发明名称 COVER FOR FLYING VEHICLE ENGINE NOZZLE
摘要 FIELD: aviation; aircraft engine foreign matter ingestion protection. ^ SUBSTANCE: proposed nozzle cover has disk over its perimeter and two swivel stops mounted on disk. Each stop is made in form of eccentric roller rigidly secured on axle of handle mounted for turn and fixation of roller in position when it is pressed to nozzle surface. Each axle of cover is located in bush secured on disk. It is provided with handle with retainer and mating slot in bush. Nozzle cover is provided with stop made in form of screw passed through bush and engageable with axle. Outer surface of eccentric rollers is equidistant relative to inner surface of engine nozzle. ^ EFFECT: ease in operation; simplified construction. ^ 2 dwg
申请公布号 RU2248309(C2) 申请公布日期 2005.03.20
申请号 RU20030110205 申请日期 2003.04.09
申请人 发明人 SHISHKINA N.A.
分类号 B64F5/00 主分类号 B64F5/00
代理机构 代理人
主权项
地址