发明名称 BURNABLE NOZZLE OF RAMJET
摘要 FIELD: engines and pumps.SUBSTANCE: burnable nozzle of ramjet is arranged inside mid-flight nozzle and composed of two interconnected elements to make acceleration mode nozzle in acceleration from subsonic to transonic and from transonic to supersonic ranges. Lengthwise ducts plugged on the side of afterburner to make a set of pylons are arranged at outer side of nozzle elements and secured to engine mid-flight nozzle inner surface. Nozzle elements are made of material wit high thermal erosion resistance to combustion products with reduction chemical potential and low thermal erosion resistance to combustion products with oxidation chemical potential.EFFECT: higher reliability of burnable nozzle in acceleration mode and efficiency of mid-flight nozzle in ramjet mode.4 cl, 3 dwg
申请公布号 RU2507409(C1) 申请公布日期 2014.02.20
申请号 RU20120127547 申请日期 2012.07.03
申请人 ROSSIJSKAJA FEDERATSIJA, OT IMENI KOTOROJ VYSTUPAET MINISTERSTVO PROMYSHLENNOSTI I TORGOVLI ROSSIJSKOJ FEDERATSII (MINPROMTORG ROSSII) 发明人 SURIKOV EVGENIJ VALENTINOVICH
分类号 F02K7/18;F02K1/82 主分类号 F02K7/18
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