SCIENTIFIC ABSTRACT PERLIN, I.L. - PERLIN, I.YA.
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP86-00513R001240110004-8
Release Decision:
RIF
Original Classification:
S
Document Page Count:
100
Document Creation Date:
November 2, 2016
Document Release Date:
June 15, 2000
Sequence Number:
4
Case Number:
Publication Date:
December 31, 1967
Content Type:
SCIENTIFIC ABSTRACT
File:
Attachment | Size |
---|---|
![]() | 3.2 MB |
Body:
SOV/136-59-7-12/20
I .7pe Ts IF -1.5
Stress Conditions in the Extrusion of Tubes of T A- 9
shows temperatures as funotions cf extrusion speed for
various degrees of defoination. A typical oscillogram is
shown in Fig 2, while Fig 3 shov;,i that for this, as for
many other alloys (Refs A-13), the friction force remaIns
at its maxi-murl value over a wide range of deformations,
The variations in the friction factor and other parameters
with temperatura (250, 275, and 3000C) are 6iven in Table 1.
Fig 4 s-viows friction force for each of these temperatures
as functions cf the ext:,iision speed. The ratio of fri.,tion
force tc the plasti--deformation stress (true resistanee
to deformation) for the average temperature was found "o
vary ~,rithin the range 0.52 - 0.66. The experiments also
enabled the DaramclUers for -'alculating tube extrusion
forces by a simplified equation to be determined (Fig 6).
The almost linear plots of minijaum extrusion force (tons)
vs natural logarithm of extensi)n for temperatures of
250, 275 and 300'C are 8hown In Fig 5. Results calculated
by the simplified equation and an analytical equation
Card 2/3 published by Perlin (Ref 9). using the authors' published
SOV/136-.59-?.-12/20
Stress Conditions in the Extrusion of Tubes of Type TsAM 9-1.5
(Ref 6) graphs, are compared in Tab'.e 3. The analytical
equation gives high values, especia:.ly at high degrees of
deformation when a greater thermal affect arises on the
production than on the laboratory s0ale. The authors
consider the optimum extrusion-speed for tubes to be lip to
8, 3 and 2 mm/sec for 250, 275 and 30COC, respectivell.
There are 6 figures, 3 tables and 15 references, 12 of
which are Soviet and 3 German.
Card 3/3
18-5ooo 78321
SOV/89-8-3-6,1/32
AUTHORS: Perlin, I. L., Nikitin, 1. D., Federchenko, V. A.,
D.-, Re3hetnikov, N. G.
TITLE: Some Force and Deformation CharacteristIC3 of Working
Uranium by Forces of Pressure
PERIODICAL: Atomnaya energiya, 1960, Vol 8, Nr 3, pp 219-227
ABSTRACT: The choice of optimum thermomechanical conditions fo-
worIcing of uranium is complicated due to possibilitie--
of allotropic transitions resultirg in modifications
having different plasticity and strength. Due to Its
high resistance to deformation and small heat capacity,
uranium is often heated considerably during extrusicn
and rolling and changes from a int8 a_ phase. Deform-
ing samples from 90 to 60 mm at 420 'C by means of one
stroke of a friction press, the t-amperature of the
metal rises from 90 to 1000 C. Strong oxidation al,3o
influences the temperature change in the metal duri!-,g
Card 1/17 working. To enable the determination of conditions
Some Force and DeformatJon Characteristics 78321
of Working Uranium by Forces of Pressure SOV/89-8-3-6,/'32
for working of uranium by forces of pressure, the
authors investigated the rolling, ressing, drawing,
P
and die forging of uranium. Figure 1 shows the
influence of the temperature on the maximum permiss-4:--le
reduction per pass of 15-mm-wide cast uranium samples.
Uranium is exceptionally sensitive to nonuniform dis-
tributions of deformations during rolling. For
example, fine uranium strips (0.01~,-0.20 mm) may be
obtained without fracture;reduction per pass 80-85%.
The augmented plasticity is expla--ned as due to
negligible nonuniformities in the distribution of
deformation in the rolled strip. However, whon rol'--
ing cold thin plates with variable rolling direction,
the resulting nonuniformities in deformations cause
fracture of the metal. Figure 2 shows the results
of investigations of the variaticn with temperat,.-ire
of the mean specific pressure pcf, of the metal on
the rollers. The temperature increase in the metal
Card 2/17 during rolling at t = 6300 C causes a transition into
Some Force and Deformation Cha -actcrl.~;tlct3
of Working Uranium by Force.,.; o Prc-,:i:~ure
E: too
0
4-)
tv
1,7
E
19
PLO 'TV JM ikl i4kl O-W 7,V 6X ,,j It)
Ralltmg tempeeature, 'C
78321
Fig. 1. Influence of temperature on rollabIlity cf
uraniumi (x) no fracture of samples was observed.
Card 3/17
Some-Force and Deformation Characteristics
sj
;z
J.,
Acc
Card 4/17
78321
SOV/89-8-3-6/32
Fig. 2. Average specific pressure of metal on rolle:,s
versus the temperaturei -first series of tests;
- - -second series of tents.
Some Force and Defoi.-Iatiun, 78 3 ~) 1
of Working Urani= by S 0": "/,-- q3 3
the pha-se .-.TIch up ag ,taggered oscillograms.
The aguthors also invcstilga'ted the mean specifIc pressure
as function of the reduction at various temperatures and
also as function of the initial state of uranium samples.
They compared the results with `.he analytic equation of
A. I. Tselikov (Proicatnye stany (Rolling Mills) M.,
Metallurgizdat, 1947) and found a satisfactory agi-ee-
ment:
-)(h
p,P
where (11 h)/H i.,,, reductio'n; hif, height of' ~,rip
in the neutral cross section; ( = ~L ~24/ j~s h-
coefficient of friction; D = diam of rc)llers);
k 1.15 nY 0 3 (nY = coefficiEnt of strengthenin,;
T 3 = yield limit in case of large plautir; deforma-
Card 5/17 tions). The value of n Y is function of the reductic.r.
Some Force and Deformation Characteristics 78321
of Working Uranium by Forces of Pressure SOV/89-8-3-6-332
and temperature, and varies between 1 and 1.6. Figure
4 shows the absolute widening 6 b - B 1 - B of a sc~_iare
sample 21 x 21 x 180 m-a with rollers 220 mm in diar7 as
function of rolling temperature, The maximum of tl.e
curves Is connected to the maxim ~m of the friction
coefficient which in the 900-950 C temperature r-2j;ion
is equal to 0.4-0.45. The authors note that uranilLm
can be extruded in the temperature interval betweei, 250
and 1,0000 C, and they discuss In detail the extr,_~.,iicn
characteristics of T - and CL -uranium. They empha-
size that during extrLsion the uranium should not ,orre
in contact either with air or steel tools. Toolz made
from heat-resistant alloys, cartides, and ceramics i,;ith
lubricants are i~sed for extrusicn of C-L -uranium.
f - 'Ically
While extrusion velocities of ~ uranium are prac,
unrestricted, CL -ur;iii-lum is extruded using -,,elocities
between 1 and 400 mtn/sec. The E.uthors investigated
further the extrusion stresses as function of extruslon
ratio, temperature (see Fig. 6), and production mode oil
Card 6/17 the sample. The extrusion stre:js depends linearly on
come Fore,- ~nd D
of Worl-:1.117~ UI-all-I l1:,. P'!-
t.
fill
poll
4
Card 7/17 te.~P(-131lt
Ila 0 11 C ha r a
Some Force and D--:~for,
of Worj~jng Uranium IDY F 3 r c e.,:c
-4
Tv w., ce
-rs
1 4,
Fir.
Card 8/17
Some Force and (,~-. _,1. L
of Working Uranl~:m i~:/ i il~
the lritei-,rul lnde-x of the degr,.e of
and Fljurc. a nomograrn whose cro3l-
hatched regloii ~3hov.,,~ the lnfl~wnce of the scale-factor
on the. pressing sl res, when the ratio of the cort&,_~ner
d la m e t e r,; e (I i, a 1 ~_~ ~ .Thtz! te~A,,,, also showed thal~
CDT) IWJ~ 1 (2~~ tht: f'ovi,, .,,, ui' i,ont:ic t 1'ri(,, t 1 on A:.~
iliirs p;i,~s throuvh
I.rom thu noiriGirrain, th,_
nate orlijn, t!ul th,~ extrusion
0, pr c.--in bt- det(,rmin,:-d from -,he eq ~.itLoii:
P', J."
Of.0 -I' ti - .VP, 1,
In analo~~y with Young's modulus the
coefficient M the mod~ilus of the
pr
Figure 9shc,)vis Lhe varlation of thIs
p e ra tu re .Extrudahl"Ity ipr or the
Card 9/17 defired as:
authors call the
?xLrusion str-ss.
rriodiil~is with ~em-
uranilim
zioine Forcc and De'lorniutlon Characterlz:tics
of Working Urani= by Forces of Presoure
IL
t f-i k") I,
-178321
sov,,/89-~-
Fig. 8. No,,n( gram fcr determination of extr-islor.
Card 10/17 stresses.
Some'Force and D:~formatLon
of Working Uranium b FDrcr~:.; oV Pre.,,,surc.
's~
3 "-'.1
`12
Fig. 9. Modulus of extrusion stress of uranitn ',Er.c;US
temperature.
Card 11/17
Some Force and Deformation Characteristic-,
-of Working Uranium by Forces of Pressure
0 Or
78 32 1
S OV118 9 -8 - 3
is shown In Fig. 10, where the tipper curve is the -aria-
tion of t~e maximum extrudabilitT tinder a pressure of
150 kg,/mm , and the lower Curve is obta--ned using pr
= 15 kg/mm 2. '/ -Uranium has extrudability above
The author3 discuss further the 3tructure of the proci-
ucts and Table 2 exhibits the mechanical propert~E,-
of the extruded uranium. The au-~hors discuss varic-uE
lubricants used during drawing, and present in Table 3
and on Fig. 11 some results concerning drawing of
uranium. WItI, heating one can obtain uranium wireZ 2
mm in diam and less. Modification of heating conditions
allows the production of 0.1-mm uranium wires. Uranium
can be die-forged in the CL and Y temperature regions
with ram velociti up to 6,000-7,000 mm/sec- Any tr-3n-
Card 12/17 sition into the )y region due to overheating, will cause
Some Porce and DA'onnaT-!o,, -1, 8 3
of Working Uranium b, Fc)r(,,2:~ o;*' SOV/89-8--)
k
tu
Card 13/17 Fig. 10. Extrudabllity of uranlum versus temperat~ire.
'78321, SOV/89-8-3-6,/'32
Table 2. Mechanical properties cf extruded
(a) Initial state of uranium; (b) tensile strengtn; (C)
elongation; (d) reduction of area; (e) extruded at; (f)
extruded in CL -phase with subsequent hardenirg fhnp-j)hase.
a b
13b,
% d
e0 350- C . . . 143,0 9.2 S. D
4!.~ 7W-7,50' C - 6t.3 9.2 4, t
V) goo, . . . 80, U 7,6 4")
41
75 7 11
6
. .
L ,
Notes (1) Each figure represents the arithmetic r
value from three measurements. (2) Small Gagarin- Ije
Card 14/17 samples were tu,,ed during tests.
Ov A.,
Table Drcv,ifi,, dra-ging radio. (a)
Initial. sllai.( t,ar; diam,;
final dlam;(d) dra.-.1:x, ~;er pa-5; (e)
of dra,.,~ing; (f) dr" (g) arineal~--~; (h) re~-
liminarily dt-Corm,--d.
a b 0,
111.7 1
2G."() 47
Card 15/17
Some.Force and Deformation Charact-eristIcs
of Working Uranium by Fcrces :;f' Pre.--s--.,re
do.
go
oPdcP6k-#~aOIOt7j
I L~
`u 32 1
SOV,
kL
U
3
Fig. 11. Relationship he-t~%reen draalng parameters an(I
Card 16/17 drawing ratio per pa:iL;.
Some Force and Deformation Characteristir3 -18321
of Working Uranium by Forces of Pressure so V/89--" - 3- "/-, 2
SUBMITTED:
crack formation. The authDrs also d:.sciss brief!" '.~,e
conditions for flat die fo-rging of' 0- andj urani-z-,.
There are 11 figures; 4 tables; and I') -Sc- ,,- referenceL.
February 23, 19'~()
Card 17/17
18.8200 '(5397
sov/149-2-5-23/32
AUTHORS: Koroll, V. K., _~erlln, I.
TITLE: Deformation Resistance of,TsA?1 9-1.5 P.lloy Within Tempera-
ture Range of Hot Working by Pressure
PERIODICAL: Izvestiya vysshilth uchebnyl(h :,avedeni~. Tsvetnaya metal-
lurgiya, 1959, Vol 2, Nr 5, Pp 159-166 (USSR)
ABSTRACT: Zinc alloys are now used by railroads and other industries
as a good substitute for antifriction bronzes. Such an
alloy is TsAM 9-1.5, consisting of 8 to 10% Al, 1 to 2%
Cu, and 0.03 to 0.06% Mg, the balance being zinc. This
alloy corresponds to state standard GOST 7117-56. Previous
studies were conducted by German authors (Beier, W., Wolf, V.,
Nr 8, 1939; W(?iss, E., Metallkunde, Nr 4,
Z. Metallkunde
,
1940), and by Vinogradov, S. 11., Dnestrovskiy, N. Z.,
"Special Bronzes and Brasses;' Metallurgizdat, 1945; they
cover, however, only slow rates of deformation (10 to
120 mm/min), while hot working by prezz-sure involves a
high rate of deformation. The authorEi studied the latter
Card 1/6 using a tension-testing machine with e. pendulum dynamometer
Deformation Resistance of To-AM 9-1.5 75397
41loy Within Temperature Range of SOV/149-2-5-2-~//-32
Hot Working by Pressure
with a ram spced of 0,2, 1.6, 2.5, and 168 /3 e a
drawing bench a- attachment for tensile Ft:,~d
a recording, device for preparing a pri:iiary dlaCram ~)~'
means of an oscillograph. Specimens w:~re rods of B-mm,
OD and a length of 40 to 80 = (GOST 1.~97-1~,`). The
installation is shown in Figs. I and 2. Th- 6eforr-natiu,~
of the specimen can be recorded simultaneo~,;sly cr, the
photographic plate and by the osci'Llog.-aph. The resu!'L3
of tests are given in Table 2. From T~ible 2 it appears
that the TsAM 9-1.5 alloy acquires a considerable streng%hen-
ing only at the beginning (up to 10% reduction), then
sof ens rapidly at 5eforniation 6peeds of 2-5-10-3; 2 .0'7-
.10- , and 6.25 -10- l/bec. However, at a deformat-11cri spoz-d of 2.1 .,,/a~c
a certain increase in the st 6ess of plastic tension is
observed, even at 300 to 350 - One can conclude that
at slow speeds the rate of deformation does not influence
substantially the resistance of the al.-.oy. The maximum
value of the speed factor (6.4, ishich --.s the ratio of
Card 2/6 the stress of plastic tension at any speed and any
75397
sov/149-2-5-2.j/')2
Now
10- 01
0
0
0
0
5 0
-.0
to
Ito
FIg. 1. Diagram of installation fDr simultaneous de,;er-
mination of applied force and cross section of the
specimen during stretchin (1) Reverser; (2) dynaino-
meter; ~3) light source; N) screen; (5) resistance
heat; ( )_plvanometer and thermocouple;,PJ93ower
supply; tdj photographic camera "Zenit-S ; time
recorder; (10) oscillograph rectifier; (11) oscillo.-
Sard 3/6 grapl~ POB-14.
7539Y
ISOV/1 4 9 - 2 -2L!
5
6
7
8
rp 9
Fii. 2. Electric circtilt for recording of tensile --tre3:3.
1 Transformer 220 '1211 v; (2) capacitors, 211 v, ~O m-i';
3 choke; (4) rectifier DGTo-211; (5) milliammeter;
~6 coil resistors (R, woricing, K, compensation); ('~)
regulating rhoostat 2 ~Q microammeter; (9) loop
Card 4/6 oscillograph.
Deformation ResiQtance of TsAM 9-1.5
Alloy Within Temperature Range of
Hot Working by Pressure
ASSOCIATION:
reduction ratio, to the stress ofc3l.astic tension at a
deformation speed = 2.5 - 10- se corresponds to a
temperature of 3500. At 200 0 it is down to 1.3. There
are 2 tables; 7 figures; and 10 references, G Soviet,
2 German, 2 U.S. The U.S. references are: Gonson,
Moor, Proc. ASTM, B. 40. 1940; Mend,,choun, J. Appl.
Mech., December, 19114.
Krasnoyarsk Institute of Nonferrous Metals. Chair of
Metal Working by Pressure (Krasnoyars'kiy institut t*vEt-
nykh metallov. Kafedra obrabotki metallov davlenien)
75397
sov/i49-2-5-2:V--,2
Card 5/6
card V6
S1 182/6O/O0C)/0T)/004/'(D 12
A 1151 /A029
AUTHORS: Perlin, I.L.; Fedorchenko, V.A.
T=% On the Press Forging TeclMology for Uranium Id Uranium Alloys
PERIODICAL~ Kuznechno-shtampovochnoye proizvodstvo, 19 0,&,No. 9, pp. 12 - 18
TEXT. The article presents a review of infDrmation on the technology Cf
forging uranium. The information sources are Ame~ricai (A.I.M.E.). or in English
language, including manuals; proceedings of two *Lnte,~national conferences in
Geneva (1955 and 1958). The two Soviet sources referred to (Refs. 5 and J5) are
only mentioned. The first deals with pecularitiev of pressing L>~Ili~um` zircc-
nium,Auranium and thorium,4and the latter with work safety. All illustra'tions
are from foreign sources. There are 11 figures and 15 references; 9 English
and 6 Soviet.
Card 1/1
PARTIN, I-L-; YNDURCHMO, V.A.
Squipment and protective devices for tho production of heat-releamiag
elements for atomic reactors. TSvet- me".- 33 no-818&93 Ag 160.
(WIRA 13:8)
Oluclear reactors--KateTials)
(Radiation protectLon)
FERLIIqP I.L.j SHAPIRO, V.Ya.
Comparative analysis of power conditions in pipe drawing with
floating and fixed cylindrical. mandrels. Sbor. nauch. trud.
GINTSVET~ET no.33:299-304 160. (WRA 15:3)
(Drawing (Metalwork))
KOROLIV V.K,; PERLIN, IJL - Prinimal uchastlye TSYUY GO-FAN [ChIU Kuo-f g),
s udre~ni_ -_ - - -,, an
Production of-bimetal tubes of TSAM9-1.5 - duralumin alloys by
means of press forging. Sbor.. nauch. trud. 3INTSVETw,r no.33:
310-317 '60. (MA 15:3)
(Laminated metal) (Forging)
IVANDV, A.I.; PERLIN,_I.L.
Establishing the basic parameters of drawing steel-alunLinum
bimetal wire. Sbor. nauch. trud. GINTSVETMET no-33:324-330
160. NIRA 15:3)
(Wire drawing) (Lamdnated metal)
S/ 136/61/000/001/005/0 10
1:193/E283
AUTHORS: Perlin 1. L. and Glebc.v, Yu. P.
TITLE: Determination of the Shape of the PLane of Contact
in Extrusion with a Ple.stic Pressare Disc
PERIODICAL: Tsvetnyye metally, 1961, Na. 1, pp. 72-75
TEXT: The problem of keeping to minimum the weight of the
discard from extrusion billet becomeE particularly important in
extruding costly metals or alloys, and the present article des-
cribes a method of achieving this end. The method proposed is
based on the application of a conical die, used in conjunction with
a spacing disc of a plastic metal (with deformation characteristics
similar to those of the extruded material), placed between the
extrusion ram and the extrusion billet. The principle of the
method- is best explained by referring to Fig. I which shows (1)
the extrusion billet; (2) plastic metal disc, and (3) extrusion
ram, before (A) and after (B) extrusion. The salient feature ot
the method consists in that the mating surfaces of the extrusion
billet and the spacing disc are not flat, but convex and concave,
respectively. If the correct shape of the curved interface (line
Card 1/3
S/136/61/000/001/005/010
E193VE283
Determination of the Shape of the Plane of Contact in Extrusion
with a Plastic Pressure Disc
D-C-E, Fig. 1,A) is chosen, it becomes flat (line D,-C'-E,, Fig.
1,B) after emerging from the die, so that. the tail end of the
extruded rod is free from the "piping" dofect and does not have to
be discarded. A method of determining the correct shape of the
curved interface from the co-ordinato net pattern, superimposed on
the meridian face of an experimental billet, is described. Apply-
ing this method to alloy,40b (D16), extruded at 420 0C from a billet
40 mm in diameter, to an 18.4 nim diameter rod, the present authors
found that the correct interface constitutes, in this case, a
quadratic paraboloid. It is concluded that if this method is
employed in extruding metals at relatively low temperatures (below
5000C), the extrusion process can be carried out without producing
a discard from the extrusion billet. TI-iere are 4 figure5 and 2
Soviet references.
Card 2/3
S/136/61/000/001/005/010
El),3/E283
Determination of the Shape of the Plane of Contact in E-xtrusion
with a Plastic Pressure Disc
Fig. I
Card 3/3
4v A
PKC, 1. CXCMa K npoUCCCy npeccommn
C I?-IaCM4CCXOfI f-POKAUKOR
A - AO HAqal- nrue:ca; F - nmie
Oxommam". "p"'Iecce;I-, npeccvem" me.
fs.na; 2 -.rII#rt"qHaR npoxAajKa: 3
npeCC-wjkA5*
S1149A
A006/AOO1
AUMORSt Perlin, I.L., Glebov, Yu.P.
TITLE: On the Shape of Elastic Zone in a Die During Pressing Through a
Single-Channel Flat Die
PERIODICALs Izvestiya vyashikh uchebnykh tavedeniy, Tsvetnaya metallurgiya,
1961, No. 2, pp. 1,31 - 133
TEM The shape of the deformation iseat in pressing.through flat dies is
determined by the elastic zone. The effect of various factors on the magnitude
of elastic zones has been dealt with in a number of publications (Ref. 1 - 4).
However, they do not explain the causes of a constantly equal shape of the sur-
face separating the elastic zone from the deforming metal volume. The shape of
this boundary represents a trajectory of the motion of peripheral layers of the
pressed metal. Investigations of this boundury provide data on: regularities in
metal flow during pressing; characteristics of the surface of slip in the de-
formation seat, and on the effect of the aforementioned boundary on force condi-
tions. The authors attempt to explain the causes determining the surface shape of
the elastic'zone. For this purpose it is suggested to use the principle of the
least work and the least time for the trajectory of motion of metal particles
1/000/0)2/014/017
Card 1/3
s/149/6 1/000/00;2/b 14/0 1 y
A006/ADOI
On the Shape of Elastic Zone in a Die During Pressing Through a Single-C haxL-iel
Flat Die
(Fig. 1). The trajectories of particles from poin-t A to B can be determined ana-
logous to the solving of Bernoulli's problem of the braohistochrone which shows
(Ref. 6) that the given curve Is a cycloid (Fig. 3" which is concave in the motion
direction of the point and resembles by its shape the boundary of the elastic zone,
Another method of demonstrating the concave shape of the curve formed by the tra-
jeatory of a point moving at high speed and mViimum time is shown in Figure 4.
The straight line m - m, parallel to axis x, c;7osses the poss1ble trajectories in
points a, d, f. Time is gained when the shortor section is passed at a lower
speed and the longer section at a higher speed,, Sections of the course, passed by
a point at the same level and by different trajectories, are in the relation Ac <
< Ad < Af, i.e. at the beginning of motion at lower speed, the concave trajec-
tory provides for a shorter course, and for a longer course at the end of motion
at maximum speed, since 'the section of the trajecto-.7. below m - m are in relation
Be ',', Bd > Bf. Thus the shape of the elastic tone surface during pressing through
flat dies, corresponds directly to the principle of the least work. This Is Im-
portant when developing methods of determining forco conditions for pressure work-
ing of metals by the least work principle, usIng variational calculus. Data ob-
Card 2/3
s/14q/6i~=/OD2/o14/oi7
AOO6/AO01
On the Shape of Elastic Zone in a Die During Prestsing Through a Single-Chermel
Flat Die
H
ta3ned may be used for designing pressing tools.
Figure 4:
Figure.13
Schematic drawing of an elastic Schematic drawing explaining the shape of the
zone during pressing with a flat boundary between the elastic and plastic
L
die. zones during pressing through a flat die.
9 A
There are 4 figures and 6 referenceas 5 sovielt and I non-Soviet.
ASSOCIATIONS: Krasnoyarskiy institut, tsvetnyXh metallov (Krasnoyarsk Institute of
Non-Ferrous Metals). Kafedra cbrabotki inetnllov davleniyem (De-
partment of Pressure Working of Metals)
Card 31-3 SUBMITTED: October 5. 1960
8/149/61/000/005/005/008
AO06/A101
AUMOR: Perlin, I. L.
TITLF: On force conditions and metal flow rates during the last stage of
pressing
PERIODICAL: Izvestiya vysshikh uchebnykh zeLvedenly, Tsvetnaya metallurgiya,
no. 5, 1961, 170-173
TEXT: An investigation was made for the purpose of analyzing and making
more precise the concepts of the effect of friction forces during the last stage
of pressing and of the nature of changes in the strained-stressed state of the
deformation seat atihis stage. The investigation was carried out with direct
extrusion of a round rod through a plane die. Factors were studied affecting
basically the slide speed of the pressed metal over the contact surfaces of the
pressing tool during the last stage of pressing when the press plate begins to
enter the reduction section of the deformation seat. Formulae are given to ca:_
culate the volume feeding the pressed work piece, the decrease per second of
the feeding volume and the rate of sliding and f'.ow through the cycl~ndrical
surface. It was found that the mean sliding ra-te of the pressed metal over the
Card 1/3
s/14q/6l/000/0()5/D05/OC8
On force conditions and metal flow rates ... A006/AlO1
contact surfaces of the press plate and the die, End the flow rate of the metal
In the plane which Is perpendicular to the pressing axis, are inversely propor-
tional to the current height of the ingot in the containers; these rates Increas~.
sharply with a rapid decrease of the height. Thin increase In the flow rate of
the pressed metal and Its sliding rate along the press plate end surfaces and the
die, when the press plate enters the reduction section of the deformation seat,
and the less marked increase of these rates prior to this, are explained as
follows: before the press plate enters the deformation seat, the volume of the
latter does practically not decrease, and the same amount of metal is supplied
as is delivered to the pressed work piece. After the press plate enters the
deformation seat, its volume decreases inevitably. This entails an increase In
the flow rate of the metal and its sliding over thu contact surfaces of the
press plate and the die, at an unchanged volume supplied to the pressed work
piece per second. Thus the basic cause of the sharp increase of the pressing
force during 'the last stage of the process, is the increased sliding rate of ~h~
pressed metal along the contact surfacen of the press plate and the die. There
are 2 figures and 1 Soviet-bloc reference.
Card 2/3
9 S/149/61/000/005/005/008
On force conditions and metal flow rates ... Aoo6/AIOI
ASSOCIATIONS: Krasnoyarskiy institut. tsvetnykh metallov (Krasoyarsk Institute
of Non-Ferrous Metals); Kafedra oorabotki metallov davleniyem
(Department of Pressure Working of Metals)
SUBM'."I"IrED: March 9, i961
k,/
Card 3/3
S/i8o/61/ooo/oWoOl/020
E193/E383
AUTHORS- Berman, S.I. and Perlin, I.L.
TITLr.. Scientific and technical problems of plastic-working
of nonferrous metals by the operations of the
squeezing group
PERIODICAL:. Akademiya nauk SSSR. Izveistiya- Otdeleniye
tekhnicheskikh nauk. Metallurgiya i toplivo,
no. 6, 1961, 3 - 7
TEXT. Rapid expansion oZ the national economy envisaged in
the new programme of the Communist Party of the Soviet Union
will necessitate a corresponding increase in the production
capacity of the nonferrous metal-workina, industry and in the
range of the materials produced. This, in turn, will necessitate
the introduction of new techniques, aggkimeration of various
fabricating processes and their intensification attained mainly
by widerapplication of electrical heating and by increasing the
speed of deformation. Some of the problems created by these
developments and means of their solution are discussed briefly
in the present paper.
Card 1/5
s/iBo/6ii/ooo/oo6/001/020
Scientific and technical .... E193/9383
1) It is suggested first that the quantity of rolling stock
produced can be increased by incorporating the malting, casting
and rolling operations in one continuous line. This system is
at present applied on a small scale in the production of aluminium
foil and wire, and work is in progress on the development of' a
similar process for the production of copper-wire and rod. The
main difficulty in applying this process -to melting two-phase
alloys is their tendency to segregate dur:Lng casting, as a
result of which, lengthy homogenizing treatment, difficult to
incorporate in a continuous line, is neceissary. In this
connection, it would be desirable to nearch for alloying
additions and/or methods of casting whi.ch would ensure homo-
gene-ity of the billets.
2) The output of tubes could be incroased by changeover from
extruded to seam (straight or helical; welded tubes fabricatod
by a continuous process. The results of tentative investigations
have shown that this technique could tie successfully employed
on an industrial scale for fabricating copper, brass, nickel,
alumir-lum, duralumin and other nonferrous--metal tubes. However,
Card 2/5
s/i8o/6i/ooo/oo6/001/020
Scientific and technical E-193/E383
before this technique can be usefully cidopted, problema will
have to be solved of producing consistently high-quality welds
which will possess practically the samo mechanical properties
and corrosion-resistance as the material outside the welds A
reliable method of continuous testing of the quality of the
welded seam would have to be developed.
3) The efficiency of extrusion processes could be increased
by reducing the percentage of wasto material; this could be
attained by extruding without the formation of extrusion
discards , by increasing the extrusion speeds and by the appli-
cation of extrusion techniques sim:Llar to those used in
cable-sheathing.
3) It would seem desirable to explore the possibilities of
using ultrahigh pressures in extruision, wire-drawing, rolling and
forging processes. In addition to other benefits, solution
of this problem would bring about an increase in the strength
of the f 'inished product and a corresponding reduction in the
quantity of metal consumed.
Card 3/5
S/180/61/oo(VO06/001/020
Scientific and technical E193/E383
The difficulties associated with the shortage of' some metals
ca-n be overcome by wider application of clad materials. In this
connection, there is a need for development of new methods of
thermal and mechanical treatment which lorould ensure the for.-
mation of a high-strength bond between the core and the cladcling
materials,
5) High priority should be given to research and development
work on powder-metallux-gy technIques, partIcularly as applied
to dispersion-hardened materials.
6) Friction between the tool and the fabricated metal is an
important aspect of all metal-working processes. A search
should be instigated for more efficient and cheaper lubricants
and more attention!hould be paid to the problem of pressure-
feopding the lubricant into the deformation region.
7) More attention should be paid to pracess-control and
intipection at every productiion stage. Work should continue
on the devel,?Rmgnt, of reliable and accurate testing methods, and the
stektiatici_ cess control should be more widely used.
Card 4/5
SABol61/ooo/oWool/020
Scientific and technical E193/Z383
8) There is an urgent need to devolop the theory of plastic
working of complex shapes or difficult materials (titanium.
tantalum, niobium, germanium, uranium, thorium, beryllium, etc.).
9) Since the number of nonferrous semi-fabricated and finished
articles of different shapes and sizes, made by plastic-working
processes, exceeds 20 000 positions, more attention should be
paid to specialization of new plants whose location should be
ch-DSen in a less haphazard manner.
Card 5/5
26798
1"54 1"0jt- !;/136/61/000/007/0C'2/002
19111/E480
AUTHORS. Berez, A.A., Koroll, V.K., Perlin, I.L.
- i__
TITLE: Experiments on the industria production of
zinc alloy- armco iron bimetal strip
PERIODICAL: Tsvetnyye metally, 1961, No-7, pp.65-69
TEXT: Laboratory investigations by the authors (Ref.l:
Koroll B.K., Bushe N.A. VNII zheleznodorozhnogo transporta,
Transzhellorizdat, Moscow, 1959 and Ref.2: Koroll B.K.,
Perlin I.L. Byull, TsIIN TsM, 1961, No.3) showed that, in
principle, bimetal strip of alloy 1AAMg-i.5 (TsAM9-1.5) with
armco iron could be produced by rolling: subseouent tests on
bearings of the material were successful. For wider service tests
a batch of the bimetal strip produced under industrial conditions
was needed. Its production served also as a check of the proposed
(Ref.2) rolling conditions consisting, essentially, in the
production of an aluminium-clad billet of TsAM9-1.5 alloy and its
combined rolling with armco iron. The aluminium was of AAl (ADI)
or AO grade and served as the binder. It was clad onto the alloy
by hot rolling (250 to 270'00 on a two-high mill (650 mm dia rolls)
Card 1/5
26798
S/136/61/000/007/0()2/002
Experiments on the industrial Elll/E480
at 1.3 m/sec rolling speed with 22 to 30% reduction per pass.
Rolling vras continued to a clad-billet thickness of 5.5 to 6 mm,
the ingot being 30 and the aluminium 1.3 to 10 inm initially, The
aluminium and TsAM9.-1.5 ingot surfaces were wire-brushed, Only
aluminium blanks thicker than 8.6 mn showed signs of creeping off,
but still to a very small extent, The work confirms results
obtained previously (Ref.2) on thinner ingots. To find the
aluminium thickness giving the best adhesion, 5,5 to 6 mm thick
alloy strips clad with various thicknesses of aluminium were
levelled and cut into 235 to 420 mm sheets- these were annealed
at 2500C and pack cold-rolled with a pickl;d 7.2 x 235 x 500 mm
billet of armco iron, A two-high nill (700 mm roll diameter) was
used with paraffin as the lubricant, The iron and aluminium
surfaces were wire-brushed. Satisfactory adhesion of tha alloy
y 8.6 and
with iron occurred only with aluminium cladding originall,
10 mm thick. Unsatisfactory adhesion was due to high residual
stresses (Ref.3: AynbInder, A.B. 12.d-vo AN Latviyskoy SSR, Riga,
1957) and irregularities of the contacting surfaces, Since
thicknesses of-base and cladding in bimetal strip are required to
Card 2/ 5
26798
S/136/61/000/007/002/002
Experiments on the industrial EIII/E480
very close tolerances, the authors studied factors influencing
distortion of the individual layers. Pack rolling of different
alloy/iron thicknesses and ratios was carried out with pack
thicknesses of 12.9 to 16.86 mm (approximating to industrial
practice). The two-high mill was used, 52 to 54% reduction being
effected per pass. After rolling, the thickness of individual
layers was measured by a published method (RefAs Gostev, B.I.,
Zillberg, Yu.Ya. Aluminium Alloy ACM(ASM) for Heavily Loaded
Bearings, GITI mashinostroitellnoy literatury, Moscow, 1959).
Neither pack thickness nor thickness rations had any effect on
deformation. The final and initial thickness ho and HO of the
pack and tile final and initial thicknesses hF and HF Of tile
iron were found to be relatod by the expression
ho /h F J-CHO/H r)0.81
Recommended rolling conditions for bimetallic strip of 3.6, 4,6
and 6.2 jnm thickness are shown in Table 3. Shear-strength
investigation of bimetal specimens taken after each pass showed
that generally this rises with increasing degree of deformation;
however, heat treatment after reductions of over 50% is essential
Card 3/5
Experiments on the industrial ...
26798
S/136/61/ooo/oo7/002/002
Elll/E48o
for highost strength. Resistance strain gauges were used to
measure rolling pret-sure. Be--aume of the different mechanical
rropertios of the layers, the equation for the average working
stresses Pav for ea-~h deformed layer assumes the form
Ptot
Bav VDA. h
where Pilot is the total roll force in kg; Bav is average strip
width be'ore and after rolling, mmi Ah Is absolute reduction of
one of the layers, mm; D is roll diameter, mm, Calculations
show that with 4.6 and 6.2 mm thick strip, a decrease in average
specific pressure in the first pass is also a factor leading to poor
adhesion, R.A.Peskina and A.S,Gul,rayev participated in the work.
There are 2 figures, 4 tables and 10 Soviet referen:es.
ASSOCIATIONSz Mikhaylovskiy zavod po obrabotke tsvetnykh metallov
(Mikhavlov Non-Ferrous Metals Treatment Works)
A.A.Berez ' Institut tsvetnykh metallov im.
M.1,Kalinina (Non-Ferrous Metals Institute imeni
Card 4/5 M.I.Kalinin) Y.K.Korol.1 and I.L.Perlin
FERLM, I,L*
Indices 'of specialization wO continuity of industriall processes
in the press forging of metals. !zv. vys. ucheb. zav.; tffvet.
met- 4 no.3:148-152 161. ORRA 15:1)
1. Krasrioyarskiy institut tsve-tnykh metallov, kafedra obrabotki
metallov davleniyem.
(Forging)
(Indust:rial organization)
BOCHVAR, A.A.; BELYAYRV, A.I.; PAVLOV, I.M.; PIAKSIN, I.P.; GIIIZHIKOV,
D.M.; PERLIN, I.L.
Iletr Stepanovich Istomin; on his 80th birthday. Izv. vys. iicheb.
zav.; tsvet. met. 4 no.4:161-1.63 161. (MIRA 14:8)
(Istomin, Fetr Stepanovich, 1881-)
PERLIN, I.L.; GLEBOV, Yu.P.
Determining tho ohape (11f cont.a- .1~rfw,-es in pre-s workil- vo, ~
I
plaatic s I ~I' ~r:,,. , :,:;!f . .34 . .]: 7-1--7 i; Ja 61. '.~JRA a".J)
1. 1 .
PERLIN., I.L.
Fressare determination in tube extrusion with use of pointed
stepped-cone mandrels. TSvet.,uet. 34 no.10:77-79 0 161.
(MIRA 14! lu.)
(Metal-working machinery)
PEFILIN _"L. doktor tekhn. nauk, prof., otv. red.; KIIDRYAVTSEVA, L.V.,
ved. red.; SUSHKOVA, L.A., tekhn. red.
[Metalworking ~y pressure; drawing. Termihology) ObvWtka
matallov davleniem; volochenie. TerminologUh. Mbb*&O Izd-
vo Akad. nauk WSR. 1962. 15 P. (Its; SbDraiki rdbraindue-
mykh terminov, no.61) (MIRA 160)
1. ":ademiya nauk S&SR. Komitet nauchno-tekhnicheskoy term,_
nologii.
(Drawing (Metalwork))-Terminology)
HASE I W07, UPLOITATION SOV/ 598.5
Rokotyan, Ye. S., Doctor of Technllctl !;oInnooo, od.
Prokatnoye proizvodntvo; sprevochnfli (Rolling Induntrjr; 11tindbook) V. 1. Moacow,
. Metallurgizdat, 1962. 743 p. Er-mtn clip inserted. 9250 copies printod.
Authors of this volumo: B. S. A!~qronkop CnndidaLe or Tctchninnl Sciences; V. D.
Afaraslyov, CandidnW) of Ttolmicol L;c1rrcof); M. Ya. Brovvin, Enginoor; M. P.
Wmilov, Enrincer; A, B. Vornik, F.-irivenrl K. A. Golubkov, En,lnoar; S. 1.
Gubkin, Acridemician, AcedriV Of SClf,13COS JCJt; A. Yo. Gurovich, F~nginoor; V. 1.
Diivydov, Candidate or Technical Scionocal V. G. Dro%d, Erginnor; N. F.
Yarinolayov, Enpinoorl Yo. A. Zh1jk(~vAcb-.Uopha, Fnpirmer; N. M. Kirilin, Cnndidate
of Technical Solonceal 14. V. Kwynov, En,-,ine(ir; A. It. Koron, Zne~nvor; A. A.
Forolev, FrofoODor; H. Ye. Kugnyonko, EnrIneorl A. V. Laskin, Engfimcr; 0. it.
loev1t&nek1y, Engincisr; V. M. LuC;(wvkoy, Enginanr; 1. H. M,)yorovich, Cnndldn%o of
Technical Sciencos; M. S. Ovchr.rov, SL)j-imor; V. 1. Panternak, Engincor; 1. L.
Perlin, Doctor of Tochnical Sc!.onoon; 1. S. Pubedin, Candidato of Tochnical
3olonass; Ye. S. Rokotyun, DoaWr of Tochnical Scioncos; M. M. Satlyan, Cardi-
date of Technical Saisnonal V. V. 31mirnov, Candidate of Tachnio4l acirincon;
Vo S. Sadmov, Corresponding Hamber, Acadomy of Sciences UMRI 0. P. Sokolovekiy,
Card 1/0
Rolling Industry; Undbook
SUI 598 5
EnCinoor; 0. P. Scolov'yav, Engino)or; M. A. Sidorkovich, En,~Jnaor; Y(q. M.
Trntlyakov, Enginoor; 1. S. Trishovskiy, Candidate of Technical Scluncoa; G. N.
Khenkin, EnGinoor; ani A. 1. TneW;ov, Corresponding 1,nnbor, Academy of Sciences
USSR. Introductiont A. 1. Trellkov, Corrosponding flonbar, Academy of Sciences
USSR; " a ~.~~Iokotyan, Doctor of Technical Sciatires; and L. S. Al'shovskly, Can-
di'date i T'.c6lcal Sciences.
Eds. cf Publishing Housoi V. 14. Gorot,inchonko, R. M. Golubehik, and V. A. Hymov;
Tech. E;d.t L. V. Dobuzhinokaya.
PURPO,,Za ThIs handbook Is Intandol for tacluilenl paroonnal of rotallurgloal and
machin-3-bullding plants, scientific recoul.ii Inotltu0a, and planning and do.-
sitm organizations. It may also be ureful to studws at achoolu of highor
education.
COV91ULEL The fundamentals Of P18Dtic deformation of motels am d1ocuoood aSong
with the theory of rc-Iling and drawing. tl3thoda of doterminine the power con-
ewq)tion and the forced In rolling with plane surface or grooved rolle,ftre
Card ;V*
Rolling lndustr~r; Handbook S)V/ 598 5
1 . Determining the capacity of a-c: motora 131
2. Determining the capacity of d-c, motors on the basis of
measured parameters of a motor 136
3. Determination of the power consumption from the experimental
curves 140
Ch. 7. Methods of Analyzing Power and Force Parameters of Rolling
Mills (I. M. Meyerovich)
1. Dateermi ning the pressure of metea on rolls 148
2. Determination of torque 153
3. Determination of tension 155
4. Determination of electric parameters of rolling-mill motors 155
5. 1--3thodsfc)r calculation of the Eiequencecr reduction 156
Ch. 8. Fundamentals of the Theory of Drawing (S. 1. Gubkin and
1. 'General Fnf7o-rmation on the process and the stress-strain
state of the deformation canter 157
Card 8/19
PERLIN, I.L.
Determining the capacity of a rolling mill drive and metal pressire
when rolling on smooth rolls. Izv. vys. ucheb. zav.; tsvet. net.
5 no.2:124-128 '62. (MIRA. 151-3)
1. Krasnoyarskiy instItut tsvetnykh metallov, kafedra obrabot.ki
metallov davleniyem.
(Rolling mills)
PERLIV, Illya Llvovich
[Theory of the extrusion of metals) Teorlia prestjovaniia
metallov. Moskva, MetallurgLia, 1964. 343 p.
(MIRA 17:12)
ACCESSION ITR: AP4015111 SIO 136/64/000/002/0062/006!)
:AUTHOR: Perlin, I.L.; Glebov, Yu.P.; Yermanok, M.Z,
Effect of temperature, degree and rate of deformation on 'the
deformation strength of aluminum alloys.
SOURCE: Tsvetny,*ye metally*, No.2, 1964, 62-65
TOPIC TAGS: aluminum alloy, D16 aluminum alloy, V95 aluminum alloy,
AD31 aluminum alloy# deformation strangthp:deformation rate, defo:M-
!
:ation temperature, deformation strength temperature funotion
ABSTRACT: The effect of different temperatures (360, 420, 4800) and
various deformation rates (0.19, 0.8, 220 and 880 mm/sec) on the de-
formation strength 8.1 was Investigated for D16, V95t and AD31 allualnum
alloys. 7he deformation rate v affects S
,4 ; and with increased &et-
gree of deformation~p, the IntensIty of the growth of 1% is decreasdd
and In some cases even lowered (for LD31 ~j Is lower at a rate of 14
seo~-l them at 4 see.-' ). The cul-Ves which show the dependence of
Q, on degree of deformation have a maximum, and It Is also showmi, that
ACCESSION HR: AP40151-1
the degree of deformation depends on temperature and rate of deform-
ation. As temperature increases the maximum on the curve is shifted
In the direction of smaller defoniation values; and with Increasing
rate of deformation, It Is shifted in the direction of larger dciform-!.
ation values. Working diagrams (fig. 1 ) of the U = f (t") relationship
were oonatruoted by extrapolation from experimental data for the 3
,temperatures investigated. Curves are also Included for the moi:'11,
probable deformation periods enootmtered In extruding the given &110~s
The lower curves 4w show the Initial values 0orresponding to S'~J~ forl
~tl = 3-6% and minimum. rate of deformation w = 0,03 seo-1 Or1g., art.1
has: 3 figures
ASSOCIATION.- None
SUB CODE: MZ DAME: ACQ: l2Har64 ENCZ: 01
rwo My SMI 009
SUBMITTED: 00 OTHEk: D03
2/f 1,
Card:
"'A CBS 0140 AWA6044/0i*
MN!e
4
latioaft be resistano6l and the 'cIT"'e, slid
Dreo Wnk o -mew 8-~.
f
Wt zo,~ i"bilya rad 96 135-, 141.'_
d" SOURCE.,
__T "TAGS
ceg-.'~ ago
6, z
be"' -a, ungat me
ou" -world-IV: 6
tOi tb
_--on
d:witfi Vie, ol""*
16 bm-`66166 R40A of ibffect
6t 6tr h; value-j4_8 -for relatIV6, stralnj~ up
d~ mwj found oorroctly t,
~he! rate
-6 rljg~,' I (if th6.1jc16vu shows the value of Od -depending onj
Wdd reases, the miximium-S shiftedAmi,
ird
an . gr _d iii
iViddbo. - 1b lbe. pteoe p*ef, the authors d6riv e s r Wing
aj; e-'of Gtrp - i
0
dePam 9,0~(~iire6amiro, reoi at bJ& degre -bf -strain. It wu -ft
hil~de-n,,wg~prooesis:~chiiigd"i along a cr as the degiee of straii Incream Bhow-,
-damped.]Purv
ec"
nt -ROOM
iZW~IA 1'ni4irMa'ODS*gy-oflpformation.Kpplroacl~losa ittainma)dra m
bg that, 0
T*O'
i of strahlt are considered In tbefirst,'at a constailf t8nipel4w X),'thD'
in. the p
N
V
A
uu#jI
sit to ittv MCI
-first
fot t3
oilcofistAl found that
xnalm*
-it
V44 'i
jo.~ &,lbeglod
Ing
ma= traijz,
tlw. I d6gr6es
d6or- 6aw -of rize 0 Sd st
we,
at
J.
VONZ
j*
ME.:
SUB
L
ZNO
mA
00
ollm
-1, Y-.
d
115
4
Jf
Ar
4
)
'0i)r to 6r
0
A(01.
,
r
/01m/u/00/m/0066
,
Vi
OQ,83 x4
jd
_t6arink.-"'
6 f -ire Id ed 1 mA1
!~v i ii
7
s
-A a
_J
-8
eta 83:
If o-A
p4hell
tt' a t-6, delve- ani~' ni 9( c v
0
b"
e
Th
e
t
L
4 i ps~
on
r eces it -o '-esta
r1mum
u t wt h
'apsirt'!_ ucb -strip's4m 14 C: a
ex- ion v a or ve I -or
used- it' beat c angers.~ -
eupross
dth, thickness-and:_91
pal4ing _fIDtCe:p 061i thevi xonge,
trip:,, -them, weld -at ng,th, d it reciprocal'of the ~Deijo
-an th
:with h a
suf Ict*nt -Accu,
61
tk _rdjjt*g_:" _4,~ Ittidd44an, _q _'-~tbel...Cqn
dgii-Uti* we 44d
in OL 02
Izj.-.
zq~
'~W:to4ftibltsb, ha -OfirmisiiblC 1~ill the i
t
i.C C --art XV
go ;:14 f
_1~777
-166
AM JE
OTMMv: ~000
p': F
I- WT ~~, i ~~ '.11 ~1~7 ---
Fz Ji
5;z
L2
IV ON
PLRLDI, I.L..:;- GLF,-,-X)V, Yu.P.; YMMMMA, M.&
ChartLcter of ',,he dependence of the resistance tz~ deformnt-"nn
on the degree of deformation In recrystallization prc)Ce:3-ges
followLng the pressure workInj of' metals. Izv. vys. uchelb. zav. ;
tsvet. me~. 7 no. 4035-141 "64 ("I,:RA 1") ~ I )
L 43713-66 WT lip t
E. MW -C )AIL
ACC NRs -~f600501 SOURCE CODE: UR/olli(-)/6(./c):)o/ool4,'Olil./0116
.Z2rlin.,. I (Professor) ; _qheliunov, V. A.
AUTHOR:
ORG: none
and Durelwuin -yT)e al.lo
_p2Lider loys
TITLE: Nmch toughness of SAP (sintered aluminum
I'
SOURCE: IVUZ. Tsiretnaya Mf!talllurgiya, no. 4, 1966, 1114-116
TOPIC TAGS: 6 Lvd alumi 4U pmiar allok, dispersion strengthened metalp motal
property/SAP aluminum alloy, D-16 aluminum alloy
ABSTRACT: In order to evaluate the behavLor of SAP alloys under conditioni3 of
.plastic working,a new criterion is proposed. The author introducer, "specific notch
toughness" (b ), which is a ratio of notci,,i toughness in mkg/cm2 to tensile st:rength
in kg/mm2. 4e temperature dependence oC bk was &termineA for five alloys:
,g&-_1 J6-9% al4minum oxides, SAP-2 q- 39 aluminum oxide)['SAP-3 (13-17% aluninum
-4 --23% alumin-umoxi&4, aad D-16 (see Fig. 1). A significant increasei
oxide) LqAL -J~7 - lk
of bk begins aPdifferent temperatures, depending on the aluminum oxide content of
alloys. The pattern of the bk-temperat'are curve reflects the actual behavioi: of
the alloy under conditions of plastic defomation and its actual toughne138, For
Card 1/2 1
L
ACC NR, AP6030501
SAP-1//
SII'-2
Fig. 1. Temperature dependence of bk for
44. S AP- SAP and D-16-type allwa.
- /SAFLSj
SILP-af
eel
SAP-1
D- 16
~D- 16..
IN too JM 40
instance, the b of SAP--3 at 500C has a magnitude identical to that of SAP-1 at 250C,
which means that the former alloy requires a higher temperature of plastic deformia-
tion than the latter. Orig. art. has: 3 figures.
SUB CODE: 1l/ SUEM DATI:: 29Mar65/ ORIG REF: 003/ ATD PRESS: 5075
^Lf2 hs
L: vc,
PERLIN, I.L.; MIRPA, I.G.
Metboas of-rating for,-03 neeipd for thi- t~parlng apart; of welded
strip. Mvet.rpt. 38 no.3!:80-83 * 165. (KTRA 18-.6)
, Tj ~F77TF7777777
'Y'
k__IDV
_9
==Off b
A
of,defojm on on be de-'
mil, `i~ Tect of e e e 00-.' alid, dgadol!
17-
I, res-i-StO-e of ~Magnesilmn ealoys!
on
777-
e-
:_A
~d -uiagnesit*~
JIM P_v_---*d6f6xIhitioA~ We e orrA,,Ion- resilftance~i, au4p iomeilii_
t ';k Wormit:'
rue j - Lon
~:b$~f preodurej tensile tes't deld point n
6~6 bf ~,the-i4jor par6etere -quired to deteftine..tbeitliermomet,baideal:
_,6:Cthiv_6~6seeslbf metalworking- a urep at', well as io~~ r:L
4-,-' prope ~q ile 0 1 gm
W, e d' 0a. i"'e8ista-ace to-def
"d f ng~`t 1 e~y e -poitit.). 8 d. 'The: authDru
]A
on
M
*~-re 84 ntal
_e ovilt - ' f OP , experize estigatioin--vf- the of ivig&sij6i~ id3.OYB
Ide'r f~iig-66ire#"oviding --td-the-pr, solng process,':; Thrie vi~~Vb couimC61Y;VSe
heli ~,~nt
4: um- aj~a auoys were o1 ected for- the t1 ent -
Y`a~ftentslym) Alp zhj, ~rangeei fr, ti, 78~'.
C_j Yq.,, Sij.-Bt oa~ 0.01
ed
*.;Ojjvted-tv_tenGi1e estop since t its, -tylie qypos
p" i U66)"'Cirmolves -the a~o'i~ e of- friction:,vhiob:~affiztjs-ria~i,'~d3~,.+tbe:
14
m
, - &~ - t
r 406"
ie Perroi a: at irei' Oxi covx'eg-~
i essi JLThq.,J~eots w4 &~. e etiperata
n .ORGJ!d~ exertei rungin
n nomal prep ing) the: tehille Sti. ' I a
V_
~779-6
*axCo"7-2 at AP.5C 1-17 6
-0
j
"hi
4 U ~' v of _S' ~__Plohed i O~L
% -be#! a of tb
d N
UAJ*~ #0 resefici 'ixed-Idepee--of de"formatfool the v6
-0 a
1.0 6. to-~ e v J~qam
a! Aefdi.
=t n ri Th llix
te-'(f.rM
Mo'A :74d~_ ie-876olnicildeslv~ h -de
grees of lAeftomations: amounting to d M_
!0 an
em - . e!l - . t
9'-t*' _--nittiNi :Ijic ~ea a- Ithe-geom ~17--Of'the sped i meas
, pe3 -makes-i posilbj~e, to. -
erw~h~ _4-16r _bicli6i_ie' ee- ,of: AeroxZ;J_on*. _-_The jreA -for t~'ii bi tt~4t-
'I may
sa'increaseln,t 8 F~ is C eloiat6t-l
-.7
ibt 'of.- -a oind deer 6n Oe. proportion - of - ibeAvM4d_deff*#on'.--. -
naterl, I cor
t6i~,hikci. The ~61rtalnj4 valu6t' Of-- 8 ~b -vaed for dynamic coumlatioj
d lqW_ e
,g kermination of. 8 it i -q;')q')eddLentilto~~Lcbn~~...i.-
lo I acU tate the dd
Abe.,
414- O'Of-D tp $feWt_ liot-dura t donni,
to
,e; A I
T1 sli Of- aourse~ provi ~s :0 tho. vpter 'Upnd Otthe ts
Od ~ fcd~ er 10und of revepce:.-
b 1
TiSorous. th deteiiir, the,
11:10 de'l;-r- a-; gxep a A-_& 6d si 1, Oj6lg
4- istion-his- nati- velop
ea
it
Mt.. `00
VC
K.
0
.ar
PERLIN) i.Id
Fcrm of thr~ of tvnt!t,tit.14. con',oct. at.rr-tinrp Jijr,~nj,
fcrg,'.ng of cylinders L~nd during rol.);np wi" 3.mootn rolls I.
IZV. VYS- "Pheb. -'v.; t!:V-t. mat. P rin.1-245-14" 16c.
1;",g,
1. Moskovskiy vE!chprrjy rif,tal',urp,-,cherk-Ay In3titut, ktAfF-dra
obrabotki metall.ov davlorilyeme
lit.
fi
r.x t
anci
GILIDENGORN, I.I.S.; FEFLIN) I.L., prof., doktor tekhn, nauk, rukuvod~',e.
raboty
Cold extrusion of bimetal pipe. '4"Svet. met. 38 no-5:73 t-~v 165,
( 1~ ipA : E : C,
FE%,ITi " I.L. i KAY,'~M)MV b A. ; KOlfAI-FVA, N,M,
S -I e: ~. lr3n c," r 11'. ing svei-.-- f ~,r zin, , '.S ;I I.. . 11 , - .
i ---,
, , ~,, D I --.z (m ~ )
PERLI N , M.S.; DOZORETS Yu.L.. PCPOVA, L.1,
Had A. na I-! *, 1 1,e L -dj no I 13i '- n I t- t - 9 -a ume n , -j f t i,.;,r a t( X, ~~O:? I s ;
resul ta of a 6- year s!~udy. Med. rad. 8 nc,.9, !~, 20 S 163.
(14IFiA )".0
1. Iz kafed-ry rontgenollarrLl I ruedi~slpsRoy radiologil (zav..-
dotsent 'A.S. Perlin) . go,3pitz--i noy kzav. - di-tsent
Yu.L. Dozcret~'I 7-ebskog-) mE)dit.,q!ngkcg(,
PERUN, M.S.
... I .
---, -1 , ,
Work of the Vitebsk Roentgenological and Radirlogical Society.
Zdrav.Bol. 7 n0-8374 Ag 161. (IffitA. 1~'2)
(VITEWIL-A&DIOLOGY, MEDIGAL)
FM ,ill" , :1 . j . " s k v ~' ~
Solut!on of the I'Irst !'o Axmi-rl- ~,u ~ i ( ' r ~ .-- I,.-- ':)I e m ~ T. t ~. -
theory of i'l-I Wea I by ~111 k~!' '-A Ivid 1.
vpl,v,re. Inzii. zhi~r. ~'~ i~! . ' z, -- 161~ ~' P. ! 7 .'Q '
. lnstitu~' mfspha-''
- Z- - , - ., P i v , - - . .
: V . .- 4 ~ I . ,
-1,.) ~ *. ,~ 1 . : I-; t ! - , , .1 ,, - r". , I .. " , , r , ~ i . '. r . i ; ". , " ., -a '. ,, .e - . . .1
. I ., r -~ ., . I . . .1
" , (,: 'I '7'f! * C, L ! , r~ - . . n.~~ . . Z- jr. " _i !-" . - : " - .-
()(Si~ l-, . -
- I : v -,: . 0 : ., ,
27798
S/1508/60/0213/000/011/,'022
D2151/D305
AUTHOR: Perlin, P.I. ~Moscow)
TITLE: Approx1mate method Of solving the elast:Lc-piasti,'-
problem
PERIODICAL: Akademiya nauk SSSR. Otdeleniye tekhniche8kikh nauk.
Inzhe:nernyy sbornik, v. 28, 1960, 145 - 150
TEXT: A method is proposed for solving the elastic-plastic p1rob-
lem with planar deformation and planar stress. A solution is then
obtained for the case of a plate; weakenA* by a circular hole Vrith
stresses at infinity. The case of completo enclosure of the PIELS-
tic zone of the hole L1 is considered. (See Fig. 1). L 2 is the
boundary of the central part of the zone. A circle L 3 is drawn
with radius through the point a,,~q = /a/, /b,/,- /a/), Kolosov-
Muskhelishvit- functions qp(z) and z) are introduced which'are
analytic in the stresses zone, i.ft the region between L 2 and L 3' if
Card 1/8 dr,
Approximate method of ...
2779n
s/aos'/6o'/02e/ 000, 0 1 1/ 022
D251/1)305
the expansions of (p(z) and V(z) Aave no singular poi-nta, then a
bolution is obtalned for the auxiliary elasilt: robi. m o' a plate
With a hole L 3 with boundary conditions cf(t) 7t !-t~T --- f ( t
Expanding f(t) in a Fourier aeries witha~,,finite number of terms gi--
ves
7-nn 2 k + I 2k+l
f(t) ~ ~ a
L-j 2k4l(~L 2k*-.- P
k=O
[Abstractor's note,~ i not defined]. Determination of .he%W-Oeff.:~--
ciente a and 0 leads simulune-3usly to finding the intermediate
points of the boundary~ A, pencil of straight lines is considere d,
commencing from the center of the circle and maiting angles (W-12,1
(1/m+l) with the ccordinate axes (m ia the nu4b~r of ine lint?),' By
the approximate solutllon of the ela.8tic-plastic problem of order m
is understood the totality of poilats 8, situated on the lineii of
the pencil and the points a and b~ satisfying the condItions ela-
ve
Card 2/6
2779n
S/508/60,1'028,/000/01 11022
Approximate method of ... D251/D305
ted below. It is assumed that the boundary passeF through some -,,o-
tality of points t i" Obtaining the components of stress tor s., ~ij
and the fig a relationship is obtained between the componenti3, hav-
ing 3m + 4 solutions. The 1, will be correctly chosen if the ecila-
tions satisfy conditions ar'laing from 2m + 2 of the unknown coeffi-
cients of the expansion of f,11t) wid the coefficients u 0 and t30 gi-
ven by
X + Y
a.,- I.P.-I .1 !~ 1; X,
4 ` 1 4
Where the boundary d--ffer.9 from a cir-le, the anC. y-[-L,, conTlnua,,~_on
of cP(z) and '0(z) right up to L3 io not. possible. The E-Ilipsea L4
passing through a and b is -onbidered (F,-,g.3).. In thIs case (1) L 2
may lie outside L 4' (2) L 2 may IiE ins.'de L 4' (3) L2 and L4 R,ay
intersecT. In case (1) applicatior of the me-. hod Is possible if in
the analytic continuation of cp(z) and J(Z) ~o L 4 there are no sin-
gular po-4Mts, In case .2') the conformal transforma--on
Card 3/8
Approximate method of
60, 1_1~9 (~'O
D2 D~ ~. 5
M.
A
is used to transforn The Interior of the uni-, cir~.e .n -uhe Tane
onto the interior of L4, Lei L; be -.he greatest contour corrE-Srond-
e f,
ing to a circle in the t-plane deEi~,,_rlbed ins,-de L2,, ThL- app.:cation
of the method is pussic,e if '~Q(zi and 14)(z) have no singuiqr points
inside L21. The conditions for appiying the method .'n case ,3) are
similar to those for (2), The so.L,tion of the problem of a p"Late
with an elliptical hole, may be -carried out as for a -r-;ular hD,.e,
by means of a conformal transformationtij ln Ihe case of large plas-
tic zones, it is not possible -1-o use the elastic soiation 'to sa-
tisfy exactly the boundary conditions on arcs of the#:ircumference.
In such cases (Fig, 4) an eilipBe L4 passing through a and b is
used. The boundary conditions for arcs of the circumference will
be satisfied for certain points. A contour L5 passing through t1l'a
points i, a, b is to beJound LAbs-tractors note-, i not defined),I,
Presumably the points f&,, ; wbleh the boundary ;:onditions hold]. ti
Card 4/8
t1K
27798
S/50 60/028/000/011/022
Approximate method of ... D251YD305
will be found from the condition that the conformal transformation
which maps the inside of the unit circle in the r' -plane onto the
inside of L5 is of the form m, + M2).
Y A(` + '3
The method given ma,Y be extended to the case of non-circular,, 'but
symmetric holes. The best case of satisfaction of control equations
takes place when -the intermediate points lie on an ellipse corres-
ponding to the solution of L.A. Galin (Ref. 3: PMM, v. 10, no. 3.
1946). There are 4 figures and 3 Soviet-bloc references.
SUBMITTEDt January 20, 1959
Card 5/8
lid rly!:-..
r r t, i r f- r I t i c i d, o I L i I -tic
colo! I-,, J!
c - T C-7
FMIN, P.L,kand.fiz.-matem.nauk
Slastoplautic distribution ofstressen miound apertures. Trady
MITI no.5:30-40 160. (MYRA 13:10)
(Illaisticity)
FUMNS P, I,, kand. fl a. -matem.nauk
Properties of Infinite
theory of elasticity o
12'5-133 160.
mys-tems of eqmstlons In probleps on the
doixbly connected bodies. Trudy WTI no.5:
(Blasticitir)
(W.PA 13 - 10)
ACCESSION NR: AP4037101
S/0256/64/004/002/0275/0280
AUTHORt Perlin, P. 1. (1.109cow)
TITLE: Solution of the first Inasic axisymmetric problem in elasticity theory for a
region bounded by an ellipsoid and a sphere
SOURCE: Inzhenerny*y zhurnal, v. 4, no. 2, 1964) 275-280
TOPIC TAGS: axisymmetric problem, elaetticity theory, stretched surface, elestic
equilib:~ium, shift modulus, PoisGon coefficient
ABSTRACTI.- The author solves anlaxiay=etrio problem for a region bounded by an
ellipsoid and a sphere by a method which is a modification of a method given by
in a previous paper for solving the first basic problem in elasticity theory -,,'or a
region bounderl by two surfaces. He effects his solution by deriving an infillite'
Wstem of equations for the unkmown coefficients in his proposed representation.
The system can be solved by successive approximations. He treats the case w1iere
the normal component is equal to I and the tangentW component is equal to 0.
Orig. art. hass 12 fornulas.
ASSOCI4TIONs Institut zekhaniki AN SSSR (Institute of Machmnlas# AN SSSR)
1/2
Cesd
ACCESSION NRt A.P4037101
SUMUTTEDs 20APr63
SIM COMO Ab, V.A
Card- 2/2
IUVE Acql 05JV=4
NO-REP SM 002
EXCLs 00
OruRl 001
FARLB. P. 1. Moskva)
I-- -
Approximate solution of clasoplastle problems. Inzhosbor. 28:145-
150 160. (MIRA 13tlO:I,
(Itinsticity) (Plasticity)
NILQWV9 M.N.; -PERLIN, S.I. --
Nature of changes in the :omposition of organic subBtaazes of peats as
related to the degree of Lheir decomposition and type. Pochvo-redeaie
no,3:77-82 Mr 163. (MIRA 115:3)
1. r,.entr&llnaya torfo-b)lotnaya opytrLaya stantsiya.
(Peat)
GILIKAN, T.F.; PARLIN. S.M.; LNMI:, A.Z.
Ilectro consistometer for determining the lprooessing time, getlatl--
alsation, and hardenizg of resins. Plast.masay no.lls68-71 160#
(HIM 13:12)
(Resins, Synthetic)
MLIN. S.M.; TUROK, N.M.; GRINIAT, V.N.
Processing of poly-vinyl chloride into articles by molding und*r
pressure* Plast.massy no.6:26-30 160. (MIRA 13:11)
(11thylene) (Plastica--Molding)
( PfRIIN, S.M.; SOBOLIT. D.Ya.
Instrument for determining the coefficient of a Up friction.
Zav.lab. 26 no.12:11406-1408 160. (MIRA 13:12)
1. Vossoy=W nauchno-lealedovateliskiy i proyektno-teklinolo-
gichaski:7 Institut UgOVU09D mehlustroyent".
(Teating mchines) Opriation)
S/"-l So/
.) / 0c,
B004,/BOtJO
AUTHORS- Perlin, S. M. , Gil' tan, T. P, ,
WAlfMIWI;.~J0
TI TLE: Stud~' of the of harJk.,r"1,6 A
Polyester Rf'3ins b~ tl~(, Mk~thl(l
PERIODICAL: Pla.stichesk-lye mass,,,, v360, No. 10, pp.
TEXT: The authois studied the ha.rdening degree of KH-1, (Pl-i) r~Zl-~
the U.Se of different initiators and cataly"s. The previojsl~- pr-rf-~rm-j
tests for Rock-well heat, bending :3trength, and water absorption 3h,~s,,J
that no clear kLowledge can be obLained concerning the hardening on -.h.---
basis of physicomechanical tests. An inveStigation was th-~ref-ie -on.1,;-t-
with a Schevenaar differential di--atometer of the firm Am3ler, D~ia-;iti
curves displayed breaks with insufficient hardening of the resin Ih.,-
following optimum values were obtained fo-- the addition 3f
catalyst: 3% cumene hydroperoxide (initia-:or) and 6-8% cclal*
(catalyst . At 1 . '5;~ benzoyl perox! de and 0. 6~o' d3. methyl an., I j ne a cor.q et t-
hardening was attained only af ter repeated heati ng, D1 latam,3 tr 1 c cul
of the following glais reinforced piastic~ were also taker,. 1) 5a~-
Card 1/2
Study of the Gcm:)letci,, -L A' ~-nirq~ ;f 6/111 11 r-C'131-c'I
U113 at ur ate d Po 1~ k-,st,~-r Rt-s . ns I,, *7~ D i I i;. t t r aB 0 0 B C " C
Method
pheno" ' f ormal dehy i,- rf~- si 1 tl~ 7 C
polyei3ter resin with -lu,s, ro(,~-
4) polyester resin with blus8 mat Th~ A'
curves showed tnal in uii specirneiis ~.ardenir,6 inc-cm-~'--'-. TI.
figures, 4 tables, and 6 references: 2 Soviet. US, a;, I
Card 212
2
3 D 2
AUTHO RS %NP E"j and Sobolev, D. Ya.
1.0 z $4
TITLE: Device for Determi~ning, the Coefficient of Slidinj~ FCLCtiOll
PERIODICAL: Zavodskaya laboratoriya, 1960, Vol. ?(,, No. 12,
PP. 1406-1406
TEXT: The device suggested perm:.ts Jetermination of the coeffi~,ieil- of
friction in the wearability teat of plastic and other materials in %ne
case of dry friction, with water, with lubricants, and in the p:7es?,,Ice of
abrasive material. The coefficiert of friction is determined hj iiz; , er t a 1 n -
ing the friction torque produceJ in tile pair of specimens teateJ, ,) 14! of
which rotates with motor drive, v!hereav the other is firmly fusten ~a to tne
axis which is connected with t:,e meEsarir~1-7 part of tile device. 'the divice
consists of three main parts, vi2,, ti,e ~~)e.-Lting, :J.Lusuring, and j it mp i-,,,
devices. By means of this device, the coefficients of' E;liJinF fric u n f
several pairs, were deti.,rminvd. T1.(j !i-ction lounui In th(i lovic4i i oll 1 1*
are determined ny the losses in the bal' bearings luring rotation
indicator and the blocks. Taring of the device is described. Tntere ..re
Card 1/2
i;evice for DeteriLining t:,e Coefficlent of
Sliding Friction B020',B056
1 figure and 1 table.
ASSOCIATION: Vs c s oy-j znyy n au c h. i o -s- s& I o vz., t e i I s,. i"ro
t; J :~ 1! e:i k i y -, n s t i t, j ' Li o In u ~;o ma sh i!i,) S t i-o y e ri iy a
(All-Union L~cienti fic Research, Design, and
Te-,hnological Institute of Coal Machinery)
Card 212
G'UBEIN. Sergey Ivanovich (deceai3edj. Prinimal uchastiye STOROZHBI', )I.T..
M IN, I.Ta., reteenze:at; SMIRNOV, V.S., red.; MLAHOVSKLYA,
.- I.-A.. r4id..izid-va; ISL311TOYETA. P.G.. takhn.red.
[Plastic deforiwtion of wtalej Plaaticheaketa deformateliej
metallov. Moskva. Gos.nauchno-tekhn.izd-vo lit-ry po chernoi
i tovetnol matallurgil. Vol.l. (Physicomachanical principles
of plastic deforwtionJ Fiziko-mokhanicheakie oanovy plai3ti-
chaskoi deformatell. 1960. 376 P. (MIRA 13:2)
(Deformations (Machaiiics)) (Physical metallurgy)
G o s ere
t r
Il not, )I
SO: