SCIENTIFIC ABSTRACT RAYER, G.A. - RAYEV, Z.A.

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP86-00513R001444410002-1
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RIF
Original Classification: 
S
Document Page Count: 
100
Document Creation Date: 
December 30, 2016
Document Release Date: 
June 19, 2000
Sequence Number: 
2
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Publication Date: 
December 31, 1967
Content Type: 
SCIENTIFIC ABSTRACT
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PDF icon CIA-RDP86-00513R001444410002-1.pdf3.15 MB
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RAYZR G. A. : llastar Tech Sci (diss) -- "Investigation of the srr-assed stare 7 5 ,. i.6,07M $-,* . 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) WE "fir tK Al -VA NO o Aty-, T~il' pi~' ,eory.-C)f;,-B as i ls'-Ii~;th6l -Tempera %4 thod 0 f~-'- Lte - 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) A& 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 ; [;-L -a f c.:.L~:tdaluional MetLOd~, t f'-;~-7.-n--.~1 lr~ L-rl cimstorovicif- Energo!:-.as',.,.l-n.:)sLro~-n-i L 101471-67 Lwr (m) IDR (w)1FdP (v)/-DJF (t)/LTI/E`tJP (k) IJPW JDIU4 ACC NRt AP0031hn3 46/- - 8- soucF. com uR/o114/66/ooo/ooq/oo oo4 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