The results of experimental studies on the manufacture of prototypes of the elements of the lining of the flame tube of the combustion chamber from a ceramic composite material are presented, the structure and physical and mechanical properties of prototype samples are investigated, high-temperature bench tests of prototypes are carried out as part of an experimental structurally similar sample of the flame tube.
Cand. tech. sciences N.E. SHCHEGOLEVA 1 (This email address is being protected from spambots. You need JavaScript enabled to view it.), S. A. EVDOKIMOV 1 , I. V. OSIN 1 , Cand. tech. Sciences A. S. CHAINIKOVA 1 , Cand. tech. Sciences A. A. SHAVNEV 1 , D. I. SEREBRYAKOV 2 ; 1 FSUE & # 171; All-Russian Research Institute of Aviation Materials & # 187; (Russia, Moscow)
2 FSUE & # 171; Central Institute of Aviation Motors. P.I.Baranova & # 187; (Russia, Moscow)
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