SCIENTIFIC ABSTRACT RAYER, G.A. - RAYEV, Z.A.
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP86-00513R001444410002-1
Release Decision:
RIF
Original Classification:
S
Document Page Count:
100
Document Creation Date:
December 30, 2016
Document Release Date:
June 19, 2000
Sequence Number:
2
Case Number:
Publication Date:
December 31, 1967
Content Type:
SCIENTIFIC ABSTRACT
File:
Attachment | Size |
---|---|
CIA-RDP86-00513R001444410002-1.pdf | 3.15 MB |
Body:
RAYZR G. A. : llastar Tech Sci (diss) -- "Investigation of the srr-assed stare
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0 f Ch,2 %lbeP ~ S 0 L centri fuga I compressor machines ". Leningrad, 195J. 13 pp
(,',',in Hig -
,her *-duc FISSR, Leningrall Polytech Inst. 'm 1,11. 1. Kalinin), 150 copies
(KI., No 7, 1951, 125)
RATER, G.A., Inzb.
- --- ---- . Calculeting the strength of runner discs of centrifugal compressor
machines. EnprgnmaRhinostroanis 4 no.7:10-14 Jl 158.
-(Turbinna) (14IRA 11:10)
KLMICATSOV, L.A., kanit. t8khn-nauk-, RAYMR- G.A..inzh.
Start voltages in seamless forged rotors of gas turbines.
Energonashinoetroenie 4 no.12ti-3 D '58. (KIRA 11:12)
(Gins turbines)
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RAUR, G.A., kand.takhn-wuk
Investigating the dynamic strength of the-wheele of certrifugal
compressors. Flnergamepthi-strpenie.7 na.9:14-17 S 161.
(MIRA 14:9)
(Compressors-Testing)
KOBRINP Mikhail Moiseyevich; ROZENBERG, A.B., retsenzent- RAYER G.A,,
nauchnyy red.; NIKITINA, R.D., red.; SHISHKO'VA:__E-'~__." tekhn.
red.
(Strength of rotating disks] Prochnost' vrashchaiushchikhsia
diskov. Leningrad, Sudpromgiz, 1963. 339 P. (MIRA 16:4)
(Disks, Rotating-Testing)
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ACCESSION NR: AP4023733 S/0114/64/000/003/0022/0025
AUTHOR; Rayer, G. A. (Candidate of technical sciences)
TITLE: Investigation of the dynamic strength of the rotor of a cantilever-type I
supercharger
SOURCE: F-nergoniashinostroyeniye, no. 3. 1964, 22-25
TOPIC TAGS: supercharger. cantilever type supercharger, supercharger rotor,
supercharger rotor strength, supercharger rotor dynamic strength,
supercharger break
ABSTRACT: It has been known that maximum aerodynamic stresses occur in the
irppeller stages next to ii diffuserless scroll. In the past four years of operating
suIperchargers with such stages, -cases of shaft and web breaks, and cracks in the
cover disks are on record. Also, rivet-head crumbling has been observed.-
Metal fatigue has been mainly responsible for, those damages. Thepresent
article reports the results of tensometric tests of impellers conducted directly at
compressor'\stations. The aerodynamic stresses in, the impeller were measured
ca'a
ACCESSION NR: AP4023733
in the entire range of the compressor output, at 20, 30, 35, and 44 atm, and
7,950 rpm. An attempt was made to assess the rivet stresses by tensodetectors
mounted inside the rivet. These conclusions are reported: (1) The poor quality
of shafts and web-fittin-r surfaces is one of the reasons for shaft breakage;
I Ij
(Z) Under max output and minimum output conditions, considerable stresses are
set up in the impeller which may result in breakage due to fatigue; (3) The canti-
lever stiffness of the principal disk (web) has an important bearing on the dynamic
strength of the disk, rivets, and cover disk; (4) Cuts in the cover disk result in
an essential reduction of the aerodynamic forces acting an the Impeller. Orig.
art. has: 5 figures and 2 formulae.
ASSOCIATION: none
SUBMITTED: 00
'SUB CODE: PR, AP
Card_
DATE ACQ: 15Apr64
NO REF SOV: 003
ENCL: 00
OTHER: 000
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AU111OR: Rayer, G, A. (Candidate of technical sciences); Vasil'y~ev, A. V. (Engineer)
ORG.- none
TITLE: Method fo--- ;ncreasing the design strength of c-,.ntrifugal c=,~resscr wheels
SOURCE: Energoriaz'~inostroyeniye, no. 9, 1966, 46-48
TOPIC TAGS: centr~'-'ueal compressor, compressor disk,f e stren zr,-
ABSTRACT: Severa.11 orntrifugal compressor wheels have been subjected to tests with
peripheral speeds ..,f 290-300 m/~ec under simultaneous action of an air jet
(combined static dynamic stresses). It was found that the wheels tested failed--
in the same manner as the wheels in actual operation. The cracks I