发明名称 AIRCRAFT POWER PLANT WITH AIR BLADE PROPULSOR AND AIRCRAFT WITH SUCH POWER PLANT
摘要 FIELD: transport. ^ SUBSTANCE: set of invention relates to transport vehicles. Proposed power plant comprises engine and blade propulsor driven thereby and furnished with circular case consisting of inlet, central and outlet parts, and casing fastener. Circular case inlet part represents a tapered nozzle and is furnished with straightening elements and inner thin-wall inserts. Circular case central part inner surface represents a diffuser that fairs smoothly with inlet and outlet parts. Aircraft comprises wing, airframe, control system and power plant. Power plant circular case outlet part represents rotary ring with vertical axle pivoted to circular case central part behind blade propulsor. ^ EFFECT: increased thrust and aerodynamic characteristics. ^ 7 cl, 4 dwg
申请公布号 RU2394731(C1) 申请公布日期 2010.07.20
申请号 RU20080147827 申请日期 2008.12.05
申请人 SHVEDOV VLADIMIR TARASOVICH 发明人 SHVEDOV VLADIMIR TARASOVICH
分类号 B64C1/16;B64D27/02;B64D35/00 主分类号 B64C1/16
代理机构 代理人
主权项
地址