SCIENTIFIC ABSTRACT FROLOV, YU.P. - FRUMKINA, R.M.
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP86-00513R002200820014-2
Release Decision:
RIF
Original Classification:
S
Document Page Count:
97
Document Creation Date:
November 2, 2016
Document Release Date:
September 17, 2001
Sequence Number:
14
Case Number:
Publication Date:
December 31, 1967
Content Type:
SCIENTIFIC ABSTRACT
File:
Attachment | Size |
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Body:
USSR UDC 669. 245'26:5 39. 43
YU. P.. KLYPIN A. A.
..11some- Methods of Hardening Ifeat-Resistant Alloysb 'i and Cr"
ased on N
Tp. Mo k. aviats. in-ta (Works of Moscow Aviation Ins~titute) 1971, vyp 228,
pp. 25-42 (from M-Net"lluts No 4, Apr.72, Abstra~ct 41732)
ost-der ition nnn(!aling
Translation:- Thermomechanical treatmentincludinr F -orm,
preceding aging increases the level. of high--terriperatu~.e strength of E1437A alloy.
as
By segregating the carbides along the grlain.boundariel it is possible to incre.. e
the high-temperature strength. Tile best properties are obtained for a combina
tion of both types of treatment. The possibility of hardening a number of
Ni-Cr alloys by preliminary jacketing at an increasedistress level and working
temperatures is derionstrated. The optimal stress lev6l of the preliminayy
jacketing was found for certain mnterials, 11 illustrittions and a 17-en(I
-ry
biblIography.
USSR UDC 669.018.44
FROLOV.'YU. P., KARYAKINAN. V.
"Variation of the Structure and Properties of Iligh-Alloy Alloys after Prolonged
Aging"
Tp. Hosk aviats. in-ta (Works of Moscow Aviation Institute), 1971, vyp 228,
pp 43-50 (from M-Metallurgiva, No 4, Apr 72, Abstract 41739)
Translation: A study was made of a high-alloy heat-re6istant alloy whose
chemical composition corresponded to technical specifications. Heat treatment
vas carried out under the following conditions: quenching from 12200 for
four hours, cooling in the air, quenching from 9500 for two hours, cooling in
the air, aging at 9800, 25, 100, 200, and 500 hours. After aging, the struc-
ture and properties of the alloy vere investigated. It was demonstrated that
during the process of prolonged aging of the alloy at