SCIENTIFIC ABSTRACT YE.I. FRIDLYAND - I.N. FRIDLYANDER
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CIA-RDP86-00513R000513710020-2
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RIF
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S
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100
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November 2, 2016
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June 13, 2000
Sequence Number:
20
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Publication Date:
December 31, 1967
Content Type:
SCIENTIFIC ABSTRACT
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L 43709-66
ACC NR, AP6023670
that will provide a maximum to the functional
Q~V-M-1-0)112LI I/ (t) dt.
Simulation arrangements are given for the problem of approximating f(t) with systems of
Legendre and Laguerre polynomials. Orig. art. has: 4 figures and 7 formulas.
SUB CODE: 09,12/ SUBM DATE: 120ct65/ ORIG REF: 001
Card
PALTARAK, M.N.; 7RIDLYAND, Ye. I _sanitarnyy vrach
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no.1l.-48-49 N 159. (MIRA 13:2)
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FRIDLYANDER, _]~. N.,, FILLITPOVAS Z. G. I MODMI M. S.
"Dependence of Temperature at Crystallization Threshold on D,.gree of Over-
cooling of the Fusion"
Izv. Sektora, Piz. Khim. Analiza IONKh AN SM, 22, 1953, pp 71-82
The temperature along the moving crystallization threshold in the over-
cooled liquid is studied. Basic measurements are processed in benzophenone.
Experimental results show a sharp temperature jump of the thermocouple junction
at the instant the moving crystallization threshold passes through. The phe-
nomenon is ascribed to the release of latent heat. (RZhFizj No 11,v 1954)
SO: W-31167~ 8 Mar 55
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berorle." -t matated into . tht cr~NIA
it, and crcatLig uew prcipertis irt k. (.-r wwa~(itlil.
G"'Is.
ALITM&N, Morita Borieovich; T-11HE BY, Alaksandr Alakeandrovich; POLYANSKIY,
Aleksey Pavlovich. CHUMmOV, Kstvay Vasiloyevich; XIMyjVj, V.I.,
professor, doktor, retsenzent; XRYMOV, Y.Y., kandidat takhnichaskikh
nauk, ratmenzent; FRIDLYANDIR. I.N., kandidat takhaicheakikh aauk,
retsenzent; TELIS,-K.U. Inkhaner.' iistsenzent-, JMYSIN, B.T., rateen2atnt;
LWEIIKOV, L.P., redaktor; XAMAYEVA,O.X., redaktor izdatel'stva;
ATTOPOVIGH, M.K., takhnichaskiy redaktor
[Halting and casting of light alloys] Plavka i lit's legkikh splavoy.
Moskva, Goa. nauchno-takhn. izd-vo lit-ry po chernoi i tayetnoi
metallurgii. 1956. 491 p. (MIRA 9:10)
(Alloys--metallurgy)
FRIDLYANDER. Iosif Haumovich, kand. tekhn. nauk; KUTAYTSEVA,
YekWt~erinalvanoimia, kand. tekhn.nauk; UDALITSOV, A.N.p
glav. red.; ALITMO, M.B., kand. tekhn. nauk, red.
[High strength V95 aluminum alloy; system aluminum -
magnesium - zinc - copper]Vysokoprochnyi aliuminevyi splav
V95; sistemy aliuminii. - magni - tsink- med'. Moskva, In-t
takhniko-ekon. informatsii, 1956. 61 P. (Informatslia o
nauchno-isoledovatellskikh rabotakh. Tema 6. No.I-56-34)
(mRA 16:3)
(Aluminum-magnesium-zine alloys)
137-1958-3-4917
Translation from: Referativnyy zhurnal, Metallurgiya, 1958, Nr 3, p 66 (USSR)
AUTHOR: Fridlyander, 1. N.
TITLE: Investigation of Light-colored Crystallites in Aluminum Alloy
Ingots Cast by the Method of Continuous Casting (Issledovaniye
svetlykh kristallitov v slitkakh nepreryvnogo litlya iz
alyuminiyevykh splavov)
PERIODICAL: V sb. : Metallurg. osnovy litlya legkikh splavov, Moscow,
Oborongiz, 1957, pp 204-214 (Article originally appeared in Liteynoye
proizvodstvo No. 10, 1956, pp 23-26.]
ABSTRACT: Bibliographic entry. Ref. RzhMet, 1958, Nr 2, 4916.
Card 1/1
&E-n-, IE I
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APOp FWl"Ir4-Ve
V, &KAPAWALi=4
"
D, (14~ 1621~16ZSJ~(In Rus%ianj, Mca-virc.-mm of d!r-
paxanictcr offt":al lallk~a of 6ic A[Afn a!k3~-i a(t~;e 641,~-vnl
typcs of hcat-trcatnwnt rjlrlsvd 01-4t tf,.:fc Aoys-, ~t+vl q~~rAM
from thi: 6q, Mir. cam confaiii in soiid wtln krTi quunl-,L4~
VfMr than Ort-,&xqu:nt
( perinf- (bc cff-~Ci of quux-hine, froxii iilc- I q. ilikfQ danu'.;u~-c,
and aw su-pensituratO wlij wIrl, I'maki &76tl ml Zx,,I-wn 4
lcoocclltlztfol~ C4. Mn c%urelmlick (ILT to the Cquilibiurn JiLlo'cezn.
The lattio: parinicter of r1loyl C9,)fite- UJI (CP J% Sin COT'~'ir-orlll
ckikly to vat=. of FA1kcrJijf-,x-, and li(ifinanp. bw. at highec Nin
JRIPT 16 4021f U0,106�4 ah, rodaktor; CHUKHROV. Katvay Yesillyevich.
rediktor; 7UWiSXAU, H.S., redaktor; ROZHIV. V.P., takhnicheskly
redaktor
[Ketallurgical principles of founding light alloys] Ketallurgi-
cheskie o9novy lit'le legkikh splavoy; abornik statei. Moskva,
Goo. Izd-vo obor. promyshl.. 1957. 442 p. (KIRA 10:7)
(Founding) (Alloys)
137-1958-2-2694
Translation from; Referativnyy zhurnal, Metallurgiya, 1958, Nr 2, p 71 (USSR)
AUTHORS: - Fridlyander, I.N,, Zahkarov, Ye.D., Podsechinov, A-V.,
Klyagina, N.S., Solov'yeva, V.V.
TITLE: Air-cooled and Water-cooled Round Ingots Cast From Alloy V95
(an Aircraft Aluminum Alloy) (Is5ledovaniye kruglykh slitkov
splava V95, otlitykh s okhlazhdeniyem vodoy i vozdukhom)
PERIODICAL: V sb.: Metallurg. osnovy lit'ya legkikh splavov. Moscow,
Oborongiz, 1957, pp 5-46
ABSTRACT: A study was made of the structure and properties of air-
cooled and water-cooled cast round ingots 1370 mm in diameter)
and of sections obtained from them. Water cooling was found to
enhance the quality and evenness of the mechanical properties and
to reduce formation of liquation bands; on the other hand, water
cooling would impair the corrosion resistance of the sections and
intensify the formation of liquation burls on the ingots. Ingots of
alloy V95 should be water-cooled.
G.S.
Card 1/1 1. Alloys--ingots-Properties,--Dete.-,minaticrn
'71
8/564/57/000/000/013/029
D258/D307
AUTHOR: Fridlyander. I. N._.
TITLE: Study of processes occurring during orystalli-
zation Xrom the melt
SOURCE*. Root kristallov; doklady na Pervom ac.veshchanii
po rostu kristallov, 1956 9* Moscow# Izd-vo
AN SSSRI 1957, 178-189
TEXT: The author studied the effects of rapid coolingt such
as is encountered during continuous casting, on Al alloys
and on some transparent organic compounds to find what properties
m-a--y--b-e---e-x-p--e--ote-d---ao---a--re-sult--of--ioontinuous casting f-to - define-- now
Possible methods of casting, and to study the effect of rapid
crystallization on metallic structures. Past cooling-of Al
alioya ioads to finer, more closely spaced dendrites, finer
inclusions of other &ases,.and.hence to improved strength pro-
perties, reaching the strength of forged alloyst and to improved
Cazd 1/2
B/564/57/000/000/fOI3/029
Study of.processes... D258/D307
elongation. The plastic properties are, however, inferior to
ill those of forget. heat-treated alloys. To ensure maximum rate
of cooling and thus the optimum properties, the author recommends
the use of an installation proposed by himself and V. G. Wolovkinl,~-
in which a thin sheet of metal is continuously cast on a moving
water-cooled grid; this sheet may then be rolled without going
through the ingot stage. Al-Mn alloys cast in this way possess
unnsually low electric resistance. For a wide range of super-
cooling, the temperature at the-front of crystallization approacb~
es the freezing point of.the metal' metastable structures and.
new alloy properties may then be, eotedo There are 10figurea.
and 1 table.
Card'2/2
137-1958-3-4918
Translation from: Referativnyy zhurnal, Metallurgiya, 1958, Nr 3, p 66 (USSR)
AUTHORS: T_rid1yande_t,_L_N., Zakharov, Ye. D., Dronova, N. P.,
Solovl yeva, V. V., Petrova, A. A.
TITLE: An Investigation of Light-colored Crystallites in Aluminum Alloys
D16 and V95 (Issledovaniye svetlykh kristallitov v
alyuminiyevykh splavakb D 16 i V 95)
PERIODICAL: V sb. : Metallurg. osnovy lit' ya legkikh splavov. Moscow,
Oborongiz, 1957, pp 215-228
ABSTRACT: The nature of the distribution of light-colored crystallites
(LC), as well as their composition, was studied on ingots and on
pressed components made of alloys D 16 and V 95; their effect
on the mechanical properties of the alloy was investigated, also
methods by which they can be eliminated. In ingots made vf alloys
D 16 and V 95, the LC are embedded in the central zone, whereas
in components manufactured by pressing, their position varies.
LC are seldom encountered in ingots 280 mm in diameter or less.
Ca In the D 16 alloy the LC exhibit a lowered Cu and Mg content.
The Cu content may decrease by 0.1 -.0.96 percent, the Mg con-
Card 1/2 tent by 0. 10 - O.Zl percent. The average values of the Cu and
VY in
perties Of
--------- -
---- ------------
71
T 1-;~ IOa~-Toj 6mv 01-rativoyy Met, llurpiyil' I'l."A
I (USS V
AUTHORS: Zakharov, Ye.D., Drono-a, N. P
solov"YCva,
TITLE- The Meclianism of flie For:-viation of Internietallic Compounda in
Ingots of Alloy V95 (an Aircraft Aluminum Alloy) (19idedovaniye
mekhanizma poyavleniya intermetallidov %, slitkakh iz splava V95)
PERIODICAL: V sb.: Metallurg. osnovy lit'ya legkikh splavov. Moscow,
Oborongiz, 1957, pp 236-285
ABSTRACT: The basic cause of the formation of coarse Cr and Mn inter-
metallic compound inclusions in alloy V95 was found :o be slow
cooling during the crystallization process. ~Vhen a melt was
cooled slowly, the increase in the Cr and Mn concentrations and
especially the addition of small quantities of Ti produced an
enlargement of the intermetallic compound inclusions. Whether
the melt was cooled rapidly or slowly, the formation o-~' inter-
metallic compound inclusions was not affected by the composition
of the original alloying element, by raising the temperature of
the heat from 730 to 7800 , or by increasing the exposure time of
Card 1 1 the molten metal at these temperatures from I to 5 hours. G.S.
1. Alloys ingoU--Applications 2. Compoiwds-Formation
137-58-2-2901
Y A 4 o I'
Translation from: Referativnyy zhurnal, Metalturgiya, 1958, Nr 2, p 99 (USSR)
AUTHOR: Fridlyander, I.N.
TITLE: A Study of the Nature of Oxide-scab-type Inclusions in Aluminum-
alloy Forgings (Issledovaniye prirody vklyucheniy tipa okisnykh
plen v shtampovkakh alyurniniyevykh .9plavov)
PERIODICAL: V sb.: Metallurg. osnovy litya legkikh splavov. Moscow,
Oborongiz, 1957, pp 286-288
ABSTRACT- Bibliographic entry. See RzhMet, 1957, Nr 1, Abstract 144"'.
1. Iluminum alloy forgings--~,-Ippurities
Card 1/1
7- V - I
d P,
13 7- 58 - 2 - 29 02
Translation from: Referativnyy zhurnal, Metallurgiya, 1958, Nr 2, p 99 (USSR)
AUTHORS: F Zakharov, V - Z., Kashcheyev, M.G.
TITLE: A Study of Oxide Scab in Aluminum- alloy Forgings (Izucheniye
okisnykh plen v shtampovkakh iz alyuminiyevykh splavov)
PERIODICAL: V sb.: Metallurg. osnovy lit'ya legkikh splavov. Moscow,
Oborongiz, 1957, pp 298-305
ABSTRACT: A study was made of the causes of oxide-scab formation in
aluminum-alloy forgings and of the relationship to scab formation
of such factors as, a) the duration of the pouring operation,
b) standing time in the holding furnace (mixer), c) forced mixing,
d) the composition of the charge, e) filtration of the metal, and
f) deformations. Data are given on oxide-scab distribution in
individual forgings. It w;ks demonstrated that the oxide scab is a
result of a reaction of oxide casting scab with the metal in the
process of being deformed. Some of it was related to the purity
of the molten metal in the smelting furnace and to the rate at
which scabs detached themselves from the stream surface while
the metal was being poured. Filtration of the niolten metal did
Card 1/2 not yield satisfactory results. The more oxide scabs there were
137-58-2-2902
A Study of Oxide Scab in Aluminum-alloy Forgings
in the ingots and the greater was the degree of deformation,
the size and number of scabs encountered in press-forgings
1. Aluminum alloy forgings-Impurities
the greater were
and drop-forgings.
P.V'
Card 2/2
1'17-58-4-6870
Translation froryl Referativnyy zhurnal, Metallurgiya 058 Nr 4. p 79 'USSR)
AUTHORS Kandrat'yev. N B , Fr,dly,snder I N
TITLE: An Investigation of the Decornposit:on of a Sold Solution of At-
Cu-Mg-Mn Alloys Crystallizing at Various Rate W Cooling
(Issledovaniye raspada tverdogo rastvora splavo-.- sistemy At-
Cu-Mg-Mn, krist.allizovavshikhsya s raznymi skorostyarni okh-
lazhdeniya)
PERIODICAL: V sb. Metallurg. omovy lit'ya splavov. Moscovv. OborongiL
1957, pp 380-393
ABSTRACT: The effect of changes in the rates, of crystdlh.,.at~on of Al-Cu-
Mg-Mn alloys having various amounts of Cu, Mg, and Mn upon
the properties of alloys at room and elevated temperatures is
investigated. An increase in the rate of cry5taliization of the &.I-
toys results in an increase in strength both at room and at, ele-
vated (1500C) temperature. The increase in the itrength of al-
loys crystallizing at high speeds is due primarily ~o the differ-
ence in the properties of the solid solution and the narure of it.~
breakdown. The difference in microhardness ait.ins a max~murn
Card 1/2 at 0.61/6 Mn content and declines when an alloy contain5 0.2 and
137-58-4-6870
An Investigation of the Decomposition (cont.
1.2% Mn. Variation in Mn content has its maximum effect in increasing the
difference in strength values relative to rate of crystallization in alloys ot.
the D16 type (with Mg), in which it attains 5-6 kg/Imi-n2- and to a les-er de-
gree in alloys of the VD17 type (with Ntg) and has pracTically no effect oil
alloys of the D20 type (without, Mg). To as-;tire maximum hi8h-temperf-iture
corrosion resistance in the alloys it is necessary that ingots be crystallized
at maximum speed. This is particularly important (or ailoys of the tvpe of
D16.
1. Alloys--Crystallization 2, Alloys--,ooling Tethods 3, Al-_Mln'~Tl. N.
--Applications 4. Copper--Applications 5. Magres4uff--App_'1c_!:f_".onF,
6, Manganese--Applications
Ca rd 2/2
y)q
137-58-1-1841
Translation from: Referativnyy zhurnal, Metallurgiya, 1958, Nr 1, p 250 (USSR)
AUTHORS: Fridlyander, I.N., Khol'nova, V.I.
TITLE: A Method of Obtaining Special Electrical Properties in Alurninum
Alloys by a Continuous Casting of Thin Sheet Blanks (Metod
polucheniya osobykh elektricheskikh svoystv alyurniniyevykh
splavov putem nepreryvnoy otlivki tonkoy listovoy zagotovki)
PERIODICAL; V sb.: Metallurg. osnovy lit'ya legkikh splavov. Moscow,
Oborongiz, 1957, 394-399
ABSTRACT: An installation has been developed for continuous production
of 6-12 mm strip from an alloy of Al containing 3-3.5 Mn. The
metal is extruded through a narrow aperture in the furnace onto
a moving screen cooled by water from beneath. Quenching from
the liquid state occurs, as a result of which a solid solution of
Mn and Al, oversaturated from the liquid phase, is formed. The
casting temperature varies within the 800_8400 interval, and
undesirable primary inclusions of intermetallic compounds appear
when the temperature is lowered. Subsequent cold rolling to a
thickness of 0, 5 mm did not cause decomposition of the solid
Card 112 solution. The resultant sheet had a C-7b of 33-37 kg/mm and
13 7- 58 - I - 184 1
A Method of Obtaining Special Electrical Properties in Aluminum Alloys (cont
8 = 2-3 percent. Measurement of the electrical properties showed that in
0-2000 interval, the temperature depe,,ndence of resistivity (X is low and
virtually invariable(=:,; Q.1"xIP -3,ohm/i C), and the resistivity is 0.110 ohm/ mm2/m.
Heating to 3001 and fiigher results in a reduction in resistivity and an increase
in its temperature dependence.
P. N.
0-1sys-Electrical propertiee-11rocesses
Card 2/2
137-1958-2-2684
'4
j
Translati6n from: Rt!ferativnyy zhurnal, Metallurgiya, 1958, Nr 2, p 69 (USSR)
AUTHORS: Fridlyander.I.N., Kondrat'yeva,N.B.
TITLE: The Structure and Properties of a Light-gage Sheet Bar of Alloy
D 1 (an Aircraft Duralumin) (Issledovaniye struktury i svoystv
tonkoy listovoy zagotovki iz splava DI)
PERIODICAL: V sb.: Metallurg. osnovy litya legkikh splavov. Moscow,
OboTongiz, 1957, pp 400-413
ABSTRACT-. A study was made of the structure and properties of a cast
billet and rolled sheets of the Al alloy D 1 (an aircraft Duralumin).
It was found that when the Fridlyander-Golovkin method was used
to cast a light-gage sheet bar, the strip was found to contain lower
zones of equilibrium crystals and upper zones of fibrous crystals
which attained a length of several meters. The appearance of the
latter was caused by superheating the melt till the moment that
crystallization began, followed by a rapid and rigidly controlled
elimination of the heat. The elongation undergone by the fibrous
crystals along the length of the fibers was extremely great, exceed-
ing by 2-4 times the elongation undergone by the transverse speci-
Card 1/2 mens and by the specimens cut from the region of equiaxial
137-1958-2-2684
The Structure and Properties of a Light-gage Sheet Bar of Alloy D 1
crystals. After thermal treatment the cast strip possessed great
strength in all regions and all directi pns. Consequently, more
propitious distribution and greater dispersion of the ingredients
are required to obtain great elongations than are needed for great
strength.
G.S.
1. Aluminum castings-.Droperties 2. Aluminum castings-Structural
analysis
Card 2/2
137-58-6-12784
Translation from: Referativnyy zhurnal, Metallurgiya. 1958, Nr 6, p 227 (USSR)
AUTHORS: Kondrat'yeva, N.B., Fridlyander
TITLE: Investigation of the ossibility of Producing Finer Grain in Wire
Made from Billets of the Cast Alloys D18, D7P, and V65
(Issledovaniye vozmozhnosti izi-nel'clioniya zeren ,, provoloke.
polucliennoy iz litoy zagotovki splavov D18, DZP i VS5)
PERIODICAL: V -qb.: Metallurg. ostiovy litlya leglukh .'-plavov. Moscow,
Oborongiz, 1957, pp 414-428
ABSTRACT- It is established, that the cause of many rejects by reason
of cracks and lumpy surface of the locking heads of xivets is
tile coar5e-grain structure in the finished wire. The possibil-
ity of producing rivet wire with fine-grain structure from cast
alloy ingots D18, DZP, and V65 has been studied-, the! effect of
the temperature of tile melt in the furnace upon tile structure
of the cast ingot and the effect of the temperature of inturmed-
iate annealings upon the structure and properties of the fin-
ished wire were examined. It lias been established that for tile
forniation of uniform fine-grain structure- in the finished wire,
Card 1/2 it is necessary to combine the lowest possible temperatures of
137-58-6-12784
Investigation of the Possibility (cont.,
casting the ingots with suffi( iently high temperatures of interi-riediate anneal-
ings. A casting temperature of 7050C and annealing temperatures of 410-
4300 are termed optimal for the abovementioned alloys. The work performed
establishes the possibility of producing high-quality riveting wire up to 5 mm
diam from ingots of the (ast alloys D18, DZP, and V65.
N.P.
1. 'd ire- -Prod licti on Wire--flechanical properties 3. Metalj--Oa3ting
4- Grains (Metallurgy)--Metaillargicai effects 5. Rivets--Effectiveness
Card 2/2
fx
137-58-3-6054
Translation from: ',Referativnyy zhurnal, Metallurgiya, 1958, Nr 3, p 231 (USSR)
AUTHORS: Drits, M. Ye. .,Fridlyander,
TITLE: All-Union Conference on Light Alloys (Vsesoyuznaya
konferentsiya po legkim splavam)
PERIODICAL: Tr. In-ta metallurgii. AN SSSR, 1957, Nr 2, pp 224-229
ABSTRACT- Called by the Institute of Metallurgy of the Acad. of Sciences
the MAP of the USSR, the 1955 all-union conference on light
alloys summarized the results of the work of the industry and of
the scientific research institutes with regard to the produ(-tion,
processing, and e.mployment oi light alloys in the national
economy. The following topics were discussed at the conference:
1) the study of the requirements relative to light alloys and
products made thereof as dictated by modern engineering
processes; 2) exploration of novel alloys and perfection of heat
treatment procedures; 3) the present state and prospects for the
future development of blank and profiled casting; 4) present state
and prospects for the future development of press working of
light alloys. A brief survey of major reports presented at the
Card 1/1 conference is given.
E. K.
AUR E4Zder, Edellman, N.M.$ Danilov, Yu.S., 20-2-25/-62
TITLE: An Investigation of the Static Endurance of the Allcys Al-Zn,kl-Mg,
and Al-Cu. (Isaledovaniye staticheskoy vynoslivosti splavov AI-Zn,
Al-Mg, i Al-Cu.)
PERIODICAM' Doklady Akad.Nauk SSSR, 1957, Vol. 115, Nr 2, pp. 287-289 (USSR)
ABSTRACTt Static (slow) repeated stresses lead in a small numbw of cycles to
the rupture as variable stresses which oscillate with great fre-
quency. In the tests made by the authors the frequency of the stres-
ses amounted to 6 to 6 cycles per minute. Three diagrams illustrate
the variation of the mechanical characteristics and of the static
endurance (number N ) of the alloys Al-Zn, Al-Mg and Al-Cu. The te-
sting was carried out in the following manners In the first stage
2ooo stresses were taken at the upper tension of 00 OH( OH signi-
B
fies here the solidity of the indented sample), then looo gycles
at do . O'B 6H and finally the testing was continued at 6 a o,96H
until the rupfure. The number N corresponds to the numberoof cyckla
at a - 0,9 dH. The lower stress amounted in all cases to o,oT a..
0 B
The nubiber N very rapidly increases when the concentration of the ad-
mixture is increased and then again strongly decreases. Above a cer-
tain concetAration a solid solution must more easily decompose than
a less concentrated solution. Less concentrated solutions (11 + 2%
Card 1/2 Cu) solidity.~ under the influence of elevated temper4ture. The more
F-4 ~r p
F RIDLYL,DER f I.!~. , Doc Toch Y.Aof." hich-
dur.,,.bili-ty aluminum, alloy:; of
coppor." 195"'. Li PI) of
of 1:on-Forrous T.'otals ---id Gold im 7,~. 1. Yaliv.in) . LLrt of aut*.ior's
13-14 (2,1 titl,~--) (17.112-5,1 10-1)
SOV/ 137-58-10-21657
Translation from: Referativnyy zhurnal, Metallurpiya, 1958, Nr 10, p 172 (USSR)
AUTHOR: Fridlyander, I.N.
TITLE- An Investigation of High-5trength Deformable Aluminum Alloys
of the Al-Zn-Mg-Cu System (Izyskaniye vysokoprochnykh
deformiruyemykh alyuminiyevykii splavov sistemy
Al-Zn-Mg-Cu)
PERIODICAL: V sb.: Legkiye splavy. Nr 1. Moscow, 1958, pp 49-85
ABSTRACT- A systernatic investigation of binary, ternary, and quater-
nary alloys (A) of the AI-Zn-Mg-Cu system was carried out in
order to determine the role of individual alloying elements in
the process of hardening of A's. The effect of Mn, Cr, Fe,
Si, and Ni on properties and kinetics of aging of A's of this
system was also studied. Processes of aging in A's of the
Al-Zn-Mg-Cu system were investigated, and hardening effects
achieved by various heat-treatment procedures were deter-
mined. The strongest A's of this system contain 9-11% Zn,
3-41o Mg, and 0.5-1.57o Cu. Lrb values of up to 75-80 kg/mmz
are achieved in extrucled components made of A's containing
Card 1/2 Mn and Cr. The compositions of industrial A's were selected
SOV/ 137-58-10- 21657
An Investigation of High-strength Deformable Aluminum Alloys (cont.)
on the basis of comprehensive tests on the mechanical properties, static
endurance, corrosion resistance, and other (.haracteristl(s of the A's. An
experimental riveting A, V94, contains 6.0- 6.7% Zn, 1.2- 1.6% Mg, 1.8-2.4%
Cu; Cr and Mn contents may not exceed 0.05 and 0. 1T4, respe( tively, and Fe
and Si may not be present in concentrations greater than 0.1514. Natural
aging of the Ats V94 and V95 proceeds very slowly, thus, even after a per-
iod of three months these A's do not attain their niaxiniuni strength. Arti-
ficial aging of these A's may be accomplished )n st!veral stages. In the case
of plated sheets of the V95 A; the regimen of aging consists of 24 hours of
soakin at a temperature of 1200C, a 16-hour soak period at a temperature
of 140sis employed in the case of non-plated components. The most exped-
ient method, from the practical point of view. is the process of aging in
stages consisting of a 3-hour soaking period at 1200, followed by three
hours at 1600. The method of step-wise aging, involving 3 hours at 1000 and
3 hours at 1600, is employed in the case of the riveting V94 A. Bibliography:
36 references.
E. K.
1. Al-urrinum-coppei,-niagne..~iurr,..zJ.nc
Card 2/2
6 6 r.-Ig
0 V/13-1-59-q-158i7
Translation from: Referativnyy zhurnal,.Metallurgiya, 1959, Nr 7,, p 230 (USSR)
AUTHOR:'-. Fridlyander, I.N.
TITLE: Investigation Into the Effect of SolidJfication Rate on the Structure
and Properties of Aluminum Alloys
PERIODICAL: V sb.: Zatverdevaniye metallov, Moscow, Mashgiz, 1958, pp 275 - 298
ABSTRACT: Investigations were carried out into the effect of crystallization rate
and overheating on the properties and structure of Al-alloys in continuous
ingot casting. It was proved that high chilling rates in crystallization
(70 degrees per second) Increased mechanical properties of Al-alloys in '
cast condition. A technological process is suggested permitting to obtain
a sheet Bemi-product.without passing through the ingot stage. The
crystallization process was observed on a transparent organic camphene
substance with the use of cinematographic means. The effect of the rate
of crystal growth on the mechanical properties and on the dimensions and
distribution of impurities is shown. The strength of cast Al-alloys in-
creases and attains in heat-treated condition the strength of deformed
CatN1 1/2.. Al-alloys; however, remains low. Maximum Increase of mechanical
q'I"-
665'19
SOV/137-59-7-15817
InvestigationInto the Effect of.Solidification Rate on the "structure and Properties
of Aluminum Alloys
properties is obtained by casting a thin liquid metal layer onto a moving water-washed
screen. A great.dropping of.true temperatures in the-crystallization area-causes-the
origination of a metastable oversaturated solid solution, yielding new properties. Ex-
ceptionally low temperature factors of electrical resistance for AI-Mn alloy can be
obtained by continuous casting-of-thin Al alloy sheets. 24 bibliographic titles.
G.E. tr
Card 2/2
SOV/1 37- 59- 3-6901
Translation from: Referativnyy zhurnal. Metallurgiya, 1959, Nr 3, p Z83 (USSR)
AUTHOR., Fridlyander, 1. N.
r__
TITLE: An Investigation of Oxide-film Inclusions in Stamp-.ngs of Aluminum
Alloys (Issledovaniye vkIyucheniy tipa ok-isnykh pl-an v slitainpovkakli
iz alyuminiyevykh splavov)
PERIODICAL: V sb.: Gidrodinarnika rasplavl. metallov. Moscow, AN SSSR,
1958, pp Z09-236
ABSTRACT: The following was established as a result of the investigation: 1) The
occurrence of oxide films (OF) in Al-alloy ingots s primarily attrib-
utable to the entrapment of OF's from the surface of the stream of
the liquid metal as it is poured from the furnace into the ladle, from
the ladle into the mixer, and, particularly, from the mixer into the
crystallizing basin of the continuous casting machine; 2) the number
and over-all area of the OF's found in fractures which are parallel
to the plane in which the dies converge increase extremely rapidly
as the degree of deformation of metal is increased; 3) in the process
of plastic deformation, the OF's are straightened and then ruptured,
Card 1/2 and the volume of metal which they affect is appreciably increased;
SOVA 37- 59-3-6901
An Investigation of Oxide-film Inclusions in Stampings of Aluminum AlloyE-
under condit,ons of severe deformation, nonuniform flow of metal throualu- it the
cross section of the article, and considerable normal pressure on the flowing
layers of the metal, considerable friction occurs between the metal and the
solid, brittle particles of the OFs; this leads to a pronounced local hardening
and heating of the metal, and results in the appearance of local laminations and
discontinuities; 4) the purity of metal is greatly enhanced if during pouring (from
the furnace into the ladle, from the ladle into the mixer, and from the mixer into
the crystallizing basin of the continuous casting machine) the liq-,Iid metal is com-
pletely encloscd in runner arid fountain tubes-, 5) after the selec-~ion of appropriate
ceramic materials, the same system of enclosed [ducted I pouring of metal may be
expediently employed in casting of ingots and shaped articles made not only of Al
alloys but of Mg, Cu, and other alloys as well.
Ye L~
Card 2/2
SOV/137-58-11 22Z57
Translation from: Referativnyy zhurnal. Metalturgiya, 1958, Nr 11, p 59 (USSR)
AUTHOR: Fridlyander, I. N.
TITLE: Special Features of Continuous Casting of Ingots of V95 Alloy
(Osobennosti nepreryvnogo lit' ya slitkov iz splava V95)
PERIODICAL: V sb.: Legkiye splavy. Nr 1. Moscow, 1958, pp 311-327
ABSTRACT: When 370-mm ingots (1) of V95 alloy are continuously cast with
air cooling, smaller liquation ("bleeding") beads aFpear on the surface
than when water cooling is used. The high rate oi liquatior. bleeding
with water cooling is due to the more significant rise in temperature
during the secondary heating of the peripheral layers of the 1,
Heating under these conditions results in fusion of the low -melting
eutectics and their expulsion to the surface due to increase in the
volume of the alloy as it enters the molten state. The mechanical
properties of the Me in I cast with water cooling are virtually iden-
tical across the entire section. The peripheral layers of an air-
cooled I have mechanical properties similar to those of I cast with
water cooling, but as one moves toward the center of the I the
Card 112 ultimate strength and ductility diminish both in the cast and in the
Special Features of Continuous Casting of Ingots of V95 Alloy
Solt/137- 58- 11-22257
heat-treated condition. Water cooling also results in higher mechanical properties
of rolled Me. At the center of an I of V95 alloy, one frequently finds structural
inhomogeneity in the form of bright crystdIlites containing 0.07-0.14910 less Cu.
0.120/o less Mg, and 0.09-0.417o less Zn. Internietallic inclusions are algo
observed in the central zone and the head portion. The composition of these
inclusions apparently corresponds to the formulds A17Cr and A161,1n. When bright
crystallites and intermetallic compounds are present, the mechanical properties
bf the alloy are impaired.. The appearance thereof is due to the chilled residue
forming beneath the bottom of the tundish, which distributes it into the molten
portion of the metal in the mold, For eliminat;on of these defects it is recom-
mended that formation of chilled residue be pre-'ented (by increasing the heating
of the tundish and increasing the distance between its botiorn and!that ~of the funnel of
molten metal), that the Cr contents of the alloy be limited (-o the 0, 10 - 0, 170/o
range), and that Mn be held to 0.25-0,il"O/O),
G. N.
Card 2/2
DRITS, M.Ye.; FRIDLYANIMR, I-.I.; SOFIANO. U.K., red.; SIVKOVA, N.M.,
tekhn.ied.-
(Aluminum-base alloys; their applications and prospects of use
in the economy] Splavy no oanove aliuminiia; primenenie i
perspektivy lspolizovaniia ikh v narodnom khozisietve. XoBkva,
Voes.i4n-t usuchn.1 takhn.informataii. 1959. 57 P. (MIRA 13:6)
(A311-in"M alloys)
FRIILTANM, Iosif Naumovich, doktor tekhn.nauk; DOBATKIN, V.I., doktor
- ZIWVA, T.K., kand.tokhn.nauk. red.;
SUVOROVA, I.A., izdat.red.; ORNSMINA, T.I., takhn.red.
[High-strength deformable aluminum alloys] Tysokoprochnys deformi-
ruemye aliuminievye splavy. Koskva, Gos.nauchno-tekhn.iod-vo.
196o. 290 1). 1 (MIRA 13:5)
(Aluminum alloys) -
19,61A
82622
S/180/60/000/004/017/027
E193/9483
AUTHORSs Archakova, Z.N., Romanova, O.A. and
Fridlyander, I.N. (Moscow)
TITLE: Inv i ktion of the Properties of Alloys of the
_Y A -5tsk-i*A
A Nn System at Room and Elevated Temperatures
PERIODICALs Izvestiya Akademii nauk SSSR, Otdeleniye tekhnicheskikh
nauk, Metallurgiya i toplivo, 196o, No.4, pp.106-110
TEXTs The alloys studied in the course of the investigation
described in the present paper contained 0 to 3% Li and 4.0 to
6-5% Cu, the content of other alloying additions being constant Ll~
and amounting to 0.1% Cd, 0.6% Mn and no more than 0.3% each of
Fe and Si. The mechanical properties of the alloys were
determined after 4 types of thermal treatmenti (1) solution
treatment, i.e. quenching from 525 to 5350c; (2) annealing,
i.e. cooling from 430 to 1500C in 7 days; (3) ageing at room
temperature for 7 days; (4) ageing at temperatures between 150
and 2000C for 12 h at 200*C and 16 h at other temperatures.
The mechanical tests were carried out both at room and elevated
(200 to 2500C) temperatures on specimens machined from extruded
rod and appropriately heat-treated. It was found that
Card 1/3
82622
s/i8o/6o/ooo/oo4/017/027
E193/E463
Investigation of the Properties of Alloys of the Al-Cu-Li-Cd-Mn
System at Room and Elevated Temperatures
simultaneous introduction of 0.9 to 1.4% Li and 0.1% Cd greatly
increased the strength of the Al-Cu-Mn alloys in the age-hardened
condition and, on the basis of the results obtained, the composition
of a new, high strength rod alloy, suitable for high temperature
service, was determined. The nominal composition of the new alloy
VAD23 iss 5.4% Cu, 1.25% Li, o.6% Mn, 0.15% Cd, remainder Alt
its U.T.S. and 0.2% proof stress at 200C are 6o aFn-d 54 kg/mm2
respectively. Regarding its room-temperature strength, the new
alloy resembles the high strength, Al-Zn-Mg-Cu alloys (tYPe V95);
its mechanical properties at high temperatures (150 to 250'C) are
better than those of any known Al-base alloy of this type and,
what is particularly important, the alloy retains its strength
after long periods at these temperatures. Thus, the U.T.S.
and elongation 6 of the VAD23 alloyt held at 2000 C for 0.5 h,
were 46.9 kg/MM2.and 6.3% respectively, the corresponding figures
for the V95 alloy being 40 kg/mm2 and 12.6%. After 100 h at the
temperature, U.T.S. and 6 of the VAD23 alloy were still
Card 9/3
82622
s/i8o/6o/ooo/oO4/0l7/027
E193/E483
Investigation of the Properties of Alloys of the Al-CU-Li-Cd-Mn
System at Room and Elevated Temperatures
42 4 kg/mm2 and 6.3%, whereas U.T.S. of the V95 alloy fell to
19:3 kg/mm2, its 6 increasing to 19.8%. The corrosion
resistance of the new alloy is not impaired by its lidium content;
its specific gravity (2.73 g/cm3) is slightly lower and its
molecules of elasticity slightly higher than those of the standard
aluminium alloys D16 and V95. There are 5 figures, 2 tables and
10 referencest 2 Soviet, 5 English and 3 German.
SUBMITTED: March 17, 196o
Card 3/3
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us to
act-: oil is 2
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---- 0 ?". C. OYS, ::-.c C.
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u U., t r C L. t* ':.0 11 t t. rf
---o-,,crties as a fur-c'ion of
99. 993 ~, T)uj - Gz ere
9". M 2.7, 3.5 ann,
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aLlOyS cOllu -3
---r Ge s - ere fo r 12
- rrot i! -- hcmou-e- L ed at
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2
LjOOC into 10 rL,:l diameter rods Cs
:)ressed at
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ca- ~ I/ .,
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fS Con.~_jn4 s
-_-;_vely viore s'.-lo,.*;,-. by z~ilo.,, -n[: 2-7
f n r-: I
i3ol,,ition :bone. to
S16~916 1
O'L aluminw~ by -.~,qGe
U L>
elon,-~.tic.- and m.~Stinc, e c---C.
./cen the
t ic ii-.itod solubility of !:,,,Ge in A-'
t
oeric,-, of t.,,e col.1pounds, "~-231 2, 11b
w~-1-ic"a tI.L, solubility decreases )ractically to 2:(~rc
to 7:,- Pb. T11cre are 5 fiLu2cs and 10 references: '.7c)vJe--b-,oc ~--(I(
kJ 4 ~~2 L - - I - - " ~)
-non-Sovie~.-bloc . The reference to the -~,ubli
:--eads as follows: L.P. 11.:ondolfo, 1:etallo6raphy of .2-.1um-inuL: -Llloys,
'T
York, 1943.
,Cord 3/3
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thc
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If" t S U_ -L
n0l. n U ,, very L'- - 0
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'In -01~C-2. :" r 0 T., U
0-
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.-L-rdneso 1,-4- - -, - c r., cojs-ucted-
5000C has b e
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ty
i3ases tlie so "er
c
- from 0.75 to 1 -5 'I'U - -t I ~nc--e'as 'S
at LJ co--~ents :) k' y 0-- CU.
ti-le 6 Q ~ i:. b i I t
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b r e S o 5 Cu 1.5
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t-E.3- of a, 1( 0
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t e r t a-, -. i c C)-- as e s a"T U--
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does -rot e--,:ceed 0.2 ~j. it :ias r.,o-;j -.o
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b s JL e tr lt e r i mu T
ved by hcat-trca u
e cor ---,-.bly ini,)ro
.aneous solubi-Lity of Cu --nd L-.; in Al corres,3on-;s '.c~ tl--e
11c (-~Vc
Simull.a-neous sciubi.Lity Of copped:, D205 J05
o f o -I i d s o 1 ui ,, n s vi i t h t'l cP, phusc. It
, i , 1
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tul-~cd- cou~-'l-i to ~,Oose.,3s
-,-,Qctz
a- c e L~ , te Lac o
fi non-Sovie-c-b o z,
a-,id c c
,in,:uae ca-J om -
I s t- t i 1 Ici60v P. 557; co:*,~;"
111 ~'-,ic)ysj X,--.-I York-Tol-onto-London, 1,058, P3 T:V
2'ilkok, Journ. In-r--t. Let. , July 1956, ). 125.
Card 3/3
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c .~,c D
b in
ty
of strc.-,.l.E;-ch cu---ves with thc- cl z:_1 C Q f t 1--,a I'l iC -1. n.,
1"ore cuenchinL;. T, -- c i v e s t 16- o n s e o a o -2 L: e d o n -c I e E; 2 D"',
, D--.-e.7,sed at
a
" " oy -)80 4000C vjitll
170. Tll~-e lleat4nn- timic before i,
-,U-a,-,l UY I UA 0 1
Qs is caused lby t .,,-i o p r o c es z; c s tu en 'U, -1 c n i ---u c.
U-on ol' zhe solid golution by nimc, Cn;
Card 1/2
S
De-uermin-ill-I.s- tine be-'o---e . . . D2
e -o'a -r L t i c) n o I :r f o' 1"',1d s o 1 u t i o ni t
ti~.,.c. nceded -~o obt~.-.,*.-
le accreas c c u Q -n crn -u ec r
e 0
Coefficient T'he correlat-Lon --'c cally
i c t e dy
0
u
10 C)*,
vi r e I; s t h e o o c i m e t C. r s0L~ r 0C. c
On. e basis of -~'onniula a c-I
n LL t
... u
-,--c'ers vms corstruc+ed. There az-e 3 fiCurcs-
C,--.i,d 2/2
/(;l2/0*l':-
6-
IX
1) 2 0 51
n,
Tul
'alat -3. D -
~W.
Of I, 'V I r,
u
I T L" ho,~ ulle
~- les cjj,~ ods
j_.L .. r
C-1 T if. T. Doboat in, and
lu V~'/
:)of or; I?uy "ilyll;"iniY("VyYL'
j.oc'cQ%'Iq 1961 95 103
"D
-1 n 4~
C'-~use Of
t c'
Of
jrLL-ion 150 b, Ll -'lc, ~' 2
e. X1 u
tu 5 lll:-s 27 ov'r-
nL;
iclcnezo 01 'o 0 c I,
es than thOsc
Mec
recor-,,ende
Sures a--,e c'-ei;-.,-;Cal
lroduc'S Use Of 'O-.CC--;se
0.7 0-9 d t'.,.
1 4 U-- C). 2
C) Zi- I-io-. =10'.c
-S
.-OporTles and n-rev'nu
card 1/2
1,:e1hods of i:.-.provin- t:ie
structure. '111-le :-2L--in, -C',
~.onlz-r-" at t-.-o --inr:o-. -ue,:.,*--pe--,,at,,,,re of, 370
fill :;s &t 410 -,'1 20C)C . '-'-1:4Ls enisures. a bet t er cu a lity cf o nrc
s-u2face and increases th-o -,roductivity of t:!c 21,3cess. T".-Iero
-~E'u--nes and 3 tables and 5 "Joviet-bloc
Ca---d 2/2
35023
~-) t) / 6/0 C, C-1 c-, rcv,-~
Z:,.,.d Z_a!-;ILLroVl
Y~T7
on the
T-,-,~,juence O.L
TITIE.
C.1" oys
6 G,~- 0:1 ,,.LyLjnde,,,, , j. V. -L.
::Oscovl, 1901, 113 115
aj C, r concerned vith
S 1
loy e C, u - syste-.,..
S 1
I.LCS 3~
C
Cu, 1.57 6
7 5.6j
.7,cd at 4800C for 24
-a!-~ed and
from 4051C after 1 110, -
c auenchi
ted oi
atu'r, 2000C c,%rer 2,
e.L.., a
_e p_nd v.: ,
lere
d c- r) e c
is
'he
.cc ted wit.-I Z110 21- e
~jrhcr stre,.,iu
a.L ; 0 ~,, S 1, -1 t~n and I L)
Cl.-Ird 11/2
35024
6, G,'~/ u 0 0./ D 15G
Vu
Ap 'q j 0 0 P)
2ridlyanduz', Zakharov, Ye.D.
4 C_.~ i or of coid-vio-rkinU, to -~nc-t
2j
.4 1 (AY,4-1
Ou"I"".. -'ridlyander, I.T.. , V. I. Do!~r~t'-in, e"",.
Jei'or.,,iiruyemyyc 2-,Iavy; I-born---k stf--.~Iey.
i..oscovi, 1961, 116 - -12'j
TEXT: T-As is an inv~-s ~i,~ation of the influence o-f cold wcr!j:inI'.
Is -uhe only mcans o--f* imurovint, -uhe s-~renlcl-th chz?.racTe--'i-,'.-ic"- Of
alloys des heat tieat-..,~ent, on the Zlcs 0
.A. k- 1 alloy. The prepared 4-nLr;o-us had the 2. 1
U
Cu, 1.83 1.21 ',, N-J, 1.36 2e, Ti, o-~'
I lo~
. j;e 4
the "13000 (.-'.VOOO) -rade. -Inoots were ;enizcd Ovell
24 hou---s and pressed to strips of 10 x- 40 -,..111 cro.;.:.-I-ection. E;,.~!y
~-e rolled at 350 - 4000C to 6 1~o. thic-ne--s. One of the f;'~ri-os
v,,L.s ;iardened and naturally z~Ced during-- 30 days, t~.e
Viere hardened and cold-worked by rollinr- viit'- 10 an--7 20
Card 1/2 a LI
PHASE I BOOK EXPLOITATION SOV/5685
Fridlyander, I. N., Doctor of Technical Sciences, and B. I.
'-'----M&VVbyev, -66-ndidate of Technical Sciences,, eds.
Teploprochnyy material Iz spechennoy alyuminiyevoy pudry [SAP]; Wmi
statey (Heat-Resistant Material From Baked Aluminum-Powder
[SAP]; Collection of Articles) Moscow, Oborangiz, 1961. 122 p.
Errata slip inserted. 3,550 copies printed.
Reviewers: M.'-F. Bazhenov, Engineer, and M. Yu. Bal'shin,
Candidate of Technical Sciences; Ed.: M. A. Bochvar, 3ngIneer;
Ed. of Publishing House: S. I. Vinogradskaya; Tech. 3d.:
V. I. Oreshkina; Managing Ed.: A. S. Zaymovakaya, EngLneers
PURPOSE : This collection of articles is intended for scientific
workers and engineers In the institute and plant laboratories
of the metallurgical and machine-building industry; it may also
be useful toAnstructors and advanced students.
COVERAGE: The 12 articles contain the results of research on the
structure, properties,and manufacture of semifinished products
Card 1/~
Heat-Resistant Material From.(Cont.)
SOV/5685
from sintered aluminum powder. The technology for the manu-
facture of aluminum powder and briquets Is described an are
sintering processes, and pressing, rolling, drawing# and
sheet-stamping methods, The dependence of the proper-ties of
semifinished products on the aluminum-oxide content of the
powder, on the degree of hot and cold deformation, and on the
stresses of pressing is investigated. Also investigated are
the mechanical and corrosive properties of semifinished pro-
ducts, the mechanism of hardening of sintered aluminum powder,
the reasons for b2later formation, and the possibility of
recrystallization. Data on sintered aluminum alloys are included.
No personalities are mentioned. References in the form of
footnotes accompany the articles.
TABLE OF CONTENTS:
Introduction 3
Gerchikova, N. S., N. I. Kolobnev, M. 0. Stepanova, and I. N.
Fridlyander. Effect.of Aluminum-Oxide Content on the Strii-e-ture
C`hrd--2~
Heat-Resistant Material From (Cont.) SOV/5685
and Properties of Pressed Articles From SAP (Sintered Aluminum
Powder] 5
Stepanova, M. G., G. P. Zenkov, Ye. M. Lekarenko, and L. A.
Sarull. Aluminum Powder for SAP 17
The work was carried out wito the participation of G. N.
Pokrovskaya, Chief of TsZL; R. V. Nesterenko, Acting
Chief Of the Shop;and Engineers L. I. Kibitova, N. D.
Chumak, and N. I. Kolobnev.
Matveyev, B. I., M. G. Stepanova, and N. I. Kolobnev. 3ffect
of Specific Pressure in Pressing on Properties of Semifinigh-
ed Products From SAP 30
Matveyev, B. I., S. I. Nomofilov, and V. A. Shelamov. Press-
ing of Semifinished Products From SAP 36
The work was carried out with the participation of Engi-
neers A. V. Fedotova and I. R. Khanova, and Senior Tech-
nician L. S. Perevyazkin.
Card 3/5
Heat-Resistant Material From (Cont.)
SOV/5685
Murzov, A. I. (Candidate of Technical Sciences], S. 1.
Nomofilov [Engineer], and V. A. Shelamov (Engineer]. Rolling
of Sheets From SAP 50
The work was carried out with the participation of Engi-
neer R. F. Filimonova and Technicians V. I. Sverlov and
0. A. Kolosov.
Matveyev, B. I., N. A. Davydova, and I. R. Khanova. Study of
the Effect of the Degree of Deformation on the Properties and
Structure of Pressed Semifinished Products and Cold-Rolled
Sheets From SAP 59
The work was carried out with the participation of L. S.
Perevyazkin and 0. A..Kolosov.-
Davydov, Yu. P., and G. V. Pokrovskiy. Stamping of Sheets From
SAP 66
Litvintsev, A. I., and E. P. Belova. X-Ray Diffraction Study of
the Oxide Phase in SAP 77
Card 4/5
Heat-Resistant Material From (Cont.) SOV/5685
Gorelik"jS. S.j A. I. Litvintsevj and E. P. Belova. Special
Featui,es of Recrystallization of Sintered Aluminum Powder (SAP) 88
Litvintsev, A.,;., and V. M. Polyanskiy. On the Nature and
Mechanism of Blister Formation in SAP 100
Matveyev, B. 112.9 P. V. Kishnev, and I. R. Khanova. Properties
of Semifinished Products From Sintered Aluminum Powder 108
KrivenRo. R. A., Ye. A. Kuznetsova, and I. N. Fridlyander.
Sintered Aluminum Alloys 113
AVAILABLE: Library of Congress
JA/wrc w
10-27~-il
Card 5/5
FRIDLYANDER, I.N., doktor tekhn. nauk; red.; ALITI-W. M.B.; kand.
fg-khr.. ~~, red.; BAZHINOV, H.F.,, inzh., retsenzent;
RZ11EZNIKOV, V.S., kand. takhn. nauk, red.; ANIKINA,M.S.,
red,izd-va,- ORESURTA, V.I., tekhn. red,
(Aluminum foundry alloys (properties, technology of malt-
ing, casting and heat treatment)] Liteirys aliuminevys
splavy (umistval tekhnologiia plavki; litlia, i termicheakoi
obrabotki); sbornik statei. Yoskva, Gos. nauchno-tekhn. izd-
vo Oborongiz, 1961. 202 p. (MIRA 15:2)
(Aluminum alloys) (Founding)
FRIDLYANDER. 1&N., doktor tekbn. nauk, red.; DOBATKIN, V.I., doktor
---- ~tekhne nauk, red.j ZAMUUI(YV) Ye.D., kand. tekhn. nauk, red*;
BAZIMNOV, M.F., inzh.,, retsenzent; 14AKOVS14ay, G.M.,, inzh.,
red.; VINOGRADSKAYA, S.I., red. izd-va; allWUKIUNA, L.A.t
tekhn. red.
(Malleable aluminum alloys] Deformiruemye aliuminievye splavy;
sbornik statei. Moakva, Gos. nauchno-tekhn. izd-vo Oborongiz,
1961. 234 P. (MIRA 15:1)
(Aluminum alloys)
S/137/62/WO/005/100/150
AOO6/A101
AUTHORS: Fridlyander, I. N., Zakharov, A. Mi.
TITLE: Strengthening aluminum by the chemical compound Mig,Ge
C_
PERIODICAL: Referativnyy zhurnal., Metallurgiya, no. 5, 1962, 70 - 71, abstract
51428 (V sb. "Deformiruyemyye alyum. sl)lavy'p' Mloscow, Oborongiz, 1961,
9 - 16)
TEM The authors studied the r,1g,2~e compound in solid Al and the mechanical
proper-ties of Al-M6,2Ge alloys depending on the heat-treatment conditions. Al-
loys containing 0.22, o.45, 0.6, 0.9, 1.35, 1.9, 2.7, 3.5 and 4.3 weight % of
1492Ge, were manufactured by alloying at, 720 - 7400C Al of 99.93% purity, MZ of
99.91% and Ge of 99.993% pur'ity. Ingots weighing I kg were homogenized at 5500C
during 12 hours and then at 4300C pressed into 10-am-diameter rods. Determina-
tion of the crystal lattice parameters, microhardness of &-solid solution and a
microscopical analysis of the alloys were carried out on specimens quench-bardened
from 0600, 500 and 3500C after annealing for 2, 4 and 8 days respectively. Yaximun.
solubility of %Ge in solid Al is about 1.2%; at 6000C it is 1.0%; 0.5% at
Card 1/2
S/137/52/000/005/100/150
Strengthening aluminum by the chemical compound Mg2Ge A006IA101~
500"C and 0 .3% at 3500C . Maximum rb in naturally or artificially aged state
,b
is 23 - 25 and 30 - 32 kg/mm2), is shown by alloys containing at>out 2,71,16 %Ge,
i.e. being beyond the single-phase zone of the cC-solid solution. Strengthening
of quenched alloys increases gradually with a highez %G~ content, without at-
taining a maximum even at 4.3%. Maximum strengthening in aging is obtained in
alloys with 1.9 - 2.7% Mg2Ge. The investigation ha.,3 confirmed regularities estab-
lished previously for Al-Mg2Si alloys.
T. Rum:jantseva
[Abstracter's note: Complete translation]
Card 212
S/137/62/000/005/112/150
A0061-1101
AUTHORS: Fridlyander, I.'N., Zaldiarov, A. M.
-----------
TITLE: Phase diagram and mechanical propertios of Al-AlAgYlg alloys
PM-IODICAL: Referativnyy zhurnal, Metallurgiya, no. 5, 1962, 74, abstract 51447
(V sb. "Deformiruyemyye alyumin. splavy", Moscow, Oborongiz, 1961,
17 - 23)
TE)(T: The authors studied solubility of the AlAgMg compound in Al and
also the mechanical properties of Al-AlAgMg alloys depending on heat treatment
conditions. Alloys containing about 2.4; 3.6; 4.8; 6.o; 8.4; 10.8; 13.2
and 106.8 weight % AlAgMZ, were prepared by melting at 720 - 7400C from Al of
99.93% purity; 11% of 99.91% and Ag of 99.98% purity. Parallel with an increase
in -:-b, and i-of the alloys decrease, to a lower degree in natural and to a
higher degree,in artificial aging. Maximum 6b in naturally an(I artificially aged
state ( b 34 - 40 kg,/mm2 respectively) is shown by alloys containing.
` - 35 and 37
about 13.2% AlAgMg. Maximum quenching effects are shown by alloys of the hetero-
geneous range, and maximum effects of natural and artificial aging are shown by
Card 1/2
S/137/62/000/005/112-/150
Phase diagram and... A006/A101.
a
"loys in the.solid solution range. In alloys containing 2.4 - io.~% of the
~
AlAgMg compound, the effect of natural aging exceeds the quenching effect, while
in more alloyed alloys it is, on the contrary, below the quenching effect. The
maximum effect of artificial aging is shown by alloys in the solid solution range
which contain 10.8 - 13.2% of theAlAgrt compound.
T. Rumyantseva
-[Abstracter's note: Complete translation]
Card 2/2
S/137/6'41/000/006/098/163
A160/AlOl
AUTHORS: Fridlyander,.I. N., Shamray, V. F.
TITLE1 The joint solubility of copper and lithium in alumirum at 500 and
2000C
PFRIODTCAT,t Referativnyy zhurnal, Metallurglya, no. 6, 1962, 17, abstract 61103
(In colleationt "Deformiruyemyyc alyumin, splavy", Moscow, Oboron-
giz, 1961, 24 - 29)
TEXT: The joint solubility of copper and lithium in aluminum alloys con-
taining a maximum of 7% Cu and 3% Li was investigated by the methods of micro-
scopical analysis and hardness measuring. The alloys were produced by melting
AOOO-grade aluminum, J13 -1 (LE-1)-grade lithjum and electrolytic copper under a
layer of LiCl + KC3 flux of eutectic composition. The alloys were annealed at
5000C for 150 hour_~ and at 2000C for 450 hours, and quenched in water. The maximum
joint solubility of copper and lithium in aluminum 13 observed at 5000C, when
the summary content of copper and lithium is 6% (46% of Cu + 1.5% of Li). With
decreasing temperature, the solubility also decreases and does nDt exceed 0.2,116
Card 1/2
The joint solubility.of,,,
S/ 13 _j
5 7/62/000/C-06/098/16-4
A160/A101
(0.1% of Gu + 041% of,Li) at 2000G..According to the data of investigations car-
ried out,on AI-Cu-Id alloys which contain up to 7% Cu and up to '~% Li, it may be
assumed that the alloys-possess a high hardening and aging effect, are heat-
resistant and can well,be machined by pressure.
Z. Rogachevskaya
[Abstracter's nota,t complete translation)
C a rd ?j 2
S/137/WWO/005/123/150
AIO'O/A!OI
Galatskiy, B. D., Talyankin, F. V., Fridlyander, 1. N.
TrIME: The determination of the duration of quenchinG heating for attaining
the maximum tensile-strength values in relation to the temperatture
of quenching and the coefficient of drawing of pressed products
from A 1 (DI) alloy
P-MIODICAL: Referativnyy zhurnal, Metallurgiya, no. 5, 1962, 129, abstract 51787
(V sb. I'Deformiruyemyye alyumin. splavy". Moscow, Oborongiz, 1961,
59 - 063).
The investigation was carried out with products made from DI Al-
alloy and pressed out at 380 - 4oo0c with a coefficient of drawing from.2.8 to
170. Me pieces were quench-heated in a potassium nitrate bath of up to 460
5100C for a period ranging from 1 minute to 15 hours. Presented is a formula
determining the duration of quenching heating I-Lmax necessary for obtaining the
maximum values of 6b:
rcmax = 2 510-t-4 (104/f.7L2),
10
Card 1/2
The determination of...
S/137/6.VOOO/005/123/150
A16DIA101.
I
where t3 = the temperature of quenching, A - the drawing coeffilc-fent, f =PPMf /?f
(P
the circumferential length of the
f = the perimeter of the profile, Pf - U
rogruonder equality conditions of the sections Pprof - Ff; for the rods f = 1,
and for the profiles f >-l). It has been established that the regularity of
in relation to A, the temperature and /~nax is completely analogous
change of 'f0.2
to the regularity of change of (5b-
A. Babayeva
[Abstracter's note: Complete translation]
Card 2/2
S/123/62/000/013/003/021
A004/Alol
AUTHORS: Galatskiy, B. D., Tulyankin, F. V., Fridlyander, I. N.
TITLE: Ways of improving the mechanical properties of pressed shapes and
bars from the A 16 (D16) alloy
FERIODICAL3 Referativnyy zhurnal, Mashinostroyeniyo, no. 13, 1962, 22, abstract
13AI41 (In collection: "Deformiruyemyye alyumin. spla,ty". Moscow,
Oborongiz, 1961, 95 - 103)
TEXT: It is pointed out that, to obtain a high level and stability of
mechanical properties and to prevent the formation of a macro-crystalline struc-
ture in shapes and bars of the D16 alloy, a more accurate chemical composition
of the D16 alloy is necessary (3.8 - 4% Cu, 1.4 - 1.6% 14g, 0.7 - 0.9% Ma, 0.2%
Zn, Si + Re up to 0.5%). Small and medium-size shapes should be pressed at a tem-
perature of 370 - 3800C, large shapes at 410 - 4200C.
Abstracter's notes Complete translation]
Card 1/1
S/137/6P-/000/006/12P-/163
A052/AIOl
AUTHORS: Galatskiy, B. D., Tulyankin, F. V., Fridlyander, I. N.
TITLE: Methods of raising mechanical properties of A 16 (D16) alloy
pressed shapes and rods
PERIODICAL: Referativnyy zhurnal, Metallurgiya, no. 6, 1962, 58, abstract 61347
(V sb. "Deformiruyeinyye alyumin. splavy". 41';~:;L;ow, Oborongiz, 1961,
95 - 103)
TE)CT: The introduction into production of D16 alloy of an improved chemical
composition (3-8 - 4% Cu, 1.4 - 1.6% Mg, 0.7 - 0.9% Mn, up to 0.5% Fe and Si each,
up to 0.2% Zn) raises the level and stability of mechanical properties and pre-
vents formation of a coarse-crystalline structure in shapes and rods. Small and
medium shapes should be pressed at the ingot temperature of 370 - 3800C and
larger shapes at the ingot temperature of 410 - 4,,DCOC, which results in a higher
efficiency of presses and a better finish of shapes. . high Mn content in DIU'
alloy (0.8 - 0.9%) does not cause a decrease of 8 in the lateral direction.
[Abstracter's note: Complete translation]
Card 1/1
T. Rumyantseva
ESKINI G.L. (Moskva); FRIDLYANDER, I.N. (Moskva)
Effect of ultrasonic waves on the shape and size of metal compound
crystals in aluminum alloys. Izv.AN SSSR.Otd,tekh.nauk.M9t,i toplo
no-5:109-112 S-0 161. O-MU 14:10)
(Allimiralm alloys-Metallography)
(Intermetallic compounds)
(ultrasonic waves-Industrial applications)
39511
0
AUTHORS: Fridlyander, I. N., Zakharov, Ye. D.
V, -
S/123/62/000/014/012/020
A004/A101
TITLE; The effect of manganese on the ageing of certain aluminum alloys
PERIODICAL: Referativnyy zhurnal, Mashinostroyeniye,,no. 14, 1962, 32, abstract
14B186 (In collection: "Deformiruyemyye alyumin. splavy". Moscow,
Oborongiz, 1961, 113 - 115)
TEXT: The authors present the comparative mechanical properties of alloys
of the Al-Cu-Mg and Al-Su-Mg-Si systems with and without 0.80 - 1.21% Mn-additions
after hardening and ageing of the extruded parts. Test specimens were quenched
in water at 4950C and aged at 200'-1C for 2, 4, 8, and 12 hotirs. The mechanical
tests were carried out immediately after hardening and after hardening and sub-
sequent ageing. It was found that Mn-additions to the alloys mentioned ensure a
faster increase of their characteristic strength values - 6~ and 6,-, during ageing
on account of an accelerated decomposition of the solid solution, caused by a
distortion of the crystalline lattice by the manganese. -The effect of the man-
ganese o~ the decomposition kinetics is analogous to that of cold plastic defor-
Card 1/2
S/123/62/000/014/012/62o
The effect of manganese on... Aoo4AI01
mation on the freshly hardened solid solution. There is I figure.
V. StasevIch
(Abstracter's note: Complete translation]
Card 2/2
S/123/62/00/013/007/021
A004/A101
AUTHOkSt Fridlyander, 1. N., Zakharov, Ya. D., Kulakov, V. I.
TTTLEt Using cold working to increase the strength of the AKq -1 (AKch-1)
alloy
PERIO.DICAL.- Referativnyy zhurnal, Mashinostroyeniye, no. 13, 1962, 28,-abstract
13B171 (In collection: "Deformiruyemyye alyumin. splavy". Oboron-
giz, 1961, 116 - 123)
TEXT: The authors investigated the effect of cold deformation on the aging
kinetics of the AKCh-1 aluminum alloy, having a composition of (in.%): 2.11 Cu,
1.83 Mg, 1.21 Ni, 1.36 Fe, 0.082 Ti, the rest being Al, uuink specimens which,
after'the casting, were subjected to diffusion annealing at 5200C for 24 hours.
Then the ingots were pressed, rolled at 350 - 4000C intoEbrips of 6 mm thickness
and were then subjected to hardening with subsequent natural ageirZ in the course
of 30 days or rolling immediately afterhardening with a degree of deformation
of 10 and 2C%. After cold working, the specimens were subjected to aitificial
ageing at *20, 170, 180, 190, 200 and 2100C. It was found that cold working con-
Card 1/2
3/078/61/006/005/010/015
Bi"21 IB208
AUTHORSs Zakharovj As Mop Fridlyanderp Is Nop and Edellmanj N. M.
TITLEt Study of the phase diagram of the quaternary system
Al-Zn-Mg-Cu in the range of high aluminum content
PERIODICALs Zhurnal neorganicheskoy khimii, v. 6, no. 5, 1961,
1165 - 1171
TEXTt In order to clarify some contradictory data on the phase composi-i
tion of the alloys of the system Al-Zn-Mg-Cu in the papers by G. V.
Kelevich-Kizilevich (Refs 24t Kandidatskaya dissertatsiyal MATI, 1947)
and by D. Go Straubridget W. Hume-Rothery, and A. T. Little (Refs 281
J. Inst. Met-9 Up 1919 1947) the authors studied various alloys of this
system at temperatures of 430 and 2000C. The alloys with compositions of
4p 6p and 8% zinop of 0,5-5% and 0,5-7% Cu and Mg, the rest Alp were
prepared in the electric furnace. 99,95% Al, 99,945% magnesium, and
99~95% Zn were used as initial materials. The alloys were microscopically
examined after hardening and annealing at the corresponding temperatures.
Card 1/3
3/078/61/006/005/010/015
Study of the phase diagram of ... B121/B208
To attain the equilibrium statet the alloys were subject to heat treat-
ment in the following way: The samples were slowly heated to 460 OC in
evacuated quartz ampule# and left for 7 hr at this temperatureo A part of
the samples was then hardened, and the rest was cooled to 430 0C. After
10 hr the samples were hardened by a stepwise thermal process for 15 hr at
3150C, and for 18 hr at 300 OC, then cooled to 2000C within 48 hr, and
hardened again with cold water. The following etching agents were used to
develop the various phases for studying the alloyst 10% NaOH, Keller
reagent (0,5 % HP + 1,5 % H01 + 2,5 % HNOS + 95.5 % H2 0) 20-30 sec,
0.5 % H1P 15-30 sec, 2% HNO3 solution 15-20 sec, concentrated ENO 3 5-7 see,
and vapors of concentrated HNO 3 7-10 sec. The phases 9 (CULI 2)'
S(Al2CuMg), and T (solution of Al 6CuKg4 and Al 2Zn 3M93) were found to be
present in equilibrium in alloys with a 5% Zn content at temperatures of
460, 430, and 2000C. The appearance of a phase Z in the alloys with 8%
zinc is possible not only at 4600, but also at lower temperatures such as
430 and 2000C. To determine the phases of the alloys with 6 and 8% zinc,
the grindings were etched with vapors of concentrated nitric acid. The
Card 2/3
S/078/61/006/005/010/015
Study of the phase diagram of ... B121/B208
stabilizing phases for the economic high-strength alloys were determined
from the results obtained. The phases M, S, and T appear as the stabi-
lizing phases for the alloys B 95 (V 95) (5-7.0 % Zn, 1.4-2.0 % Cu,
1.8-2.8 % Mg, 0.2-0.6 % Mn, 0.1-0.25 % Cr, rest Al), j~ 96 (V 96) (7.6-8.6
Zn, 2.2-2.8 % Cu, 2.5-3.2 % Mg, 0.2-0-5 % Mn, 0.1-0.25 % Cr, rest Al)l
and the phases M and S for the alloy B 94 (V 94) (6.0 6.7 % Zn, 1.8-2-4%,
Cu, 1.2-1.6 % Mg, 0.02-0.08 % Ti, rest Al). For the alloy ~ 93 (V 93)
(6-8-7.8 % Zn, 0.8-1.2 % Cu, 1.7-2.1 % Mg, rest Al) the phase M, and for
the alloy 4 93 - 1 (V 93 - 1)(5-0-5.6 % Zn, 0.8-1.2 % Cu, 2.8-3.6 % Mg,
rest Al) the phases T, S, and possibly M appear as the stabilizing
phases. There are 4 figures and 39 references: 17 Soviet-bloc and 22
non-Soviet-bloc. The four most recent references to English-language
publications read as follows: Ref. 91 W. Oster, W. Dullenkopf, J. Met-
als, 28, 363 (1936); Ref. 10s W.L. Fink, L.A. Willey, TAIMME, 124, 78 V/
(1937T,- Ref. 11: E. Butchers; G. V. Raynor, W. Hume-Rothery# J. Inst.
Met., 69, 209 (1943); Ref. 12; A. T. Little, G. V. Raynor, W. Hume-
Rothery, J. Inst. Met., 69, 423 (1943).
SUBMITTED: April 22, 1960
Card 3/3
5/129/62/000/004/005/010
E021/E135
AUTHORS: Eskin, G.I., Engineer, and
Doctor of Tachnical Sciences, Professor.
TITLE: Crystallization of alloys of aluminium and copper
under the effect of ultrasonic vibrations
PERIODICAL. 11-1,et al love de niye i termicheskaya obrabotka me-tallov,
no.4, 1962, 32-36 (+ 1 plate)
TEXT: Alloys containing 0, 2, 4, 6. 12 and 335~ Cu were used.
J~Te It 31-_0 OC above the liquidus were cast in a chill mold
(solidification at 120-150 OC/min) and in a mold of a gypsum-
asbestos mixture (10-40 OC/min). The melts were degassed before
casting. Ultrasonic vibrations were applied to the melt from
below. The frequency was 19-21 kcs, the intensity 18-20 w/cm2,
the amplitude 18 IL; in addition, a piezoelectric device with
frequency 800 kcs and an intensity 10-12 ir/cn,2 was used. Macro-
and micro-sections were examined, the grain size of the alloys
and the microhardness were measured. Tensile tests were made and
the Cu segregation was determined by spectral photography.
Card 1/3
Crystallization of alloys Of s/129/62/000/004/005/010
E021/E135
The most effective action of ultrasonic vibrations occurred on
the solid solution type alloy. The vibrations resulted in a
finer grain and an increase in tensile strength. At higher Cu
contents the effect is less pronounced, The presence of a
modifier (0.20,j Ti in this case) considerably intensifies the
effect. Ultrasonic treatment only slightly affects the copper
segregation in the alloys studied; however, it accelerates the
diffusion of copper during crystallization of the solid solution.
The experiments on pure alloys and alloys containing modifying
additions confirmed the theory that the ultrasonic vibrations
act by breaking up the solid firnt formed during, solidification.
However, the possibi)ity is aLso put forward that the formation
of nucleating crystallites may also be accelerated under the
action of the energy given to the melt by the ultrasonic waves or
by activation of the impurities. it was also shown that ultra-
sortic vJbrixtiotis docreasod the intordendritic liquation a.,q a
rentlit of necolol-i% ( ioll 0t' klii.Yllh toll of, C.L11111111. ill ( hil procls-Sh Of'
crystallization of the solid solution. U I Ll-a:30 I kI.C v ibra L W tin
cause marked changes in the microstructures of Ole alloys,
Card 2/3
Crystallization of alloys of ... s/i2g/62/000/004/005/0.Lo
E021/EI35 I
whereas 1011-frequelicY vibrations change only the macrostructure.
There are 6 figures and I table.
Card 3/3
S/137/62,/O()0/008/()36/065
A006/AIOI
ALMIORS: Fridlyander, 1. N., Zakharov, Ye. D.
Tr=-: The effect of manganese upon aging of some aluminum alloys
PENIODICAL: Reforativnyy zhurnal, Metallurgiya, no: 8, lc-~S)2, 34, abstract 81209
(In collection; "Doformiruyemyyo alyuml.n. ";plavy", Moscow,
9,14, 1961, 113 - 115)
TEXT: The authors investigated the effect of Mn upon kinetics of aging
Al-alloys manufactured from grade 00, Cu and Mg-Al. The heat treating conditions
were: 1) Holding at 11950C for I hour and quenching from this temperature in
cold water; 2) aging at 7000C for 2, 4, 8 and 12 hours. The presence of Yh
promotes a substantial'increase of the strength ofthe alloys in freshly quenched
state. During the aging process the alloys with Mn are strengtnened more rapidly
and acquire higher -'b and is values. The addition of Mn to these alloys entails
substantial distortions in the crystal lattice of the solid solution, accelerating
separation of Ou, Mg and Si out of the oversaturated solid solu7.ion.
[Abstracter's note; Complete translation] T. Rumyantseva.
Card 1/,,
s/839/62/000/000/001/004
E193/E383
AUTHOR: ~ Fridlyander, I.N., Doctor of Technical Sciences
TITLE: Present-day aluminium alloys
SOURCE: Stroitellnyya konstruktsii iz alyuminiyevy1ch splavov.
Ed. by S.V. Taranovskiy. Moscow, Gosstroyizdat, 1962.
22 - 43
T BXT: This is a review article in which the possibilities and
limitations of aluminium alloys as materials of construction and
decorative trim in the building and civil-engineering industries
are discussed.- A short historical survey of the development of
aluminium alloys is given in the introducioxy chapter, which also
deals briefly with the theroetical basis of formulating now,
industrial, aluminium-ba5C materials. The next chapter is devoted
to wrought aluminium alloys, including pure aluminium and alloys
of the following systems: Al; Al-N1n; Al-,Nlg; Al-Mg-Si;
J\l-Zn-Mg(Cu); Al-Cu-blg; Al-Mg-Si-Cu; Al-Cu-Nin(Li, Cd). Aluminium'
cast alloys are discussed next and the last two chapters deal with
s i n t e r e d. Al and Al-base alloys and with foamed Al. Typical
alloy compositions are given, the effect of heat-treatment (preci-
pitahiy~jhardening) on the mechanical properties and the corrosion-
Car
s/83q/62/000/Ooo/ool/oo4
Present-day aluminium alloys E193/E383
resistance of various alloys is discussed, the weldability of
various alloys is assessed and the methods of preparation of isome
lo.4s common maLcrials are briofly described. The paper is general
in character but numerical data are frequently given to illustrate
the general argument. There are 4 tables.
Card 2/2
S/129/62/000/011/002/007
E193/E383
AUTHORS: Galatskiy, B.D., Engineer and fridlyander, I.N.,
Doctor of Technical Sciences, Prof-eisor
TITLE: Determination of the heating time during the solution-
treatment of extruded duralumin-parts
PERIODICAL: Metallovedeniye :k termicheskaya obrabotlca metallov,
no. 11, 1962, 13 - 17
TEXT: The mechanical properties of solution-treated and,
consequently, of age-hardened duralumin depend on the time at the
solution-treatment temperature. The object of the present investi-
gation was to determine the optimum value'of this parameter in
the heat-treatment of extruded duralumin parts. Analysis of experi-
mental data for extruded rods of alloy's "l (Dl) and 0,16 (D16)
(with average 'analysis 4-30,; Cu, 0.6 and 1.54% Mg and 0.6% Mn) showed
that the lieating time, T; max' ensuring the maximum UTS of the
alloy, increases with decreasing -.solution-:treatment'. - I I
temperature, tZI and reduction, X , attained in extrusion. This
relationship is described by
Card 1/4
S/129/6'2/000/011/002/007
Determination of .... 4 E193/r,3'83
1" 510 - t3 10
max 2 10 (1)
It was found, however, that Eq. (1) was not applicable to extruded
shapes, -_ in this case being considerably shorter than that
max
for rods extruded to the same X A series' of comparative tests
was therefore conducted on vods and shapes of the same cross-
section, extruded simultaneously to the same X through a single-
multihole die. The results showed that:
p
ma pro (2)
--prof
max prof
wh e r c z, i s -K, of a rod, is of a profile
max 111ax max -,max
with the same cross-sectional area and P prof' P( denote* respectively,
Y I'
circumference of the rod and profile section. The term "shape
coefficient" was ascribed to th~! ratio:
Card 2/4
Determination of ....
P
pro
PkJ(
and Eq. (1) became:
10-t:-
2 10
max
S/129/62/000/011/002/007
E193/E383
(2a)
104
(3)
2
where Vj = 1 for rods and is greater than 1 for other shapes.
The results of the next series of experiments showed that 'r,
max
depended also on the Cu, 1161g and Mn content of the alloy, the
effect of Mn being most pronounced. Analysis of the experimelital
results showed that if the effect of the variation in the Mn
content was taken into account, formulae (2)- became:
I
Card 3/4
S/129/62/000/011/002/007 ~
Determination of .... E193/E383
YZIn-O. 6 510-t3
0.1 1 .10 104
rU '- 2 0 2 0 (7) -
max '.0% X 2
There are 6 figures and 1 table.
Card 4/4
S/123/62/000/023/005/008
A004/A1Ol
AUTHORS: Fridlyander, 1. N~, Romanova, 0. A.
TITLE- The effect of cold working on the mechanical properties of
aluminum alloys of different phase composition
PERIODICAL: Referativnyy zhurnal, Maohlnostroyenlye, no. 23, 1962, 17,
abatrnct 21AIP3 (In collection: "Issled. aplavov tsvetn.'
metallov". 3. Moscow, AN SSSR, 1962, 43 - 47)
TEXT: Tho authors g1ve an-account of the results of Investigating the
effect of hammer cold working (upsetting) with deformation degree3 of 0.5, 10,
15, 20, and 25% both in the freshly hardened state and after a 24-hour aging on
the mechanical properties of the. A 16 (D16), AK ~-l (AK 4-1), AK 8 CAK8) and
J1 20 (D20) aluminum alloys. Based on the test data, the following conclusions
are drawn. Cold working carried out between hardening and aging Increases the
strength of the alloys to different degrees. In proportion to the increase in
the degree of cold deformation, the strength grows nearly rectilinearly, while
the relative elongation drops sharply, particularly with deformations in the
range of 5 - 101%. The maximum strength increase by cold working is obtained in
Card 112
:-,/12-3/62/000/023/005/008
The effect of cold working on the... A004/AlOl
fned pieces of the D16 and AK 4-1 alloys, both at room temperature and at
150 C(with 30 minutes and 100 hours holding at the test temperature). With forged
pieces from the AK8 and D20 alloys, cold0working does not result in a considerable
increase In strength during tests at 150 C. The different effect of cold working
is caused by the different phase and structural nature of the alloys.
CAbstracter's note: Complete translation]
Card 2/2
FRIDLYANDER I N. (Moskva); ROMANOVA, O.A. (Moskva); AJOIATOVA, Z.N.
C )7,- Prinimali uchastiye; RE2VIK, P.G.; LEBEDEVA, N.S.
Mechanical properties of heat-resistant aluminum alloys with
lithium and cadmiumI Izv.AN SSSR. Otd.tekh.nauk. Met.i topl.
no.4182-89 Jl-Ag 62. (MIRA 15:8)
(Aluminum alloys-Testing)
(Heat-resistant alloys--Te3ting)
5/806/62/000/003/005/018
AT4!rHORS: Fridlyander, I.N., Zakharov, Ye.D., Tigina, L.P.
TITLE: The kinetics of the aging of aluminum alloys of the Al-Cu-Mg system.
S*RCE: Akademiya nauk SSSR. Institut metallurgil. Iosledovaniye splavov
tevetnykh metallov, no.3. 1962, 58-61.
TEXT: The paper reports an experimental investigation of the effect of both
aging temperature and aging time on the decomposition of a supersaturated, quench-
ha'rdened, solid solution in alloys of the Al-Gu-Mg system. The objective of the in-
v4stigation was to determine the usability of the aging time as an indicator of the
time rate of the diffusion flux in an alloy. Four AI-Cu-Mg alloys were tested (com-
positions tabulated); three of them contained appx. 6.6% Cu + Mg, but in different
proportions: 2.1, 1.37. 0.95. The fourth alloy contained also 0.820/6 Fe. 0.83016 Ni,
and 0.11016 Ti. The alloy wa's prepared in an electric muffle furnace and cast into a
watercooled Z8Oxl6OxZ6-mmtnold at 680-7000C. The ingots were homogenized for
24 hrs at 4800, milled to ZOOxI5Ox2I mm, and rolled on a two-roll mill at 420-4300C.
First rolling (6-10 passes) reduced the billet thickness to 12-14 mm, second rolling
(3-6 passes) to 5-6 mm. Hardness-test specimens were cut, heated in a saltpeter
bath to 4950, ooaked for 60 min, and water-quenched. This was followed by aging
at 160, 180, ZOO, and. 2100C and 30-sec Brinell testing with a load of 1,000 kg on a
10-mm. diarn ball. The hardne s a -v9. -aging- time curves show that the solid-solution
transformations are accelerated by an increase in aging T; however, the time for
Card 1/2
xrr,, Uerrnan, and- "gure, 2 tables,
2En9lishAa,g,ag4
TUMANOV, A.T., glav. red.; VYATKIN, A.Ye., red.; GARBAR,
red.; ZAYMOVSKIY, A.S., red.; KARGIN, V.A., red.;
KISHKIN, S.T., rod.; KISHKINA-RATNER, S.I., doktor tekhn.
nauk, red.-; PANSHIN, B.I., kand. tekhn. nauk, red.;
ROGOVIN, Z.A., red.; SAZHIN, N.P., red.; SKIYAROV, N.M.,
doktor tekhn. nauk, red,; BIPLYANDER, I.N., doktor tekhn.
nquIC,- red.; SHUBNIKOV, A.V., red.; SHCHERBINA, V.V., doktor
geol.-miner. nauk, red.; SHRAYBER, D.S., kand. tekhn. ne(ukp
red.; GENELI, S.V., kand. tekhn. nauk, red.; VINOGRADOV, G.V.,
doktor khoz. nauk, red.; NOVIKOV, A.S., doktor khoz. nauk,red.;
KITAYGORODSKIY, I.I., doktor tekhn. nauk, red.; ZHEREBKOV,S.K.,
kand. tekhn. nauk, red.; BOGATYIREV, P.M., kand. tekh-a. nauk,red.;
SANDOMIRSKIY, D.M., D.I.S., kand. tekhn. nauk, red.; BUROV, S.V.,
kand. tekhn. nauk, red *; POTAK, Ya.M., doktor tekhn.nauk, red.;
KUKIN, G.N., doktor tekhn. nauk, red.; KOVALEEV, A.I., kand.tekhn.
nauk, red.; YAMANOV, S.A., kand. tekhn. nauk, red.; SHEKEL',
I.A., kand. khoz. nauk, st. nauchn. red.; BABERTSYAN, A.S., inzh.,
nauchn. r ed.; BRAZIRIIKOVA, Z. I. I nauchn. red.; KALININA, Ye.M. ,
mlad. red.; SOKOLOVA, V.G., red.-bibliograf; ZENTSELISKAYA, Ch.A.,
tekhn. red.
[Building materials; an encyclopedia of modern technology) Kon-
struktsionnye materialy; entsiklopediia sovremennoi tekhnikl.
Glav. red. A.T.Tumanov. Moskva, Sovetskaia entsiklopediia.
Vol.l. Abliatsiia - korroziia. 1963. 416 p. (MIRA 17:3)
1. Chlen-korrespondent AN SSSA (for Kishkin).
A
CCESSIONNR: AT4012706 S/2981/63/000/002/0005/0012
AUTHOR: Matvcyov, B.I.; Fridlyander I N Agarkov, G.D.; Stepanova, MeGe;
Vlasova, P. T.
TITLE: Properties and application of blanks made of sintered aluminum powder (SAP)
SOURCE: Alyuminiyevy*ye splavy*. Sbornik Btatay, no. 2. Spechenny*ye 6plavy*.
Moscow, 1963, 5-12
A
TOPIC TAGS: powder metallurgy, aluminum powder, sintered powder, sintered aluminum
powder, SAP, SAP blank
ABSTRACT: la a general review of the uses and properties of SAP, it is pointed out that
heat-resistant deformed alloys of sintered aluminum powder at 350-500C are significantly
stronger than standard deformed aluminum alloys. This is explained by the finely dispersed
oxide phase uniformly distributed in the aluminum matrix. Parts made of SAP, whether
from APS-1 or APS-2 powder, show corrosion resistance practically equal to that of ordi-
nary aluminum. Ile technology of the briquetting, sintering and pressing of SAP is de
scribed. Ile following blanks are commonly made of SAP-1: rods and pipes up to 200 mm,
in diameter, sections up to 100 sq. cm and over, sheets 900 mm wide, up to 3 m in lengthA
Isard 1/2
ACCESSION NR: AT4012706
and up to 0. 8 mm thick, rivet wires, foil up to 0. 03 mm thick, pressed blanks. SA13-2 is
used for parts of the same type, only of lower workability. The fatigue strength of both
SAP-1 and SAP-2 exceeds that of all aluminum alloys. Some representative data are tabu-
lated. These metals may be soldered and welded, machined, finished, cut and pressed.
The will thickness and radii of the tubes which can be pressed from SAP are smaller, the
lower the content of A1203 in the initial material. These features show that the existing
opinion concerning the brittleness of sintered materials has nothing to do with SAP. It can
be machined in the same way as common aluminum, and now fields of application are
constantly opening. "The corrosion tests were carried out by V. S. Komissarova. " Orig.
art. has: 3 figures and 6 tables
ASSOCIATION: None
SUBMITTED: 00 DATE ACQ: 13Feb64 ENCL: 00
SUB CODE: MM NOREF SOV: 000 OTHER: 000
isard
Epp r (M) /M/P -r3P(cj
29NORAff"t: AT4012-726 a/2q8l/65/boq/oo2/6ij5bfG16&
AUMOR: Fridlyanderp 1. He., KEYMLM, No SO; lftvenko. He A*
TITM- 51-lican-alumirtun elloy vith a low coefficient of linear expansion
8 OUWE e. A1yuuiuiy4vy" splavy*. Sbornik statey,, no. 2* Spechenny+je Gj)laV*#
Moscow# 1963,9 i6o-i6S
linear
TOPIC TAGS:- --all-4nma-~11py,, silicon alloy, silicon altmdatm alloy, SAq
expansion Coaqicient, alloy linear expozw1cu, alloy plasticity, _trc!p?,4crLtain1n&
alloy, nicke 'Joataining alloy,, zirconitm containing alloy, titaniumcontain-Ing
alloy., silicoa carbide-
AMTRACT: Binary alvatintm-silicoa alloys; (4-314 Si and those with aAm-f S
of - Fe (up to 9% ),, Ni(5-17~),, Zr(2.yp),, T:L(up to 1%~, and. SiC(10 and 24:t were
prepared by pulveeLzing and grinding processes and were tested for stren~;th and
linear expansicae Ole higIiest strength w= exhibited by U-Si alloys CC close-
to-eutectic composition (25-340Q, their plasticity decreasing as the St conteut
increased* Additions of M had a more favorable effect than additions w' Fee
The beat mechanical properties were obtained vith a&liticas of 5-1~ His Iftile
adfiitiaw of Zu prodwed no a5realable effect,* Additions of SO goodacad qu&Uf4r
Card 1/2
ACCMI(IT im: AT4oM28
-allqm -ana -ad4liticno-of Ti produced markedly greater stivngth In alloys -prepared.
y ;Zerizing. The lowest coefficient. of linear expaasion was obtained vith
Ir
a&Utioas of His Additions of Ti were fa=d. to hame a (peater lowering effect
than adBItiona of Sio Alloys composed of Al, Si, and SW possess high neeb-Scal.
properties and exhibit a low coef~Ucient of Mnear expazu;ioa,, which decreases as
the SiC content inamaseat The processes of preparing the alloys and eyomining
their microatructure are givxm sal disoussed at great leigthe Orig* arto bas:
2 tables, 4 figures an& 5 grephze