot" Plant,
the Vladimirov Tractor Plant started the casting. of arankshaf to for the
J)V-30 engine. The authors enumerate the deficiencies occurring during the
casting of the crankshaft for the CMPr7 (BUD-7) engine at the "Berp i molottl
Plant and point out that the elimination of black spots by increasing the
machining tolerances is not expedienti therefore, it is necessary to pre-
vent the origination of black spots which can be attained by the desulfuri-
zation of the cast iron, bringing the S-content down to 0.008 - 0.005%.
This is possible if the cast iron is smelted in a basic electric furnace.
Attempb were made to eliminate the technioal difficulties connected with the
Card 1/3

B/128/60/000/010/008/016/XX
Technological process of casting crankshafts ... A033/Al.33
shell molds. Besides, specimens were cast to determine the maoro- and
microstructure and the mechanical properties. Table 1 shows the results
obtained. The sand-resin mixture was prepared in a mixer of N11LITMASh de-
sign, model B21, the shell mold was made on a model 830 machine of NIILITMM
design. The cast crankshaft structure contained ledeburite cementite. The
crankshafts were annealed as to the following conditionst holding at 9500C
for 2 - 5 hours, cooling in the furnace to 6300C, holding at 6300C for 1
hour, cooling in the furnace to 4500c, further cooling in the air. In com-
parison to die-forged crankshafts 22 kg metal were saved with each cast
crankshaft. The economic effect amounts to 15~'6 of the crankshaft cost
price. There are 4 figures, 2 tables and 4 Soviet-bloc references.
Card 31

-PLESHRO, A.P.; PERFIL'YEV. V.V.
liffecrof auxil.lary connectirw abannels on the operp-tion of strain
gaurev. Ism. tekh. no.3:LI-44 MY-Je '37. (NLRA 10A)
(Strailb gauges)

PAPMOV, V.A. (Parfionavas, V.];,SLIZHIS, V.A. [Blizys,V.l
Problem of the influence of cwAensation on the speed of reaction
of calcium hydroxide with quartz under hydrothermal processing
conditions. Liet ak darbai B no.1:153-163 160. (EEAI 9:10)
1. Institut khImU i khimicheskoy tekhnologAA AN Litovskoy SSR.
(Calcium hydroxide) (Quartz)

Vasi I i .. . IDAVYDDVA, Yu.F.,, red.;
URMU P, - - ~. I A~o'ksandrovich;
ATROSHCERkbo L.Ye.q tekhn. red.
[Four "big chemistry"] Za bollshuiu J~hirdiu- MOskva, Izd-
vo "Znanie," 1964. 47 p. (Novoe v zhizni, nauke, tekhnike.
I Seriia: Istoriiap no.6) (MIRA 17:3)
I
I

PARFENDVv V.A.; SLIZHIS,, V*A. [S:Lizys,V.]
Investigation of hydrothemal proceBses in lim-montmori3-lonite
;and line-hydramica aystems. Liet ak darbai B no.3:93-125 6o.
(EEAI 10:3)
1. Institut khisiA i khiydcheskoy tekhnologli Akadexii nauk
Utovskoy SSR. -
(Lime) (Montmorillonite) (Hydromica)

GELIITW, V.S.; PARFENOV, V.I.
Formation .of speckled elder associations and theix succession
by spruce. Sbor. nauch. rab. Bel. otd. VBO no-3:5-14 161.
(VIIU
14:12)
(Alder) (Spruce) (Forest ecology)

YURKEVZCH., I.D.;.__~A~ ~FJMV, V
Effect of the total of effective tomperaturao on the phonological
phases of woody plants. Biul. Inut. biol. All BSSR no.6:16-26
161. (IMA 15-3)
(Wo=-Pums)
(PLARtBot KFFM OF TRUTSUM CN)

PAMWCfV., V.I.
Differentiation of trees in the plant associations of oak
plantations. Sbor. bot. rab. Bel. otd. VBO no.2:219-223 F60,
(MIRA 3~5: 1)
(Oak) (Forest ecology)

XUROv- p L.-D.1 FLRFENOV, V.I.
Study of trunk shape and size of the speckled alder growing in
the White Russiem SeS.R. Bful. Inst. biol..AN bSSR no.5:71-78
1609 - 4AIWM' - ~W O-M& 14:7)
-P - -W,
. .4-oid"", - a

PARFENOV.,Vasiliy Maksimovich; ZVDFLYKINA, L.N., red.; MIKHEYEVA,
A.A., e
[Safety manual for blasters (in open areas)] Paniatka po
tekhnike bezopasnosti dlia vzryvnika (na otkrytykh rabotakh)
Izd.w., perer.i dop. Moskva, Gosstroiizdat, 1963. 29 p.
(MIRA 160)
(Blasting-Safety measures)

PAUrSHOV, V.P.
Brief news. Geog. v shkole 23 no. 6:83-84 N-D 160.
(MIRA 13:11)
1. Zaveduyusbably kabinetom geografti lialmytekogo instituta
asovershenstvovantya uohiteley, Z.Mlista.
(Teachers) (Decorations of honor)
(Kalnyk A.S.S.R.-Geograpby--Study and teaching)

FIRMOV,, V.P., kand.tekhn.nauk, dotsent
Methods for working out efficient systems
yards. SbDr. LIIZHT no.153:196-208 158.
(Railroads--Yards)
for classification
(MIRA 11:8)

?ARFENOV,, V.P., inz.
Practices in using epoxy compounds in railroad construction
!m the U.S.A. Trudy MIIT no.191:119-133 164.
(MIRA 18:6)

N o k V
32N PHASE I BOOK EXIWITATION SOV/1525
Bartenev, PrDkofiy Vasillyevich, and Viktor Prokhorovich Farfenov
Vodnyy, avtodorozhnyy, vozdushnyy i proinyahlennyy transport (Water, Highway,
JArj, and Industrial Transport) Moscow, Transzheldorizdat, 1958. 303 P.
4,000 copies printed.
Ed.: A.P. Tuarenko; Tech. Ed.: P.A. Khitrov.
PRIME- This book Is approved by the Minietry of Higher Education of the USSR as
a. textbook for students of transportation vuzies specializing in construction
and operatiot. It is also Intended for use by engineering personnel engaged in
the plamnitg, designp and use of the vaL~ious types of transportation.
COVERAGE: This book contains basic information on the design, construction-,
installation and exploitation of a:il means of transport. It provides data on
technical and economic problems conne,?ted with the applicability of each type
of transportation. Docent V.P. Parfenov, Candidate of Technical Sciences wrote
Chapters- IVY VP VII, VIIIY XIV, KV, kTIII, =, and parts of Chapters- I, II,
X~ XVI, XX, XXII~ UVII; Docent S.U. Podkaliner, Candidate of Technical Sciences,
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Water, Highway, Airand Industrial Transpoit SM/1525
vrote Chapter XI; Docent P.S. Labazin wrote Chapters XII and XIII; Professor
P.V. Barteiriev Doctor of Technical Sciences wrote Chapters: VI., IX, XVI, XIX,
YXI, XXII, XXIV, XXV., and parts of Ch-apters XI and XII. The book is divided
into four -parts. P#Lrt One was edited by Professor V.Ye. Lyakhnitskiy,
Doctor of ;Technical. Sciences; Part Two by Engineers: A.F. Solovlyev and
N.A. Tyumenev; Part Three by Chief Marshal of Aviation A.A. Novikov; Part
Four by the Chief Engineer of the Leningrad Department of the Institute
of Industrial-Transportation Planning, A.V. Tepl-itakly. Professor
F.V. Bartenev was the general editor. There are 31 Soviet references.
TAHLE OF COMOTS:
Preface
PPHr 1~ WATER TRANSPORT
3
Ch. I. Gener4a InformLation on Water Tr?~~,nrziport 4
1. Brief mirvey of the developrpnt of water transport 4
2. Types Emd. basic means of water tr6nsport 6
3. Special featureE of water trampp-)rt 7
4. Fleet for the waterways 9
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gater., Highway, Air, and Industrial 1~-vzzporL SOV/1525
Ch. II. Waterways 3-8
1. Waterway requimments and navigation conditions 18
2. Rivers in the zatural state 19
3. Artifizial vatAmmyB and water system 22
4. Sea waterways 32
5. Navigation buo3v and markers 34
Ch. III. River and Ccean Harbors 35
1. general concelts and harbor operations 38
2. MAssification of harbors 39
3- Plan for harbors 42
4. Basic elements of a harbor
5- Harbar equipment
6. CalexiLating di-nen ions for basic hsxbor facilities 6r)
Ch. IV. Funilamentals of the Organtzat-daa of Water Transport
Ope:nations 63
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Water,, Hlgbvay, Air and Industrial TranBport
V. Genexal Infortiation oJ2 the Development of Highway Ccnstraction
and the Class:Xication of kutr-smobile Roads
1. Develojiment of Ug1my constraction
2. Classification of automobtle reds.
Ch. VI. Automobile Traffic
1. Types of motor irehicles
2. Fundamentals of the theory of autamobi-le movement
3. PundmentalB of the calculation of tra-c-tion.
Ch. VIL Technical Mements of Autamobile Rc*As
1. Subgrade
2. Roadway-
3. Layout of the rced in the plan
4. Layout of the road in profile
5. Special features in the design of saperhighways
6. Special featarest of road building In mountainous regions
7- Bridges, culverts, etc.

Water, Highway, Air and Iridustrial Transport SGV/1525
Ch. VM . Road Surfaces 97
1. Parposes of pavements 97
2. C hoice of type of road surface 1010
'J'
,1. Construction of basic types of pavements 101
Ch. IK. Brief Information on Construction,, Repair and Mintenance of
Roads. Economic Efficiency of Design Computations 104
1. Design and construction of roads 104
1
2. Repair and maintenance of roads 1o6
3. Economic e,raluation of design computations lo8
Ch. X. Organization of Transport. Installations for Transport Servicing
and Highiniy Signal;3 and Signs 113
1. Organization of freLght and passenger transport 1-13
2'. InstaLlations for servicing passenger and freight transport 1-14
3. Traffic Wety and -~he highway signals and signs 218
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Wab3r, Highway, Air and Industrial Tran port SOV/1525
PART 111. 61P TWSFORT
Ch. X1. General 'Information 121
:L.'Bri6f survey of the develolment of aAr transport 121

2. Special feahures of air transport
1
123
3. Air lines of the "Aeroflot" 124
Ch. XII. Aircraft of the ' ivil Aviation 125
1. Classification of cl-vil-aviation aircraft 125
2. Design laMits of aircraft
150
!i. Helicopters
4. Basic flight and technical characteristics of aircraft and
helicopters 133
5i. Organization of repair in an airplaxle and engine shop of the
civil aviation fleet of the USSR 155
Ch. XIII. Airfields and Airports of the Civil Aviation and the
OrganiZation of Airline FUghtE 136
1. Classification of airfields and &lrports 136

e.. Organizational structure and technical equ~Lpment of airfields 137
3. Planning the airport's area 138
4. Design of airports 141
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Water, Highway, Air and Industrial Transport SOV/1525
5. Seaplane jorts 142
6. Organization of flights and aircraft traffic control in the airlines
of the USSR 142
PART IV. TRANSPORMION in iNDaSTRM
Ch. XIV. General Information 145
1. Significance of transportation in the prodnction organization 145
2. Brief sury-ey of the development of the industrial railroad transport 146
3. Approach routes 149
Ch. XV. Broad Gage Industrial Railroads 152
1. Classification of railroads (by purpose] 152
2. Basic technical requirements in the design of broad gage sidings 153
3. ConditionE for the design of intraplant broad gage railroads 157
4. Joining sidings to the general redl-road system 16o
5. CrossroadB 161
6. Loading and unloading devices and station equipment 162
7. Rolling stock 164
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Water, Highway, Air and Industrial Transport SOV/1525
Cit. XVI. Narrow Gage Railroad Sidings 178
1. General ir.Lformation 178
2. Profile and plan of narrow gage sidingE (750 mm) 179
3. Profile and track plen for division points 180
k. Profile exid plan of intrafartory Tiarraw gage lines 183
5. Division joints and installations of the ST,B, (signal, centra-
lization tind blocking Bystert) and commmicetions 183
6. Locomotive! and car management 184
7. Rolling stock 185
Ch. XVII. Special Roads 189
1. General ideas 189
2. Snow and Ice roads 189
3. Log roads 191
4. Elevated equilibrated railroads 19-
5. Elevated monorail (hanging) roads 195
6. Back railxoads 195
7. Ground ftaicular railroads 199
8. Suspension railways 201
!). Suspension railways for peasenger transport 213
10. Suspensiorn railroads -with cable trw-tion 215
11. Dumping, suspension cableways 217
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12. Susp--nsion monocablewaYs 217
13. Portable suspension cableways 2185
Ch. XVIII. Pipeline Transport 219
1. General information 219
2. Pipelines for the transport of liquids 220
3. Gas pipelines PPI
4. other types of pipeline transport 222
Ch. XIK. General Conditions in Designing the General Plan of an
Induatkial Enterprise 223
1. Basic information 223
2. Placement of buildings of an industrial establishment in the plan 225
Placement of buildings of an industrial establishment in the
profile 227
4. Organizing transportation of workers 228
5. Location of the locomotive establishment 229
6. Junction and classification stations 229
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