"SCIENTIFIC ABSTRACT LOKSHIN, I. KH. - LOKSHIN, V. A."

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP86-00513R000930420014-8
Release Decision: 
RIF
Original Classification: 
S
Document Page Count: 
100
Document Creation Date: 
November 2, 2016
Sequence Number: 
14
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Publication Date: 
December 31, 1967
Content Type: 
SCIENTIFIC ABSTRACT
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PDF icon CIA-RDP86-00513R000930420014-8.pdf2.75 MB
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Fig. 1. Diagram of rig for vibratory-thermal stabilizing treatment at 160, 260, 535 and 550'C (their regular aging and tempering temperatures). The effectiveness of this 4, treatment was evaluated by comparing the extent of the surviving residual. stresses with the stresses pro- sent following vibration-free heating at the same tem- peratures. Findings: this effectiveness is the greater the higher the amplitude and frequency of vibrations are. Thus, e.g. for specimens of 35L steel at 550"C, treated with vibrations of 80-cps frequency and 0. 2 mv amplitude, residual stresses are 26.2% smaller-thm following the same heating without vibration, and at vibrations of 250-cps frequenoy these stresses are 4. 1 times smaller Thus high-temperature vibration . , 2/3 7 ACC HRs AY6031837 - - ';"'ACC AUTHOR: Khenkin, M, L.-, jook~hinq I. Kh.; Levina, N. K.; Sidokhin, Ye. F.' Simeonov, 8,L.i Minina, Pa-iiIAktoya, Ye.V. ORG: none TITLE: Effect of cy;lic heat treatment on the properties and structure of alloys containing phases with different expansion coefficients SOURCE: Fizika metallov i metallovedeniye v. 22, no. 6, 1966, 896-903 ~Nr-,IFWMIL SrPES.5s CC04 IV(37, 194 0-771AIVI" VZ.Loc-1. TOPIC TAGS: A 0141CdAl C0AFr0?1MjNa alloy, magnesium containing alloy, alloy heat treatment, cyclic heat treatment,-.qkl*a~m-mechanical property, stress relaxation, cyclic heat treatment effect/AL2 alloy, AL9T2 RZ I CC-/ ABSTRACT: An investigation has been made of the effect of cyclic heat treatment (CHT) on the internal stresses and relaxation characteristica of alloys containing phases with different expansion coefficien,;n. Each cycle in CHT consisted of cooling to subzero temperatures ,-40 to -190), holding for 10-120 min, followed by heating to relatively low temperatures (UP to 150C) and holding at these temperatures for 15- 240 min. It was found that CHT reduced internal stresses and increased the relaxation strength in all investigated alloys. The greatest decrease in internal stresses was observed in AL2 (12.1%Si) and AL9T2 (7%Si, 0.3% Mg) aluminum alloys. The CHT had no effect on the tensile and yield Card 1 /2 uDc: 669.017': 1548-735+62o.1871 ACC NRI AP700274o strengths and the ductility of Al-Si alloys, but it increased the elastic limit by 20-500P and the relaxation strength of AL2 alloy by 300% in short-time and prolonged testa. Thus , CHT effectively inhibited the negative effect of the increased silicon content, thereby incre"in the strength characteristics, but lovers the relaxation strength of Al-Si alloys. The effect of CHT on the relaxation strength decreasea_ as the.upper temperature of the cycle increases above 150C, andapproach- es zero when this temperature is increased to 280C. The first three cycles of CHT are the most effective regardless of the holding time at the extreme temperatures of the cycle. The same effect of MIT was observed in other alloys consisting of the phases with different expan-~ sion coefficients, e9go, Al-Ge, and sintered W-Ni-Fe and W-Ni-Cu alloys, ! In such alloys, CHT promoted formation of a stable dislocation structure with minimum micro-and macrostreases, which increased the elastic limit and relaxation strength.- Orige arts haos 5 figures and 3 tables, SUB CODEs 13, ll/ SUBM DAM 108ep65/ OHIO REP: 008/ OTH REP: 00 p Card SOV/124 58 11-1?45~ Translation from: Referat;vnyy zhurnal, Me~hijril