SCIENTIFIC ABSTRACT MALININ, N.I, - MALININ, R.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001031810014-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Sequence Number: 14
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

L
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AP6023392 SOURCE CODE: tIR/0374/66/000/00310330/0336
Panshin, B. 1.
AUTHOR- BuyMov. G. 1. Kasyuk, V. D. Malinin, N. 1.
ORG: none
TITLE: The creep of polymer materials subjected to cyclic loads A:3
SOURCE: Mekhanika polimerov, no. 3, 1966, 330-336
TOPIC TAGS: creep, thermoplastic material, polymer
A13STRACT: A method for constru.cting the cree Vcurve of one-dimensional
5 proposedL
polymer material subjected to periodically applied alternating stresses i
The creep curves obtained by tests under constant loads were used as basis for
calculation. The mathematically derived curves agree within 1016 with the experi-
mental results, thus proving the applicability of the nonlinear heredity theory
(viscoelasticity) expressed by M. 1. Rozovskiy's equation. Experimental examina-~
tion has shown that the proposed method may be used with sufficient accuracy for
Card 1/ 2 UDC: 678. 744. 325:539. 388. 1

ACC NRI AP6023392
predictions of creep behavior of thermoplast polymers
ic cler periodically
applied (cyclic) loads. Diagrams showing the constant-load creep curves obtained
experimentally, and the cyclic-load creep curves obtained mathematically and
experimentally are presented in the original article. Orig. art. has: 5 figures,
and 11 formulas. [KPI
SUB CODE: 20/ SUBM DATE: 02Nov65/ ORIG REF: 012/
Card 2/2

V.I., kand.tekhn.nauk; M&~ ~IN ~ inzh.; MATVIYENKO, N,I,,
student; ZUBAMV, V.V., student
Determination of th- optimum operation of a hydroel6CLr~- power
stationwith seasorall regulation using analog computpers. Trudy
MEI no.46.s13-24 163. (MIRA 19,3)
1. Kafedra gidroenergetiki Moskovskogo ordena Lenina energetJ-
cheskogo instituta.

LANDAU? M.A.1 MALININO N.K.
Trimerization of chloroclanogen. Zhur. fis. khim. 39 no.3t779
W f65. (MIRA 18.-7)

One dimenrional problem,
r4or'-stat4onar'Y creer. 1., 1951.
W)NTHLY L.T-'r Library cf Convr,ss
-!a
""

- I '-' - -T-,- 1 ~' - - V~.- . -.1 V. i,%)
- - -.- ~ I- - .I - 1-1 , - I .
Mzchinery - Constrliction
7
"Principles of modern methods of calculatinL durability of machine constx-,Iction.
Reviewed by Prof. A. A. i1olov. Vest. mash. 31 no. 12, 1-)51-
Montbly List of Russian Accessions, Library of Congress, Septeliber 1~52. ~,",!(MASSSIFIZD.

Trea3ure island BibliograFliic Report
00COCC63
BOOK Call No.: AF58002
Authors: PONOMARE71, S.D. ; BIDERMAN, V.L.; LIMAR01, K.R.; MMISHITI, V.M.;
MALININ, N.N.; FEDDSIYEV, V.I.
Full Title: ' VIMMIENTALS OF ;.'ODMN METHODS FOR STRENGTH CO11'.PUTATIONS IN 'MACHINE-
BUILDIUG. (Computations of dynamic loads. Stability. Creep).
Transliterated Title: Osnovy so-~rremennykh metodov rascheta na prochnost'v
mashlnostroyenii. (Raschety pri dinamicheskoy nagruzke,
Ustoychivost'. Polzuchest').
PubUahit*. Data
Originating Agency: None.
Publishing House; (MASHGIZ), State Scientific and Technical Publishing House
of Literature on Machine Building.
Date: 1952 No. pp.; 862 No. copies: 10,000
Editorial Staff
Editor: Prof. Ponomarev, D.D., Technical Editor: None.
Dr. Erg. Sci.
Editor-in-Chief: None. Appraiser: None.
Others: Golovin, S. Ya., Eng., editor of literature on heawj machine tA.,ilding.
Text Data
Coverage: The three parts of this book discuss: 1) the stren0h computation
of various machine elements under dynamic loads, 2) the stability
computation of machine elements, 3) the creep computation of machine
parts working at high temperatures. The first section describes
the computation of the strength of moving machine elements, particularly
1/2

00~)00063
2/2
Call No.: AF58002
Full Title: FUNWMFULS OF _-0DMJN !.TE'rhODS FOR STRMIGTH COMMATIONS IN 7,%CHPTE-
BUITDING. (Computations of dynamic loads. Stability. Creep).
Text Data
Coverage: (continued)
discs and wheels; investigates questions of elastic vibfation
in connection with various practival problems (harmonic, non-
harmonic, quasi-harmonic, non-linear and other types of vibration);
and analyzes the strength of elements under variable loads. The
second part concerns methods of computing the stability of rods and
springs (twisted and compressed-coiled), or rings and flat shapes
of curved thin strips, of the elements of thin-wall construction
and non-symmetric profiles, of thin rectangular plates, and of rota-
ting casings. The thrid section analyzes the questions of creep
and relaxation of tension, permanent deformation, and aging of parts
subjected to the action of high temperatures..
Purpose: A textbook for design engineers in the field of machine building and
students of the technical colleges and also for scientific workers.
Facilities: None.
No. Russian and Slavic References: 382 of total 409.
Available: Library of Congress.

"Computing a Rota:ting Disc Attached to a Shaft" an article in the book "Computing the
Stability, Hardness and Creep of Elements in Machine Constructio2Z' Mashgiz, 1953- P-

"Calculating Round Symmetrically Loaded Discs of Variable Thickness." an article in
the book "Computing the Stability, Hardness and Creep of Elements in Machine Construc-
tion," Mashgiz, 1953, P- 36-

"Steady Creep of Round Symmetrical Loaded Plates" an article in the book "Computing
the Stability, Hardness and Creep of Elements in Machine Construction", Mas 1953,
p. 221.

KALININ, U.N., doteent, kandidat takhaichaskikh nank.
--"
Calculation of rotating disks taper-fitted on shafts.[Trudy] MTTU no.26:
5-21 153. (HLRA 7:5)
(Disks, Rotating)

W-1911, N.M., doteent, kandidat teWmichaakikh nauk.
Calcm1ation of round mad annular symetrically loaded plates of varylag
thickmess. [Trudy]KVTU no.26:]8-6) '53." NEIRA 7:5)
(Blades)

luLININ, U.S.0 dotsent, kandidBt tekhrdcheskikh nauk.
7 --
Continuous creep of round symetrically loaded plates. [Trudyj.14V=
no.26:221-238 '53. (MLF-A 7:5)
(Elastic plates and shells) (Creep of metals)

Ponoma-rev, S.D.
Viderman, V.L.
Likharev, K.K.
Malinin, N.H.
Yakushin, V.M.
Feodoslyev, V.I.
"Elements of Modern Methods Moacow Highier Technical School
of Calculating Strength in imeni B
Machine Building"

No. 37763--Netod povysh~,-'e~niya nesushehey sposobnosti pruzhin. V sb;
Povyshen4t prochnosti d~~taley M.-L., 1~49, S 136-45--Bibliogr:
9 Nazv.
So: Letopis' Zhurnelinykk Statey, Vol. 7, 1049.

ran nr,)' so
k
diclat taV7),nlc nklkh nat~k: 9.~ f p -,r
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cheskikh nank; BCGWl-AVSK,.,'Y. P.Ye., tBadltd;)t tekhnicesk,,h nank:
BORUVLCH. L.S.. kandiiat telfticheskikh nsul~; VOLIAIR,
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'1.0.. Drofessor; MANNTBERG, Y.P. , kandidat tekhni-Keskl;rb nauk.
-DO&ChATOV. V.V., in7hener, WAAW. A.G, kandidat tevhnlr,pskikh
nank; KI"S05FI-111. R.S., orofessor; KODULP, D.S., 'mi-Ai,isT
f-heskikh neuk; A.i-., kandid-91, tekhnicneskikh riaiik:
KRUTIK(M. I.P., knrididat, talchnit~hp.,~lrrilch nauk-, KWAU,'~', kandi-
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inzhener; MkLlltli. ',-andidst te~7~--iiheqsk-ilch nauk: MAR'v,'-OY.
ksri~idat teklinIFFMIT natik: NU.,MG, lf.Ya., kandidat teO-.ni-,~Pskikh
aatil:; NIKOLAW, G.A., nrcfessor, dn;-tnr tek-hnicbeskikh riwik;
P-3TRUSEVICH, A.T., dokft~y takhnichesklikt. aruk: P022)HY,-.F~V, S.N.,
dotsent: PONLI(OPEV, L.J., orofessor, d~kt~,,r tekhnicheslrikh nsi)V;
?RIGORMUY, H.I., orrf(-.--r4or, doktor te'khnicheskilcb FR(,.,vill,
B.A.. knrLdidat tekhni-i-ec-kikh nank, RZS~TTOV, D.N.. nrrfe-nr, do!-tor
to-khnicheskikh nauk: SPTE-". E.A.. orcfeE~5!,~r, tioktar
nouk; SMNSEN. S.V. ; SLObODKIN, M.6- , inzhener: SPITSYN,
orcfespor, doktor te~tnlr-henkikh nauk; STCLMll. G.R. , kandl+ t
tsklinichaskikh nauk. TAYT!:~. B.A., kandiat tal-l~ntchenktkh n~!ulk;
TETELIBAMI. 1.M.. kar-didat talkhnicheskiMi na-l-; UMANISKlY, 1-1- ,
nrofescor, doktor nank. nQDl,;S'Y'&V, V.I.
dnktor takhnicbselrikh ns,:t~: (Continued or next card)

(corAtinwd) Carl
IMAYT, D.1%. kam!i-Int te',~nicheslrikh rauk-, --'Yj1J,.V. V-Yz~., -,indijat
takhr4chark-ikh nai.,-; Y.Y.. Inshenpr, is, I%rr.7 rt~~Ialrt-r;
,iMROV, V.S.. kan~iilgt tel-hnirheakikk naub-, nw:c..%~7,- r:,i~-Irtcr;
TSVETJiQV, A.F., dctf-ont, rn!.,chnvy redairtor; irzhener,
nauchxkvy redektor; M.Ya.. iazhener. w-.6invy rpf-'Aktor;
KARGAIM. V.G., inzi-,enur, nsuchnyy redu'ctmr: N.',., dolr-tcr
takhnichaskikh nauk, professor. redal-tor; T-F.. tekliniche-
skiy radaktor
Narual of Tachir~,ry r-.u-f'Fi c+ tire i SDr,-- r~-ntic
v trak'n Uos.nauchnc-
lit-ry, Vol.!. 1 51 1099 p.
1. Deyst-titel' r-- A*csde~*- L-2: ,frr Serena,?-.)

ANDRETW, L.Te., kandidat takhnichaskikh nauk; BIDERIW, T.L., kandidat
takhaichaskikh nauk; BOYARSHIBUT, S.T.. Itandidat tekhaicheakikh
nauk; VOLINIR, A.S., doktor takhnichaskikh nank. DIMEMIRG, F.M.
kandidat taktinichaskikh nauk; ZASELATEW, S.H., inshener;
KINASOSHVILI. R.3., doktor takhnichaskikh nauk. professor;
KOVALEM. A.D..; KAKUSHIN, V.14.. kandidat takhaichaskikh mim,
14ALININ H.N . krandidat takhnichookikh nauk; POKOHAREW. S.D.,
*ottrr%47-hi~k;hask1kb nauk; PRIGOROVSKIT, H.I., doktor takhal-
chaskikh nauk; TXTELIBAUH, I.K., kandidat takhnichaskikh nauk;
UKANSKIY, A.A., doktor takhnichadlkikh nauk, professor; MBOSITIV,
V.L. doktor takhnichookikh nauk; SMNSU, S.T., radaktor;
TRAPEZIN, I.I., kandidat tak-linichaskikh nank. radaktor; KARGMT,
V.G., inzhener, redaktor; SOKOIDVA. T.F.. tokbnichaskly redaktor.
[Mechanical engineer's mannal; in 6 volumes) Spravochulk mashlno-
stroitelia; v sheatt tomakh. lzd.2-e, ispr. i'dop. Koakva, Goa.
nauchno-takhn.izd-vo mashinostroit. lit-ry. Val-3. 1955. 563 P.
(Mechanical engineering) (HLRA 8:12)

SOV,/124- 57-4-4q70
Translation from: Referativnyy zhUrnal. Mekhanika, 1957, Nr 4, p 146 (USSR)
AUTHOR: Malinin, N. N.
TITLE: The Design Calculation of an Unevenly-heated Rotating Disk of
Variable Thickness in the General Case of Axisymmetric Deformation
(Raschet vrashchayushchegosya neravnomerno nagretogo diska
peremennoy tolshchiny v obshchem stuchaye osesimmetrichnoy
deformatsii)
PERIODICAL: V sb,: Raschety na prochnost' v mashinostroyenii. Moscow,
Mashgiz, 1955, pp 124-153
ABSTRACT: Ref. RZhMekh, 1954, abstract 4177
Card 1/1

KALININ, ff. N.
"POTOW? I
Momentless states rotating slightly beat bars* [Trudy]W*-U no*31:
29-34 155 (HIBA 8: 5 )
(;UAes) (Homents of inertia)

NALIMY, N.N.
Design of non!--uniformly heated
noo3li46-62 155,
(Pipe) (Turbomchines)
thick-walled pipes.
(Thermodynamics)
(Trudy] KM
(HrHA 8:5)
-V

KALININ, N.H., kandidat tekhnicheskikh nauk, dotsent.
Calculation of a rotating, irregularly heated disk of varying
thickness in the general case of eqaiaxial strain. [Trudyl
KM no.46:124-153 155. (MM 9:4)
(Disks, Rotating)

PONOMARNV, S.D., d&tor takhaicheakikh asuk. profersor; BID11,11MAN, VA.;
LIKHAREV. K.K,,,- MAMMSHIN, VAL, KALI14IN N.11.- YBODWYNT, V.I.;
Z-z
FOPOVA~ S.M.. tokfinichaskiy r(jrbikT6P%-" Y-6.11., telchnicb-a-
skiy redaktor
CCalculations of the strength of materials in machine manufacturej
Rascbety na prochnost' v manhiaostroenii. Pod red. S.D.Pollomareva.
Hoskva, Goa. nauchno-takha. Izd-vo usstAnostroit. lit.-ry. Vol. 1.
CTheoretical priaciplas and experimental methods. Calculations for
atractural rod elements under atativ load] Teoratichaskia oanovy i
akaperimentallnya metody. RaDchoty starzhnavykh elamento-v konotruk-
tvii pri Btaticheskot nagruzka. 1956. 984 p. (HLRA 10:3)
(Strength of materials) 011asticity)

SOV/124-58-3-3277D
Translation from: Referativnyy zhurnal, Mekhanika, 1958, Nr 3, p 106 (USSR)
AUTHOR: Malinin, N. N.
TITLE: Strength and Creep Calculation of Rotary Blades and Discs of
Turbines (Ra-~,chet na prochnost' i polzuchest' rabochikh
lopatok i diskov turbomashin)
ABSTRACT: Bibliographic entry on the author's dissertation for the degree
of Doctor of Technical Sciences, presented to the Mosk. vyssh.
tekhn. uch-shche im. Baumana (Moscow Higher Technical School
im. Bauman), Moscow, 1957
ASSOCIATION: Mosk. vyssh. tekhn. uch-shche im. Baumana (Moscow Higher
Technical School im. Bauman), Moscow.
Card 1/1

124(0)~,'235(2) PHASE I BOOK EXPLOITATION SOV/2037
Moscow. Vyssheye tekhnicheskoye uchilishche Imeni N.E. Baumana
Raschety na prochnost' v mashinostroyenil; [sbornik] Design for
Strength in Mechanical Engineering; Collectio of Articles)
Moscow, Mashgiz, 1958. 244 p. (Series: Its: FTrudy] 89)
3,300 copies printed.
Ed.: G.A. Nikolayev, Doctor of Technical Sciences, Professor,
Honored Worker in Science and Technology; Ed. of Publishing House:
N.P. Chernysheva; Tech. Ed.: B.I. Model'; Managing Ed. for
Literature on Heavy Machine Building (Mashgiz): S.Ya. Golovin,
Engineer.
PURPOSE: This collection of articles is intended for engineering staffs
in the machine-building Industry and may be useful to scientific
workers and senior students of mechanical engineering vtuzes.
Card 1/8

Design for Strength in Mechanical (Cont.) SOV/2037
COVERAGE: The articles cover the graphoanaly-tical method of
designing circular symmetrically loaded reinforced plates,
methods of designing rotating heated disks for transverse bending,
and calculation of preloaded belleville springs. Also discussed
are differential equations for deformation of rubber-cord shells
of rotation, the theory of flexure of rubber-cord hose, and
stability problems of elastic cylindrical shells. Results of
experimental investigations of strength and ductility of
constructional steels and other materials are preaented. Several
articles are devoted to problems of vibrations in machinery.
There are 78 references; 71 Soviet, 4 German, 2 Englishand
1 French.
TABLE OF CONTENTS:
Foreword
3
Sergey Dmitriyevich Ponomarev (on his 50th birthday) 7
Ponomarev, S.D., Doctor of Technical Sciences, Professor.
Graphoanalytical Method for Designing Circular Symmetrically
Loaded Ring-ribbed Plates 12
Card 2/ 8

Design for Strength in Mechanical (Cont.) SOV/2037
The method of design discussed is claimed to be less time
consuming and simpler than the existing analytical methods.
It allows for easier evaluation of the stiffening effect of
shape and location of the ring rib.
Malinin,-N-_N. , Doctor of Technical Sciences, Docent. Radial and
Transverse Bending of Disks 43
The author gives an approximate method for determining
stress relieving coefficients in transverse bending
(symmetrical to the axis) of a rotating, nonuniformly
heated disk of variable thickness. "Radial bending" mears
the effect of radial forces, (e.g., centrifugal) analogous
to the effect of axial tension forces acting on lateral-y
loaded beams. This method allows for quick evaluation of the
stress relieving effect due to rotation of the disk while taking
into account changes in the elastic properties of the marerial
due to temperature.
Card 3/ 8

Design for Strength In Mechanical (Cont.) SOV/2037
Sokolov, S.V., Candidate of Technical Sciences. Design of
Preloaded Belleville Springs and Experimental Investigations
of Springs 63
A method of designing plastically preloaded belleville springs
is presented. Change of the disk and residual stresses
equalizing nominal stresses in operation are discussed.
(This fact causes an increase of carrying capacity of the
springs). The theory was experimentally checked.
Alfutov, N.A., Candidate of Technical Sciences; V.F. Sokolov,.
Engineer. Determining the Lower Critical Pressure for an Elastic
Cylindrical Shell and Behavior of the Shell Following Buckling 95
Solution of the problem is claimed to be new and simple.
Examples of design are presented. A comparison Is made with
results obtained by methods of other authors.
Lapin, A.A.,. Candidate of Terhnical Sciences, Docent. Investi-
gation of Flexure of Rubber-cord Cylindrical Shells ill
This article presents results of w9rk done in 1950 with
V.L. Bideman at the Nauchno-issledovatollskiy institut
shinnoy promyshlennosti (Scientific Research Institute
for the Tire Industry). Me possible forms of elastic
Card 4/8

Design for Strength in Mechanical (Cont.) SOV/2037
equilibrium of a rubber-cord flexible hose under internal
pressure are analyzed.
Biderman, V.L., Candidate of Technical Sciences. Differential
Equations for Deformation of Rubber-cord Shells of Rotation 119
The article Investigates general cases of deformation in
rubber hoses, tires, shock absorbers, etc., subjected to
internal pressure. A method is presented for analyzing a
cylindrical longitudinally fastened shell under arbitrary
periodic loading.
Sapozhkov, N.M., Engineer. Investigation of Optimum Dimensional
Proportions In T and I Sections 147
The author finds conditions for most rational configuration
of T, I, and I cross sections for castings or weldments
designed for bending.
Card 5/8

.Design for Strength in Mechanical (Cont.) SOV/2037
Likharev 11 K.K.P Candidate of Technical Sciences, Docent.
Comparison of Characteriaties of Materials Under Unlaxial
Tension and Compression 168
The article is based on experimental data obtained at the
Department of "Strength of Materialp" at MVTU (Moscow
Highe'r Technical School imeni N.Ye. Bauman). The author
points out the necessity of establishing a method for complete
testing of materials in tension and compression in order to
correct some not too well-founded views on the characteristics
of materials. Many stress-strain diagrams and tables showing
the mechanical properties of several materials are included.
Konyushko, Z.M., Candidate of Technical Sciences, Docent.
Construction of Stress-Strain Diagrams for Shear of Brittle
Materials Based on Results of Tension and Compression Tests 197
A method is described for obtaining stress-strain diagrams
for shear from stress-strain diagrams for tension and
compression of materials with different characteristics in
tension and compression. Results of experiments are compared
with theoretical conclusions.
Card 6/8

Design for Strength in Mechanical (Cont.) SOV/2037
BlinnikJ, S.I., Candidate of Technical Sciences, Docent.
Calculation of Free Vibrations in a Four-column Press 210
A method for determining the fundamental natural frequency
of a four-column press, allowing for elasticity tf the
foundationlis discussed. The formulas derived can also be
used for cases of very rigid foundations by putting the
coefficient of soil compressibility equal to zero.
Kolesnikov., K.S.J. Candidate of Technical Sciences, Docent.
Deflections of Beams in the Case of Vibration of Their Supports 226
A method is presented for determining the deflection of
variable cross-section beams subjected to forced vibrations
arising from the periodic motion of supports.
Svetlit5kiy, V.A., Engineer. Determination of Basic Premises for
Forced Motion 234
The paper presents a method for checking whether the forced
motion analyzed is in accordance with the initial assumptions
used for the theoretical solution. The possibility of
Card 7/8

Design for Strength in Mechanical (Cont.) SOV/2037
deviation of existing conditions from initial assumptions
is discussed.
AVAILABLE: Library of Congress
GO/Jmr
8-25-59
card 8/8

PU= I met CMT4jTA=M
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F-Cret" 'Amo Revabud, F~r... F~-'-
Todmjc~4 geleame. Professor. gmdl_

24(6) PHASE I BOOK EXPLOITATION SOV/2397
Ponomarev, S.D., V.L. Biderman, K.K. Likharev, V.M. Makushin,
N.N. Malinin, and V.L. Feodos'yev
Raschety na prochnost' v machinostroyenii. t. II: Nekotoryye zadachi
prikladnoy teorii uprugosti. Raschety za predelami uprugosti.
Raschety na polzuchest' (Design for Strength In MWhinery Construction. Val 2-
Some Problems 6 the Applied Theory of Elasticity. Calculation
Beyond Elastic Limits. Design for Creep) Moscow, Mashgiz, 1958.
974 p. Errata slip inder,4ed. 15,000 copies printed.
Ed.: S.D. Ponomarev, Doctor of Technical Sciences, Professor; Ed.
of Publishing House: N.P. Chernysheva; Tech. Ed.: B.N. Model';
Managing Ed. for Literature of Heavy Machine Building (Mashgiz):
S.Ya. Golovin, Engineer.
PURPOSE: The book is intended for engineers, designers, and process
engineers in the,field of machinery design and construction. It
may also be useful to students, aspirants, and scientific workers.

Design for Strength in Machinery Construction (Cont.) SOV/2397
COVERAGE: Thts book deals with some problems of the applied theory
of elasticity and the calculation of plastic deformation and creep.
Design methods for circular and rectangular plates, shells of
rotation,and thick-walled tubes are presented. The theory of
contact stresses, the design of structural elements made of rubber
and rubberized cord, calculations of elastoplastic strains, and
calculations of steady and unsteady states of creep are discussed.
No personalities are mentioned. References follow each chapter.
TABLE OF CONTENTS:
Preface
SECTION 1. DESIGN OF PLATES AND SHELLS
3
Ch. 1. Theory of Flexure of Circular Plates and Its
Technical Applications 7

S/124
/61/000/009/029/058
D234/D303
MTHOR: Malinin, P.N.
TITIZ Radial-transverse bending of disco
PERXODMU.: Referativnyy zhurnal. Melchanika, no. 9, 19619 a f
abstract 9 V69 (V sb. Raschcty na prochnout v mashi.
n
tr. Q-IVTU, 89), 14, 1958, 43-62)
os
TE)CV: An.aiwproximate method is given of determining un-
loading coefficient;pt-at the axially symmetrical radial-tranrverse
bendin
gof a rotatfiJ,-, inhomoge-neously lae-ated disc of variable
thick~7ess. The unloading coefficients are understood as the ratios
of deflections determined Twithout using the principLe of conserva-
ith t
tion o-! initial dimensions, and the deflections determimd i-r he
use of this principle. Variation of elastic characteristics with
the radius,, due to temperature variation, is taken into account;
..,variatiori of the characteristics with thicImese is neglected.
Abstracter's note: Complete translation 7
Card

MALINIM, dots., ioktor tekhn.nauL-
Proof stress analysis of disks. ffauch.dokl.v7a.ghkoly;mash.1
prib. no.1:49-61 ' 58. (MIRA 12:1)
1. PrdAeta'vle"no kafedroy "Soprotivleniye materialov" Moskov-
skogo *ygihe~o tekhutcheskogo uchilishchs Iment N.B. Baumana.
(Steam-Turbine disks)

Ob .41-fied k
to ble.
uc~ iyi~,yj-o
no low
7L 11 rj JI, 6 Iii
G46 -Tut Ane Ob rud lon,wo
-Owl.
di-iLb .41
. . . . . . . . . .
NO

M
v4:;-;2;;27/a
ti~ilt - ~-co n, f e r e n e, o i i h e st re, h~~, t 6 67f
cin un'. drya
t elevated temapp arures.
r
-vatem in hich ithe follo-i-Anc ele.-itl,antr om?rate so-i
shdlls and xin;S~shaped rods.
T4i his- paper "CC-tt'ain Methoda of Solving thp- Axis-
Sl,~,=Metrilcdl Problem of the Theory of Slanticity Taking-
4eraii.6n Mass Porce-_ th- TeMrjtirat~~e"
'Into. conni
lp
t e me
Umansir-i- e1widated. an appro- Lm -thod -of,
n1culation Vf? the stresc state.'
The paper -of V. J.-Danilovskiye(Mechanics In's'itute
Ac.3c. USSR) was devoeed- to calculatin~j tha teaperature.
f-4c-,lds "In trLirrsbells,
The p f A 1. Ve:~nlk'(Pov,,ur lrfntit.,uca, AcSc. Byglo-
n5er o
w r
w, L6 3-a rqipro, - iil_,W vauthod of* solvirig

7.1
~ax.4
4/9
Wk, L"j(j -60 !Jn~
j _: ~ ~_a 75 1 ~ ~_It h
I A'b dioaj
"Tblhp_qr~' uria' Stresses' hi Thin 71al-lad _Struc:t&eYjn
by I. A. Bir B. F. 8hor"dealt' t~ith, tEa
-tlon.-.cn"ipd out by TsMI on tho th,3.7~mal ~tres'sav_
"E.;j
in. lpto consid-eratlon variable elaovicity
of Olln a I I!q d
lli(-h aro Co t
(A,
~11;rovrvfl i-11 Eluiilvllt~,; of GaLl
Illul"1~1jiuo UnA,3r CrAiditiont) Of ljoll-ntollfly stato 'Thermal

,. ~t`m
211-2-27/26
ihq_;--cpnf arpne e. on the stran-,th -of elametit-;; of, turbq-
tit, elevated tumperatures..-
r, A. -G. ko s tyuk. ~- IW3 Iconhidercd. the tbod 'of
.1pproximate solution of the pr6blo_n of tl c non-steady
state, temp ri3ure fiold. I~a which- the omponont Is.,
'd red a s , aso-mi-inf iziite body during- the initi4l
of

-A
-de-alt.--witv-
G~ t
Yi6v
C.
~he tatiperattire tb in V, 01 led
~-'i~ulaxrly- In bodles of aviation
1~. S. Kurmtov-~TMI) qn.,l'Yd. M.,Molchan.,m~tM)
reported -on cbraple;e invostigat-_4ons of 4'110 V 130.ratU3N3"'l--`~~
: - I:, VS;
fie-1&3 -th6 st- tat -wid thci th '~Suti'gup' P't-
rp e
rotoirs 0l def ibi . ....
-to turbines~
Tl
al
In his ptiper-~Ex~erimentz -Investigation of 06- ~8~pa a
-strasseb 'in Plally Porged RotorsP G. A. Rd t
experizental investitpaftdxin 'cb---rried out a 11'
t.the- aw~~

ei:111ipmd_iit`-_t or - I -
-heating -ihdiv a
idu the- -
-4: 'turbine'. durlng -st-arting.,
RT 2,~
The recond
part o;r i;he confegence was -~Ae voted. td
Droblem6 of the. cobstr~ctiojiall Etrength of. elementS
o
n turbo-machinery At elevated tempq Ur
. rat i's.
In his paper "Work o� the-institute of 'Metallo;,,er=iCs
and Special Alloys, Itrainian, Ac.Sc. In the Field of
r-nthll G. S. Pisarerfko"*
*igh 'Ntltporature -at ecribed-
cQ;rtLjia _rasults,,Obtained by the(-Paam of the 4t
rongth
oo
Divisidn of-the Inatiruto its re'g%rds the davl6lobmeut of

no ;nr,.Vtoda and tent equipmet
-it for-cttwlying 'he mochtiaibaj-

h
crlaractpi~lrtica of -h tomperaturt ilaterialn 41t

,
Q ro 8 14P t) 158
o 0 for h4l.
-
ton a o f
Ic an" 9-Lilv
t r ::iot 1 OC0,11am rind o f
11
ajol aluc> cartsin rorultt~ uf-

at "UIL
J nd ~v6tod t
f G. ftolchin A.' B. PliltoW-11xid
24o cjr o

NA

96iiaintiri
o. Collfo~oneo DII :-tfie stron6th o f u I ri t
U;I~
0 xl~r a, 'a 10V 71turen.
ated t e _410 r
"T,~chnlquo of 111 gh Temperatu-pe Tw3tr- App*d by W-11115"
q;_14 I'd th~..m~ of YQ,.p V G P. rA or. - (VLU, ) "On Certai-rl New methodn~
srature Metallocqgr.-.~rAc. Ma-terialt" - wid
of Tps~ing RiGh Tci:i L
P
pvtpat, of V. Z. TpeytlU', M4. A. Filatoval--A-V Ryabehbiko
and A. 1. IM a 121-&r.-iov ~(TsNIITUASI,) I'lon& Dura tijon.. and 74tiV
S iW~ t h in Air rira~ in Gageoub Media of a
A-Uoy Used fwl Trant, Gas) Turbines" warf) ail
portatibn
devoted to the E~tudy of hi6b teraperature -pterfrl-
-sults-of natural"invebti-ationr, of f-
The. 3~e U
tuYb6-machindry woriiderlt with in papors presantog! by i-
tba pprf~onnel of TsXTI imeni Polzunov.
21. -KaIIIIoVskiy,(IIiIj- dealt ;E6ith the- resulte of
~0
inves
tiCation, of the carrying capacity and 'Uhe long
d% -of specim
e-ns cTf eas tu_rbi;jp discs io~
qation Btrength
_
nevi desIgti and a complicatLid_-donfig~ration tind,er
ra-onditIoma -Similai-to the opewating: conditipiz. _itbe
~'iuiho d or;*Ibed the -featu*res of -the:-heatihg SY'Ste -an&
c_
of am-p3mg equipLq-ent whi h eAsu:ras thepossil
-m of
of :kiDng uratimi 'tepts of hatiiral discs by. ie~ans
at a. high temperatu.~e'lantil disruption 0 C, c ur s. '=d- Aie~.

,considered the deforimations of
,of
6 di-se- in

87506
3/1 2416,010a-lo i 21rx,~410(,~,
A005/A001
Translation from: Referativnyy zhurnal, Mekhanika, 1~160, N~_), 12, pp. 204-205,
# 16700
AUTHOR: Malinin, N.N._
%_ -1
TITLE: The Creep Calculation of the Operating Blades of Turbines
PERIODICAL: V sb.; Raschety na prochnost', No. _3, Moscow, Mashgiz, 1958, pp. 252-
286
TEXT: The blade is conqidered to be a three-dimensional, weakly bent, natur-
ally twisted rod of variable cross section, uniformly heated over its cross se,-;-
tion. The calculation is performed for, stretching and bending with the neutral
line beyond the cross section, In the conditions of the stationary Oreep land m0n0_
axial stretch, the dependence is assumed of the creep strain ir zp on the tension
z p n (-,) ,
6z and the function of temperature and time Q In the form t z 1. For a
variable temperature, is a sumed to be the product of the temperature !'~_,nctlor
and the time function t 1: n = T 0 1. On the basis of trie hypcthesi5 on the
plane cross sections, the correlation Is obtained:
Card 1/ 2

87506
S/124/6o/Ooo/o12/0oq/(,,oq
A005/A0O1
The Creep Calculation of the Operating Blades of Turbines
1/n
6zps 1/n
z Q 1/rn + S )
where ~_ z is the deformation in the gravity center of the croas section,~ Is the
ratio of ?hSe plastic bending deformation to the plastic stretch deformation in the
gravity center. Under the assumption that 6 is small and independent of the time.,
two cases are considered:
+ C~ ) 1/n + /n
1 /n n-1