发明名称 TUNNEL NANOTURBOCOMPRESSOR
摘要 FIELD: gas-turbine engineering; superlow power gas-turbine engines. SUBSTANCE: use of tunnel nanoturbocompressor in gas-turbine engineering, owing to use of constructional ceramics, makes it possible to solve the problem of creating effective gas-turbine engines of superlow power output. Such gas-turbine engines can be used in space vehicles, power plants with electrochemical fuel elements and in other power-generating systems, for instance, in steam-gas plants, and in road vehicles as engines. To increase efficiency of nanoturbomachines special tunnel channel are proposed for use in flow passage parts. Gas in said tunnel channels flows at high Reynolds numbers and, consequently, at low hydraulic resistance. Cylindrical rotor of turbocompressor is made shaftless, with gas static support and thrust being arranged on periphery of rotor to increase vibration reliability of turbocompressor. EFFECT: enlarged operating capabilities. 3 cl, 1 dwg
申请公布号 RU2227850(C2) 申请公布日期 2004.04.27
申请号 RU20020100717 申请日期 2002.01.17
申请人 发明人 SUDAREV A.V.;SUR'JANINOV A.A.;TIKHOPLAV V.JU.;PODGORETS V.JA.;GRISHAEV V.V.;MOLCHANOV A.S.
分类号 F04D17/02 主分类号 F04D17/02
代理机构 代理人
主权项
地址